AIRBUS A320
ES-LAA
AIRCRAFT MAINTENANCE
PROGRAM
AMP REF: AEG/MP/A320
CAM
Oliver Loorits
+372 55944332
A320 Aircraft Maintenance Program
0.1. Table of content
PART 0 GENERAL
0.1. Table of content 2
0.2. List of effective pages 3
0.3. Record of revision 4
0.4. AMP Amendment procedures 5
PART 1. INTRODUCTION 6
1.1. General 6
1.2. Applicability 6
1.3. Operator, Owner Name and Address 6
1.4. Maintenance Program Reference 6
1.5. Maintenance Program Source Documents 6
PART 2. OPERATOR STATEMENT 7
2.1. Corporate Commitment 7
PART 3. GENERAL PROCEDURES 8
3.1. Introduction 8
3.2. Utilization of aircraft 8
3.3. Program Review 8
3.4. Escalation of the Inspection Intervals 8
3.5. Systems, APU and Power Plant Inspection Program 8
3.6. Structures Inspection Program / Corrosion Prevention Control Program 9
3.7. Zonal Inspection 9
3.8. Critical Design Configuration Control Limitations 10
3.9. Fuel Airworthiness Limitations: 10
3.10. Power-plant / APU Limitations 10
3.11. Pre-flight Checks 11
3.12. Mandatory Requirements 11
3.13. Airworthiness Directives 11
3.14. Non-Mandatory Changes 11
3.15. Category II/III Landing, RVSM 12
3.16. Reliability Program 12
3.17. Sampling program 12
3.18. Structural Repair 13
3.19. Weighing of aircraft 13
PART 4. MAINTENANCE SCHEDULE 14
4.1. Inspection Standards 14
4.2. Maintenance Checks 14
4.3. Storage 15
4.4. Permitted Variations of Maintenance Periods 15
4.5. Abbreviations 15
APPENDICIES:
Appendix A: Scheduled Maintenance Tasks
Appendix B: Component Maintenance Requirments
Appendix C: Daily and Weekly Check
Appendix D: Repetitive Airworthiness Directives
Appendix E: Aircraft Maintenance Programm Bases
Appendix F: Program review Checklist
Appendix G: Structural Repairs Inspection
Appendix H: Additional Maintenance Tasks
PART 0 Page 2 Rev. 2, 01.06.2020
A320 Aircraft Maintenance Program
0.2. List of effective pages
Pages Content Revision Date
1-5 PART 0 - General 2 01.06.2020
6 PART 1 - Introduction 0 30.08.2019
7 PART 2 – Operator Statement 0 30.08.2019
9-13 PART 3 – General Description 1 10.12.2019
14-15 PART 4 – Maintenance Schedule 0 30.08.2019
Appendices
1-256 Appendix A 2 01.06.2020
1-10 Appendix B 0 30.08.2019
1-6 Appendix C 2 01.06.2020
1-4 Appendix D 2 01.06.2020
1 Appendix E 1 10.12.2019
1 Appendix F 0 30.08.2019
1 Appendix G 1 10.12.2019
1 Appendix H 1 10.12.2019
Submitted for approval by: Approved by Estonian CAA:
Oliver Loorits Ermo Uuspuu
//Digitally Signed //Digitally Signed
PART 0 Page 3 Rev. 2, 01.06.2020
A320 Aircraft Maintenance Program
0.3. Record of revision
Revision, Date Contents
Rev 0, 30.08.19 Initial issue
Rev 1, 10.12.19 Changes related to MPD new revision no 46. Appendix G and H added
Rev 2, 01.06.20 Changes related to new DY/WK Checklist and new AD’s. Changed Appendix A, C, D
PART 0 Page 4 Rev. 2, 01.06.2020
A320 Aircraft Maintenance Program
0.4. AMP Amendment procedures
Each page shall be identifiable by a unique heading and footer. The heading of each page contains the title and
is identical on all pages. The footer contains revision status, part, and page number of the applicable Part.
The original/basic issue will be given Rev. 0. When this chapter is revised the first time it will be stated in the
footer - Rev. 1 and so on.
Each revision will, in addition to change of revision status in the footer be marked with a blue color or lines on
the left boarder. Each revision shall be distributed in accordance with the distribution list and signed for in the
record of revision.
All applicable changes to the AMP require competent authority approval if not otherwise specified in indirect
approval procedures (CAME CH1.2).
Indirect approval procedures
Changed or added pages shall be included to the maintenance program together with additional List of
Effective Pages (LEP) and Record of Revision (ROR). It means that Competent Authority approved LEP and ROR
shall remain in the manual. All revised pages not requiring prior approval shall be clearly indicated as such
(font: red):
• In footer: APPROVED INDIRCETLY
• Revision number and a date in LEP and on revised page footer shall be changed with adding a letter
“A” to revision number or in case of several changes then next letter of the alphabet.
• Text in LEP approval field shall be replaced with: Approved by AIREST AS in accordance with CAME ch
1.2.
Distribution List
The CAM is responsible for the preparation, distribution and revision of AMP. Once approval has been issued,
the revised copies are distributed to the other recipients:
• CAM: master copy (electronic copy)
• ECAA: copy (electronic copy)
• Contracted MO: copy (electronic copy)
• Sub-contractor: copy (electronic copy)
PART 0 Page 5 Rev. 2, 01.06.2020
A320 Aircraft Maintenance Program
PART 1. INTRODUCTION
1.1. General
This Aircraft Maintenance Program (AMP) provides maintenance instructions necessary for the safe, airworthy
and reliable operation of all applicable Airbus A320-232 operated by AIREST The AMP is based on, and reflects,
the Airbus A320 Maintenance Schedule, and is approved by the ECAA. This program shall only be used in
conjunction with the A320 Maintenance Planning Document (MPD) latest revision. Unscheduled and off-wing
maintenance tasks are not included in this Maintenance Program. For unscheduled and off-wing maintenance,
the contracted EASA Part-145 Maintenance Organization must follow the relevant manufacturer's instructions
for continuing airworthiness.
1.2. Applicability
Type/model and registration of the aircraft:
Registration Manufacturer Model Serial TCDS
ES-LAA AIRBUS A320-232 2157 EASA.A.064
Type/model of the Engines/APU.
Name TC Holder Model
Engines IAE Aero Engines V2527-A5
APU Honeywell 131-9A
1.3. Operator, Owner Name and Address
CAMO Operator Owner
AS AIREST AS AIREST CRA Aircraft Ireland No.1 Ltd
Lõõtsa 8c Lõõtsa 8c Riverside One, Sir John Rogerson’s
11415, Tallinn Estonia 11415, Tallinn Estonia Quay, Dublin, Ireland
(Approval ref: EE.MG.0019) (AOC ref: EE-016)
1.4. Maintenance Program Reference
The Maintenance Program bears the following reference: AEG/MP/A320
1.5. Maintenance Program Source Documents
Following sources of documents have been used to build up the Maintenance Program for A320 fleet:
- Type Certification Recommended Documentation;
- EASA requirements (AD’s, SIB’s) affecting the scheduled maintenance of the aircraft;
- Manufacturers` Service Bulletins, Service Letters as applicable for aircraft and components;
- Instructions of Continuing Airworthiness data as applicable from installed modifications
Technical publication references with latest revision numbers are listed in Appendix E
PART 1 Page 6 Rev. 0, 30.08.2019
A320 Aircraft Maintenance Program
PART 2. OPERATOR STATEMENT
2.1. Corporate Commitment
In the preparation of this approved maintenance program to meet the requirements of EASA Part M, M.A. 302,
the recommendations made by the TC holder and engine and Original Equipment Manufacturer (OEM´s), have
been evaluated. The recommendations from the TC holder and engine and equipment manufacturers (OEM´s)
have been incorporated in this approved maintenance program.
The practices and procedures in this approved maintenance program meets the standards specified in the TC
holder´s and OEM´s Maintenance Instructions.
This approved maintenance program establish compliance with instructions for continuing airworthiness
issued by the TC holder, OEM´s or Supplementary Type Certificate holders and any organization that publishes
such data in accordance with EASA Part 21, or instructions issued by ECAA, if they differ from what is written
above, or in the absence of specific recommendations, or instructions defined by AIREST and approved by the
ECAA. This approved maintenance program lists the tasks and identifies the practices and procedures, which
form the basis for the scheduled maintenance of the aircraft(s) listed in Paragraph above. AIREST undertakes
to ensure that these aircraft will continue to be maintained in accordance with this approved maintenance
program.
The data contained in this approved maintenance program will be reviewed for continued validity at least
annually in the light of operating experience. This approved maintenance program will be updated as required.
It is accepted that this approved maintenance program does not prevent the necessity for complying with any
new or amended regulation published by the EASA, from time to time where these new or amended
regulations may override elements of this maintenance program.
It is understood that compliance with this approved maintenance program does not release AIREST from the
need to ensure that the approved maintenance program reflects the maintenance needs of the aircraft, such
that continuing safe operation can be assured. It is further understood that the ECAA reserves the right to
suspend, vary or cancel approval of the approved maintenance program if the ECAA has evidence that
requirements of the approved maintenance program are not followed, or standards not upheld.
Dated 30.08.2019
Signed digitally by:
Oliver Loorits
For and on behalf of AIREST CAMO(Approval Ref: EE.MG.0019)
PART 2 Page 7 Rev. 0, 30.08.2019
PART 3. GENERAL PROCEDURES
3.1. Introduction
This program includes the Systems, Powerplants, APU, Structures and Zonal requirements set forth by the
manufacturer as specified by the Airbus A320 Maintenance Planning Document (MPD). Maintenance
requirements planning and control is performed by the maintenance planning tools Alaskar.
Maintenance planning tool lists all tasks related to this specific Maintenance Program with:
References to TC Holder Task number
Current limits (threshold and repeat inspections).
Additional codes by custom installations, limitations or repairs
Certificate of Release to Service (CRS) is required by an approved Part 145 Organization after each
maintenance action other than Pre-, Post-flight. Service Check and other must be signed off in the Technical
Log (ATL) as described in the CAME.
3.2. Utilization of aircraft
The application of this maintenance program is based on an average utilization from 1,800 to 4,400 Flight
Hours and 1000 to 2,500 Flight Cycles. In the event that an airplane’s annual utilization differs significantly
from this figure, or the type of operation differs significantly from this profile, CAM will have to undertake a
review of all tasks in this Maintenance Program with the manufacturer. If the annual utilization varies by more
than 25% from the stated, the operator accepts that the AMP shall be reviewed in order that any necessary
adjustments to the maintenance tasks and periods may be made.
3.3. Program Review
Data contained in this Maintenance Program will be reviewed at least annually and amended accordingly
when necessary. The review will ensure that the AMP continues to be valid in light of the operating experience
and instructions from the competent authority whilst considering new and/or modified maintenance
instructions promulgated by the TC and STC and EASA including AD, SB, etc.
After the review the checklist should be signed and stored in the Appendix F to this AMP.
3.4. Escalation of the Inspection Intervals
The individual maintenance tasks and frequencies shown in this document are marked with “YES” text in AWL
column in Appendix A of this AMP, may be adjusted/escalated, where applicable, shall by controlled by
procedures acceptable to EASA/ECAA. No Escalation of inspection intervals are envisaged except if published
by The Type Certificate Holder or/and acceptable for Competent Authority.
3.5. Systems, APU and Power Plant Inspection Program
This Maintenance Program includes the requirements of the Avionics, Systems, APU and Power Plant
inspection program recommended by the manufacturer and detailed in the MRBR. A complete set of
MPD/MRB/AMM cross-reference indexes can be found in Appendix 2 of the Airbus A320 MPD.
Refer to Appendix A for List of tasks (Section No 2)
A320 Aircraft Maintenance Program
3.6. Structures Inspection Program / Corrosion Prevention Control Program
This Maintenance Program includes the requirements of the structures inspection and corrosion control
program recommended by the aircraft manufacturer and detailed in the MRBR. The structures inspection
program will ensure that catastrophic failure due to the deterioration process will be avoided throughout the
operational life of the aircraft.
The Corrosion Prevention and Control Program (CPCP) lists specific, directed inspections intended to prevent
structural degradation caused by environmental deterioration. The CPCP is established to maintain the
aircraft’s corrosion protection against age related deterioration caused by environmental interaction. This
program is expected to allow control of the corrosion on the aircraft to Corrosion Level 1 or better.
Refer to Appendix A for a list of tasks(Section 3).
CPCP Rules
The effectiveness of the Corrosion Prevention and Control Program is determined by following the General
Rules applicable to the Structures section and the rules listed below.
Level 1 Corrosion Findings - Should inspections consistently reveal corrosion Level 1 findings for a given area
during repeat inspections on particular aircraft operated in similar conditions, then the existing task is
considered effective for the concerned area, and no change to the program is necessary.
Level 2 Corrosion Findings - Should inspections reveal that corrosion is Level 2 for a given area during repeat
inspections, then the existing task is not effective for the concerned area of the particular fleet. In order to
control corrosion to Level 1 or better, consideration should be given to one or more of the following corrective
actions:
– Decreasing the inspection threshold/interval
– Considering a higher inspection level
– Reconsidering the Concept (Sampling or 100%)
– Application/More frequent application of Temporary Protection System
– Embodiment of preventive modifications, where applicable
– Installation of parts with improved protection standard, where applicable.
In this way, the CPCP is self-regulating and will adjust itself to the optimum program.
Level 3 Corrosion Findings - Should inspections reveal that corrosion is Level 3 in a given area, then the existing
task is not effective for the concerned area. In addition to the considerations given for Level 2 corrosion, an
action plan calling for a one-time inspection of the concerned area should be expeditiously agreed with the
local Aviation Authority and carried out on all aircraft of a similar age or older.
Airbus may be consulted to determine whether or not the airworthiness is affected. In this case all details of
findings are to be promptly reported for detailed evaluation and the assistance required clearly expressed. A
periodic review of the Structures section, with particular attention to reported fleet data shall be scheduled to
maintain the target of this program to control corrosion to Level 1 or better on all structural details, elements
or assemblies which contribute significantly to carrying flight, ground, pressure or control loads, and whose
failure could affect the structural integrity necessary for the safety of the Aircraft.
3.7. Zonal Inspection
This Maintenance Program includes the requirements of the zonal inspections program recommended by the
aircraft manufacturer and is detailed in the MRBR. The Zonal Inspection Program lists general visual
inspections requirements for each aircraft zone to inspect system and powerplant installations for security and
general condition, structure for general condition and Electrical wiring installation for general condition.
Refer to Appendix A for List of tasks(Section 4ZL)
PART 3 Page 9 Rev. 1, 10.12.2019
A320 Aircraft Maintenance Program
3.8. Critical Design Configuration Control Limitations
This maintenance program includes all the scheduled maintenance tasks related to the aircraft systems and
components, APU and Power Plants in depending of Fuel Tanks Safety requirement.
A CDCCL is a limitation requirement to preserve a critical ignition source prevention feature of the fuel system
design that is necessary to prevent the occurrence of an unsafe condition. Airbus AMM has a warning note in
front of all CDCCL related tasks:
WARNING: THIS PROCEDURE USES A FUEL SYSTEM ITEM THAT IS IN A CATEGORY KNOWN AS A CRITICAL
DESIGN CONFIGURATION CONTROL LIMITATION. CDCCL IDENTIFIES AN ITEM THAT CAN BE THE
SOURCE OF A POSSIBLE FUEL TANK IGNITION. YOU MUST KEEP ALL CDCCL ITEMS IN THE
APPROVED CONFIGURATION. DAMAGE, WEAR OR CHANGES TO A CDCCL ITEM CAN CAUSE A
POSSIBLE FUEL TANK EXPLOSION.
The Fuel Airworthiness Limitations result from the compliance with JAA’s Interim policy on Fuel Tank Safety
(INT/POL/25/12) and FAA’s Special Federal Aviation Regulation (SFAR) 88. They have been derived in
accordance with guidance material published in attachment to the EASA policy statement on fuel tank safety
(ref EASA D 2005/CPRO/RH/50213) and FAA’s Advisory Circular (AC) 25.981-1B. The nomenclature and means
of promulgation follow the FAA’s memorandum ref ANM112-05-001 „Policy Statement on Process for
Developing SFAR 88- related Instructions for Maintenance and Inspection of Fuel Tank Systems”.
There is Airworthiness Limitation Section part 5 document with name “A318/A319/A320/A321 Fuel
Airworthiness Limitations”.
3.9. Fuel Airworthiness Limitations:
Fuel ALI’s fall into two categories:
Maintenance Inspection Tasks
These tasks are equivalent to Certification Maintenance Requirements but since they have been identified
after initial certification of the design, in accordance with EASA’s AMC 25-19 and FAA’s AC 25-19, they cannot
be identified as CMRs
Critical Design Configuration Control Limitations
A CDCCL is a limitation requirement to preserve a critical ignition source prevention feature of the fuel system
design that is necessary to prevent the occurrence of an unsafe condition.
The purpose of the CDCCL is to provide instructions to retain the critical ignition source prevention feature
during configuration change that may be caused by alterations, repairs, or maintenance actions. A critical
ignition source prevention feature may exist in the fuel system and its related installation or in systems that, if
a failure condition were to develop, could interact with the fuel system in such a way that an unsafe condition
would develop in the fuel system without this limitation.
Airest is responsible for ensuring that their internal documentation is amended to reflect the data contained
within this section and provides appropriate text to highlight the existence of each CDCCL. Such identification
is necessary in the instructions used by the person performing an installation, alteration, repair or modification
to minimize the risk that the work performed compromises the original design criteria. Regulatory oversight of
the operator’s compliance with this mandatory requirement is based on the appropriate identification of the
CDCCL in the accomplishment instructions associated with the installation, alteration, repair or modification.
3.10. Power-plant / APU Limitations
The IAE V2500 Series engines are maintained in accordance with V2500 A1/A5 Engine Manual Chapter 05
requirements. V25000 engines are operated under the Task Oriented “On Condition” Maintenance Program
thus having no scheduled Overhaul or Hot Section inspection maintenance. This Maintenance Program
includes “installed engine” repetitive visual borescope inspections of the external and internal components,
specific maintenance checks, and a required Trend Monitoring program which is performed “On-Wing”.
PART 3 Page 10 Rev. 1, 10.12.2019
A320 Aircraft Maintenance Program
The engine Rotating Parts with Life Limits are defined in Reference V2500-77445-A4408-00-008 - V2500-A1/A5
Series Time Limits Manual.
Refer to Appendix B for the Hard Time and Life Limited Part.
3.11. Pre-flight Checks
Before the flight a complete external safety inspection, external walk around, normal power up check and
system check shall be performed. This Maintenance Program does not include the pre-flight maintenance
tasks. Pre-Flight inspections performed by the flight crew and by the contracted maintenance organization will
be performed in accordance with the approved manuals. Pre-flight checks can be performed by Flight crew,
maintenance personnel or any other trained and authorized person.
The Commander may designate a flight crewmember to perform all external airplane inspections and checks
while the other flight crewmember prepares the flight deck and performs the cockpit checks (Systems Check).
The technical acceptance is confirmed by the Commander’s signature in the airplane technical log (ATL).
3.12. Mandatory Requirements
The maintenance tasks identified in Appendix A are based on Airworthiness Limitations (ALI) (ALS Part 1),
Damage-Tolerant Airworthiness Limitations (DT-ALI) (ALS Part 3), Certification Maintenance
Requirements(CRM)(ALS Part 3), Systems Equipment Maintenance Requirements (SEMR)(ALS Part 4), Fuel
Airworthiness Limitations (FAL)(ALS Part 5), CDCCL (Critical Design Configuration Control Limitations) and
components having an life limit items (LLI or LLP) are considered mandatory and may not be extended or
escalated under the normal extension or escalation procedure.
For the extension and/or escalation of these mandatory tasks, prior approval from the TC-holder, CAA and/or
EASA is required.
Repetitive ADs are incorporated in this MP in ‘’Appendix D’’ requirements requested by CAA are also
mandatory and may not be extended or escalated under the normal escalation procedure. All Airworthiness
Notices are assessed for applicability as appropriate for this type of airplane and where necessary relevant
maintenance tasks will be included in this program.
3.13. Airworthiness Directives
The following groups of Airworthiness Directives (AD) are applicable to the aircraft maintained in accordance
with this Maintenance Program.
1. EASA Airworthiness Directives (Airframe, Engine, APU and Equipment)
2. FAA Airworthiness Directives (APU and Equipment)
3. ECAA Airworthiness Directives (as applicable)
It is the responsibility of AIREST to check the applicability of above ADs as they are issued, and also to check
the EASA bi-weeklies as they are issued. All ADs are assessed for applicability and where necessary relevant
maintenance tasks are included in the Maintenance Program.
Refer to Appendix D for list of Repetitive AD’s.
3.14. Non-Mandatory Changes
The embodiment policy of non-mandatory modification is defined in the CAME Part 1.6. Additional
airworthiness instruction based on STC or Part-21 design organization approved document are included into
this maintenance program.
Refer to Appendix H for list of additional tasks.
PART 3 Page 11 Rev. 1, 10.12.2019
A320 Aircraft Maintenance Program
3.15. Category II/III Landing, RVSM
Category II/III landing capabilities and RVSM capability are inherent functions of the basic design standard of
the aircraft. Scheduled tasks necessary for these operations have been considered in the development of this
program
3.16. Reliability Program
The purpose of a Reliability Program is to ensure that Maintenance Program tasks are effective, and their
periodicity is adequate. In addition, the effectiveness of the Maintenance Program is subject to periodical
review in accordance with the procedures detailed in CAME 1.2 and 1.5.
Reliability program applicability when Airest fleet(less than 6 aircraft) is small should be used very carefully.
When amount of available data is very limited, Airest engineering judgement is used very carefully to avoid
statistical calculation mistakes, which can rather cause potential problems. Airest understands that when the
fleet is small the only one single event may cause alert level. Airest reliability analysis is based on the
communication with manufacturer, Airest and the contracted EASA Part-145 facility. Other organizations
which uses the same type of aircraft and also if the aircraft manufacturer does the reliability by itself, Airest
should try to use this data as well. ECAA also can impose additional maintenance restrictions on the Airest
aircraft fleet.
With the collected information the reliability report for A320 fleet will be conducted on an annual basis by
Airbus "pooled" from a number of same type of aircraft.
3.17. Sampling program
The purpose of the Sampling Program is to detect systematic deterioration caused by the environment and/or
fatigue by performing inspections on specific aircraft selected from those which have the highest operating
usage in order to identify the first evidence of deterioration in their condition caused by fatigue damage or
corrosion.
The Sampling Program is applicable to both Environmental Deterioration (ED) and Fatigue Damage (FD) SSIs,
where the deterioration, should it occur, is considered as being progressive with age or operating usage.
Aircraft being part of the sampling fleet are continuously inspected in advance of the rest of the fleet at the
sampling inspection threshold and afterwards following the sampling interval inspection requirement. All
other aircraft in Airest fleet should follow 100% threshold and 100% interval.
Example:
Sampling inspection requirement with 100% threshold (CPCP)
MPD Task 535151-01-1
- Sampling threshold 12 YE; sampling interval 12 YE;
- 100% threshold 24 YE, 100 % interval 12 YE
Sampling fleet aircraft inspection dates: First inspection at 12 YE, repetitive inspection 12 YE after first
inspection performed (24 YE, 36 YE…)
Non sampling fleet aircraft (sampling fleet installed): First inspection at 24 YE, repetitive inspection 12 YE after
first inspection performed (36 YE, 48YE…)
Adding the A/C to the fleet
The principle of the sampling policy is that any aircraft in a fleet is protected by the respective sample aircraft
out of that operator’s fleet. A/C transferred from other Operator to Airest are protected by the sampling fleet
of the previous operator. If a “non-sampling” aircraft would be integrated into Airest fleet it may become a
sampling aircraft. However, no retroactive maintenance is required i.e. all inspections are to be performed at
their next scheduled due. The performance of sample tasks is not a prerequisite for incorporation of this
aircraft into Airest fleet.
PART 3 Page 12 Rev. 1, 10.12.2019
A320 Aircraft Maintenance Program
Example:
An aircraft, which was not a sample A/C, is 7 years old has been acquired by another operator. “100% concept”
6 YE threshold inspection requirements have been accomplished during a maintenance visit when the A/C was
5.5 YE. No sampling inspection was performed (non sampling A/C). In the new fleet, the A/C became part of
the sampling fleet. The next sampling inspection for this A/C (6 YE / 6 YE sampling tasks) should be performed
6 YE after the last maintenance visit, therefore at the A/C age of 11.5 YE. Presumably, this would be the next
12 YE inspection event for this A/C, therefore the 12 YE sampling threshold inspection would be performed at
this aircraft age, too.
NOTE: - If an sample fleet consists of only 1 aircraft, the next check containing sampling inspections (e.g.
6 YE inspection) should be performed on this aircraft before it is removed from the sample fleet and
replaced by another one (change of status). This is to achieve inspection data which are representative
for the specific environment / operation.
Sampling Inspection findings
Based on the results of Sampling Program inspections the following applies:
– In case of findings operator should report it to aircraft manufacturer and consult with manufacturer
for taking appropriate corrective actions, such as change of program concept, decrease in interval,
application of TPS etc.
– In case of no finding, the current inspections continue to apply.
Airest policy: The Sampling Program inspections are to be performed on the oldest 1/5 aircraft of the Airest
AIRBUS-family fleet.
The oldest aircraft are defined as the aircraft with the highest age in years since their initial manufacturer’s
delivery date. Operators with a mix of A318, A319, A320 and A321 aircraft can consider this as a combined
fleet for the purpose of sample aircraft selection.
If the number of aircraft selected is not a whole number, the number can be decreased to the next lower
whole number. The minimum sample size is one aircraft. The maximum number of aircraft to be sampled is 5
aircraft even if the total fleet size would lead to a higher number applying the 20% rule.
− If the 1/5 sample of the fleet is not a whole number of aircraft, the number can be decreased to the
next lower whole number.
− A minimum of one aircraft must be selected for the Sampling Program.
− Any significant change to Airest AIRBUS-family fleet will require a review of the Sampling Program
aircraft. This includes buying and/or selling aircraft and retiring aircraft from the fleet.
Following are the selected sampling aircraft:
Aircraft Type Registration Number MSN:
A320 ES-LAA 02157
3.18. Structural Repair
Details for the execution of structure repairs can be found in the A320 Structural Repair Manual (SRM) Chapter
51 thru 57. Structure and corrosion repairs should be performed i.a.w. the SRM. Repairs (structure / corrosion)
which are not covered in the SRM must be performed i.a.w. Part 21 or TC holder requirements. All significant
structural damages and /or major corrosion findings must be reported to the TC/STC holder and ECAA.
Refer to Appendix G for list of tasks with thresholds and repetitive intervals.
3.19. Weighing of aircraft
Aircraft weighing will be performed at least every 4 years [as required by Commission Regulation (EU) No
965/2012 CAT.POL.MAB.100 (b)]. If major modification or repair will be made, affecting weight and C.G of
aircraft, additional weighing shall be performed.
PART 3 Page 13 Rev. 1, 10.12.2019
A320 Aircraft Maintenance Program
PART 4. MAINTENANCE SCHEDULE
4.1. Inspection Standards
The standards applied to the individual task inspections of this Maintenance Program meet the requirements
of the airplane, engine and component TC / STC Holder’s recommended standards and practices detailed by
Type Certificate Holder in order to ensure safe, airworthy and reliable condition of operation. The
Maintenance Program includes all scheduled maintenance tasks for the aircraft and systems, as well as the
“on-wing” engines/apu tasks.
The contracted Part 145 approved maintenance organization must ensure that the standards applied to the
individual task inspections meet the requirements of the airplane, engine and component TC / STC Holder’s
recommended standards and practices and any additional standards specified by Airest CAME.
4.2. Maintenance Checks
The tasks identified in the MPD have specific accomplishment intervals. These intervals are controlled by the
following usage parameters; Flight Hours (FH), Flight Cycles (FC), Engine Hours (EH), Engine Cycles (EC), APU
Hours (APUH), and Calendar time (Months or Days).
The term "Check/Inspect," as used in this document, is construed to mean a maintenance action requiring a
thorough examination of an item, component, system or structure for general condition, as applicable, with
special emphasis directed to the following areas:
Proper attachment, safety wiring, cotter pins, fasteners, clamps, latches, tubing, plumbing, electrical wiring
and connections, linkages, bearings, alignment, clearance, lubrication, obvious damage, cracks, delamination,
fraying, operating pressures, fluid leakage, excess wear or play, corrosion, evidence of overheating, rubbing,
aging, preservative coating or finish, cleanliness and general appearance.
This Maintenance Program provides all the technical information necessary for planning and preparing the
maintenance tasks for a Maintenance Program. The periodic maintenance and inspection requirements for the
planning purposes are detailed in the preceding paragraphs.
Check AIRBUS A320 MPD INTERVAL
Pre-Flight Pre-Flight Check Before each flight.
48 Hour (Daily) Check 48 Hour (Daily) Check Not exceeding 48 Hours Elapsed Time.
Weekly Check Not Exceeding 8 Days Elapsed
SYSTEM AND ZONAL TASKS
A-Check Not exceeding 750 Flight Hours, 750 Flight Cycles or 4 Months (Whichever
Occurs First).
C-Check 1C Check & multiples - Not exceeding 7,500 Flight Hours or 5,000 Flight Cycles
or 24 Months (Whichever Occurs First).
STRUCTURES TASKS
6 Year Check Not exceeding 6 Years
12 Year Check Not exceeding 12 Years
Notes
Adjustments for training flights can be made by considering a full stop landing or two touch-and-go landings
equivalent to one flight cycle.
Refer to Appendix A for List of tasks
Refer to Appendix D for Daily and Weekly Check.
PART 4 Page 14 Rev. 0, 30.08.2019
A320 Aircraft Maintenance Program
4.3. Storage
Whenever the aircraft is not operatable for an extended time period, the Storage maintenance practices in
accordance with AMM chapter 10, 49, 72 will be applied.
An aircraft scheduled for storage must have calendar inspection tasks that become due during storage. These
tasks can be carried over and completed before the aircraft returns to service.
4.4. Permitted Variations of Maintenance Periods
For planning purposes, it may become necessary to postpone a periodical check (items) for a short time to
beyond the interval limit as stipulated in this Maintenance Schedule.
Items Controlled by Flying Hours.
• Up to 5000 flying hours .....................10%,
• More than 5000 flying hours ............500 flying hours
(b) Items Controlled by Landing/Cycles
• Up to 500 landings/cycles ................5% or 25 landings/cycles, whichever is the lesser
• More than 500 landings/cycles ....... 5% or 250 landings/cycles, whichever is the lesser
(c) Items Controlled by Calendar Time.
• Up to 1 year ............................................................. 10% or 1 month whichever is the lesser
• More than 1 year, but not exceeding 3 years ......... 2 Months
• More than 3 years ................................................... 3 Months
For items controlled by more than one limit, e.g. items controlled by flying hours and calendar time or flying
hours and landings/cycles, the more restrictive limit shall be applied.
The variations permitted above do not apply to:
Those components for which an ultimate scrap life or retirement life has been prescribed (e.g. primary
structure, components with fatigue lives, and high energy rotating parts for which containment is not
provided). Details concerning all items of this nature are included in the Type Certificate Holders documents or
manuals, and are to be included in the Maintenance Program.
Those tasks included in the Maintenance Program which have been classified as mandatory by the Type
Certificate holder or EASA/FAA. Certification Maintenance Requirements (CMR) and Airworthiness Limitations
(ALI) unless specifically approved by the manufacturer and agreed by the ECAA.
For an overhauled landing gear or a new landing gear installed after first Transfer of Title: the start date for
Calendar Time tasks is the date of the gear’s first flight after installation. If this first flight takes place more
than 90 days after installation contact Airbus Maintenance Programs Engineering front desk:
[email protected]. For the original LDG, paragraph ‘A. General Rule’ applies
4.5. Abbreviations
All significant terms and abbreviations used within this Program are defined in accordance with the Type
Certificate Holders definitions, current EASA, FAA and NAA definitions or, in the absence of formal definitions,
those quoted in the World Airlines Technical Operations Glossary (WATOG).
PART 4 Page 15 Rev. 0, 30.08.2019
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200001-01-1 571 FNC HIRF/LIGHTNING PROTECTION-WING EL MRB L/HIRF MRB 20-00-01-1 249200-210-022 36 MO N/A
671
CHECK BONDING MEASUREMENT OF CLAMPS WITH A LOOP
TESTER FROM FUSELAGE TO RIB 9
2-20 200001-02-1 511 FNC HIRF/LIGHTNING PROTECTION-WING EL MRB L/HIRF MRB 20-00-01-2 249200-210-023 72 MO APPL
520 MRB 20-00-01-3
611 CHECK THAT THE CONNECTOR IS CORRECTLY TIGHTENED BY
620 MEASUREMENT OF THE RESISTANCE WITH A LOOP TESTER:
- 4005VC, 4007VC, 4009VC, 4011VC, LH SIDE
- 4013VC, 4015VC, 4017VC, 4019VC, LH SIDE
- 4006VC, 4008VC, 4010VC, 4012VC, RH SIDE
- 4014VC, 4016VC, 4018VC, 4020VC, RH SIDE
2-20 200002-01-1 334 GVI HIRF/LIGHTNING PROTECTION-THS T/E EL MRB L/HIRF MRB 20-00-02-1 249200-210-018 36 MO APPL
344
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES:
- 405VB, 406VB, 407VB, 408VB, 409VB, LH SIDE
- 400VB, 401VB, 402VB, 403VB, 404VB, RH SIDE
2-20 200003-01-1 321 GVI HIRF/LIGHTNING PROTECTION-VERTICAL FIN EL MRB L/HIRF MRB 20-00-03-1 249200-210-019 72 MO APPL
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES:
- 4202VB, 4204VB
2-20 200003-02-1 322 GVI HIRF/LIGHTNING PROTECTION-VERTICAL FIN EL MRB L/HIRF MRB 20-00-03-2 249200-210-020 72 MO APPL
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES:
- 4202VB, 4204VB
2-20 200003-03-1 324 GVI HIRF/LIGHTNING PROTECTION-VERTICAL FIN EL MRB L/HIRF MRB 20-00-03-3 249200-210-021 72 MO APPL
GENERAL VISUAL INSPECTION OF ELEMENTS FITTED ON THE
FOLLOWING HARNESSES:
- 4202VB, 4204VB
2-20 200121-01-1 121 RST FORWARD AVIONIC COMPARTMENT AF MRB MRB 20.0.121/01 249200-100-004 48 MO APPL
122
CLEANING OF EWIS INSTALLED IN THE FORWARD AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)
200121-02-1 ************** TASK DELETED ************** N/A
2-20 200121-03-1 121 GVI FORWARD AVIONIC COMPARTMENT AF MRB MRB 20.0.121/03 249200-210-028 72 MO APPL
122
GENERAL VISUAL INSPECTION OF 90, 108, 109 VU IN THE
FORWARD AVIONIC COMPARTMENT (EWIS)
2-20 200121-04-1 121 DET FORWARD AVIONIC COMPARTMENT AF MRB MRB 20.0.121/04 249200-220-005 72 MO APPL
122
DETAILED INSPECTION OF G, E AND P ROUTES IN THE
FORWARD AVIONIC COMPARTMENT (EWIS)
2-20 200125-01-1 125 RST LATERAL AVIONIC COMPARTMENT AF MRB MRB 20.0.125/01 249200-100-031 72 MO APPL
126
CLEANING OF EWIS INSTALLED IN THE LATERAL AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200125-02-1 125 RST LATERAL AVIONIC COMPARTMENT AF MRB MRB 20.0.125/02 249200-100-028 72 MO N/A
126
CLEANING OF EWIS INSTALLED IN THE LATERAL AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
APPENDIX A
AEG/AMP/A320 Page 1 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
200125-03-1 ************** TASK DELETED ************** N/A
200125-04-1 ************** TASK DELETED ************** N/A
2-20 200125-05-1 125 GVI LATERAL AVIONIC COMPARTMENT AF MRB MRB 20.0.125/05 249200-210-030 72 MO APPL
126
GENERAL VISUAL INSPECTION OF 105, 106, 103, 107 AND
70 VUS INSTALLED IN THE LATERAL AVIONIC COMPARTMENT
(EWIS)
2-20 200125-06-1 125 DET LATERAL AVIONIC COMPARTMENT AF MRB MRB 20.0.125/06 249200-220-008 72 MO APPL
126
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED IN
THE LATERAL AVIONIC COMPARTMENT (EWIS)
2-20 200125-07-1 125 DET LATERAL AVIONIC COMPARTMENT AF MRB MRB 20.0.125/07 249200-220-009 72 MO N/A
126
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED IN
THE LATERAL AVIONIC COMPARTMENT (EWIS)
200127-01-1 ************** TASK DELETED ************** N/A
2-20 200127-02-1 127 RST REAR AVIONIC COMPARTMENT AF MRB MRB 20.0.127/02 249200-100-013 72 MO APPL
128
CLEANING OF EWIS INSTALLED IN THE REAR AVIONIC
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
200127-03-1 ************** TASK DELETED ************** N/A
200127-04-1 ************** TASK DELETED ************** N/A
2-20 200127-05-1 127 GVI REAR AVIONIC COMPARTMENT AF MRB MRB 20.0.127/05 249200-210-034 72 MO APPL
128
GENERAL VISUAL INSPECTION OF 80, 63, 187, 188 VU
INSTALLED IN THE REAR AVIONIC COMPARTMENT (EWIS)
200127-06-1 ************** TASK DELETED ************** N/A
2-20 200127-07-1 127 DET REAR AVIONIC COMPARTMENT AF MRB MRB 20.0.127/07 249200-220-007 72 MO APPL
128
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED IN
THE REAR AVIONIC COMPARTMENT (EWIS)
2-20 200129-01-1 129 RST STAIR BAY AF MRB MRB 20.0.129/01 249200-100-032 72 MO N/A
CLEANING OF EWIS INSTALLED IN THE STAIR BAY (ONLY IF
CONTAMINATED) (EWIS)
2-20 200129-02-1 129 GVI STAIR BAY AF MRB MRB 20.0.129/02 249200-210-809 48 MO N/A
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
STAIR BAY (EWIS)
2-20 200129-03-1 129 DET STAIR BAY AF MRB MRB 20.0.129/03 249200-220-010 72 MO N/A
DETAILED INSPECTION OF G, E AND P ROUTES INSTALLED IN
THE STAIR BAY (EWIS)
2-20 200131-01-1 131 RST FORWARD CARGO COMPARTMENT AF MRB MRB 20.0.131/01 249200-100-025 72 MO APPL
132
CLEANING OF EWIS INSTALLED IN THE FORWARD CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200131-02-1 131 GVI FORWARD CARGO COMPARTMENT AF MRB MRB 20.0.131/02 249200-210-805 144 MO APPL
132
GENERAL VISUAL INSPECTION OF G, E AND P ROUTES
INSTALLED IN THE FORWARD CARGO COMPARTMENT (EWIS)
2-20 200131-03-1 131 GVI FORWARD CARGO COMPARTMENT AF MRB MRB 20.0.131/03 249200-210-048 72 ACT MO N/A
132
GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THE
ACT(S) (EWIS)
NOTE:
THIS TASK COULD BE PERFORMED AT THE OPPORTUNITY OF
R/I
2-20 200133-01-1 133 RST UNDERFLOOR BAY OF FWD CARGO COMPARTMENT AF MRB MRB 20.0.133/01 249200-100-024 72 MO APPL
134
CLEANING OF EWIS INSTALLED IN THE UNDERFLOOR BAY OF
FORWARD CARGO COMPARTMENT (ONLY IF CONTAMINATED)
(EWIS)
APPENDIX A
AEG/AMP/A320 Page 2 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200137-01-1 137 RST BAY BEHIND FWD CARGO COMPARTMENT AF MRB MRB 20.0.137/01 249200-100-029 72 MO APPL
138
CLEANING OF EWIS INSTALLED IN THE BAY BEHIND FWD
CARGO COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200141-01-1 141 GVI WING CENTRE BOX AF MRB MRB 20.0.141/01 249200-210-026 144 MO APPL
142
GENERAL VISUAL INSPECTION OF EXPOSED EWIS INSTALLED
IN THE WING CENTRE BOX (EWIS)
2-20 200145-01-1 145 RST ZONE UNDER CABIN FLOOR AF MRB MRB 20.0.145/01 249200-100-015 72 MO APPL
146
CLEANING OF EWIS INSTALLED IN THE ZONE UNDER CABIN
FLOOR (ONLY IF CONTAMINATED) (EWIS)
2-20 200151-01-1 151 RST AFT CARGO COMPARTMENT AF MRB MRB 20.0.151/01 249200-100-026 72 MO APPL
152
CLEANING OF EWIS INSTALLED IN THE AFT CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200151-02-1 151 GVI AFT CARGO COMPARTMENT AF MRB MRB 20.0.151/02 249200-210-806 144 MO APPL
152
GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED IN
AFT CARGO COMPARTMENT (EWIS)
2-20 200151-03-1 151 GVI AFT CARGO COMPARTMENT AF MRB MRB 20.0.151/03 249200-210-046 72 ACT MO N/A
152
GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THE
ACT(S) (EWIS)
NOTE:
THIS TASK COULD BE PERFORMED AT THE OPPORTUNITY OF
R/I
2-20 200161-01-1 161 RST BULK CARGO COMPARTMENT AF MRB MRB 20.0.161/01 249200-100-030 72 MO APPL
162
CLEANING OF EWIS INSTALLED IN THE BULK CARGO
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200161-02-1 161 GVI BULK CARGO COMPARTMENT AF MRB MRB 20.0.161/02 249200-210-047 72 ACT MO N/A
162
GENERAL VISUAL INSPECTION OF EWIS INSTALLED AT THE
ACT(S) (EWIS)
NOTE:
THIS TASK COULD BE PERFORMED AT THE OPPORTUNITY OF
R/I
2-20 200171-01-1 171 RST AFT CABIN UNDERFLOOR COMPARTMENT AF MRB MRB 20.0.171/01 249200-100-001 144 MO APPL
172
CLEANING OF EWIS INSTALLED IN THE AFT CABIN
UNDERFLOOR COMPARTMENT (ONLY IF CONTAMINATED)(EWIS)
2-20 200191-01-1 191 RST AIR CONDITIONING COMPARTMENT AND FAIRINGS AF MRB MRB 20.0.191/01 249200-100-027 72 MO APPL
192
CLEANING OF EWIS INSTALLED IN THE AIR CONDITIONING
COMPARTMENT AND FAIRINGS (ONLY IF CONTAMINATED)
(EWIS)
2-20 200211-01-1 211 RST COCKPIT AF MRB MRB 20.0.211/01 249200-100-016 144 MO APPL
212
CLEANING OF EWIS INSTALLED IN THE COCKPIT (ONLY IF
CONTAMINATED) (EWIS)
2-20 200211-02-1 211 RST COCKPIT AF MRB MRB 20.0.211/02 249200-100-017 72 MO APPL
212
CLEANING OF EWIS INSTALLED IN 49VU AND 120VU (ONLY IF
CONTAMINATED) (EWIS)
2-20 200211-03-1 211 GVI COCKPIT AF MRB MRB 20.0.211/03 249200-210-035 144 MO APPL
212
GENERAL VISUAL INSPECTION OF EWIS OF 49VU AND THE
120VU (EWIS)
APPENDIX A
AEG/AMP/A320 Page 3 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200221-01-1 221 RST FORWARD CABIN UTILITY AREA AF MRB MRB 20.0.221/01 249200-100-007 144 MO APPL
222
CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN
UTILITY AREA (ONLY IF CONTAMINATED) (EWIS)
2-20 200223-01-1 223 RST FORWARD CABIN OVERHEAD COMPARTMENT AF MRB MRB 20.0.223/01 249200-100-010 144 MO APPL
224
CLEANING OF EWIS INSTALLED IN THE FORWARD CABIN
OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200223-02-1 223 GVI FORWARD CABIN OVERHEAD COMPARTMENT AF MRB MRB 20.0.223/02 249200-210-029 144 MO APPL
224
GENERAL VISUAL INSPECTION OF EWIS OF THE 2000VU
(EWIS)
2-20 200231-01-1 231 RST FORWARD PASSENGER COMPARTMENT AF MRB MRB 20.0.231/01 249200-100-002 144 MO APPL
232
CLEANING OF EWIS INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200231-02-1 231 RST FORWARD PASSENGER COMPARTMENT AF MRB MRB 20.0.231/02 249200-100-012 144 MO N/A
232
CLEANING OF EWIS INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200231-03-1 231 GVI FORWARD PASSENGER COMPARTMENT AF MRB MRB 20.0.231/03 249200-210-036 72 MO N/A
232
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEAT AND A/C INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT (EWIS)
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS BETWEEN SEAT AND A/C ONLY
2-20 200233-01-1 233 RST FORWARD PASSENGER COMPARTMENT OVERHEAD COMPARTMENT AF MRB MRB 20.0.233/01 249200-100-005 144 MO APPL
234
CLEANING OF EWIS INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT OVERHEAD COMPARTMENT (ONLY IF
CONTAMINATED) (EWIS)
2-20 200233-02-1 233 RST FORWARD PASSENGER COMPARTMENT OVERHEAD COMPARTMENT AF MRB MRB 20.0.233/02 249200-100-011 144 MO N/A
234
CLEANING OF EWIS INSTALLED IN THE FORWARD PASSENGER
COMPARTMENT OVERHEAD COMPARTMENT (ONLY IF
CONTAMINATED) (EWIS)
APPENDIX A
AEG/AMP/A320 Page 4 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200233-03-1 233 GVI FORWARD PASSENGER COMPARTMENT OVERHEAD COMPARTMENT AF MRB MRB 20.0.233/03 249200-210-810 144 MO APPL
234
GENERAL VISUAL INSPECTION OF ALL G & P ROUTES
INSTALLED IN THE FORWARD PASSENGER COMPARTMENT
OVERHEAD COMPARTMENT (EWIS)
2-20 200233-04-1 233 GVI FORWARD PASSENGER COMPARTMENT OVERHEAD COMPARTMENT AF MRB MRB 20.0.233/04 249200-210-811 144 MO N/A
234
GENERAL VISUAL INSPECTION OF ALL G & P ROUTES
INSTALLED IN THE FORWARD PASSENGER COMPARTMENT
OVERHEAD COMPARTMENT (EWIS)
2-20 200241-01-1 241 RST CENTER PASSENGER COMPARTMENT AF MRB MRB 20.0.241/01 249200-100-003 144 MO APPL
242
CLEANING OF EWIS INSTALLED IN THE CENTER PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200241-02-1 241 RST CENTER PASSENGER COMPARTMENT AF MRB MRB 20.0.241/02 249200-100-008 144 MO N/A
242
CLEANING OF EWIS INSTALLED IN THE CENTER PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200241-03-1 241 GVI CENTER PASSENGER COMPARTMENT AF MRB MRB 20.0.241/03 249200-210-031 144 MO APPL
242
GENERAL VISUAL INSPECTION OF G ROUTES INSTALLED
AROUND FR 47/48 (A320)/FR 47.1 (A321)/FR 47/51
(A319)/FR 47/54 (A318) (EWIS)
2-20 200241-04-1 241 GVI CENTER PASSENGER COMPARTMENT AF MRB MRB 20.0.241/04 249200-210-037 72 MO N/A
242
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE CENTER PASSENGER
COMPARTMENT (EWIS)
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS BETWEEN SEAT AND A/C ONLY
2-20 200243-01-1 243 RST CENTER PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.243/01 249200-100-009 144 MO APPL
244
CLEANING OF EWIS INSTALLED IN THE CENTER PASSENGER
OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200243-02-1 243 RST CENTER PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.243/02 249200-100-014 144 MO N/A
244
CLEANING OF EWIS INSTALLED IN THE CENTER PASSENGER
OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200243-03-1 243 GVI CENTER PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.243/03 249200-210-041 144 MO APPL
244
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE CENTER PASSENGER OVERHEAD COMPARTMENT (EWIS)
2-20 200243-04-1 243 GVI CENTER PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.243/04 249200-210-038 144 MO N/A
244
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE CENTER PASSENGER OVERHEAD COMPARTMENT (EWIS)
APPENDIX A
AEG/AMP/A320 Page 5 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200251-01-1 251 RST AFT PASSENGER COMPARTMENT AF MRB MRB 20.0.251/01 249200-100-018 144 MO N/A
252
CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200251-02-1 251 RST AFT PASSENGER COMPARTMENT AF MRB MRB 20.0.251/02 249200-100-019 144 MO APPL
252
CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200251-03-1 251 GVI AFT PASSENGER COMPARTMENT AF MRB MRB 20.0.251/03 249200-210-039 72 MO N/A
252
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE AFT PASSENGER
COMPARTMENT (EWIS)
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS BETWEEN SEAT AND A/C ONLY
2-20 200253-01-1 253 RST AFT PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.253/01 249200-100-021 144 MO APPL
254
CLEANING OF EWIS INSTALLED IN THE AFT PASSENGER
OVERHEAD COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200253-02-1 253 GVI AFT PASSENGER OVERHEAD COMPARTMENT AF MRB MRB 20.0.253/02 249200-210-042 144 MO APPL
254
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE AFT PASSENGER OVERHEAD COMPARTMENT (EWIS)
2-20 200261-01-1 261 RST AFT CABIN UTILITY AREA AF MRB MRB 20.0.261/01 249200-100-022 144 MO APPL
262
CLEANING OF EWIS INSTALLED IN THE AFT CABIN UTILITY
AREA (ONLY IF CONTAMINATED) (EWIS)
2-20 200261-02-1 261 GVI AFT CABIN UTILITY AREA AF MRB MRB 20.0.261/02 249200-210-044 144 MO APPL
262
GENERAL VISUAL INSPECTION OF P ROUTES INSTALLED IN
THE AFT CABIN UTILITY AREA (EWIS)
2-20 200261-03-1 261 GVI AFT CABIN UTILITY AREA AF MRB MRB 20.0.261/03 249200-210-040 72 MO N/A
262
GENERAL VISUAL INSPECTION OF EWIS CONNECTIONS,
ATTACHMENT POINTS AND ELECTRICAL CONNECTORS BETWEEN
SEATS AND A/C INSTALLED IN THE AFT CABIN UTILITY AREA
(EWIS)
NOTE:
THIS TASK IS APPLICABLE FOR A/C VERSIONS WITH SEATS
AND WITH EWIS CONNECTIONS BETWEEN SEAT AND A/C ONLY
2-20 200263-01-1 263 RST AFT CABIN OVERHEAD COMPARTMENT AF MRB MRB 20.0.263/01 249200-100-023 144 MO APPL
264
CLEANING OF EWIS INSTALLED IN THE AFT CABIN OVERHEAD
COMPARTMENT (ONLY IF CONTAMINATED) (EWIS)
2-20 200263-02-1 263 GVI AFT CABIN OVERHEAD COMPARTMENT AF MRB MRB 20.0.263/02 249200-210-043 144 MO APPL
264
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE AFT CABIN OVERHEAD COMPARTMENT (EWIS)
APPENDIX A
AEG/AMP/A320 Page 6 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200263-03-1 263 GVI AFT CABIN OVERHEAD COMPARTMENT AF MRB MRB 20.0.263/03 249200-210-045 144 MO APPL
264
GENERAL VISUAL INSPECTION OF ALL EWIS OF 2001 VU
(EWIS)
2-20 200315-01-1 315 GVI TAIL CONE AND APU ACCESSORY COMPARTMENT AF MRB MRB 20.0.315/01 249200-210-025 72 MO APPL
316
GENERAL VISUAL INSPECTION OF G AND P ROUTES INSTALLED
IN THE TAIL CONE AND APU ACCESSORY COMPARTMENT (EWIS)
2-20 200413-01-1 413 DET UPPER FORWARD PYLON AF MRB MRB 20.0.413/01 249200-220-001 72 MO APPL
414
423 DETAILED INSPECTION OF EWIS INSTALLED IN THE UPPER
424 FORWARD PYLON (EWIS)
2-20 200413-02-1 413 DET UPPER FORWARD PYLON AF MRB MRB 20.0.413/02 249200-220-002 24 MO N/A
414
423 DETAILED INSPECTION OF EWIS INSTALLED IN THE UPPER
424 FORWARD PYLON (EWIS)
2-20 200413-03-1 413 DET UPPER FORWARD PYLON AF MRB MRB 20.0.413/03 249200-220-001 72 MO N/A
414
423 DETAILED INSPECTION OF EWIS INSTALLED IN THE UPPER
424 FORWARD PYLON (EWIS)
2-20 200413-04-1 413 GVI UPPER FORWARD PYLON AF MRB MRB 20.0.413/04 249200-210-818 48 MO N/A
414
423 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
424 UPPER FORWARD PYLON (EWIS)
2-20 200413-05-1 413 GVI UPPER FORWARD PYLON AF MRB MRB 20.0.413/05 249200-210-819 48 MO N/A
414
423 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
424 UPPER FORWARD PYLON (EWIS)
2-20 200415-01-1 415 GVI PYLON PRIMARY STRUCTURE AF MRB MRB 20.0.415/01 249200-210-816 48 MO N/A
425
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
PYLON PRIMARY STRUCTURE (EWIS)
2-20 200415-02-1 415 GVI PYLON PRIMARY STRUCTURE AF MRB MRB 20.0.415/02 249200-210-821 48 MO N/A
425
GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
PYLON PRIMARY STRUCTURE (EWIS)
2-20 200435-01-1 435 DET FAN COMPARTMENT AF MRB MRB 20.0.435/01 249200-220-003 24 MO APPL
436
445 DETAILED INSPECTION OF EWIS IN THE FAN AND ACCESSORY
446 GEAR BOX (EWIS)
2-20 200435-02-1 435 DET FAN COMPARTMENT AF MRB MRB 20.0.435/02 249200-220-802 24 MO N/A
436
445 DETAILED INSPECTION OF EWIS INSTALLED IN THE FAN
446 COMPARTMENT (EWIS)
2-20 200435-03-1 435 DET FAN COMPARTMENT AF MRB MRB 20.0.435/03 249200-220-804 24 MO N/A
436
445 DETAILED INSPECTION OF EWIS INSTALLED IN THE FAN
446 COMPARTMENT (EWIS)
2-20 200453-01-1 453 DET CORE COMPARTMENT AF MRB MRB 20.0.453/01 249200-220-004 24 MO APPL
454
463 DETAILED INSPECTION OF EWIS INSTALLED IN THE HOT
464 SECTION (EWIS)
2-20 200453-02-1 453 DET CORE COMPARTMENT AF MRB MRB 20.0.453/02 249200-220-803 24 MO N/A
454
463 DETAILED INSPECTION OF EWIS INSTALLED IN THE CORE
464 COMPARTMENT (EWIS)
2-20 200453-03-1 453 DET CORE COMPARTMENT AF MRB MRB 20.0.453/03 249200-220-805 24 MO N/A
454
463 DETAILED INSPECTION OF EWIS INSTALLED IN THE CORE
464 COMPARTMENT (EWIS)
2-20 200471-01-1 471 GVI PYLON TO WING LEADING EDGE AF MRB MRB 20.0.471/01 249200-210-817 48 MO N/A
472
481 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
482 PYLON TO WING LEADING EDGE (EWIS)
APPENDIX A
AEG/AMP/A320 Page 7 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-20 200471-02-1 471 GVI PYLON TO WING LEADING EDGE AF MRB MRB 20.0.471/02 249200-210-820 48 MO N/A
472
481 GENERAL VISUAL INSPECTION OF EWIS INSTALLED IN THE
482 PYLON TO WING LEADING EDGE (EWIS)
2-20 200540-02-1 540 GVI WING FUEL TANK AF MRB MRB 20.0.540/02 249200-210-801 144 MO APPL
640
GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE
WING FUEL TANK (EWIS)
2-20 200540-03-1 540 GVI WING FUEL TANK AF MRB MRB 20.0.540/03 249200-210-801 144 MO N/A
640
GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE
WING FUEL TANK (EWIS)
2-20 200550-01-1 550 GVI VENT SURGE TANK AF MRB MRB 20.0.550/01 249200-210-802 144 MO APPL
650
GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE
VENT SURGE TANK (EWIS)
2-20 200560-01-1 560 GVI DRY BAY (OUTBOARD) AF MRB MRB 20.0.560/01 249200-210-803 144 MO APPL
660
GENERAL VISUAL INSPECTION OF EXPOSED EWIS WITHIN THE
DRY BAY (OUTBOARD) (EWIS)
2-20 200571-01-1 571 GVI MLG BAY AF MRB MRB 20.0.571/01 249200-210-804 144 MO APPL
671
GENERAL VISUAL INSPECTION OF P ROUTE PUMP FEEDER
(EWIS)
2-21 212100-01-1 131 RST AIR DISTRIBUTION AND RECIRCULATION AF LUR MRB 21.21.00/05 212149-100-001 180 MO APPL
MRB 9 OR
CLEAN COCKPIT AIR SUPPLY DUCTING GRID 24000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
212100-02-1 ************** TASK DELETED ************** N/A
2-21 212141-01-1 130 DIS RECIRCULATION FILTER AF LUR MRB 21.21.00/02 212141-920-002 36 MO APPL
MRB 9 OR
DISCARD FILTER ELEMENTS OF RECIRCULATION SYSTEM 5000 FH
212300-01-1 ************** TASK DELETED ************** N/A
2-21 212300-02-1 200 DIS LAVATORY AND GALLEY VENTILATION AF LUR MRB 21.23.00/03 212300-600-001 12 MO APPL
MRB 7 OR
DISCARD LAVATORY AIR EXTRACTION FILTER ELEMENT 1000 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-21 212300-04-1 200 DIS LAVATORY AND GALLEY VENTILATION AF LUR MRB 21.23.00/04 443435-920-001 12 MO N/A
MRB 9 OR
DISCARD FILTER ELEMENT OF GSM ON BOARD EQUIPMENT RACK 1200 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-21 212600-01-1 210 OPC AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/02 212600-710-001 6 MO APPL
MRB 9 MRB 26.15.00/01 OR
OPERATIONAL CHECK OF SYSTEM VIA MCDU 750 FH
APPENDIX A
AEG/AMP/A320 Page 8 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-21 212600-02-1 210 OPC AVIONICS EQUIPMENT VENTILATION AF MRB 8 MRB 21.26.00/03 212600-710-002 36 MO APPL
OR
OPERATIONAL CHECK OF OVERRIDE FUNCTION (BLOWER AND 10000 FH
EXTRACT)
2-21 212600-03-1 210 OPC AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/04 212600-710-003 108 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF SMOKE CONFIGURATION CONTROL 12000 FH
CIRCUIT
2-21 212600-04-1 210 OPC AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/05 212600-710-004 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF DITCHING CONFIGURATION CONTROL 24000 FH
CIRCUIT
2-21 212600-05-1 120 DET AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/06 212642-200-003 252 MO APPL
MRB 9 OR
DETAILED INSPECTION OF SKIN HEAT EXCHANGER DRAIN HOSE 36000 FH
CONNECTION AREA
2-21 212600-06-1 120 DET AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/08 212642-210-001 252 MO N/A
MRB 9 OR
DETAILED INSPECTION OF DEMISTER DRAIN HOSE CONNECTION 36000 FH
AREA
2-21 212600-08-1 127 OPC AVIONICS EQUIPMENT VENTILATION AF MRB 9 MRB 21.26.00/16 212656-280-002 24 MO APPL
OPERATIONAL CHECK OF AIR INLET CHECK VALVE 2150 HM
2-21 212600-09-1 120 RST AVIONICS EQUIPMENT VENTILATION AF MRB 9 MRB 21.26.00/19 122113-100-002 48 MO APPL
NOTE
CLEAN GRID OF RELAY BOX VU PANELS
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-21 212600-11-1 127 DIS AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/21 212643-600-016 36 MO N/A
MRB 6 OR
DISCARD DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE 3600 FH
(LE BOZEC) NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-21 212641-01-1 128 DET AVIONICS EQUIPMENT VENTILATION AF MRB 9 MRB 21.26.00/07 212641-210-001 144 MO APPL
DETAILED INSPECTION OF CHECK VALVE FLAPPERS FOR
CONDITION AND OPERATION
2-21 212643-01-1 120 DIS AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/09 212643-600-001 6 MO N/A
MRB 6 OR
DISCARD DEMISTER FILTER ELEMENT (LE BOZEC) 600 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 212643-02-1 120 DIS AVIONICS EQUIPMENT VENTILATION AF LUR MRB 21.26.00/10 212643-600-002 12 MO N/A
MRB 6 OR
DISCARD FILTER CARTRIDGE (LE BOZEC) 1000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
APPENDIX A
AEG/AMP/A320 Page 9 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-21 212643-06-1 120 DET AVIONICS VENTILATION DEMISTER AF LUR MRB 21.26.00/11 212643-200-001 6 MO N/A
MRB 6 OR
CHECK DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE 600 FH
CLOGGING INDICATORS (POP OUT INDICATOR NOT VISIBLE) NOTE
(LE BOZEC)
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 212643-07-1 120 DIS AVIONICS VENTILATION DUST SEPARATOR AF MRB 6 MRB 21.26.00/13 212643-920-001 NOTE YES APPL
DISCARD FILTER CARTRIDGE (PALL)
NOTE:
INTERVAL:
- DISCARD INTERVAL FOR FILTER CARTRIDGE (PALL) IS
SPECIFIED BY P/N: - P/N QB0511: 1000 FH - P/N
QB0639: 1600 FH - P/N QB0776: 2000 FH
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 212643-09-1 120 OPC AVIONICS VENT. WATER/MOISTURE SEP. EL LUR MRB 21.26.00/14 212643-710-001 12 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF NRV FOR FREE MOVEMENT 1500 FH
2-21 212643-10-1 120 DET AVIONICS VENT. WATER/MOISTURE SEP. EL LUR MRB 21.26.00/15 212643-100-001 36 MO APPL
MRB 9 OR
INSPECTION OF THE SIPHON ASSEMBLY (STRAINER) FOR 3000 FH
CLEANLINESS
2-21 212643-11-1 120 DET AVIONICS VENTILATION DEMISTER AF LUR MRB 21.26.00/17 212642-200-004 6 MO N/A
MRB 6 OR
CHECK DEMISTER FILTER ELEMENT AND FILTER CARTRIDGE 500 FH
USING PRESSURE PORTS (LE BOZEC) NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 212700-01-1 210 OPC AVIONICS EQUIPMENT GROUND COOLING AF MRB 9 MRB 21.27.00/02 212700-710-001 48 MO N/A
OR
OPERATIONAL CHECK OF FAULT WARNING 12000 FH
2-21 212700-02-1 210 OPC AVIONICS EQUIPMENT GROUND COOLING AF LUR MRB 21.27.00/01 212742-200-002 72 MO N/A
MRB 9 OR
CHECK DRAIN TAPPING FOR CONDITION 5500 FH
2-21 212700-03-1 210 DET AVIONICS EQUIPMENT GROUND COOLING AF MRB 9 MRB 21.27.00/03 212742-210-001 72 MO N/A
OR
DETAILED INSPECTION OF DEMISTER DRAIN HOSE CONNECTION 22000 FH
AREA
2-21 212700-05-1 120 OPC AVIONICS EQUIPMENT GROUND COOLING AV MRB 9 MRB 21.27.00/05 212756-280-001 40 MO N/A
OPERATIONAL CHECK OF AIR INLET CHECK VALVE 2250 HM
2-21 212742-01-1 127 RST FILTER - GROUND COOLING AF LUR MRB 21.27.00/06 212742-600-001 6 MO YES N/A
MRB 7 OR
REMOVE FILTER (2200HM) FOR IN SHOP CLEANING 500 FH
212800-01-1 ************** TASK DELETED ************** N/A
2-21 212800-02-1 152 OPC CARGO COMPARTMENT, VENTILATION AND HEATING AND AFT AF LUR MRB 21.28.00/03 212800-710-007 108 MO N/A
CARGO COMPARTMENT GROUND COOLING SYSTEM MRB 8 OR
12000 FH
OPERATIONAL CHECK OF GROUND COOLING ISOLATION VALVE
TO VERIFY CLOSING IN CASE OF THE BULK CARGO DOOR
"FULL OPEN" SWITCH ACTUATION
2-21 212800-03-1 210 OPC CARGO COMPARTMENT, VENTILATION AND HEATING AND AFT AF CMR** CMR 212800-00001-1-C 261600-710-008 108 MO N/A
CARGO COMPARTMENT GROUND COOLING SYSTEM LUR MRB 21.28.00/04 OR
MRB 8 12000 FH
OPERATIONAL CHECK OF THE GROUND COOLING ISOLATION
VALVE TO VERIFY CLOSING IN CASE OF SMOKE WARNING
APPENDIX A
AEG/AMP/A320 Page 10 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-21 212800-04-1 152 DET CARGO COMPARTMENT, VENTILATION AND HEATING AND AFT AF MRB 6,9 MRB 21.28.00/05 212842-920-001 160 MO N/A
CARGO COMPARTMENT GROUND COOLING SYSTEM OR
18000 FC
DETAILED INSPECTION OF GROUND COOLING CHECK VALVE
FLAPPERS FOR CONDITION AND OPERATION
2-21 213100-01-1 210 OPC PRESSURE CONTROL AND MONITORING AF LUR MRB 21.31.00/02 213100-710-002 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF SYSTEM VIA MCDU 12000 FH
2-21 213100-02-1 210 FNC PRESSURE CONTROL AND MONITORING AF LUR MRB 21.31.00/03 213100-710-003 108 MO APPL
MRB 6,9 OR
OPERATIONAL CHECK OF MANUAL MODE SELECTION AND MANUAL 12000 FH
MODE PRESSURE CONTROL AND FUNCTIONAL CHECK OF MANUAL
MODE CABIN ALTITUDE INDICATION AND OUTFLOW VALVE
POSITION INDICATION
2-21 213100-03-1 210 OPC PRESSURE CONTROL AND MONITORING AF LUR MRB 21.28.00/02 213100-710-004 180 MO APPL
MRB 9 MRB 21.31.00/04 OR
OPERATIONAL CHECK OF OUTFLOW VALVE CLOSING IN 24000 FH
DITCHING CONFIGURATION
2-21 213100-04-1 210 OPC PRESSURE CONTROL AND MONITORING AF LUR MRB 21.31.00/05 213100-710-005 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF OUTFLOW VALVE PARTIAL OPENING BY 24000 FH
EMERGENCY RAM AIR SWITCH
NOTE:
PLANNING:
- TASK MAY BE COMBINED WITH TASK 215500-01-1.
2-21 213100-05-1 210 FNC PRESSURE CONTROL AND MONITORING AF CMR** CMR 213100-00001-1-C 213100-720-001 80 MO APPL
MRB 6,9 CMR 213100-00001-2-C OR
FUNCTIONAL CHECK OF POSITIVE/NEGATIVE DELTA "P" CMR 213100-00001-3-C 24000 FH
PROTECTION OF THE SAFETY VALVES. MRB 21.31.00/06
NOTE:
- THE FUNCTIONAL CHECK MAY ALTERNATIVELY BE
ACCOMPLISHED AS AN OFF AIRCRAFT TASK.
- THE CHECK OF POSITION INDICATION OF SAFETY VALVES
IS PART OF THIS TASK AFTER THE FUNCTIONAL
CHECK/RE-INSTALLATION.
- REFER TO ALS PART 3 FOR THE CMR** REQUIREMENTS
COVERED BY THIS TASKS FOR DIFFERENT AIRCRAFT
CONFIGURATIONS.
2-21 213100-08-1 260 RST PRESSURE CONTROL AND MONITORING AF MRB 9 MRB 21.31.00/07 213100-600-001 210 MO 210 MO YES APPL
SEMR SEMR 213100-00001-1-E OR OR
REMOVE SAFETY VALVE FOR IN SHOP RESTORATION 50000 FH 50000 FH
NOTE
NOTE:
THRESHOLD:
- FIRST ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER
THAN:
- 27/MAY/2018 (CORRESPONDING TO 24 MONTHS
FROM THE EFFECTIVE DATE OF THE EASA AD MANDATING
THE REVISION 03 AT ISSUE 02 OF A320FAM ALS PART 4)
OR
- WITHIN THE DUE THRESHOLD AND/OR INTERVAL (50
000 FH OR 210 MO, WHICHEVER OCCURS FIRST) WHICHEVER
OCCURS LATER.
2-21 215000-02-1 130 DET AIR COOLING AND TEMPERATURE CONTROL AF MRB 9 MRB 21.50.00/06 215243-210-001 144 MO APPL
190 OR
DETAILED INSPECTION OF PACK AIR CHECK VALVES FLAPPERS 36000 FH
FOR CONDITION AND OPERATION
2-21 215000-03-1 190 DET PACK RAM AIR INLET AF LUR MRB 21.50.00/13 216151-200-001 12 MO N/A
MRB 9 OR
DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLET 1800 FH
FLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLET
NOSE AND DIFFUSER RAMP
APPENDIX A
AEG/AMP/A320 Page 11 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-21 215000-03-2 190 DET PACK RAM AIR INLET AF LUR MRB 21.50.00/14 216151-200-001 108 MO APPL
MRB 9 OR
DETAILED INSPECTION OF ACTUATOR MECHANISM AND INLET 12000 FH
FLAP FOR EXCESSIVE PLAY AND CHECK GAP BETWEEN INLET
NOSE AND DIFFUSER RAMP
2-21 215000-04-1 190 DET PACK RAM AIR OUTLET AF LUR MRB 21.50.00/20 216152-200-001 72 MO N/A
MRB 9 OR
DETAILED INSPECTION OF RAM AIR OUTLET FLAP AND CHECK 6000 FH
FOR EXCESSIVE BACKLASH OF OUTLET FLAP
2-21 215000-04-2 190 DET PACK RAM AIR OUTLET AF LUR MRB 21.50.00/21 216152-200-001 108 MO N/A
MRB 9 OR
DETAILED INSPECTION OF RAM AIR OUTLET FLAP AND CHECK 12000 FH
FOR EXCESSIVE BACKLASH OF OUTLET FLAP
2-21 215141-01-1 191 FNC AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.50.00/10 215141-920-001 72 MO YES N/A
192 MRB 9 OR
REMOVE OZONE CONVERTER FOR IN SHOP FUNCTIONAL CHECK 9000 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-21 215200-01-1 191 RST AIR CONDITIONING PACK AF LUR MRB 21.50.00/12 215200-100-001 108 MO YES APPL
192 MRB 9 OR
REMOVE PRIMARY AND MAIN HEAT EXCHANGERS FOR IN SHOP 12000 FH
CLEANING. NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- IT IS RECOMMENDED TO PERFORMED THIS TASK AT THE
SAME TIME AS TASK 215222-01-1.
2-21 215200-02-1 191 RST AIR CONDITIONING PACK AF LUR MRB 21.50.00/18 215200-100-002 72 MO YES N/A
192 MRB 9 OR
REMOVE REHEATER FOR IN SHOP CLEANING. 5500 FH
2-21 215200-02-2 191 RST AIR CONDITIONING PACK AF LUR MRB 21.50.00/15 215200-100-002 108 MO YES APPL
192 MRB 9 OR
REMOVE REHEATER FOR IN SHOP CLEANING. 12000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 215200-04-1 191 FNC AIR CONDITIONING PACK AF LUR MRB 21.50.00/16 215200-790-001 144 MO YES APPL
192 MRB 9 OR
REMOVE CONDENSER FOR IN SHOP LEAK CHECK 18000 FH
2-21 215200-07-1 191 DIS AIR COOLING AND TEMPERATURE CONTROL AF MRB 6,9 MRB 21.50.00/17 215200-920-001 48 MO N/A
192 OR
DISCARD COMBO SEALS AND PERISEALS ON HOT AIR INLET 12000 FH
DUCTING, PACK DUCTING AND TRIM AIR DUCTING. NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- TASK MAY BE COMBINED WITH TASK 361100-05-1.
APPENDIX A
AEG/AMP/A320 Page 12 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-21 215200-08-1 191 DIS AIR COOLING AND TEMPERATURE CONTROL AF MRB 6,9 MRB 21.50.00/17 215200-920-002 48 MO APPL
192 OR
DISCARD O-RING SEALS ON HOT AIR INLET DUCTING, PACK 12000 FH
DUCTING AND TRIM AIR DUCTING. NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 215222-01-1 191 DET PLENUM CHAMBER AF LUR MRB 21.50.00/19 215200-200-001 108 MO APPL
192 MRB 9 OR
DETAILED INSPECTION OF INTERIOR AND EXTERIOR OF 12000 FH
PLENUM CHAMBER (10HM5 AND 11HM5) FOR SIGNS OF NOTE
DELAMINATION
NOTE:
PLANNING:
- IT IS RECOMMENDED TO PERFORMED THIS TASK AT THE
SAME TIME AS TASK 215200-01-1.
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-21 215500-01-1 210 OPC EMERGENCY RAM AIR INLET AF LUR MRB 21.50.00/04 215500-710-001 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET SYSTEM 24000 FH
NOTE:
PLANNING:
- TASK MAY BE COMBINED WITH TASK 213100-04-1.
2-21 215500-02-1 210 OPC EMERGENCY RAM AIR INLET AF LUR MRB 21.50.00/11 215500-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF EMERGENCY RAM AIR INLET AND FLOW 24000 FH
CONTROL VALVE CLOSING IN DITCHING CONFIGURATION
2-21 215541-01-1 137 DET EMERGENCY RAM AIR INLET CHECK VALVE AF LUR MRB 21.50.00/07 215541-210-001 252 MO APPL
MRB 9 OR
DETAILED INSPECTION OF EMERGENCY RAM AIR/LP GROUND 36000 FH
AIR CHECK VALVE FLAPPERS FOR CONDITION AND OPERATION
2-21 215800-01-1 191 RST AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.58.00/01 215800-200-001 72 MO YES N/A
MRB 9 OR
REMOVE CSAS OZONE CONVERTER FOR IN SHOP CLEANING 6000 FH
NOTE
NOTE:
INTERVAL:
- IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL REACTIVATION.
2-21 215800-02-1 191 RST AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.58.00/02 215800-100-001 108 MO YES N/A
MRB 7 OR
REMOVE CSAS HEAT EXCHANGER FOR IN SHOP CLEANING 12000 FH
2-21 216000-01-1 200 RST AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.50.00/02 216300-100-801 72 MO APPL
MRB 9 OR
CLEANING OF CABIN SENSOR DUCT AND TEMPERATURE SENSOR. 7500 FH
2-21 216000-02-1 210 OPC AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.50.00/03 216300-710-002 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF ZONE CONTROLLER (BACK UP 12000 FH
SWITCHING) VIA CFDS/MCDU
2-21 216242-01-1 191 DET AIR COOLING AND TEMPERATURE CONTROL AF LUR MRB 21.50.00/05 216342-210-001 108 MO APPL
MRB 9 OR
DETAILED INSPECTION OF TRIM AIR CHECK VALVES FLAPPERS 12000 FH
FOR CONDITION AND OPERATION
2-22 221000-01-1 210 OPC AUTO PILOT/FLIGHT DIRECTOR (AP/FD) AV LUR MRB 22.10.00/01 221000-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF AP DISENGAGEMENT AND LOCKING 24000 FH
DEVICES OF SIDE STICK CONTROLLER AND RUDDER PEDALS
2-22 221000-02-1 210 OPC AUTO PILOT/FLIGHT DIRECTOR (AP/FD) AV MRB 9 MRB 22.10.00/02 221000-710-009 40 MO N/A
OPERATIONAL CHECK OF TRUE NORTH REFERENCE SELECTION
APPENDIX A
AEG/AMP/A320 Page 13 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-22 223000-01-1 210 OPC AUTOTHRUST AV LUR MRB 22.30.00/01 223000-710-003 252 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF ENGINE/AUTOTHRUST SYSTEM 36000 FH
ISOLATION
2-22 223000-02-1 210 OPC AUTOTHRUST EL LUR MRB 22.30.00/01 223000-720-002 252 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF ENGINE/AUTOTHRUST SYSTEM 36000 FH
ISOLATION
226000-01-1 ************** TASK DELETED ************** N/A
2-23 233300-01-1 200 OPC PASSENGER ENTERTAINMENT (MUSIC AND VIDEO) RA LUR MRB 23.33.00/01 233600-710-007 144 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF IFES POWER SHUTDOWN FUNCTION BY 18000 FH
USING THE VCC MASTER POWER OR VCC MAIN POWER SWITCH
IN VIDEO CONTROL CENTER.
2-23 233300-02-1 200 OPC PASSENGER ENTERTAINMENT (MUSIC AND VIDEO) EL LUR MRB 23.33.00/02 233300-710-006 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF IFES POWER ISOLATION FUNCTION 15000 FH
USING PAX-SYS SWITCH(ES)
2-23 233300-03-1 200 DIS PASSENGER ENTERTAINMENT (MUSIC AND VIDEO) EL LUR MRB 23.33.00/03 233600-920-802 12 MO N/A
MRB 9 OR
DISCARD VCC AIR FILTER ELEMENT 1200 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-23 234300-01-1 200 OPC CABIN AND FLIGHT CREW INTERPHONE SYSTEM RA LUR MRB 23.73.00/06 237300-710-040 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF CABIN / COCKPIT INCIDENT ALERT 15000 FH
SYSTEM
2-23 235100-01-1 210 OPC AUDIO MANAGEMENT RA LUR MRB 23.50.00/01 235100-710-003 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF CAPT. AND F/O AUDIO CONTROL 24000 FH
PANELS SWITCHING TO THIRD AUDIO CONTROL PANEL
2-23 237100-01-1 210 OPC COCKPIT VOICE RECORDER RA MRB 9 MRB 23.71.00/01 237100-710-001 36 MO APPL
OPERATIONAL CHECK OF CVR AND CVR-CHANNEL RECORDING
2-23 237100-02-1 210 OPC COCKPIT VOICE RECORDER RA LUR MRB 23.71.00/02 237100-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF CVR RECORDING LOGIC INCLUDING 24000 FH
TIME DELAY RELAY
2-23 237135-01-1 312 DIS COCKPIT VOICE RECORDER RA MRB 9 MRB 23.71.00/03 237135-920-001 NOTE YES APPL
DISCARD ULB BATTERY
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-23 237135-02-1 312 OPC COCKPIT VOICE RECORDER AV MRB 9 MRB 23.71.00/04 237100-720-001 36 MO APPL
OPERATIONAL CHECK OF ULB
2-23 237300-01-1 210 OPC CABIN INTERCOMMUNICATION DATA SYSTEM RA LUR MRB 23.73.00/01 237300-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK FOR SECONDARY POWER SUPPLY TO 22500 FH
DIRECTORS AND DECODER/ENCODER UNITS, AND
DECODER/ENCODER UNITS-A CUT OFF FUNCTION
2-23 237300-02-1 210 OPC CABIN INTERCOMMUNICATION DATA SYSTEM RA LUR MRB 23.73.00/02 237300-710-015 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF POWER TRANSFER FUNCTION 22500 FH
2-23 237300-04-1 200 OPC CABIN INTERCOMMUNICATION DATA SYSTEM RA LUR MRB 23.73.00/04 237300-710-038 252 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF DECODER/ENCODER UNITS ESSENTIAL 36000 FH
POWER SUPPLY, AND DECODER/ENCODER UNITS-A CUT OFF
FUNCTION
APPENDIX A
AEG/AMP/A320 Page 14 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-23 237300-05-1 200 OPC CABIN INTERCOMMUNICATION DATA SYSTEM CA LUR MRB 23.73.00/05 237300-710-803 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF EVAC FUNCTION 22500 FH
2-23 237300-08-1 200 OPC CABIN INTERCOMMUNICATION DATA SYSTEM RA LUR MRB 23.73.00/08 237300-710-042 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF BATTERY BUS POWERED PA 15000 FH
2-23 237300-09-1 200 OPC CABIN INTERCOMMUNICATION DATA SYSTEM RA LUR MRB 23.73.00/09 237300-710-802 24 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF CABIN BULB SIGNS VIA MCDU 2000 FH
2-24 242000-01-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/19 244100-740-002 12 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF GAPCU VIA CFDS 1000 FH
2-24 242000-20-1 438 DIS AC GENERATION EN CMP CMP 24-2-0000-001 242100-920-801 6 MO N/A
448 LUR MRB 24.20.00/20 OR
- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER MRB 6 800 FH
ELEMENTS, NOTE
- DRAIN AND REPLENISH OIL SYSTEM
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY
INTO SERVICE. THEREAFTER REFER TO INTERVAL.
2-24 242000-21-1 438 DIS AC GENERATION EN CMP CMP 24-2-0000-001 242100-920-040 6 MO N/A
448 LUR MRB 24.20.00/20 OR
- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER MRB 6 800 FH
ELEMENTS, NOTE
- DRAIN AND REPLENISH OIL SYSTEM
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY
INTO SERVICE. THEREAFTER REFER TO INTERVAL.
2-24 242000-22-1 438 DIS AC GENERATION EN CMP CMP 24-2-0000-001 242100-920-041 6 MO N/A
448 LUR MRB 24.20.00/20 OR
- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER MRB 6 800 FH
ELEMENTS, NOTE
- DRAIN AND REPLENISH OIL SYSTEM
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY
INTO SERVICE. THEREAFTER REFER TO INTERVAL.
2-24 242000-23-1 438 DIS AC GENERATION EN CMP CMP 24-2-0000-001 242100-920-802 6 MO N/A
448 LUR MRB 24.20.00/20 OR
- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER MRB 6 800 FH
ELEMENTS, NOTE
- DRAIN AND REPLENISH OIL SYSTEM
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY
INTO SERVICE. THEREAFTER REFER TO INTERVAL.
2-24 242000-24-1 438 DIS AC GENERATION EN CMP CMP 24-2-0000-001 242100-920-803 6 MO N/A
448 LUR MRB 24.20.00/20 OR
- REMOVE AND DISCARD SCAVENGE AND CHARGE FILTER MRB 6 800 FH
ELEMENTS, NOTE
- DRAIN AND REPLENISH OIL SYSTEM
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENTS, DRAIN IDG OIL AND
REPLENISH AT 150 FH OR 1 MO AFTER AIRCRAFT ENTRY
INTO SERVICE. THEREAFTER REFER TO INTERVAL.
APPENDIX A
AEG/AMP/A320 Page 15 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-24 242100-01-1 438 FNC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/07 242100-210-043 24 MO N/A
448 MRB 9 OR
CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION 2400 FH
BOLT
2-24 242100-02-1 438 SVC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/05 242100-210-046 2 MO N/A
448 MRB 6 OR
CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE 300 FH
INDICATOR NOTE
NOTE: Included into Weekly
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS Checklist
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-24 242100-03-1 438 DIS INTEGRATED DRIVE GENERATOR EN CMP CMP 24-2-0000-001 242100-920-040 6 MO N/A
448 LUR MRB 24.20.00/06 OR
- REMOVE AND DISCARD SCAVENGE FILTER ELEMENT MRB 6 800 FH
- DRAIN AND REPLENISH OIL SYSTEM NOTE
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH
AT 150 FH OR 1 MO AFTER AIRCRAFT DELIVERY.
THEREAFTER REFER TO INTERVAL.
2-24 242100-04-1 438 OPC INTEGRATED DRIVE GENERATOR AF MRB 9 MRB 24.20.00/11 242100-710-040 NOTE N/A
448
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG)
DISCONNECT AND RECONNECT FUNCTION.
NOTE:
TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.
2-24 242100-05-1 437 RST INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/12 731160-100-040 252 MO YES N/A
447 MRB 6 OR
REMOVE IDG COOLER FOR IN-SHOP CLEANING 36000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE
SHOP VISIT.
2-24 242100-06-1 438 FNC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/07 242141-200-010 24 MO APPL
448 MRB 9 OR
CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION 2400 FH
BOLT
2-24 242100-07-1 438 SVC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/05 242151-200-010 2 MO APPL
448 MRB 6 OR
CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE 300 FH
INDICATOR NOTE
Included into Weekly
NOTE: Checklist
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-24 242100-08-1 438 DIS INTEGRATED DRIVE GENERATOR EN CMP CMP 24-2-0000-001 242100-920-041 6 MO APPL
448 LUR MRB 24.20.00/06 OR
- REMOVE AND DISCARD SCAVENGE FILTER ELEMENT MRB 6 800 FH
- DRAIN AND REPLENISH OIL SYSTEM NOTE
NOTE:
INTERVAL:
- REPLACE FILTER ELEMENT, DRAIN IDG OIL AND REPLENISH
AT 150 FH OR 1 MO AFTER AIRCRAFT DELIVERY.
THEREAFTER REFER TO INTERVAL.
2-24 242100-09-1 438 OPC INTEGRATED DRIVE GENERATOR EN MRB 9 MRB 24.20.00/11 242100-710-042 NOTE APPL
448
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG)
DISCONNECT AND RECONNECT FUNCTION.
NOTE:
TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.
APPENDIX A
AEG/AMP/A320 Page 16 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-24 242100-10-1 437 RST INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/12 242142-100-040 252 MO YES APPL
447 MRB 6 OR
REMOVE IDG COOLER FOR IN-SHOP CLEANING 36000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE
SHOP VISIT.
2-24 242100-13-1 438 FNC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/07 242141-200-001 24 MO N/A
448 MRB 9 OR
CHECK TORQUE OF QUICK-ATTACH-DETACH (QAD) TENSION 2400 FH
BOLT
2-24 242100-14-1 438 SVC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/05 242100-210-801 2 MO N/A
448 MRB 6 OR
CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE 300 FH
INDICATOR NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-24 242100-15-1 438 OPC INTEGRATED DRIVE GENERATOR AF MRB 9 MRB 24.20.00/11 242100-710-801 NOTE N/A
448
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG)
DISCONNECT AND RECONNECT FUNCTION.
NOTE:
TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.
2-24 242100-16-1 437 RST INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/12 792143-100-801 252 MO YES N/A
447 MRB 6 OR
REMOVE IDG COOLER FOR IN-SHOP CLEANING 36000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE
SHOP VISIT.
2-24 242100-17-1 435 FNC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/21 242141-200-802 12 MO N/A
445 MRB 9 OR
CHECK TORQUE OF IDG QAD TENSION BOLT. 1200 FH
2-24 242100-18-1 435 FNC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/21 242141-200-803 12 MO N/A
445 MRB 9 OR
CHECK TORQUE OF IDG QAD TENSION BOLT. 1200 FH
2-24 242100-19-1 438 SVC INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/05 242100-210-808 6 MO N/A
448 MRB 6 OR
CHECK IDG OIL LEVEL AND DIFFERENTIAL PRESSURE 300 FH
INDICATOR. NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-24 242100-20-1 437 RST INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/12 242142-100-804 252 MO YES N/A
447 MRB 6 OR
REMOVE IDG COOLER FOR IN-SHOP CLEANING 36000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE
SHOP VISIT.
APPENDIX A
AEG/AMP/A320 Page 17 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-24 242100-21-1 437 RST INTEGRATED DRIVE GENERATOR EN LUR MRB 24.20.00/23 242142-100-802 252 MO YES N/A
447 MRB 6 OR
REMOVE IDG COOLER FOR IN-SHOP CLEANING AND FUEL-OIL 36000 FH
COOLER THERMAL VALVE REPLACEMENT. NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT THE OPPORTUNITY OF ENGINE
SHOP VISIT.
2-24 242100-22-1 438 OPC INTEGRATED DRIVE GENERATOR AF MRB 9 MRB 24.20.00/11 242100-710-803 NOTE N/A
448
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG)
DISCONNECT AND RECONNECT FUNCTION.
NOTE:
TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.
2-24 242100-23-1 438 OPC INTEGRATED DRIVE GENERATOR AF MRB 9 MRB 24.20.00/11 242100-710-805 NOTE N/A
448
OPERATIONAL CHECK OF INTEGRATED DRIVE GENERATOR (IDG)
DISCONNECT AND RECONNECT FUNCTION.
NOTE:
INTERVAL:
- TASK TO BE PERFORMED AT OPPORTUNITY OF ENGINE CHANGE OR IDG CHANGE.
2-24 242200-01-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/08 242200-710-002 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF TRANSFER INHIBITION 12000 FH
2-24 242400-01-1 210 OPC AC EMERGENCY GENERATION EL MRB 8 MRB 24.20.00/01 242400-710-001 36 HR N/A
MRB 24.30.00/01
OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM MRB 24.50.00/01
2-24 242400-01-2 210 OPC AC EMERGENCY GENERATION EL CMR* CMR 242000-00002-1-C 242400-710-001 1 MO OR APPL
LUR MRB 24.20.00/15 120 FH
OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM MRB 8 MRB 24.30.00/08 Included into Weekly
MRB 24.50.00/06 Checklist
2-24 242400-01-3 210 OPC AC EMERGENCY GENERATION EL CMR* CMR 242000-00002-2-C 242400-710-001 1 MO N/A
LUR MRB 24.20.00/16 OR
OPERATIONAL CHECK OF EMERGENCY GENERATING SYSTEM MRB 8 MRB 24.30.00/09 90 FH
MRB 24.50.00/07
2-24 242400-02-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/10 242400-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF EMERGENCY GCU VIA CFDS 24000 FH
2-24 242500-01-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/09 242500-710-001 72 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF AC ESS GENERATION SWITCHING 7500 FH
2-24 242600-01-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/13 242600-710-001 108 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY 12000 FH
SHEDDING
2-24 242600-02-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/14 242600-710-002 180 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY AND 24000 FH
BUS SHEDDING
2-24 242600-03-1 210 OPC AC GENERATION EL LUR MRB 24.20.00/22 242600-710-002 108 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF MANUAL AND AUTOMATIC GALLEY AND 15000 FH
BUS SHEDDING
2-24 242800-01-1 210 OPC STATIC INVERTER EL MRB 8 MRB 24.20.00/02 242800-710-001 36 HR N/A
MRB 24.30.00/02
OPERATIONAL CHECK OF STATIC INVERTER MRB 24.50.00/02
2-24 242800-01-2 210 OPC STATIC INVERTER EL CMR** CMR 242000-00001-2-C 242800-710-001 6 MO APPL
LUR MRB 24.20.00/17 OR
OPERATIONAL CHECK OF STATIC INVERTER MRB 8 MRB 24.30.00/10 750 FH
MRB 24.50.00/08 Included into Weekly
Checklist
2-24 242800-01-3 210 OPC STATIC INVERTER EL CMR* CMR 242000-00001-1-C 242800-710-001 1 MO OR N/A
LUR MRB 24.20.00/18 90 FH
OPERATIONAL CHECK OF STATIC INVERTER MRB 8 MRB 24.30.00/11
MRB 24.50.00/09
APPENDIX A
AEG/AMP/A320 Page 18 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-24 243200-01-1 210 OPC DC GENERATION EL LUR MRB 24.30.00/04 243200-710-001 72 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF DC GENERATION SWITCHING 7500 FH
2-24 243400-01-1 210 OPC DC GENERATION EL LUR MRB 24.30.00/06 243400-710-001 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF "DC EMERG. CONFIG" CAUTION 12000 FH
2-24 243800-01-1 210 OPC DC MAIN GENERATION EL LUR MRB 24.30.00/03 243800-710-001 12 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF BATTERY CHARGE LIMITER NO 1 AND 1000 FH
NO 2 VIA CFDS
2-24 243851-01-1 126 RST DC GENERATION EL MRB 6 MRB 24.30.00/05 243851-280-001 12 MO YES APPL
NOTE
REMOVE BATTERY FOR OVERHAUL
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-24 243851-02-1 126 RST DC GENERATION EL MRB 6 MRB 24.30.00/12 243851-280-802 NOTE YES APPL
REMOVE BATTERY FOR CHECK IN WORKSHOP
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYST EM SECTION INTRODUCTION FOR ADDITIONALGUIDANCE.
2-24 244100-01-1 210 OPC AC EXTERNAL POWER CONTROL EL LUR MRB 24.20.00/03 244100-740-004 12 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF GPCU VIA CFDS 1000 FH
2-24 245100-01-1 210 OPC AC/DC ELECTRICAL LOAD DISTRIBUTION EL LUR MRB 24.50.00/04 242200-710-001 180 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF GENERATOR LINE CONTACTOR OPENING 24000 FH
2-24 245100-02-1 210 OPC AC/DC ELECTRICAL LOAD DISTRIBUTION EL LUR MRB 24.50.00/05 245100-710-001 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF COMMERCIAL ELECTRIC LOAD 24000 FH
SHEDDING
2-25 251100-01-1 210 DET COCKPIT SEATS AF LUR MRB 25.11.00/01 251100-200-001 252 MO APPL
MRB 9 OR
DETAILED INSPECTION OF SEAT STRUCTURE AND SEAT 36000 FH
ATTACHMENT OF ALL FLIGHT DECK SEATS
2-25 252100-01-1 200 DET PASSENGER COMPARTMENT SEATS AF LUR MRB 25.21.00/01 252100-210-001 144 MO APPL
MRB 8 OR
DETAILED INSPECTION OF SEAT ATTACHMENTS, SEAT 18000 FH
STRUCTURE, SEAT BELTS, BUCKLES AND BAGGAGE BAR.
2-25 252100-03-1 200 OPC PASSENGER COMPARTMENT SEATS EL LUR MRB 25.21.00/03 252100-710-802 36 MO YES N/A
MRB 8 OR
OPERATIONAL CHECK OF AIRBAG SYSTEM BY DIAGNOSTIC TOOL 4000 FH
(V23) OR EMA PTT PROCEDURE (NEXGEN).
2-25 252100-04-1 200 DIS PASSENGER COMPARTMENT SEATS CA MRB 8 MRB 25.21.00/04 252158-920-001 84 MO YES N/A
NOTE
REMOVE EMA OF AIRBAG SYSTEM FOR IN SHOP DISCARD OF
BATTERY.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 19 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 252100-05-1 200 DIS PASSENGER COMPARTMENT SEATS CA MRB 7,8 MRB 25.21.00/05 252158-920-802 120 MO YES N/A
NOTE
DISCARD AIRBAG INFLATOR ASSEMBLY.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 252100-06-1 200 DET PASSENGER COMPARTMENT SEATS CA LUR MRB 25.21.00/06 252100-710-006 36 MO YES N/A
MRB 8 OR
DETAILED INSPECTION OF AIRBAG SYSTEM COMPONENTS. 4000 FH
2-25 252100-07-1 200 DIS PASSENGER COMPARTMENT SEATS CA MRB 8 MRB 25.21.00/07 252158-920-803 120 MO YES N/A
NOTE
DISCARD EMA OF AIRBAG SYSTEM.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 252200-01-1 200 DET CABIN ATTENDANT SEATS AF LUR MRB 25.22.00/01 252200-210-001 108 MO APPL
MRB 8 OR
DETAILED INSPECTION OF CABIN ATTENDANT SEAT 15000 FH
ATTACHMENTS, SEAT STRUCTURE AND SEAT BELT (INCLUDING
SEAT BELT ATTACHMENTS AND BUCKLES).
2-25 252200-03-1 200 OPC CABIN ATTENDANT SEATS AF LUR MRB 25.22.00/03 252200-710-801 144 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF SEAT BELTS (INCLUDING HARNESS 18000 FH
ROLL-UP MECHANISM).
2-25 253000-01-1 200 DET BUFFET AND GALLEY CA MRB 9 MRB 25.30.00/01 253000-210-001 72 MO APPL
DETAILED INSPECTION OF ATTACHMENT POINTS
2-25 253000-02-1 200 DIS BUFFET AND GALLEY AF LUR MRB 25.30.00/04 253000-920-001 72 MO N/A
MRB 7 OR
REMOVE AND DISCARD FILTER ELEMENT 7500 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-25 253400-01-1 200 RST GALLEY COOLING AF LUR MRB 25.34.00/01 253400-100-001 12 MO N/A
MRB 9 OR
CLEAN "CHILLED AIR IN" AND "CHILLED AIR OUT" GRILLES/ 1500 FH
FILTERS IN GALLEY CABINET NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-25 253400-02-1 200 RST GALLEY COOLING AF LUR MRB 25.34.00/02 253400-100-002 12 MO YES N/A
MRB 9 OR
CLEAN AIR CHILLER CONDENSER AIR FILTER 1500 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
APPENDIX A
AEG/AMP/A320 Page 20 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 254000-01-1 200 DET LAVATORIES CA LUR MRB 25.40.00/01 254000-210-001 72 MO APPL
MRB 9 OR
DETAILED INSPECTION OF WASTE COMPARTMENT INCLUDING 8000 FH
WASTE FLAP AND OPERATIONAL CHECK OF WASTE FLAP
2-25 254000-02-2 200 DET LAVATORIES CA MRB 9 MRB 25.40.00/03 254000-210-002 90 MO APPL
DETAILED INSPECTION OF UPPER AND LOWER LAVATORY
ATTACHMENT POINTS.
NOTE:
PLANNING: LOWER LAVATORY ATTACHEMENT POINTS:
- CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
254000-03-1.
2-25 254000-03-1 200 DET LAVATORIES CA MRB 9 MRB 25.40.00/02 60 MO N/A
DETAILED INSPECTION OF LAVATORY WALL AND LOWER
ATTACHMENT POINTS.
2-25 254000-04-1 200 DET LAVATORIES CA LUR MRB 25.40.00/04 254000-210-004 72 MO N/A
MRB 9 OR
DETAILED INSPECTION OF LAVATORY FLOOR PAN 6000 FH
2-25 254000-04-2 200 DET LAVATORIES CA LUR MRB 25.40.00/05 254000-210-004 108 MO APPL
MRB 9 OR
DETAILED INSPECTION OF LAVATORY FLOOR PAN 12000 FH
2-25 255000-01-1 130 VCK CARGO COMPARTMENTS AF CMP CMP 25-2-0000-001 255000-200-002 8 DY APPL
150 MRB 8 MRB 25.50.00/01 Included into Weekly
160 VISUAL CHECK OF CARGO COMPARTMENT DECOMPRESSION, Checklist
LINING, FLOOR PANELS AND PRESSURE COMPENSATION VALVE
(AS FAR AS VISIBLE, IF ACT(S) OR SLIDING CARPET
SYSTEM INSTALLED).
2-25 255000-02-1 130 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/03 255000-210-001 72 MO APPL
150 MRB 8 OR
PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OF 8000 FH
XZ-LATCHES
2-25 255000-03-1 130 DET CARGO COMPARTMENTS AF MRB 8 MRB 25.50.00/02 255000-210-002 12 MO APPL
150 OR
PERFORM OPERATIONAL CHECK AND DETAILED INSPECTION OF 4000 FH
YZ DOOR SILL LATCHES
2-25 255000-04-1 150 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/11 255000-200-011 36 MO N/A
MRB 8 OR
OPERATIONAL CHECK AND DETAILED INSPECTION OF AFT 3000 FC
CARGO DOOR SILL LATCH AROS
255000-05-1 ************** TASK DELETED ************** N/A
2-25 255000-06-1 150 OPC LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/13 255200-710-014 72 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF RETRACTABLE DOOR SILL ROLLER AT 5000 FC
AFT CARGO DOOR
2-25 255000-08-1 150 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/14 255000-200-012 180 MO N/A
MRB 8 OR
REMOVE XZ-ENDSTOPS AND YZ-LATCHES FOR DETAILED 24000 FH
INSPECTION.
2-25 255000-10-1 150 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/16 255000-200-015 180 MO N/A
MRB 8 OR
REMOVE XZ-LATCHES ACT FOR DETAILED INSPECTION 24000 FH
APPENDIX A
AEG/AMP/A320 Page 21 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 255000-11-1 130 VCK CARGO COMPARTMENTS AF LUR MRB 25.50.00/17 255000-200-016 12 MO APPL
150 MRB 8 OR
VISUAL CHECK OF XZ-LATCHES AND DOOR SILL LATCHES 1000 FH
NOTE:
FOR A319 DOOR SILL LATCHES ONLY TO BE CHECKED IN FWD
CC
2-25 255000-12-1 150 VCK CARGO COMPARTMENTS AF LUR MRB 25.50.00/18 255000-200-017 12 MO N/A
MRB 8 OR
VISUAL CHECK OF DOOR SILL LATCH ARO 1000 FC
2-25 255000-13-1 131 LUB CARGO COMPARTMENTS AF LUR MRB 25.50.00/20 122225-640-001 72 MO N/A
151 MRB 9 OR
LUBRICATION OF SCREW SHAFT OF DRIVE UNIT OF SLIDING 5000 FC
CARPET SYSTEM
2-25 255000-14-1 131 OPC CARGO COMPARTMENTS AF LUR MRB 25.50.00/21 255200-710-016 72 MO N/A
151 MRB 9 OR
OPERATIONAL CHECK OF THE SLIDING CARPET SYSTEM 5000 FC
EMERGENCY STOP AND OF LOAD/UNLOAD LIMIT SWITCH
INDICATION
2-25 255000-16-1 130 DET CARGO COMPARTMENTS AF LUR MRB 25.50.00/04 255000-200-025 12 MO APPL
150 MRB 9 OR
160 DETAILED INSPECTION OF DIVIDER NETS, DOOR NETS AND 1000 FH
NET ATTACHMENT POINTS
NOTE:
THE NUMBER OF AFFECTED ZONES MAY VARY ACCORDING TO
THE CARGO SYSTEMS INSTALLED.
2-25 255000-23-1 130 GVI CARGO COMPARTMENTS AF MRB 9 MRB 25.50.00/23 255000-200-022 72 MO N/A
150 NOTE
GENERAL VISUAL INSPECTION OF CRASHSTOPPERS
NOTE:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
- TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE.
CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF THE TASK
AT THIS OPPORTUNITY.
2-25 255000-24-1 160 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/24 255000-200-026 180 MO N/A
MRB 8 OR
REMOVE XZ-ENDSTOPS AND Y STOP ASSY FOR DETAILED 24000 FH
INSPECTION
2-25 255000-25-1 130 DET CARGO COMPARTMENTS AF LUR MRB 25.50.00/25 255000-200-802 180 MO APPL
150 MRB 8 OR
REMOVE XZ-LATCHES FOR DETAILED INSPECTION 24000 FH
2-25 255000-26-1 133 OPC CARGO COMPARTMENTS AF MRB 8 MRB 25.50.00/26 255000-200-803 72 MO N/A
153
REMOVE AIR STOP VALVE FOR IN SHOP OPERATIONAL CHECK
2-25 255000-60-2 150 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/14 255000-200-019 180 MO N/A
MRB 8 OR
REMOVE XZ-ENDSTOPS AND YZ-LATCHES FOR DETAILED 24000 FH
INSPECTION.
2-25 255000-61-1 150 DET LOWER DECK CARGO LOADING AF LUR MRB 25.50.00/16 255000-200-020 180 MO N/A
MRB 8 OR
REMOVE XZ-LATCHES ACT FOR DETAILED INSPECTION 24000 FH
2-25 256141-01-1 210 DET DESCENT DEVICE EMERGENCY AF MRB 8 MRB 25.61.41/01 256141-200-001 84 MO APPL
DETAILED INSPECTION OF EMERGENCY ESCAPE ROPE AND ROPE
ATTACHMENT
2-25 256241-01-1 800 VCK DOOR ESCAPE SLIDE AF LUR MRB 25.62.00/01 256200-210-001 6 MO APPL
MRB 8 OR
CHECK DOOR AND OFFWING ESCAPE SLIDE/RAFT INFLATION 750 FH
RESERVOIR PRESSURE.
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/
CREW DOORS/EMERGENCY EXITS.
APPENDIX A
AEG/AMP/A320 Page 22 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 256241-02-1 831 FNC DOOR ESCAPE SLIDE AF MRB 6,8 MRB 25.62.00/02 256200-750-001 60 MO YES APPL
832 NOTE
841 REMOVE DOOR ESCAPE SLIDE/RAFT FOR HYDROSTATIC TEST OF
842 INFLATION RESERVOIR
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/
CREW DOORS.
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256241-03-1 831 RST DOOR ESCAPE SLIDE AF MRB 8 MRB 25.62.00/03 256244-920-001 NOTE YES APPL
832
841 REMOVE DOOR ESCAPE SLIDE/RAFT FOR IN SHOP OVERHAUL
842
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/ CREW DOORS.
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO SYSTEM SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
2-25 256241-04-1 831 OPC DOOR ESCAPE SLIDE CA MRB 8 MRB 25.62.00/04 256200-710-001 NOTE APPL
832
841 OPERATIONAL CHECK OF FWD AND AFT PAX/CREW DOOR ESCAPE
842 SLIDE/RAFT DEPLOYMENT.
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW DOORS.
INTERVAL:
- ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED.
2-25 256241-05-1 221 RST DOOR ESCAPE SLIDE AF LUR MRB 52.10.00/07 531100-210-034 24 MO APPL
222 MRB 9 OR
261 CLEAN DOOR GIRT BAR FITTING STOP LEVERS 1110 FC
262
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS.
2-25 256242-01-1 151 FNC OFFWING ESCAPE SLIDE AF MRB 6,8 MRB 25.62.00/02 256200-750-002 60 MO YES APPL
152 NOTE
REMOVE OFFWING ESCAPE SLIDE INFLATION RESERVOIR FOR
HYDROSTATIC TEST
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256242-02-1 191 RST OFFWING ESCAPE SLIDE AF MRB 8 MRB 25.62.00/03 256242-920-001 NOTE YES APPL
192
REMOVE OFFWING ESCAPE SLIDE FOR IN SHOP OVERHAUL
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 23 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 256242-02-2 193 RST OFFWING ESCAPE SLIDE AF MRB 8 MRB 25.62.00/03 256242-920-001 3 YE 3 YE YES N/A
194 SEMR SEMR 256200-00001-1-E OR
REMOVE OFFWING ESCAPE SLIDE FOR IN SHOP OVERHAUL CE
NOTE
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO APPENDIX 6 - VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256242-03-1 830 OPC OFFWING ESCAPE SLIDE CA MRB 8 MRB 25.62.00/04 256200-710-002 NOTE APPL
840
OPERATIONAL CHECK OF OFF WING EMERGENCY EXIT ESCAPE
SLIDE DEPLOYMENT
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
INTERVAL:
- ALTERNATE DOOR POSITION AT NEXT INTERVAL
RECOMMENDED.
*NOTE 15 CAN BE FOUND IN THE APPLICABLE MPD REVISION.
2-25 256247-01-1 131 RST DOOR 2 AND 3 ESCAPE SLIDE AF MRB 8 MRB 25.62.00/03 256247-920-001 NOTE YES N/A
132
151 REMOVE DOOR 2 AND 3 ESCAPE SLIDE FOR IN SHOP OVERHAUL
152
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256247-02-1 833 OPC DOOR 2 AND 3 ESCAPE SLIDE AF MRB 8 MRB 25.62.00/04 256200-710-003 NOTE N/A
834
843 OPERATIONAL CHECK OF DOOR SLIDE DEPLOYMENT
844
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCYEXITS.
INTERVAL:
- ALTERNATE DOOR POSITION AT NEXT INTERVAL RECOMMENDED.
2-25 256249-01-1 231 FNC DOOR 2 AND 3 ESCAPE SLIDE AF MRB 6,8 MRB 25.62.00/02 256200-750-003 60 MO YES N/A
232 NOTE
251 REMOVE DOOR 2 AND 3 ESCAPE SLIDE INFLATION RESERVOIR
252 FOR HYDROSTATIC TEST
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED EMERGENCY
EXITS.
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
256532-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 24 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 256532-02-1 200 OPC PORTABLE EMERGENCY BEACON TRANSMITTER CA MRB 9 MRB 25.65.32/02 256500-720-802 60 MO YES N/A
NOTE
REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER FOR IN
SHOP OPERATIONAL CHECK
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256532-03-1 200 DIS PORTABLE EMERGENCY BEACON TRANSMITTER CA MRB 9 MRB 25.65.32/03 256500-920-804 NOTE YES N/A
REMOVE SURVIVAL EMERGENCY LOCATOR TRANSMITTER FOR IN
SHOP BATTERY REPLACEMENT
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256533-01-1 200 DIS EMERGENCY LOCATOR TRANSMITTER(COCKPIT) EL MRB 9 MRB 25.65.33/01 256533-710-001 NOTE YES N/A
DISCARD TRANSMITTER BATTERY AND PERFORM OPERATIONAL
CHECK OF TRANSMITTER AFTER BATTERY REPLACEMENT
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256534-01-1 200 FNC PORTABLE VHF TRANSCEIVER EL MRB 9 MRB 25.65.34/01 256534-000-001 24 MO YES N/A
REMOVE PORTABLE VHF TRANSCEIVER FOR SHOP INSPECTION.
2-25 256535-01-1 200 OPC ELT (REAR FUSELAGE) RA MRB 8 MRB 25.65.35/01 256500-710-001 24 MO APPL
OPERATIONAL CHECK OF ELT SYSTEM BY MANUAL ACTIVATION
2-25 256535-02-1 200 OPC ELT (REAR FUSELAGE) EL MRB 8 MRB 25.65.35/02 256500-720-004 72 MO YES APPL
REMOVE ELT FOR IN SHOP OPERATIONAL CHECK OF
ACCELERATION SENSOR
NOTE:
- CREDIT CAN BE TAKEN FOR PREVIOUS ACCOMPLISHMENT OF
TASK 256535-03-1.
2-25 256535-03-1 200 DIS ELT (REAR FUSELAGE) EL MRB 8 MRB 25.65.35/03 256500-920-802 NOTE YES APPL
REMOVE ELT FOR IN SHOP DISCARD OF BATTERY PACK OF ELT
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256551-01-1 200 DIS MEGAPHONE BATTERIES CA MRB 9 MRB 25.65.51/01 256551-920-001 12 MO YES APPL
DISCARD AND REPLACE MEGAPHONE BATTERIES
256551-02-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 25 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-25 256600-01-1 200 RST SUPPLEMENTAL LIFE RAFT AF MRB 8 MRB 25.66.41/01 256641-920-001 NOTE YES N/A
REMOVE LIFE RAFT FOR IN SHOP OVERHAUL.
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256600-02-1 200 VCK SUPPLEMENTAL LIFE RAFT AF MRB 8 MRB 25.66.41/02 256641-210-001 4 MO N/A
CHECK PRESSURE AT LIFE RAFT PRESSURE GAUGE (IF
CONFIGURATION INCLUDES VISIBLE GAUGE)
2-25 256642-01-1 200 RST BABY SURVIVAL RAFT CA MRB 8 MRB 25.66.42/01 256641-920-002 NOTE YES N/A
REMOVE BABY FLOATING SURVIVAL COT FOR IN SHOP
OVERHAUL.
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-25 256652-01-1 200 RST LIFE VESTS CA MRB 8 MRB 25.66.52/01 256652-920-001 NOTE YES APPL
NOTE
REMOVE LIFE VESTS FOR IN SHOP OVERHAUL.
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 261200-01-1 210 OPC ENGINE FIRE AND OVERHEAT DETECTION EL LUR MRB 26.12.00/01 261200-710-001 12 MO APPL
MRB 8 MRB 26.21.00/01 OR
OPERATIONAL CHECK OF LOOP/SQUIB 1000 FH
2-26 261300-01-1 210 OPC APU FIRE AND OVERHEAT DETECTION EL LUR MRB 26.13.00/01 261300-710-001 24 MO APPL
MRB 8 MRB 26.22.00/01 OR
OPERATIONAL CHECK OF LOOP/SQUIB 2000 FH
2-26 261500-03-1 128 RST AVIONICS COMPARTMENT SMOKE DETECTION AF LUR MRB 26.15.00/03 261500-100-001 108 MO APPL
MRB 9 OR
CLEAN AVIONICS SMOKE DETECTION PICCOLO TUBES 15000 FH
2-26 261500-04-1 128 RST AVIONICS COMPARTMENT SMOKE DETECTION AV LUR MRB 26.15.00/04 261500-100-002 108 MO YES N/A
MRB 6,9 OR
REMOVAL OF IONIC SMOKE DETECTOR FOR FOR CLEANING IN 15000 FH
SHOP
2-26 261600-03-1 210 OPC CARGO COMPARTMENT SMOKE DETECTION EL LUR MRB 26.16.00/01 261600-710-001 24 MO APPL
MRB 8 MRB 26.23.00/02 OR
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE 2000 FH
DETECTION BY PTT
2-26 261600-04-1 210 OPC CARGO COMPARTMENT SMOKE DETECTION EL LUR MRB 21.28.00/06 261600-710-003 24 MO N/A
MRB 8 MRB 26.16.00/02 OR
OPERATIONAL CHECK OF CARGO COMPARTMENT SMOKE 2000 FH
DETECTION BY CFDS TO CONFIRM ISOLATION VALVES
LATCHING CIRCUIT INTEGRITY.
2-26 261600-05-1 130 RST CARGO COMPARTMENT SMOKE DETECTION AV LUR MRB 26.16.00/05 261615-100-001 144 MO YES APPL
150 MRB 8 OR
160 REMOVE CARGO COMPARTMENT SMOKE DETECTORS FOR CLEANING 18000 FH
2-26 261700-02-1 200 RST LAVATORY SMOKE DETECTION AF LUR MRB 26.17.00/03 261715-100-002 12 MO N/A
MRB 9 OR
CLEAN SMOKE DETECTOR AIR DUCT 1600 FH
APPENDIX A
AEG/AMP/A320 Page 26 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-26 261700-03-1 210 OPC LAVATORY SMOKE DETECTION EL LUR MRB 26.17.00/01 261700-710-001 36 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF LAVATORY SMOKE DETECTION BY CFDS 3000 FH
TO CONFIRM WARNINGS CAN BE DISPLAYED
2-26 261700-04-1 200 RST LAVATORY SMOKE DETECTION EL LUR MRB 26.17.00/04 261715-100-003 108 MO YES APPL
MRB 9 OR
REMOVE SMOKE DETECTOR FOR CLEANING 12000 FH
2-26 261800-01-1 200 RST AUXILIARY AREAS SMOKE DETECTION AF MRB 7,8 MRB 26.18.00/01 261815-100-001 24 MO YES N/A
OR
REMOVE SMOKE DETECTOR IN GSM-RACK FOR IN SHOP 8000 FH
CLEANING
2-26 261800-02-1 200 OPC AUXILIARY AREAS SMOKE DETECTION EL MRB 8 MRB 26.18.00/02 261800-710-001 24 MO N/A
OR
OPERATIONAL CHECK OF STAND-ALONE SMOKE DETECTION 8000 FH
SYSTEM INCLUDING MONITOR FUNCTION IN GSM-RACK
2-26 261800-03-1 200 RST AUXILIARY AREAS SMOKE DETECTION AF MRB 7,8 MRB 26.18.00/03 261815-100-802 24 MO YES N/A
OR
REMOVE SMOKE DETECTOR IN VCC-RACK FOR IN SHOP 8000 FH
CLEANING
2-26 261800-04-1 200 OPC AUXILIARY AREAS SMOKE DETECTION EL MRB 8 MRB 26.18.00/04 261800-710-803 24 MO N/A
OR
OPERATIONAL CHECK OF STAND-ALONE SMOKE DETECTION 8000 FH
SYSTEM INCLUDING MONITOR FUNCTION IN VCC-RACK
2-26 262100-02-1 210 OPC ENGINE FIRE EXTINGUISHING EL LUR MRB 26.21.00/02 262100-710-002 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF BOTTLE LOW PRESSURE INDICATING 12000 FH
CIRCUIT
2-26 262100-03-1 415 OPC ENGINE FIRE EXTINGUISHING EL LUR MRB 26.21.00/03 262100-720-001 144 MO APPL
425 MRB 9 OR
CHECK FIRING CIRCUIT CONTINUITY 18000 FH
2-26 262100-04-1 415 FNC ENGINE FIRE EXTINGUISHING AF LUR MRB 26.21.00/04 262100-720-003 72 MO N/A
425 MRB 8 OR
CHECK DISTRIBUTION PIPING TO DETECT LEAKAGE AND 8000 FH
OBSTRUCTION.
2-26 262100-04-2 415 FNC ENGINE FIRE EXTINGUISHING AF LUR MRB 26.21.00/09 262100-720-003 72 MO APPL
425 MRB 8 OR
CHECK DISTRIBUTION PIPING TO DETECT LEAKAGE AND 7500 FH
OBSTRUCTION.
2-26 262100-04-3 415 FNC ENGINE FIRE EXTINGUISHING AF LUR MRB 26.21.00/10 262100-720-003 72 MO N/A
425 MRB 8 OR
CHECK DISTRIBUTION PIPING TO DETECT LEAKAGE AND 7000 FH
OBSTRUCTION.
2-26 262100-05-1 210 OPC ENGINE FIRE EXTINGUISHING EL LUR MRB 26.21.00/08 262100-710-004 144 MO APPL
MRB 8 MRB 36.11.00/06 OR
OPERATIONAL CHECK OF FIRE CONTROL PUSH BUTTON SWITCH 18000 FH
SUB FUNCTIONS RELATED TO ENGINE SHUTDOWN AND
ISOLATION
2-26 262100-06-1 415 FNC ENGINE FIRE EXTINGUISHING AF LUR MRB 26.21.00/11 262100-720-802 108 MO N/A
425 MRB 8 OR
CHECK DISTRIBUTION PIPING TO DETECT LEAKAGE AND 12000 FH
OBSTRUCTION.
2-26 262100-07-1 415 FNC ENGINE FIRE EXTINGUISHING AF LUR MRB 26.21.00/12 262100-720-803 108 MO N/A
425 MRB 8 OR
CHECK DISTRIBUTION PIPING TO DETECT LEAKAGE AND 12000 FH
OBSTRUCTION.
2-26 262141-02-1 415 FNC ENGINE FIRE EXTINGUISHER BOTTLES CA MRB 6,9 MRB 26.21.00/07 262141-280-002 NOTE YES APPL
425 NOTE
REMOVE ENGINE FIRE EXTINGUISHING BOTTLE FOR IN SHOP
HYDROSTATIC TEST AND CHECK PRESSURE SWITCH SETTING.
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 27 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-26 262142-01-1 415 DIS ENGINE FIRE EXTINGUISHER BOTTLE CARTRIDGES EL MRB 9 MRB 26.21.00/06 262141-920-001 NOTE YES APPL
425 NOTE
DISCARD CARTRIDGE
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262200-02-1 210 OPC APU FIRE EXTINGUISHING EL LUR MRB 23.42.00/01 262200-710-002 36 MO APPL
MRB 8 MRB 26.22.00/02 OR
OPERATIONAL CHECK OF AUTOMATIC FIRE EXTINGUISHING MRB 28.29.00/01 3000 FH
CIRCUIT AND TEST APU LP FUEL VALVE OPERATION USING MRB 28.29.00/03
EACH INDIVIDUAL MOTOR IN TURN AND TEST APU EMERGENCY MRB 49.62.00/01-13
SHUTDOWN CIRCUIT MRB 49.62.00/01-32
MRB 49.62.00/01-36
MRB 49.62.00/03-13
MRB 49.62.00/03-32
MRB 49.62.00/03-36
2-26 262200-03-1 210 OPC APU FIRE EXTINGUISHING EL LUR MRB 26.22.00/07 262200-720-001 180 MO APPL
MRB 8 OR
CHECK FIRING CIRCUIT CONTINUITY 24000 FH
2-26 262200-04-1 313 DET APU FIRE EXTINGUISHING AF LUR MRB 26.22.00/05 262200-210-001 180 MO APPL
MRB 8 OR
DETAILED INSPECTION OF DISTRIBUTION PIPING 24000 FH
2-26 262200-05-1 210 OPC APU FIRE EXTINGUISHING EL LUR MRB 26.22.00/06 262200-710-003 180 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF LOW PRESSURE INDICATING CIRCUIT 24000 FH
2-26 262200-06-1 210 OPC APU FIRE EXTINGUISHING EL MRB 8 MRB 26.22.00/09 262200-710-004 80 MO APPL
MRB 49.62.00/02-13 OR
OPERATIONAL CHECK OF APU FIRE PUSH BUTTON SWITCH MRB 49.62.00/02-32 30000 FH
FUNCTIONS (IN SINGLE CHANNEL CONFIGURATION) AND TEST MRB 49.62.00/02-36
APU LP FUEL VALVE OPERATION USING EACH INDIVIDUAL
MOTOR IN TURN AND TEST APU EMERGENCY SHUTDOWN CIRCUIT
2-26 262241-01-1 313 FNC APU FIRE EXTINGUISHER BOTTLE CA MRB 6,8 MRB 26.22.00/03 262241-280-002 120 MO YES APPL
NOTE
REMOVE APU FIRE EXTINGUISHER BOTTLE FOR IN SHOP
HYDROSTATIC TEST AND CHECK PRESSURE SWITCH SETTING.
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262242-01-1 313 DIS APU FIRE EXTIR BOTTLE CARTRIDGE EL MRB 8 MRB 26.22.00/04 262242-920-001 NOTE YES APPL
DISCARD CARTRIDGE
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262300-02-1 132 OPC CARGO COMPARTMENT FIRE EXTINGUISHING EL CMR** CMR 262300-00001-1-C 262300-720-001 108 MO APPL
162 LUR MRB 26.23.00/03 OR
172 CHECK FIRING CIRCUIT CONTINUITY MRB 8 12000 FH
2-26 262300-03-1 132 FNC CARGO COMPARTMENT FIRE EXTINGUISHING CA CMR** CMR 262300-00002-1-C 262300-200-001 144 MO APPL
162 LUR MRB 26.23.00/04 OR
172 CHECK FIRE EXTINGUISHING LINES FOR LEAKAGE AND MRB 8 18000 FH
OBSTRUCTION
APPENDIX A
AEG/AMP/A320 Page 28 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-26 262300-04-1 132 DIS CARGO COMPARTMENT FIRE EXTINGUISHING AV MRB 8 MRB 26.23.00/05 262341-920-001 NOTE YES APPL
162 NOTE
172 REMOVE AND DISCARD CARGO COMPARTMENT FIRE
EXTINGUISHER BOTTLE CARTRIDGES
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262300-05-1 132 FNC CARGO COMPARTMENT FIRE EXTINGUISHING EL MRB 9 MRB 26.23.00/13 262300-710-004 72 MO N/A
162 OR
172 PERFORM FUNCTIONAL CHECK OF TIME DELAY FOR 16500 FH
210 ILLUMINATION OF "DISCH AGENT 2" REMINDER LIGHT
2-26 262300-06-1 132 OPC CARGO COMPARTMENT FIRE EXTINGUISHING EL CMR** CMR 262300-00001-1-C 262300-710-003 72 MO N/A
162 LUR MRB 26.23.00/07 OR
172 CHECK FIRING CIRCUIT CONTINUITY AND PERFORM MRB 8 7500 FH
210 OPERATIONAL CHECK OF PRIORITY SWITCHING
2-26 262300-07-1 132 FNC CARGO COMPARTMENT FIRE EXTINGUISHING AF CMR** CMR 262300-00002-1-C 262300-200-003 108 MO N/A
162 LUR MRB 26.23.00/04 OR
172 REMOVE THE PRESSURE REDUCER FOR IN-SHOP FUNCTIONAL MRB 8 MRB 26.23.00/08 14000 FH
CHECK INCLUDING CHECK OF FIRE EXTINGUISHING LINES FOR
LEAKAGE AND OBSTRUCTION
2-26 262300-08-1 132 DET CARGO COMPARTMENT FIRE EXTINGUISHING AF LUR MRB 26.23.00/09 262300-200-002 108 MO N/A
162 MRB 8 MRB 26.23.00/10 OR
172 -REMOVE HALON FILTER, CHECK VALVE AND DIAPHRAGM MRB 26.23.00/11 14000 FH
-INSPECT HALON FILTER -DO A DETAILED INSPECTION OF
CHECK VALVE -DO A DETAILED INSPECTION OF DIAPHRAGM
-REINSTALL HALON FILTER, CHECK VALVE AND DIAPHRAGM
2-26 262300-09-1 132 DIS CARGO COMPARTMENT FIRE EXTINGUISHING AF MRB 8 MRB 26.23.00/12 262314-920-001 15 MO YES N/A
162
172 DISCARD WATER ADSORBING FILTER
2-26 262318-01-1 132 DIS PRESSURE REDUCER AF CMP CMP 26-2-0000-003 262300-920-802 240 MO N/A
REPLACE PRESSURE REDUCER (P/N D41428 AND D41552)
2-26 262341-01-1 132 FNC CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA MRB 8 MRB 26.23.00/01 262341-280-001 72 MO YES APPL
162 OR
172 REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE FOR 22500 FH
IN SHOP WEIGHT CHECK.
2-26 262341-02-1 132 FNC CARGO COMPARTMENT FIRE EXTINGUISHER BOTTLE CA MRB 6,8 MRB 26.23.00/06 262341-280-002 120 MO YES APPL
162 NOTE
172 REMOVE CARGO COMPARTMENT FIRE EXTINGUISHER FOR IN
SHOP HYDROSTATIC TEST AND CHECK OF PRESSURE SWITCH
SETTING
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262441-01-1 200 VCK PORTABLE FIRE EXTINGUISHER CA LUR MRB 26.24.00/01 262400-210-002 24 MO APPL
MRB 9 OR
CHECK PRESSURE GAUGE READING 2000 FH
2-26 262441-02-1 200 FNC PORTABLE FIRE EXTINGUISHER CA MRB 9 MRB 26.24.00/02 262400-280-001 NOTE YES N/A
NOTE
HYDROSTATIC TEST OF BOTTLES
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 29 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-26 262441-03-1 200 FNC PORTABLE FIRE EXTINGUISHER CA MRB 9 MRB 26.24.00/03 262400-210-003 24 MO YES APPL
NOTE
WEIGHT CHECK OF PORTABLE FIRE EXTINGUISHER
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262441-04-1 200 FNC PORTABLE FIRE EXTINGUISHER CA MRB 9 MRB 26.24.00/04 262400-280-002 12 MO YES N/A
NOTE
WEIGHT CHECK OF PROPELLANT CARTRIDGE
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262441-05-1 200 DIS PORTABLE FIRE EXTINGUISHER CA MRB 9 MRB 26.24.00/05 262400-280-001 NOTE YES APPL
NOTE
DISCARD PORTABLE FIRE EXTINGUISHER
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-26 262541-01-1 200 DET LAVATORY FIRE EXTINGUISHER CA MRB 9 MRB 26.25.00/01 262500-200-002 72 MO APPL
DETAILED INSPECTION OF LAVATORY FIRE EXTINGUISHER FOR
SIGNS OF LEAKAGE/DISCHARGE
2-26 262541-02-1 200 FNC LAVATORY FIRE EXTINGUISHER BOTTLE CA MRB 9 MRB 26.25.00/02 262500-200-003 72 MO YES APPL
REMOVE LAVATORY FIRE EXTINGUISHER BOTTLE FOR WEIGHT
CHECK
2-26 262541-03-1 200 DET LAVATORY FIRE EXTINGUISHER CA LUR MRB 26.25.00/03 262500-200-004 12 MO N/A
MRB 9 OR
DETAILED INSPECTION OF LAVATORY FIRE EXTINGUISHER 750 FC
INCLUDING NOZZLE FOR SIGNS OF LEAKAGE/DISCHARGE
2-26 262541-04-1 200 VCK LAVATORY FIRE EXTINGUISHING AF MRB 9 MRB 26.25.00/04 262500-200-005 36 MO APPL
VISUAL CHECK OF FIRE EXTINGUISHER BOTTLE PRESSURE
READING
2-27 271400-01-1 210 OPC AILERON HYDRAULIC ACTUATION EL CMR** CMR 271400-00001-1-C 279600-710-007 36 MO APPL
LUR MRB 27.14.00/01 OR
OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE MRB 8 5000 FH
271400-01-2 ************** TASK DELETED ************** N/A
2-27 271400-02-1 575 FNC AILERON HYDRAULIC ACTUATION AF LUR MRB 27.14.00/03 271400-220-001 72 MO N/A
675 MRB 9 OR
CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR 5500 FH
EXCESSIVE PLAY AND CONDITION
2-27 271400-02-2 575 FNC AILERON HYDRAULIC ACTUATION AF LUR MRB 27.14.00/04 271400-220-001 144 MO APPL
675 MRB 9 OR
CHECK AILERON SERVO CONTROL AND HINGE BEARINGS FOR 18000 FH
EXCESSIVE PLAY AND CONDITION
2-27 271400-03-1 575 OPC AILERON HYDRAULIC ACTUATION AF CMR** CMR 271400-00002-1-C 271400-220-002 180 MO APPL
675 LUR MRB 27.14.00/02 OR
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC MRB 8 24000 FH
RESERVOIR DEPRESSURIZED
271400-03-2 ************** TASK DELETED ************** N/A
272100-01-1 ************** TASK DELETED ************** N/A
2-27 272100-02-1 100 DET RUDDER MECHANICAL CONTROL AF MRB 6 MRB 27.21.00/03 272100-210-002 108 MO APPL
OR
DETAILED INSPECTION OF CONTROL CABLES 36000 FH
272100-03-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 30 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 272100-04-1 325 OPC RUDDER MECHANICAL CONTROL AF LUR MRB 27.21.00/04 272641-280-001 180 MO YES APPL
MRB 9 OR
REMOVE YAW DAMPER SPRING ROD FOR IN SHOP OPERATIONAL 24000 FH
CHECK.
2-27 272100-05-1 210 OPC RUDDER MECHANICAL CONTROL AF MRB 8 MRB 27.21.00/05 272100-710-001 72 MO APPL
OR
OPERATIONAL CHECK OF CENTERING SPRING ROD 24000 FH
2-27 272100-07-1 325 DET RUDDER MECHANICAL CONTROL AF MRB 6,8 MRB 27.21.00/07 272100-210-003 72 MO APPL
OR
DETAILED INSPECTION OF MECHANICAL CONTROL LINKAGE IN 24000 FH
FIN
2-27 272100-08-1 210 LUB RUDDER MECHANICAL CONTROL AF MRB 6 MRB 27.21.00/09 272143-600-001 24 MO APPL
LUBRICATION OF RUDDER PEDAL ADJUSTMENT MECHANISM
2-27 272100-10-1 320 FNC RUDDER MECHANICAL CONTROL AF MRB 8 MRB 27.21.00/10 272149-200-001 108 MO APPL
OR
FUNCTIONAL CHECK OF RUDDER SERVOCONTROL ACTUATING 36000 FH
SPRING RODS
2-27 272100-11-1 325 DET RUDDER MECHANICAL CONTROL AF MRB 9 MRB 27.21.00/11 272100-220-004 108 MO APPL
OR
DETAILED INSPECTION OF RUDDER SERVOCONTROL ACTUATING 36000 FH
SPRING RODS AND RUDDER SERVOCONTROL FEEDBACK ROD
ATTACHMENTS
2-27 272145-01-1 125 FNC RUDDER CABLE TENSION REGULATOR AF MRB 9 MRB 27.21.00/02 272100-220-002 40 MO APPL
FUNCTIONAL CHECK OF TENSION REGULATOR (POINTER WITHIN
THE LIMITS)
2-27 272400-01-1 210 OPC RUDDER HYDRAULIC ACTUATION AF LUR MRB 27.24.00/01 272400-710-002 6 MO APPL
MRB 8 MRB 29.10.00/15 OR
OPERATIONAL CHECK OF RUDDER SERVOCONTROLS WITH MRB 29.30.00/01 750 FH
INDIVIDUAL HYDRAULIC SYSTEMS MRB 29.30.00/02
2-27 272400-02-1 325 FNC RUDDER HYDRAULIC ACTUATION AF LUR MRB 27.24.00/02 272400-200-001 144 MO N/A
MRB 9 OR
CHECK RUDDER SERVOCONTROL AND HINGE BEARINGS FOR 18000 FH
EXCESSIVE PLAY AND CONDITION
2-27 272400-03-1 325 LUB RUDDER HYDRAULIC ACTUATION AF MRB 9 MRB 27.24.00/03 122255-640-001 15 MO
OR
LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE 5500 FH
MAT. NO. 04-004
N/A
NOTE:
ALTERNATIVELY TASK 272400-05-1 CAN BE APPLIED.
2-27 272400-05-1 325 LUB RUDDER HYDRAULIC ACTUATION AF MRB 9 MRB 27.24.00/03 122255-640-002 24 MO
OR
LUBRICATION OF RUDDER HINGE BEARING NO 6 WITH GREASE 10000 FH
MAT. NO. 04-037
NOTE:
THIS IS AN ALTERNATIVE TASK TO 272400-03-1.
APPL
2-27 272400-06-1 325 LUB RUDDER HYDRAULIC ACTUATION AF MRB 9 MRB 27.24.00/05 122227-640-804 24 MO
OR
LUBRICATION OF RUDDER SERVOCONTROL ROD EYE END 10000 FH
BEARING
N/A
2-27 273400-01-1 210 OPC ELEVATOR AND HYDRAULIC ACTUATION EL CMR** CMR 273400-00001-1-C 279600-710-008 36 MO APPL
LUR MRB 27.34.00/01 OR
OPERATIONAL CHECK OF DAMPING MEASUREMENT BY BITE MRB 8 5000 FH
273400-01-2 ************** TASK DELETED ************** N/A
2-27 273400-02-1 334 FNC ELEVATOR AND HYDRAULIC ACTUATION AF MRB 9 MRB 27.34.00/03 273400-200-001 24 MO APPL
344 EASA AD 2007-0163R1 OR
CHECK ELEVATOR SERVOCONTROL AND HINGE BEARINGS FOR 12000 FH
EXCESSIVE PLAY AND CONDITION
2-27 273400-02-2 334 FNC ELEVATOR AND HYDRAULIC ACTUATION AF MRB 9 MRB 27.34.00/03 273400-200-001 24 MO 24 MO N/A
344 SEMR SEMR 273400-00001-1-E OR OR
CHECK ELEVATOR SERVOCONTROL AND HINGE BEARINGS FOR 12000 FH 12000 FH
EXCESSIVE PLAY AND CONDITION
APPENDIX A
AEG/AMP/A320 Page 31 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 273400-03-1 334 OPC ELEVATOR AND HYDRAULIC ACTUATION AF CMR** CMR 273400-00002-1-C 273400-220-001 180 MO APPL
344 LUR MRB 27.34.00/02 OR
CHECK FLUID RESERVE PISTON POSITION WITH HYDRAULIC MRB 8 24000 FH
RESERVOIR DEPRESSURIZED.
273400-03-2 ************** TASK DELETED ************** N/A
2-27 273400-04-1 334 VCK ELEVATOR AND HYDRAULIC ACTUATION AF CMR* CMR 273400-00002-3-C 273400-220-002 252 MO APPL
344 LUR MRB 27.34.00/04 OR
CHECK OF THE DIFFERENTIAL PRESSURE INDICATOR AND MRB 8 36000 FH
POSITION OF FLUID RESERVE PISTON OF ELEVATOR SERVO
CONTROLS
273400-04-2 ************** TASK DELETED ************** N/A
2-27 273400-08-1 334 LUB ELEVATOR AND HYDRAULIC ACTUATION AF MRB 9 MRB 27.34.00/06 122227-640-803 24 MO APPL
344 OR
LUBRICATION OF ELEVATOR SERVOCONTROL ROD EYE END 10000 FH
BEARING
2-27 274000-01-1 310 LUB TRIMMABLE HORIZONTAL STABILIZER AF MRB 9 MRB 27.40.00/04 122253-640-001 15 MO
OR
LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH 5500 FH
GREASE MAT. NO. 04-004
N/A
NOTE:
ALTERNATIVE TASK 274000-07-1 CAN BE APPLIED.
2-27 274000-02-1 210 OPC TRIMMABLE HORIZONTAL STABILIZER (THS) AF CMR** CMR 274000-00002-1-C 274400-710-002 750 FH APPL
MRB 8 MRB 27.40.00/01
OPERATIONAL CHECK OF THS ACTUATOR WITH INDIVIDUAL
HYDRAULIC SYSTEMS
2-27 274000-03-1 210 OPC TRIMMABLE HORIZONTAL STABILIZER (THS) AF CMR** CMR 274000-00003-1-C 274400-710-001 36 MO APPL
LUR MRB 27.40.00/02 OR
OPERATIONAL CHECK OF THS ACTUATOR JAMMING PROTECTION MRB 8 4000 FH
DEVICE
2-27 274000-04-1 210 OPC TRIMMABLE HORIZONTAL STABILIZER AF LUR MRB 27.40.00/06 279600-710-006 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF THS ACTUATOR WITH ELECTRICAL 24000 FH
MOTOR NO 3
2-27 274000-07-1 310 LUB TRIMMABLE HORIZONTAL STABILIZER AF MRB 9 MRB 27.40.00/04 122253-640-002 24 MO APPL
OR
LUBRICATE THS BEARINGS AND ATTACHMENT FITTINGS WITH 7500 FH
GREASE MAT. NO. 04-037
NOTE:
THIS IS AN ALTERNATIVE TASK TO 274000-01-1
2-27 274100-01-1 100 DET THS MECHANICAL CONTROL AF MRB 6 MRB 27.40.00/12 274100-210-001 108 MO APPL
310 OR
DETAILED INSPECTION OF THS MECHANICAL CONTROL 36000 FH
274100-02-1 ************** TASK DELETED ************** N/A
2-27 274100-03-1 120 LUB THS MECHANICAL CONTROL AF MRB 6 MRB 27.40.00/20 122227-640-007 20 MO N/A
310
LUBRICATION OF THS MECHANICAL CONTROL CHAINS AND REAR
CABLE (AREA OF TENSION REGULATOR) WITH GREASE MAT.
NO. 04-004
NOTE:
THIS IS AN ALTERNATIVE TASK TO 274100-05-1
2-27 274100-05-1 120 LUB THS MECHANICAL CONTROL AF MRB 6 MRB 27.40.00/20 122227-640-805 24 MO APPL
310
LUBRICATION OF THS MECHANICAL CONTROL CHAINS AND REAR
CABLE (AREA OF TENSION REGULATOR) WITH GREASE MAT.
NO. 04-037
NOTE:
THIS IS AN ALTERNATIVE TASK TO 274100-03-1
2-27 274142-01-1 310 FNC THS TRIM CTL CABLE TENSION COMPENSATOR AF MRB 6 MRB 27.40.00/07 274100-220-001 40 MO
FUNCTIONAL CHECK OF POINTER ON TENSION COMPENSATOR
(SCALE WITHIN LIMITS)
APPL
APPENDIX A
AEG/AMP/A320 Page 32 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 274400-01-1 310 FNC THS HYDRAULIC ACTUATION AF LUR MRB 27.40.00/14 274454-720-001 252 MO APPL
MRB 9 OR
FUNCTIONAL CHECK OF THS ACTUATOR PRESSURE OFF BRAKE 36000 FH
(APPLY TORQUE TO MANUAL CRANKING INPUT)
274400-02-1 ************** TASK DELETED ************** N/A
2-27 274400-03-1 310 OPC THS ACTUATOR AF LUR MRB 27.40.00/18 274451-710-001 180 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF THS ACTUATOR NO-BACK DEVICE 24000 FH
2-27 274451-01-1 310 LUB THS ACTUATOR AF LUR MRB 27.40.00/03 122227-640-003 12 MO APPL
MRB 6 OR
LUBRICATE THS ACTUATOR BALL SCREW NUT 1600 FH
2-27 274451-02-1 311 SVC THS ACTUATOR AF LUR MRB 27.40.00/05 274451-210-004 36 MO APPL
312 MRB 6,9 OR
CHECK OIL LEVEL OF THS ACTUATOR GEARBOX 3000 FH
2-27 274451-02-2 311 SVC THS ACTUATOR AF LUR MRB 27.40.00/23 274451-210-004 72 MO N/A
312 MRB 6,9 OR
CHECK OIL LEVEL OF THS ACTUATOR GEARBOX. 6000 FH
274451-03-1 ************** TASK DELETED ************** N/A
2-27 274451-04-1 310 DET THS ACTUATOR AF LUR MRB 27.40.00/09 274451-220-001 108 MO APPL
MRB 6,9 OR
DETAILED INSPECTION OF THS ACTUATOR BALL SCREW NUT 12000 FH
BODY AND SCREW AND CLAW STOPS
2-27 274451-05-1 310 DET THS ACTUATOR AF MRB 6,8 MRB 27.40.00/10 274451-220-002 40 MO APPL
OR
DETAILED INSPECTION OF UPPER AND LOWER THS ACTUATOR 12000 FH
ATTACHMENT (PRIMARY AND SECONDARY)
NOTE:
FOR NEO A/C ONLY:
PLANNING:
- ENSURE THAT INSPECTIONS ACCORDING 274451-10-1 AND
274451-11-1 ARE CARRIED OUT PRIOR TO TASK
274451-05-1 (AND PRIOR TO ANY CLEANING), WHEN
PLANNED AT THE SAME TIME
2-27 274451-06-1 310 VCK THS ACTUATOR AF LUR MRB 27.40.00/11 274451-210-002 108 MO APPL
MRB 8 OR
VISUAL CHECK OF THS ACTUATOR THREADED NUT (FAIL SAFE 12000 FH
NUT)
274451-07-1 ************** TASK DELETED ************** N/A
2-27 274451-08-1 310 FNC THS ACTUATOR AF CMR* CMR 274000-00001-1-C 274451-280-001 108 MO APPL
LUR MRB 27.40.00/16 OR
CHECK INTEGRITY OF THS ACTUATOR BALL SCREW SHAFT MRB 6,8 12000 FH
(PRIMARY AND SECONDARY LOAD PATH)
2-27 274451-09-1 310 SVC THS ACTUATOR AF LUR MRB 27.40.00/21 274451-610-001 144 MO APPL
MRB 9 OR
DRAIN AND REFILL THS ACTUATOR GEARBOX 18000 FH
2-27 274451-10-1 310 DET THS ACTUATOR AF SEMR SEMR 274000-00002-1-E 274451-220-003 20 MO 20 MO N/A
DETAILED INSPECTION OF THSA LOWER ATTACHMENTS FOR
PRIMARY AND SECONDARY LOAD PATH
NOTE:
PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF
PLANNED AT THE SAME TIME) AND PRIOR TO ANY CLEANING.
INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT
AND NOT DELIVERY FLIGHT.
2-27 274451-11-1 310 DET THS ACTUATOR AF SEMR SEMR 274000-00003-1-E 274451-220-004 10 MO 10 MO N/A
DETAILED INSPECTION OF THSA UPPER ATTACHMENTS FOR
PRIMARY AND SECONDARY LOAD PATH
NOTE:
PERFORM INSPECTION PRIOR TO TASK 274451-05-1 (IF
PLANNED AT THE SAME TIME) AND PRIOR TO ANY CLEANING.
INTERVAL STARTING POINT IS THE AIRCRAFT FIRST FLIGHT
AND NOT DELIVERY FLIGHT.
APPENDIX A
AEG/AMP/A320 Page 33 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 274451-13-1 310 SDI THS ACTUATOR NDT SEMR SEMR 274000-00001-1-E 274451-220-804 30000 FC NOTE N/A
OR
SPECIAL DETAILED INSPECTION OF THSA (HIGH TIME THSA 48000 FH
INSPECTION)
NOTE:
INTERVAL:
- FOR INTERVAL TIME SCALE REFER TO SEMR
274000-00001-1-E.
2-27 274451-14-1 310 OPC THS ACTUATOR AF LUR MRB 27.40.00/22 274451-710-802 108 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF THS ACTUATOR ELECTRICAL LOAD 15000 FH
SENSING DEVICE
2-27 274451-15-1 310 RST THS ACTUATOR AF SEMR SEMR 274000-00004-1-E 274451-960-802 30000 FC 30000 FC YES N/A
REMOVE COMPLETE THSA FOR NO BACK BRAKE (NBB) CARBON
DISKS DISCARD AND REPLACE WITH SERVICEABLE THSA UNIT.
2-27 275100-01-2 210 OPC FLAPS AF CMR** CMR 275000-00001-1-C 275100-710-001 108 MO APPL
LUR MRB 27.50.00/04 OR
OPERATIONAL CHECK OF WTB/POB MRB 6,8 MRB 27.50.01/04 12000 FH
NOTE:
FLAP SURFACES MOVE AUTOMATICALLY
2-27 275100-01-3 210 OPC FLAPS AF CMR** CMR 275000-00001-2-C 275100-710-001 72 MO N/A
LUR MRB 27.50.00/04 OR
OPERATIONAL CHECK OF WTB/POB MRB 6,8 7500 FH
NOTE:
FLAP SURFACES MOVE AUTOMATICALLY
2-27 275100-02-1 210 OPC FLAPS AF LUR MRB 27.50.00/05 275100-710-002 108 MO APPL
MRB 8 MRB 27.50.01/05 OR
OPERATIONAL CHECK OF FLAP INTERCONNECTING STRUT AND 12000 FH
FLAP DISCONNECT PROXIMITY SENSORS
2-27 275100-03-1 575 CHK FLAPS AF CMR** CMR 275000-00001-1-C 275400-210-002 108 MO APPL
675 LUR MRB 27.50.00/04 OR
CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, MRB 6,8 MRB 27.50.01/04 12000 FH
INCLUDING INSPECTION OF SEAL WITNESS DRAINS.
2-27 275100-03-2 575 CHK FLAPS AF CMR** CMR 275000-00001-2-C 275400-210-002 72 MO N/A
675 LUR MRB 27.50.00/04 OR
CHECK OF FLAPS TRANSMISSION SHAFTING INTEGRITY, MRB 6,8 7500 FH
INCLUDING INSPECTION OF SEAL WITNESS DRAINS.
2-27 275117-01-1 212 FNC FLAP/SLAT COMMAND SENSOR UNIT AF MRB 8 MRB 27.50.00/07 275117-280-001 40 MO YES APPL
MRB 27.50.01/07
REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE MRB 27.80.00/05
2-27 275117-01-2 212 FNC FLAP/SLAT COMMAND SENSOR UNIT AF MRB 8 MRB 27.50.00/16 275117-280-001 144 MO YES N/A
MRB 27.50.01/14
REMOVE CSU FOR WORKSHOP CHECK OF FRICTION BRAKE MRB 27.80.00/08
2-27 275144-01-1 580 DET FLAP INTERCONNECTING STRUT AF LUR MRB 27.50.00/06 275144-200-001 108 MO APPL
680 MRB 8 MRB 27.50.01/06 OR
DETAILED INSPECTION OF INTERCONNECTING STRUT AND 12000 FH
ATTACHMENTS
2-27 275400-01-1 570 DET FLAP TRANSMISSION ASSY AF MRB 6 MRB 27.50.00/08 275400-200-001 80 MO APPL
670 MRB 27.50.01/08 OR
DETAILED INSPECTION OF TRANSMISSION ASSY 24000 FH
2-27 275446-01-1 530 LUB FLAP TRACKS AF MRB 6,9 MRB 27.50.00/02 122227-640-004 10 MO APPL
630 MRB 27.50.01/02 OR
LUBRICATE ALL CARRIAGE ROLLERS ON ALL FLAP TRACKS 1800 FC
2-27 275446-02-1 530 DET FLAP TRACKS AF MRB 6,9 MRB 27.50.00/09 275446-200-001 80 MO APPL
630 OR
DETAILED INSPECTION OF TRACKS, ROLLERS AND SPHERICAL 24000 FH
BEARINGS (AS FAR AS VISIBLE).
APPENDIX A
AEG/AMP/A320 Page 34 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 275446-04-1 530 DET FLAP TRACKS AF MRB 6,9 MRB 27.50.01/09 275446-200-802 80 MO N/A
630 OR
DETAILED INSPECTION OF TRACKS, ROLLERS, SPHERICAL 24000 FH
BEARING AND TAB DRIVE KINEMATIC (AS FAR AS VISIBLE)
NOTE:
CREDIT CAN BE TAKEN FROM PREVIOUS ACCOMPLISHMENT OF
TASK 275446-02-1.
2-27 275449-03-1 575 SVC ACTUATOR ASSEMBLY AF MRB 6 MRB 27.50.00/12 121327-612-004 72 MO N/A
675 MRB 27.50.01/11 OR
DRAIN AND REFILL OFFSET GEARBOXES OF ROTARY ACTUATORS 24000 FH
WITH SEMI-FLUID
2-27 275449-05-1 575 LUB ACTUATOR ASSEMBLY AF MRB 6 MRB 27.50.00/15 122227-640-008 72 MO N/A
675 MRB 27.50.01/13 OR
REMOVE FLAP ROTARY ACTUATOR ASSEMBLIES FOR 18000 FC
REGREASING. OR
24000 FH
2-27 275449-06-1 575 SVC ACTUATOR ASSEMBLY AF MRB 6 MRB 27.50.00/13 121327-612-005 72 MO APPL
675 MRB 27.50.01/12 OR
DRAIN AND REFILL FLAP ACTUATOR ASSEMBLIES WITH 24000 FH
SEMI-FLUID
2-27 275451-01-1 147 SVC FLAP POWER CONTROL UNIT AF MRB 6 MRB 27.50.00/03 121327-612-002 36 MO APPL
MRB 27.50.01/03
REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL
2-27 276400-01-1 575 LUB SPOILER AND HYDRAULIC ACTUATION AF LUR MRB 27.64.00/02 122227-640-005 24 MO APPL
675 MRB 9 OR
LUBRICATE SPOILER NO 1 TO 5 ACTUATOR ATTACHMENTS 2000 FH
2-27 276400-02-1 575 FNC SPOILER AND HYDRAULIC ACTUATION AF LUR MRB 27.64.00/03 276400-200-001 144 MO APPL
675 MRB 9 OR
CHECK SPOILER SERVOCONTROL BEARING AND HINGE BEARINGS 18000 FH
FOR EXCESSIVE PLAY AND CONDITION
2-27 278100-03-1 210 OPC SLATS AF CMR** CMR 278000-00001-1-C 278100-710-001 48 MO APPL
MRB 6,8 MRB 27.80.00/04 OR
OPERATIONAL CHECK OF WTB/POB 12000 FH
2-27 278100-03-2 210 OPC SLATS AF CMR** CMR 278000-00001-2-C 278100-710-001 48 MO N/A
MRB 6,8 MRB 27.80.00/04 OR
OPERATIONAL CHECK OF WTB/POB. 7500 FH
2-27 278100-04-1 520 CHK SLATS AF CMR** CMR 278000-00001-1-C 278400-210-002 48 MO APPL
620 MRB 6,8 MRB 27.80.00/04 OR
CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, 12000 FH
INCLUDING INSPECTION OF SEAL WITNESS DRAINS
2-27 278100-04-2 520 CHK SLATS AF CMR** CMR 278000-00001-2-C 278400-210-002 48 MO N/A
620 MRB 6,8 MRB 27.80.00/04 OR
CHECK OF SLATS TRANSMISSION SHAFTING INTEGRITY, 7500 FH
INCLUDING INSPECTION OF SEAL WITNESS DRAINS
2-27 278400-01-1 147 DET SLAT TRANSMISSION ASSY AF MRB 6 MRB 27.80.00/06 278400-200-001 80 MO APPL
190 OR
520 DETAILED INSPECTION OF TRANSMISSION ASSY 24000 FH
620
2-27 278451-01-1 147 SVC SLAT POWER CONTROL UNIT AF MRB 6 MRB 27.80.00/03 121327-612-003 36 MO APPL
REPLENISH PCU GEARBOX TO CONFIRM FLUID LEVEL
APPENDIX A
AEG/AMP/A320 Page 35 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-27 278468-01-1 520 LUB SLAT TRACKS AF MRB 6,9 MRB 27.80.00/02 122227-640-006 20 MO APPL
620 OR
LUBRICATE ALL TRACK ROLLERS AND PINIONS 4500 FC
2-27 278468-02-1 520 DET SLAT TRACKS AF MRB 6,9 MRB 27.80.00/07 278400-210-001 80 MO APPL
620 MRB CPCP MRB 574206-01-1 OR
DETAILED INSPECTION OF SLAT TRACKS, ROLLER BEARINGS, MRB 574306-01-1 24000 FH
PINION BEARINGS AND CURVED RACK GEARS - AS VISIBLE. MRB 574406-01-1
MRB 574506-01-1
MRB 574606-01-1
2-27 279000-05-1 210 OPC ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) AV CMR* CMR 279000-00001-1-C 279600-710-018 80 DY APPL
LUR MRB 27.90.00/02 OR
OPERATIONAL CHECK : MRB 8 MRB 27.90.00/05 400 FH
- OF LOGICS ACTIVATING ELAC 1, ELAC 2 AND SEC.1
STANDBY POWER SUPPLIES
- TO CONFIRM ABILITY OF SEC.1 AND SEC.2 TO ACHIEVE
PITCH CONTROL
- TO CONFIRM ABILITY OF SIDESTICK PRIORITY FUNCTION
2-27 279000-07-1 210 OPC ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) AV LUR MRB 27.90.00/07 279600-740-001 6 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF EFCS BY BITE (GROUND SCANNING) 750 FH
2-28 281100-01-2 190 SVC TANKS AF MRB 9 MRB 28.42.00/02 123228-281-001 10 DY APPL
500 NOTE
600 DRAIN WATER CONTENT Included into Weekly
Checklist
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-28 281100-02-1 196 OPC TANKS AF LUR MRB 28.11.00/02 281100-200-002 12 MO APPL
MRB 9 MRB 28.13.00/02 OR
OPERATIONAL CHECK OF LEAK MONITOR FOR EVIDENCE OF 1000 FH
FUEL LEAKAGE AND CORRECT CLOSURE OF THE VALVE
2-28 281100-05-1 190 GVI TANKS AF MRB 9 MRB 28.11.00/07 281100-210-801 6 MO APPL
500
600 GENERAL VISUAL INSPECTION OF FUEL TANKS FOR MINOR
EXTERNAL LEAKS
2-28 281100-06-1 190 OPC TANKS AF MRB 9 MRB 28.11.00/01 6 MO APPL
500
600 OPERATIONAL CHECK OF WATER DRAIN VALVES
281142-01-1 ************** TASK DELETED ************** N/A
2-28 281200-01-1 500 VCK TANK VENTING SYSTEM AF LUR MRB 28.12.00/02 281200-210-001 6 MO APPL
600 MRB 9 OR
VISUAL CHECK OF VENT SURGE TANK BURST DISC (EXTERNAL) 750 FH
2-28 281247-01-1 550 VCK NACA VENT INTAKE AF MRB 9 MRB 28.12.00/01 281247-200-001 36 MO APPL
650
VISUAL CHECK OF NACA INTAKE FOR SIGNS OF BLOCKAGE
2-28 281343-01-1 148 VCK DRAIN MAST AF MRB 9 MRB 28.13.00/01 281300-200-001 4 MO APPL
MRB 28.22.00/03
VISUAL CHECK OF DRAIN MAST FOR OBSTRUCTION
2-28 281500-01-1 210 OPC INTERCELL TRANSFER SYSTEM AV CMR** CMR 281500-00001-1-C 281500-710-002 72 MO APPL
LUR MRB 28.15.00/02 OR
OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO MRB 8 10000 FH
ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION
2-28 281500-01-2 210 OPC INTERCELL TRANSFER SYSTEM AV CMR** CMR 281500-00001-2-C 281500-710-002 72 MO N/A
LUR MRB 28.15.00/02 OR
OPERATIONAL CHECK OF INDIVIDUAL TRANSFER VALVES TO MRB 8 7500 FH
ENSURE VALVE SHAFT ROTATES VALVE TO OPEN POSITION
2-28 281600-01-1 471 OPC FUEL RECIRCULATION COOLING AF LUR MRB 28.16.00/01 281600-710-002 108 MO APPL
481 MRB 8 OR
OPERATIONAL CHECK OF PYLON CHECK VALVE TO ENSURE 12000 FH
VALVE NOT FAILED OPEN
2-28 281600-04-1 471 VCK FUEL RECIRCULATION COOLING AF LUR MRB 28.16.00/04 281600-210-801 108 MO N/A
481 MRB 9 OR
VISUAL CHECK OF RECIRCULATION RETURN LINE SHROUD 12000 FH
APPENDIX A
AEG/AMP/A320 Page 36 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 281800-01-1 137 FNC IGNITION PREVENTION AF FAL FAL 281800-00001-1-F 281800-700-001 72 MO APPL
138 MRB 8 MRB 28.13.00/03 OR
FUNCTIONAL CHECK OF TANK VAPOUR SEAL AND VENT DRAIN MRB 28.13.00/05 36000 FH
SYSTEM (SFAR88) MRB 28.18.00/04
2-28 281800-02-1 191 DET IGNITION PREVENTION AF FAL FAL 281800-00002-1-F 281800-200-001 72 MO APPL
192 MRB 8 MRB 28.18.00/03
DETAILED INSPECTION OF VAPOUR SEAL (SFAR88)
2-28 281800-03-1 140 DET IGNITION PREVENTION AF MRB 9 MRB 28.18.00/01 281800-200-002 144 MO APPL
540
550 DETAILED INSPECTION OF TANK BONDING LEADS (SFAR88)
640
650
2-28 281800-04-1 140 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/02 281844-210-001 144 MO APPL
540
550 GENERAL VISUAL INSPECTION OF INTERNAL TANK WIRING AND
640 PROBE ATTACHMENTS (SFAR88)
650
2-28 281800-05-1 137 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/05 281852-210-001 72 MO APPL
138
GENERAL VISUAL INSPECTION OF CENTER TANK FWD CARGO
BAY ISOLATION MATS (SFAR88)
2-28 281800-06-1 145 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/06 281842-210-001 144 MO APPL
146
GENERAL VISUAL INSPECTION OF WIRING HARNESSES ABOVE
CENTER TANK (SFAR88)
2-28 281800-07-1 520 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/07 281841-210-001 144 MO APPL
570
620 GENERAL VISUAL INSPECTION OF WING LEADING EDGE AND
670 TRAILING EDGE ELECTRICAL WIRING AND CONNECTIONS
(SFAR88)
2-28 281800-08-1 540 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/08 281843-210-001 144 MO APPL
640
GENERAL VISUAL INSPECTION OF WING FUEL PUMP
ELECTRICAL CONNECTIONS AND UNDERWING ELECTRICAL
SUPPLY CABLE (SFAR88)
2-28 281800-09-1 140 GVI IGNITION PREVENTION AF MRB 9 MRB 28.18.00/09 281851-210-001 144 MO APPL
540
640 GENERAL VISUAL INSPECTION OF FUEL PUMP CANISTERS
(SFAR88)
2-28 281800-10-1 122 OPC IGNITION PREVENTION AV MRB 8 MRB 28.18.00/10 281800-710-801 24 MO APPL
OPERATIONAL CHECK OF CENTRE TANK FUEL PUMP GFI
(SFAR88)
APPENDIX A
AEG/AMP/A320 Page 37 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 281800-10-2 122 OPC IGNITION PREVENTION AF FAL FAL 281800-00003-1-F 281800-710-801 24 MO N/A
MRB 8 MRB 28.18.00/10 OR
OPERATIONAL CHECK OF CENTRE TANK FUEL PUMP GFI 4000 FH
(SFAR88)
2-28 281800-12-1 411 VCK IGNITION PREVENTION AF MRB 8 MRB 28.18.00/11 281800-210-801 144 MO N/A
421
VISUAL CHECK OF THE PROTECTIVE SHIELD BETWEEN THE
FUEL RECIRCULATION RETURN LINE AND THE BLEED AIR
PRESSURE SENSORS
2-28 282100-01-1 210 OPC MAIN FUEL PUMP SYSTEM AF LUR MRB 28.21.00/04 282100-710-002 252 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF WING TANK PUMP PRESSURE SENSE 36000 FH
LINE CHECK VALVES
2-28 282100-02-1 140 OPC MAIN FUEL PUMP SYSTEM AF LUR MRB 28.21.00/05 282100-710-003 180 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF CENTER TANK PUMP CANISTER CHECK 24000 FH
VALVES
2-28 282100-03-1 210 OPC MAIN FUEL PUMP SYSTEM AF CMP CMP 28-2-0000-002 282100-710-008 NOTE 216 MO APPL
LUR MRB 28.21.00/08 OR
OPERATIONAL CHECK OF AIR RELEASE VALVES TO ENSURE MRB 8 30000 FH
ADEQUATE FUEL FLOW UNDER SUCTION FEED CONDITIONS
NOTE:
FOR ETOPS A/C ONLY: THRESHOLD:
- AT A MAINTENANCE OPPORTUNITY BETWEEN 750 FH AND
1000 FH AFTER AIRCRAFT DELIVERY AND AFTER ANY TANK
REPAIR (TANK ENTRY WHERE SIGNIFICANT DEBRIS MAY BE
GENERATED).
- PRIOR TO ETOPS OPERATIONS IF MORE THAN 1000 FH
SINCE AIRCRAFT DELIVERY OR TANK REPAIR AND TASK WAS
NOT ACCOMPLISHED.
2-28 282100-04-1 210 OPC MAIN FUEL PUMP SYSTEM AF CMR** CMR 282100-00001-1-C 282100-710-005 72 MO APPL
LUR MRB 28.21.00/03 OR
OPERATIONAL CHECK TO ENSURE THAT BOTH CENTER TANK MRB 8 10000 FH
PUMPS FEED FOR 2 MINUTES AFTER ENGINE START
2-28 282100-05-1 410 VCK FUEL PUMP SYSTEM AF LUR MRB 28.21.00/02 282100-790-002 108 MO APPL
420 MRB 9 OR
520 VISUAL CHECK OF PIPES, COUPLINGS AND LP VALVE 12000 FH
620 EXTERNAL TO TANK FROM FRONT SPAR TO DISCONNECT PANEL
FOR LEAKS WITH BOOSTER PUMP ON AND LP VALVE OPEN
2-28 282100-10-1 540 FNC MAIN FUEL PUMP SYSTEM AF MRB 8 MRB 28.21.00/10 282100-720-802 144 MO YES APPL
640
REMOVE AIR RELEASE VALVE FOR FUNCTIONAL CHECK OF
FLOAT
2-28 282200-02-1 148 OPC APU FUEL PUMP SYSTEM AF LUR MRB 28.22.00/01 282200-210-001 6 MO APPL
MRB 9 OR
CHECK FOR LEAKAGE FROM SHROUD DRAIN MAST AND APU 750 FH
COMPARTMENT DRAIN MAST WITH APU FUEL PUMP RUNNING
2-28 282300-01-1 210 OPC CROSSFEED SYSTEM AF CMP CMP 28-2-0000-001 282300-720-001 72 MO N/A
LUR MRB 28.23.00/01 OR
OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL MRB 8 6000 FH
MOTORS AND CHECK FUEL FLOW IN "OPEN" AND FUEL SHUT
OFF IN "CLOSED" POSITIONS
2-28 282300-01-2 210 OPC CROSSFEED SYSTEM AF LUR MRB 28.23.00/01 282300-720-001 108 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL 12000 FH
MOTORS AND CHECK FUEL FLOW IN "OPEN" AND FUEL SHUT
OFF IN "CLOSED" POSITIONS
2-28 282300-01-3 210 OPC CROSSFEED SYSTEM AF CMP CMP 28-2-0000-003 282300-720-001 72 MO N/A
LUR MRB 28.23.00/01 OR
OPERATIONAL CHECK OF CROSSFEED VALVE USING INDIVIDUAL MRB 8 5800 FH
MOTORS AND CHECK FUEL FLOW IN "OPEN" AND FUEL SHUT
OFF IN "CLOSED" POSITIONS
APPENDIX A
AEG/AMP/A320 Page 38 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 282400-01-1 210 OPC ENGINE LOW PRESSURE SHUT OFF AF LUR MRB 28.24.00/01 282400-790-003 108 MO APPL
MRB 8 OR
OPERATIONAL CHECK OF LP SHUT OFF VALVES AND THEIR 15000 FH
CONTROLS TO ENSURE NO FLOW WHEN SELECTED CLOSED WITH NOTE
BOOSTER PUMP ON
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED
2-28 282400-02-1 210 OPC ENGINE LOW PRESSURE SHUT OFF AF LUR MRB 28.24.00/02 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF LP SHUT OFF VALVES INCLUDING 24000 FH
OPERATION BY INDIVIDUAL MOTORS
2-28 282541-01-1 522 DET COUPLING REFUEL/DEFUEL AF LUR MRB 28.25.00/02 282541-200-001 72 MO APPL
622 MRB 6 OR
DETAILED INSPECTION OF COUPLING REFUEL/DEFUEL. 5000 FC
282600-01-1 ************** TASK DELETED ************** N/A
2-28 282800-01-1 190 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF CMP CMP 28-2-0000-004 282800-200-003 6 MO N/A
LUR MRB 28.28.00/01 OR
OPERATIONAL CHECK OF LEAK MONITOR FOR EVIDENCE OF MRB 8 750 FH
FUEL LEAKAGE NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-03-1 190 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 9 MRB 28.28.00/03 123228-281-005 4 MO N/A
NOTE
OPERATE WATER DRAIN VALVES IN INSTALLED ACT(S) TO
DRAIN ACCUMULATED WATER
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-28 282800-04-1 200 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/04 282800-710-002 180 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF MOTOR 1 OF TRANSFER VALVE 22500 FH
NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-05-1 200 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF CMR** CMR 282800-00001-1-C 282800-710-001 72 MO N/A
LUR MRB 28.28.00/13 OR
OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM MRB 9 7900 FH
NOTE:
CMR APPLICABLE ONLY IF FQIC 6 IS INSTALLED.
EMBODIMENT OF FQIC 7 OR LATER STANDARD CANCELS THE
CMR STATUS AND REQUIRES ACCOMPLISHMENT OF TASK
282800-05-2.
THAT FOR A321 POST 28653, FQIC 6 IS PERMITTED ONLY
WITH ONE ACT REMOVED.
IF NO ACT(S) ARE FITTED WHEN THE TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE.
CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF THE TASK AT
THIS OPPORTUNITY.
APPENDIX A
AEG/AMP/A320 Page 39 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 282800-05-2 210 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/13 282800-710-001 180 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM 22500 FH
NOTE
NOTE:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
- TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE.
CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF THE TASK
AT THIS OPPORTUNITY
- CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF TASK
282800-05-1 (CMR** REQUIREMENT FOR A321 A/C WITH
FQIC 6 STANDARD, WHICH MAY BE INCLUDED IN THE
APPLICABILITY OF THIS TASK).
2-28 282800-06-1 150 DIS ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/06 282839-920-001 108 MO N/A
MRB 6 OR
REPLACE ACT AIR INLET FILTER 15000 FH
NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-07-1 150 FNC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/07 282800-720-001 180 MO N/A
MRB 9 OR
FUNCTIONAL CHECK OF ACT PRESSURE REDUCING VALVE 22500 FH
NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-08-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 9 MRB 28.28.00/08 282800-720-002 72 ACT MO N/A
NOTE
OPERATIONAL CHECK OF ACT(S) INWARD RELIEF VALVE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
- ACT SERIAL NUMBER TO BE TRACKED SINCE TASK
ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT
AIRCRAFT AGE.
2-28 282800-09-1 150 GVI ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/09 282800-200-002 6 MO N/A
MRB 8 OR
GENERAL VISUAL INSPECTION OF THE INTEGRATED IMPACT 750 FH
WALL(S) (IF INSTALLED)
2-28 282800-18-1 150 FNC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/12 282800-790-004 60 MO N/A
NOTE
FUNCTIONAL CHECK OF THE VENT/TRANSFER PIPE SHROUDS
AND ACT DRAIN PIPE CONNECTORS
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-18-2 150 FNC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF CMR* CMR 282800-00002-1-C 282800-790-004 60 MO N/A
MRB 8 MRB 28.28.00/12 OR
FUNCTIONAL CHECK OF THE VENT/TRANSFER PIPE SHROUDS 10700 FH
AND ACT DRAIN PIPE CONNECTORS NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
APPENDIX A
AEG/AMP/A320 Page 40 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 282800-20-1 120 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/20 282800-740-801 12 MO N/A
MRB 9 OR
READ CFDIU DISPLAY FOR FAULTS 1000 FH
NOTE
NOTE:
INTERVAL:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-21-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/19 282800-710-802 60 MO N/A
NOTE
OPERATIONAL CHECK OF ACT FWD (4.1) OVERPRESSURE
PROTECTOR
NOTE:
INTERVAL:
- IF ACT NO 4 IS NOT FITTED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL NEXT ACT NO 4
INSTALLATION.
2-28 282800-55-1 210 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/13 282800-710-007 180 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF THE ACT MANUAL TRANSFER SYSTEM 22500 FH
NOTE
NOTE:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
- TASK IS INCLUDED IN THE ACT INSTALLATION PROCEDURE.
CREDIT CAN BE TAKEN FOR ACCOMPLISHMENT OF THE TASK
AT THIS OPPORTUNITY.
2-28 282800-58-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 9 MRB 28.28.00/08 282800-710-009 72 ACT MO N/A
NOTE
OPERATIONAL CHECK OF ACT(S) INWARD RELIEF VALVE
NOTE:
- IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
- ACT SERIAL NUMBER TO BE TRACKED SINCE TASK
ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT
AIRCRAFT AGE.
2-28 282800-59-1 150 GVI ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/09 282800-200-006 6 MO N/A
MRB 8 OR
GENERAL VISUAL INSPECTION OF THE INTEGRATED IMPACT 750 FH
WALL(S) (IF INSTALLED)
2-28 282800-60-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF LUR MRB 28.28.00/18 282500-710-004 6 MO N/A
MRB 9 OR
READ AFMS FAULT DISPLAY ON REFUEL/DEFUEL CONTROL 750 FH
PANEL FOR FAULTS NOTE
NOTE:
IF NO ACT(S) ARE FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT INSTALLATION.
2-28 282800-61-1 148 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/14 282800-710-015 60 MO N/A
REMOVE AND CARRY OUT OPERATIONAL CHECK OF VENT LINE
CHECK VALVES
2-28 282800-62-1 130 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/15 282800-710-010 60 MO N/A
NOTE
OPERATIONAL CHECK OF FORWARD ACT VENT ISOLATION VALVE
NOTE:
INTERVAL:
- IF ACT NO 4 IS NOT FITTED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL NEXT ACT NO 4
INSTALLATION.
APPENDIX A
AEG/AMP/A320 Page 41 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-28 282800-63-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/16 282800-710-011 60 MO N/A
NOTE
OPERATIONAL CHECK OF ACT 4 OVERPRESSURE PROTECTOR
NOTE:
IF ACT NO 4 IS NOT FITTED WHEN TASK BECOMES DUE, TASK
MAY BE POSTPONED UNTIL NEXT ACT NO 4 INSTALLATION.
2-28 282800-64-1 150 OPC ADDITIONAL CENTER TANK TRANSFER SYSTEM AF MRB 8 MRB 28.28.00/17 282800-710-012 60 MO N/A
NOTE
OPERATIONAL CHECK OF FORWARD ACT ISOLATION VALVE
NOTE:
INTERVAL:
- IF ACT NO 4 IS NOT FITTED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL NEXT ACT NO 4
INSTALLATION.
3-28 282801-01-1 151 DET ACT EXTERNAL SURFACE AF MRB CPCP MRB 282801-01-1 282800-200-004 6 ACT YE 6 ACT YE N/A
152
DETAILED INSPECTION OF ADDITIONAL CENTER TANK (ACT),
EXTERNAL SURFACE
NOTE:
ACT SERIAL NUMBER TO BE TRACKED SINCE TASK
ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT OF
AIRCRAFT AGE
3-28 282802-01-1 151 DET ACT INTERNAL STRUCTURE AF MRB CPCP MRB 282802-01-1 282800-200-005 12 ACT YE 12 ACT YE N/A
152
DETAILED INSPECTION OF ADDITIONAL CENTER TANK (ACT),
INTERNAL STRUCTURE
NOTE:
ACT SERIAL NUMBER TO BE TRACKED, SINCE TASK
ACCOMPLISHMENT IS A FUNCTION OF ACT AGE AND NOT OF
AIRCRAFT AGE
3-28 282803-01-1 151 SDI ACT EXTERNAL SURFACE NDT MRB MRB 282803-01-1 282800-200-008 32000 ACT 13300 ACT N/A
152 FC FC
SPECIAL DETAILED INSPECTION (HFEC) OF ADDITIONAL
CENTER TANK (ACT), EXTERNAL SURFACE, IN AREA OF
TANKPLATE PROFILES
NOTE:
ACT SERIAL NUMBER TO BE TRACKED, SINCE TASK
ACCOMPLISHMENT IS A FUNCTION OF ACT USAGE PARAMETER
(ACT FC) AND NOT OF AIRCRAFT USAGE PARAMETER
2-28 282900-02-1 210 OPC APU LOW PRESSURE FUEL SHUT OFF AF LUR MRB 28.29.00/02 282900-710-002 252 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF APU LP FUEL VALVE FOR EVIDENCE 36000 FH
OF INTERNAL LEAKAGE WITH LEFT WING TANK PUMP ON
2-28 284200-01-1 210 OPC QUANTITY INDICATING AF CMR* CMR 284200-00001-1-C 284200-710-802 31600 FH N/A
OPERATIONAL CHECK OF FUEL TEMPERATURE INDICATIONS.
2-29 290000-01-1 100 VCK HYDRAULIC POWER AF LUR MRB 29.10.00/06 291000-200-004 12 MO N/A
MRB 9 OR
CHECK CLOGGING INDICATORS OF THE FOLLOWING FILTERS ( 1000 FH
POP OUT NOT PROTRUDING )
- HIGH PRESSURE DELIVERY
- GROUND SERVICING ( RESERVOIR FILLING )
- RETURN ( LOW PRESSURE )
- BLUE HYD SYS ELECTRICAL PUMP CASE DRAIN
- HIGH PRESSURE BLEED AIR
- LOW PRESSURE BLEED AIR
2-29 290000-02-1 435 VCK HYDRAULIC POWER AF LUR MRB 29.10.00/06 291000-200-007 12 MO N/A
445 MRB 9 MRB 29.10.00/28 OR
CHECK CLOGGING INDICATOR ON ENGINE DRIVEN PUMP (EDP) 1000 FH
CASE DRAIN FILTER ( POP OUT NOT PROTRUDING )
APPENDIX A
AEG/AMP/A320 Page 42 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-29 290000-03-1 435 VCK HYDRAULIC POWER AF LUR MRB 29.10.00/06 291000-200-006 12 MO APPL
445 MRB 9 MRB 29.10.00/28 OR
CHECK CLOGGING INDICATOR ON ENGINE DRIVEN PUMP (EDP) 1000 FH
CASE DRAIN FILTER ( POP OUT NOT PROTRUDING )
2-29 290000-04-1 435 DET HYDRAULIC POWER AF VSB 291000-200-009 600 FH 2400 FH N/A
445 VSB RA320 029-9
DETAILED INSPECTION OF HYDRAULIC PRESSURE SWITCH
LINE (P/N 642-5658-501/505) FOR CLAMP CHAFING DAMAGE
AND PRELOAD CONDITION
2-29 290000-05-1 100 VCK HYDRAULIC POWER AF LUR MRB 29.10.00/28 291000-210-002 24 MO APPL
MRB 9 OR
CHECK CLOGGING INDICATORS OF THE FOLLOWING 2000 FH
FILTERS(POP OUT NOT PROTRUDING) -HIGH PRESSURE
DELIVERY -GROUND SERVICING (RESERVOIR FILLING)
-RETURN (LOW PRESSURE) -BLUE HYDRAULIC SYSTEM
ELECTRICAL PUMP CASE DRAIN -RESERVOIR PRESSURIZATION
FILTER -WATER SEPARATOR
2-29 291000-01-1 100 DET MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/01 291000-200-001 6 MO APPL
MRB 6 OR
CHECK FLUID LEVEL ON RESERVOIR INDICATORS 750 FH
2-29 291000-02-1 100 DET MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/02 291000-200-002 6 MO APPL
MRB 6 OR
CHECK RESERVOIR AIR PRESSURE ON RESERVOIR GAUGE 750 FH
2-29 291000-03-1 100 FNC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/03 291000-200-003 6 MO N/A
MRB 9 OR
CHECK NITROGEN CHARGE PRESSURE ON THE YELLOW AND 400 FH
GREEN MAIN SYSTEM ACCUMULATORS.
2-29 291000-04-1 210 FNC MAIN HYDRAULIC POWER AF MRB 6 MRB 29.10.00/38 292300-710-002 72 MO APPL
OR
FUNCTIONAL CHECK OF PTU GREEN TO YELLOW 24000 FH
2-29 291000-05-1 195 SVC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/13 291400-680-001 24 MO APPL
MRB 9 OR
DRAIN WATER SEPARATOR 2250 FH
2-29 291000-06-1 210 FNC MAIN HYDRAULIC POWER AF MRB 6 MRB 29.10.00/37 292300-710-003 36 MO APPL
OR
FUNCTIONAL CHECK OF PTU YELLOW TO GREEN 12000 FH
2-29 291000-08-1 210 FNC MAIN HYDRAULIC POWER AF MRB 6,8 MRB 29.10.00/19 291000-720-002 144 MO APPL
OR
FUNCTIONAL CHECK OF PRIORITY VALVES IN GREEN, BLUE 36000 FH
AND YELLOW SYSTEM
2-29 291000-09-1 574 OPC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/14 291000-710-001 108 MO APPL
674 MRB 8 OR
OPERATIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVES 12000 FH
AND ASSOCIATED INDICATING SYSTEM.
NOTE:
APPLICABLE FOR PRE 22155 IF ACTUATOR P/N E0 1100
AMENDMENT A, OR P/N E0 1100 AMENDMENT AB, OR P/N E0
1100 AMENDMENT AC, OR P/N E0 1100 AMENDMENT BC, OR
P/N E0 1100 AMENDMENT C, OR P/N A06 A00 IS INSTALLED
2-29 291000-10-1 210 FNC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/20 291000-720-001 180 MO APPL
MRB 8 OR
FUNCTIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVES 24000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED
2-29 291000-13-1 100 SVC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/25 291400-680-002 6 MO N/A
MRB 6 OR
DRAIN FILTER BOWLS OF THE AIR PRESSURIZATION MANIFOLD 500 FH
VIA DRAIN VALVES
2-29 291000-14-1 100 FNC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/22 291000-200-008 6 MO APPL
MRB 9 OR
CHECK NITROGEN CHARGE PRESSURE ON HYDRAULIC POWER 600 FH
ACCUMULATORS
APPENDIX A
AEG/AMP/A320 Page 43 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-29 291000-15-1 100 DET MAIN HYDRAULIC POWER AF MRB 9 MRB 29.10.00/23 123229-281-001 24 MO APPL
OR
ANALYZE HYDRAULIC FLUID 7500 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-29 291000-16-1 100 SVC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/24 291400-680-003 6 MO N/A
MRB 6 OR
DRAIN FILTER BOWLS OF THE AIR PRESSURIZATION MANIFOLD 500 FH
2-29 291000-18-1 148 SVC MAIN HYDRAULIC POWER AF LUR MRB 29.10.00/32 291700-680-001 12 MO APPL
MRB 9 OR
DRAIN RECOVERY TANK 1500 FH
2-29 291000-19-1 210 OPC MAIN/AUXILIARY POWER EL LUR MRB 29.10.00/35 292300-710-006 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF PTU IN-FLIGHT INHIBITION LOGIC 15000 FH
2-29 291000-20-1 210 OPC MAIN/AUXILIARY POWER AF MRB 9 MRB 29.10.00/36 291000-710-004 36 MO APPL
OR
OPERATIONAL CHECK OF EDP DEPESSURIZATION 12000 FH
2-29 291000-21-1 210 OPC MAIN/AUXILIARY POWER AF LUR MRB 29.10.00/39 292300-710-803 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF PTU THERMAL INHIBITION LOGIC 15000 FH
2-29 291000-22-1 210 FNC MAIN/AUXILIARY POWER AF LUR MRB 29.10.00/40 291000-720-802 108 MO N/A
MRB 8 OR
FUNCTIONAL CHECK OF HYDRAULIC FIRE SHUT OFF VALVES 16000 FH
NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED.
2-29 291200-03-1 100 FNC BLUE MAIN HYDRAULIC POWER AF CMR** CMR 291000-00004-1-C 291000-200-005 6 MO N/A
LUR MRB 29.10.00/04 OR
CHECK NITROGEN CHARGE PRESSURE ON THE BLUE MAIN MRB 9 400 FH
SYSTEM ACCUMULATOR.
291900-01-1 ************** TASK DELETED ************** N/A
2-29 291900-02-1 210 FNC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00003-1-C 291000-220-002 108 MO APPL
LUR MRB 29.10.00/05 OR
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF MRB 8 MRB 29.10.00/12 12000 FH
BLUE HYDRAULIC SYSTEM
2-29 292000-01-1 190 FNC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00001-1-C 292200-720-001 8 MO N/A
MRB 8 MRB 24.50.00/03 OR
OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND MRB 29.10.00/07 1500 FH
FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT,
FOLLOWED BY CHECK OF FILTER INDICATOR
2-29 292000-02-1 210 OPC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00002-1-C 292200-710-001 18 MO N/A
MRB 8 MRB 29.10.00/08 OR
OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC 3600 FH
DEPLOYMENT
2-29 292000-04-1 190 FNC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00001-2-C 292200-720-003 18 MO APPL
MRB 8 MRB 24.50.00/10 OR
OPERATIONAL CHECK OF RAT MANUAL DEPLOYMENT AND MRB 29.10.00/29 3600 FH
FUNCTIONAL CHECK OF RAT USING GROUND TEST UNIT,
FOLLOWED BY CHECK OF FILTER INDICATOR
2-29 292000-05-1 210 OPC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00002-1-C 292200-710-006 18 MO APPL
MRB 8 MRB 29.10.00/08 OR
OPERATIONAL CHECK OF RAM AIR TURBINE (RAT) AUTOMATIC 3600 FH
DEPLOYMENT
2-29 292000-06-1 190 FNC MAIN AND AUXILIARY HYDRAULIC POWER AF CMR** CMR 291000-00005-1-C 292200-920-002 144 MO YES N/A
MRB 8 MRB 29.10.00/26 OR
REMOVE RAM AIR TURBINE AGCM AND PUMP FOR IN SHOP 24000 FH
FUNCTIONAL CHECK.
2-29 292000-07-1 190 FNC MAIN AND AUXILIARY HYDRAULIC POWER AF MRB 8 MRB 29.10.00/27 292200-280-002 108 MO APPL
FUNCTIONAL CHECK OF ANTI-ICING DEVICE MAGNETS
APPENDIX A
AEG/AMP/A320 Page 44 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-29 292000-09-1 190 DET MAIN AND AUXILIARY HYDRAULIC POWER AF CMR* CMR 291000-00006-1-C 292200-220-002 18 MO N/A
MRB 8 MRB 29.10.00/34 OR
DETAILED INSPECTION OF RAT CARBON BLADES FOR EVIDENCE 3600 FH
OF PLATING CRACKS
2-29 292000-11-1 195 RST MAIN AND AUXILIARY HYDRAULIC POWER AF SEMR SEMR 292200-00001-1-E 292200-960-001 240 MO 240 MO YES APPL
REMOVE RAT AND ACTUATOR FOR OVERHAUL AND REPLACE WITH
NEW OR RECONDITIONED UNITS.
2-29 292000-12-1 195 RST MAIN AND AUXILIARY HYDRAULIC POWER AF SEMR SEMR 292200-00002-1-E 292200-960-002 240 MO 240 MO YES N/A
REMOVE RAT (INCLUDING TURBINE, LEG AND PUMP),
EJECTION JACK AND AGCM FOR OVERHAUL AND REPLACE WITH
NEW OR RECONDITIONED UNITS.
2-29 292251-01-1 195 DET RAM AIR TURBINE AF MRB 8 MRB 29.10.00/33 292251-210-001 16 MO N/A
DETAILED INSPECTION OF RAT ASSEMBLY AND DOORS IN
DEPLOYED POSITION AND LUBRICATION OF DOORS LINKAGE
STRUT JOINTS, BEARINGS AND SWIVEL PIN.
2-29 292251-02-1 195 DET RAM AIR TURBINE AF MRB 8 MRB 29.10.00/09 292251-200-003 20 MO APPL
DETAILED INSPECTION OF RAT ASSEMBLY AND DOORS IN
DEPLOYED POSITION AND LUBRICATION OF DOORS LINKAGE
STRUT JOINTS AND BEARINGS.
2-29 293100-01-1 190 FNC HYDRAULIC FLUID QUANTITY INDICATING AF LUR MRB 29.30.00/05 293100-710-001 252 MO APPL
MRB 9 OR
FUNCTIONAL CHECK OF RESERVOIR LOW LEVEL WARNING 36000 FH
2-29 293400-01-1 210 OPC RESERVOIR PRESSURIZATION INDICATING AF LUR MRB 29.30.00/04 293400-710-001 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF RESERVOIR LOW AIR PRESSURE 12000 FH
WARNING
2-30 301151-01-1 522 DIS WING ANTI-ICE CONTROL VALVE AF MRB 6 MRB 30.11.00/02 301151-960-001 5500 FH N/A
622
REPLACE WING ANTI-ICING FILTER
2-30 301151-01-2 522 DIS WING ANTI-ICE CONTROL VALVE AF LUR MRB 30.11.00/03 301151-960-001 180 MO N/A
622 MRB 6 OR
REPLACE WING ANTI-ICING FILTER 24000 FH
2-30 301151-02-1 522 RST WING ANTI-ICE CONTROL VALVE AF LUR MRB 30.11.00/04 301151-960-802 180 MO YES APPL
622 MRB 6 OR
REMOVE WING ANTI-ICING FILTER FOR IN SHOP CLEANING 24000 FH
2-30 302100-02-1 210 OPC ENGINE AIR INTAKE ICE PROTECTION EL CMP CMP 30-2-0000-001 302100-710-002 72 MO N/A
OPERATIONAL CHECK OF ENGINE AIR INTAKE ICE PROTECTION
SYSTEM.
302100-C1-1 ************** TASK DELETED ************** N/A
302100-I1-1 ************** TASK DELETED ************** N/A
2-30 302100-I3-1 437 DET ENGINE AIR INTAKE ICE PROTECTION AF LUR MRB 30.21.00/03-I2 302149-200-804 108 MO APPL
438 MRB 8 OR
447 DETAILED INSPECTION OF THE ENGINE ANTI-ICE SUPPLY 12000 FH
448 DUCTS METALLIC FIRE SEAL.
302100-P1-1 ************** TASK DELETED ************** N/A
2-30 302100-P6-1 433 DET ENGINE AIR INTAKE ICE PROTECTION AF LUR MRB 30.21.00/03-P6 302149-220-803 108 MO N/A
443 MRB 9 OR
DETAILED INSPECTION OF INLET COWL PRESSURE RELIEF 12000 FH
DOOR MECHANISM.
2-30 302149-03-1 438 DET ENGINE AIR INTAKE PROTECTION DUCTS AF CMP CMP 30-2-0000-002 302149-220-801 15000 FH N/A
448
DETAILED INSPECTION OF ENGINE AIR INTAKE PROTECTION
DUCTS.
2-30 302149-04-1 438 DET ENGINE AIR INTAKE ICE PROTECTION SWIRL NOZZLE AF CMP CMP 30-2-0000-003 716100-220-802 15000 FH N/A
448
DETAILED INSPECTION OF ENGINE AIR INTAKE ICE
PROTECTION SWIRL NOZZLE.
2-30 302149-05-1 438 DET ENGINE AIR INTAKE ICE PROTECTION DUCTS, NOZZLES AND AF CMP CMP 30-2-0000-004 302149-200-803 15000 FH N/A
448 INJECTOR
DETAILED INSPECTION OF ENGINE AIR INTAKE ICE
PROTECTION DUCTS, NOZZLES AND INJECTORS.
APPENDIX A
AEG/AMP/A320 Page 45 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-30 302149-06-1 438 VCK ENGINE ANTI ICING DUCTS AF CMP CMP 30-2-0000-005 302149-200-803 15000 FH N/A
448
VISUAL CHECK OF ENGINE ANTI ICING DUCTS.
2-30 302149-C1-1 438 DET ENGINE AIR INTAKE ICE PROTECTION AF LUR MRB 30.21.00/01-C5 302149-200-001 108 MO N/A
448 MRB 6 OR
DETAILED INSPECTION OF INLET COWL ANTI-ICE SUPPLY 12000 FH
DUCTS AND ASSOCIATED HARDWARE IN THE CORE AND FAN
COMPARTMENTS.
2-30 302149-I2-1 437 DET ENGINE AIR INTAKE ICE PROTECTION AF LUR MRB 30.21.00/01-I2 302149-200-010 72 MO APPL
438 MRB 9 OR
447 DETAILED INSPECTION OF THE VISIBLE PART OF INLET COWL 6000 FH
448 ANTI-ICE SUPPLY DUCTS AND ASSOCIATED HARDWARE IN THE
451 CORE AND FAN CASE COMPARTMENTS.
452
461
462
2-30 302149-P3-1 433 DET ENGINE AIR INTAKE ICE PROTECTION AF LUR MRB 30.21.00/01-P6 302149-200-802 108 MO N/A
443 MRB 9 OR
DETAILED INSPECTION OF NOSE COWL ANTI-ICE DUCT AND 12000 FH
ASSOCIATED HARDWARE IN U-TUNNEL.
2-30 303100-01-1 120 FNC PROBE ICE PROTECTION EL MRB 9 MRB 30.31.00/02 303100-720-001 24 MO APPL
FUNCTIONAL CHECK OF THE INSULATION RESISTANCE OF THE
PITOT PROBE HEATER
2-31 312100-01-1 210 DIS CLOCK BATTERY EL MRB 9 MRB 31.21.00/01 312121-920-002 24 MO YES N/A
REMOVE CLOCK AND DISCARD BATTERY
2-31 313000-01-1 210 OPC CFDS AND DATA RECORDING SYSTEM AV LUR MRB 21.21.00/01 313200-869-002 6 MO APPL
MRB 9 MRB 21.26.00/01 OR
READ CENTRALIZED FAULT DISPLAY SYSTEM (CFDS) FOR MRB 21.28.00/01 750 FH
CLASS 3 FAULTS MRB 21.31.00/01
MRB 21.50.00/01
MRB 24.20.00/04
MRB 24.40.00/01
MRB 26.12.00/02
MRB 26.13.00/02
MRB 27.50.00/01
MRB 27.50.01/01
MRB 27.80.00/01
MRB 28.15.00/01
MRB 28.28.00/10
MRB 28.42.00/01
MRB 28.46.00/01
MRB 29.30.00/03
MRB 30.31.00/01
MRB 30.42.00/01
MRB 31.33.00/09
MRB 32.40.00/04
MRB 36.11.00/01
MRB 49.40.00/01-13
MRB 49.40.00/01-32
MRB 49.40.00/01-36
MRB 49.51.20/01-36
MRB 49.61.00/01-36
2-31 313300-01-1 312 DIS DFDR SYSTEM INTERCONNECTION AV MRB 9 MRB
MRB49.70.00/01-32
31.33.00/02 313355-920-001 NOTE YES APPL
NOTE
DISCARD UNDERWATER LOCATOR BEACON BATTERY
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-31 313300-03-1 312 OPC DFDR SYSTEM INTERCONNECTION AV MRB 9 MRB 31.33.00/04 313300-710-015 36 MO APPL
OPERATIONAL CHECK OF ULB
2-31 313300-06-1 121 OPC DFDR SYSTEM INTERCONNECTION AV LUR MRB 31.33.00/06 313600-710-021 180 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF WGL-DAR INTERLOCK LOGIC 24000 FH
APPENDIX A
AEG/AMP/A320 Page 46 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-31 313300-07-1 121 OPC DFDR SYSTEM INTERCONNECTION AV LUR MRB 31.33.00/07 313300-710-803 180 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF WGL-QAR INTERLOCK LOGIC 24000 FH
2-31 313300-08-1 312 OPC DFDR SYSTEM INTERCONNECTION AV MRB MRB 31.33.00/FAA 24 MO N/A
DOWNLOAD AND READOUT OF DFDR DATA TO ENSURE RECORDED
PARAMETERS MEET THE RANGE AND ACCURACIES REQUIRED BY
14 CFR PART 121, APPENDIX M.
2-31 313300-09-1 121 OPC DFDR SYSTEM INTERCONNECTION AV LUR MRB 31.33.00/08 313600-710-802 180 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF CELLULAR RADIO INTERLOCK LOGIC 24000 FH
2-31 315000-01-1 210 OPC CENTRAL WARNING SYSTEMS/ELECTRONIC INSTRUMENT SYSTEM AV LUR MRB 31.60.01/02 316000-740-005 108 MO N/A
(EIS) MRB 9 OR
15000 FH
OPERATIONAL CHECK OF CORRECT OPERATION OF PFD-ND AND
ECAM-ND MANUAL TRANSFER
2-31 315000-02-1 210 OPC CENTRAL WARNING SYSTEMS/ELECTRONIC INSTRUMENT SYSTEM AV LUR MRB 31.60.01/04 316000-710-005 108 MO N/A
(EIS) MRB 9 OR
15000 FH
OPERATIONAL CHECK OF CORRECT OPERATION OF EFIS AND
ECAM DMC AUTOMATIC AND MANUAL TRANSFER
2-31 315000-04-1 210 OPC CENTRAL WARNING SYSTEMS/ELECTRONIC INSTRUMENT SYSTEM AV LUR MRB 31.60.01/03 316000-710-006 108 MO N/A
(EIS) MRB 9 OR
15000 FH
OPERATIONAL CHECK OF DMC3 POWER SUPPLY TRANSFER WHEN
BUSBAR 101XP IS LOST
2-31 316000-01-1 210 OPC ELECTRONIC INSTRUMENT SYSTEM AV LUR MRB 31.50.00/01 316000-710-002 72 MO APPL
MRB 9 MRB 31.60.00/01 OR
OPERATIONAL CHECK OF EFIS/ECAM SWITCHING FUNCTIONS: 7500 FH
- MANUAL DMC 1 + 2 TO DMC 3 SWITCHING
- MANUAL PFD/ND TRANSFER
- MANUAL ECAM/ND TRANSFER
- AUTOMATIC UPPER DU/LOWER DU TRANSFER
- AUTOMATIC PFD/ND TRANSFER
2-32 321000-01-1 731 LUB MAIN LANDING GEAR AND DOORS AF MRB 5,8 MRB 32.11.00/02 122232-640-001 4 MO APPL
741 MRB 32.11.00/18 OR
LUBRICATION OF MAIN LANDING GEAR AND DOORS MRB 32.30.00/03 500 FC
2-32 321100-01-1 731 VCK MAIN LANDING GEAR AF MRB 9 MRB 32.11.00/01 321100-210-001 36 HR N/A
741
CHECK OF MLG BOGIE PITCH TRIMMER OVERBOARD DISCHARGE
INDICATOR
2-32 321100-02-1 731 FNC MAIN LANDING GEAR AF MRB 9 MRB 32.11.00/07 321141-720-002 90 MO N/A
741
FUNCTIONAL CHECK OF MLG HYDRAULIC FUSE IN BOGIE PITCH
TRIMMER SUPPLY LINE
NOTE:
MAY BE ACCOMPLISHED AT OPPORTUNITY OF GEAR REMOVAL
2-32 321100-15-1 731 SDI MAIN GEAR AF MRB 5,8 MRB 32.11.00/15 321100-220-006 20000 FC APPL
741
SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS
IN MLG AIRFRAME ATTACHMENT FITTINGS
NOTE:
MAY BE ACCOMPLISHED AT OPPORTUNITY OF LANDING GEAR
REMOVAL.
2-32 321100-16-1 731 GVI MAIN LANDING GEAR AF MRB 6,9 MRB 32.11.00/16 321100-210-007 36 HR N/A
741
GENERAL VISUAL INSPECTION OF MLG BOGIE PITCH TRIMMER
HIGH PRESSURE RELIEF VALVE AND HYDRAULIC FUSE ON
BOGIE ALIGNMENT MANIFOLD
3-32 321101-01-2 731 DET MAIN GEAR AF MRB CPCP MRB 321101-01-2 321100-200-008 6 YE 6 YE APPL
741
DETAILED INSPECTION OF MAIN LANDING GEAR, SLIDING
TUBE (TWIN WHEEL), BRAKE ATTACHMENT FLANGE, UPPER AND
LOWER TORQUE LINKS, UPPER AND LOWER TORQUE LINK PINS
AND APEX PIN & NUT - EXTERNAL SURFACES, EXCEPT WHERE
COVERED BY DRESSINGS AND BUSH FLANGES.
APPENDIX A
AEG/AMP/A320 Page 47 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-32 321103-01-1 731 DET MAIN GEAR AF MRB CPCP MRB 321103-01-1 321100-200-009 6 YE 6 YE APPL
741
DETAILED INSPECTION OF MAIN LANDING GEAR, MAIN
FITTING, FORWARD PINTLE PIN, FORWARD PINTLE PIN LOCK/
STUB BOLTS, REAR PINTLE PIN & NUT, RETRACTION
ACTUATOR ATTACHMENT PINS & UPPER DIAPHRAGM CROSS PIN
- EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS & BUSH FLANGES.
2-32 321111-01-2 731 SDI MAIN LANDING GEAR AF MRB 5,8 MRB 32.11.00/14 321111-920-001 120 MO YES APPL
741 MRB CPCP MRB 32.11.00/19 MPD APPENDIX 7 OR
REMOVE MAIN LANDING GEAR FOR SPECIAL DETAILED MRB 32.30.00/22 20000 FC
INSPECTION IN SHOP MRB 321105-03-1
MRB 321110-03-1
NOTE: MRB 321111-02-1
PLANNING: MRB 321116-02-1
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE MRB 321128-03-1
WITH RELEVANT CMM. MRB 321141-01-1
- FOR THE PURPOSE OF THIS TASK, MLG LRU'S ARE: MRB 321169-01-1
SIDESTAY, AND LEG AND DRESSING.
- INTERVAL CAN BE MANAGED SEPARATELY FOR LRU'S P/N
NON-10-XXXXXX (SUBJECT TO TASK 321111-01-2) AND
10-XXXXXX (SUBJECT TO TASK 321111-01-3).
2-32 321111-01-3 731 SDI MAIN LANDING GEAR AF MRB 5,8 MRB 32.11.00/14 321111-920-001 144 MO YES APPL
741 MRB CPCP MRB 32.11.00/19 MPD APPENDIX 7 OR
REMOVE MAIN LANDING GEAR FOR SPECIAL DETAILED MRB 32.30.00/22 20000 FC
INSPECTION IN SHOP MRB 321180-01-1
MRB 321181-01-1
NOTE: MRB 321182-01-1
PLANNING: MRB 321183-01-1
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE MRB 321185-01-1
WITH RELEVANT CMM.
- FOR THE PURPOSE OF THIS TASK, MLG LRU'S ARE:
SIDESTAY, AND LEG AND DRESSING.
- INTERVAL CAN BE MANAGED SEPARATELY FOR LRU'S P/N
NON-10-XXXXXX (SUBJECT TO TASK 321111-01-2) AND
10-XXXXXX (SUBJECT TO TASK 321111-01-3).
2-32 321111-03-1 731 FNC MAIN LANDING GEAR AF LUR MRB 32.11.00/13 321111-200-001 24 MO APPL
741 MRB 6,9 OR
FUNCTIONAL CHECK OF MLG TORQUE LINK DAMPER FLUID 1500 FC
LEVEL
3-32 321111-07-1 731 SDI MAIN LANDING GEAR, SIDE STAY AF MRB CPCP MRB 321111-03-2 321100-220-012 8 YE 8 YE YES N/A
741 MPD APPENDIX 7
SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR,
SIDE STAY CARDANS COMPRISING:
- UPPER CARDAN
- LOWER CARDAN
- UPPER CARDAN NUT
- LOWER CARDAN NUT
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
2-32 321113-03-1 731 FNC MAIN LANDING GEAR SHOCK ABSORBER AF MRB 6 MRB 32.11.00/04 121232-611-004 80 MO APPL
741 OR
FUNCTIONAL CHECK OF MLG SHOCK ABSORBER FLUID LEVEL 16000 FC
2-32 321113-04-1 731 FNC MAIN LANDING GEAR SHOCK ABSORBER AF MRB 6 MRB 32.11.00/03 121432-614-003 36 MO APPL
741 OR
FUNCTIONAL CHECK OF MLG SHOCK ABSORBER CHARGE 8000 FC
PRESSURE
2-32 321127-01-1 731 DET MAIN LANDING GEAR TORQUE LINK AF MRB 6 MRB 32.11.00/05 321127-200-001 16000 FC APPL
741
FUNCTIONAL CHECK OF MLG TORQUE LINKS FOR EXCESSIVE
PLAY
3-32 321138-01-1 731 DET MAIN GEAR AF MRB CPCP MRB 321138-01-1 321100-200-012 6 YE 6 YE N/A
741
DETAILED INSPECTION OF MAIN LANDING GEAR, BOGIE BEAM-
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
APPENDIX A
AEG/AMP/A320 Page 48 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-32 321139-01-1 731 DET MAIN GEAR AF MRB CPCP MRB 321139-01-1 321100-200-013 6 YE 6 YE N/A
741
DETAILED INSPECTION OF MAIN LANDING GEAR, SLIDING
TUBE (BOGIE) - EXTERNAL SURFACES, EXCEPT WHERE
COVERED BY DRESSINGS AND BUSH FLANGES.
3-32 321141-01-2 731 SDI MAIN LANDING GEAR COMPONENTS AF MRB CPCP MRB 321141-01-2 321100-220-013 8 YE 8 YE YES N/A
741 MPD APPENDIX 7
SPECIAL DETAILED INSPECTION OF MAIN LANDING GEAR,
MAIN FITTING COMPRISING:
- MAIN FITTING
- UPPER DIAPHRAGM TUBE
- SLIDING TUBE
- LOWER BEARING HOUSING (TWIN WHEEL)
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
3-32 321146-01-1 731 DET MAIN LANDING GEAR PARTS AF MRB CPCP MRB 321146-01-1 321100-200-018 6 YE 6 YE APPL
741
DETAILED INSPECTION OF MAIN LANDING GEAR, RETRACTION
ACTUATOR - EXTERNAL SURFACE, EXCEPT WHERE COVERED BY
DRESSINGS & BUSH FLANGES.
3-32 321156-01-1 731 DET MAIN LANDING GEAR PARTS AF MRB CPCP MRB 321156-01-1 321100-200-019 6 YE 6 YE N/A
741
DETAILED INSPECTION OF MAIN LANDING GEAR, UPPER &
LOWER SIDESTAY, UPPER & LOWER CARDANS AND NUTS, UPPER
& LOWER LOCK LINKS, LOCKSTAY CARDAN, LOCKSTAY CARDAN
BRACKET & BOLTS, CUFF, TRIANGULATION LINK, BANANA
LINKS, UPPER & LOWER CARDAN PINS, SIDESTAY PIVOT PIN,
UPPER PIN (SPRINGS), LOCKSTAY CARDAN PIN, UPPER &
LOWER LOCK LINK PINS, LOCK LINK CENTER PIN,
TRIANGULATION LINK PINS, LOCK LINK/BANANA LINK PIN,
CUFF PINS & LOWER (SPRINGS) PIN - EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS, BUSH FLANGES &
FITTINGS.
3-32 321156-01-2 731 DET MAIN LANDING GEAR PARTS AF MRB CPCP MRB 321156-01-2 321100-200-019 6 YE 6 YE APPL
741
DETAILED INSPECTION OF MAIN LANDING GEAR, UPPER &
LOWER SIDESTAY, UPPER & LOWER CARDANS AND NUTS, UPPER
& LOWER LOCK LINKS, LOCKSTAY CARDAN, CUFF,
TRIANGULATION LINK, BANANA LINKS, UPPER & LOWER
CARDAN PINS, SIDESTAY PIVOT PIN, UPPER PIN (SPRINGS),
LOCKSTAY CARDAN PIN, UPPER & LOWER LOCK LINK PINS,
LOCK LINK CENTER PIN, TRIANGULATION LINK PINS, LOCK
LINK/BANANA LINK PIN, CUFF PINS & LOWER (SPRINGS) PIN
- EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS, BUSH FLANGES & FITTINGS.
3-32 321163-02-1 731 DET MAIN LANDING GEAR PARTS AF MRB CPCP MRB 321163-02-1 321100-200-021 6 YE 6 YE N/A
741
DETAILED INSPECTION OF MAIN LANDING GEAR, PIVOT PINS
AND BRAKE ROD PINS (BOGIE) - EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES.
3-32 321166-01-1 731 DET MAIN LANDING GEAR PARTS AF MRB CPCP MRB 321166-01-1 321100-200-022 6 YE 6 YE N/A
741
DETAILED INSPECTION OF MAIN LANDING GEAR, BRAKE RODS
(BOGIE) - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS AND BUSH FLANGES.
2-32 322000-01-1 710 LUB NOSE LANDING GEAR AND DOORS AF MRB 5,8 MRB 32.21.00/01 122232-640-002 4 MO APPL
MRB 32.30.00/03 OR
LUBRICATION OF NOSE LANDING GEAR AND DOORS MRB 32.50.00/01 500 FC
2-32 322100-07-1 710 SDI NOSE GEAR AF MRB 5,8 MRB 32.21.00/07 322100-200-016 20000 FC APPL
SPECIAL DETAILED INSPECTION OF BUSHINGS AND BEARINGS
IN NLG AIRFRAME ATTACHMENT FITTINGS.
NOTE:
MAY BE ACCOMPLISHED AT OPPORTUNITY OF LANDING GEAR
REMOVAL.
APPENDIX A
AEG/AMP/A320 Page 49 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-32 322111-01-1 710 SDI NOSE LANDING GEAR AF MRB 5,8 MRB 32.21.00/05 322100-200-802 120 MO YES APPL
MRB CPCP MRB 32.30.00/23 MPD APPENDIX 7 OR
REMOVE NOSE LANDING GEAR FOR SPECIAL DETAILED MRB 32.50.00/02 20000 FC
INSPECTION IN SHOP MRB 322105-03-1
MRB 322110-03-1
NOTE:
PLANNING:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
- FOR THE PURPOSE OF THIS TASK, NLG LRU'S ARE:
DRAGSTAY, AND LEG AND DRESSING.
- INTERVAL CAN BE MANAGED SEPARATELY FOR LRU'S P/N
NON-10-XXXXXX (SUBJECT TO TASK 322111-01-1) AND
10-XXXXXX (SUBJECT TO TASK 322111-01-2).
2-32 322111-01-2 710 SDI NOSE LANDING GEAR AF MRB 5,8 MRB 32.21.00/05 322100-200-802 144 MO YES N/A
MRB CPCP MRB 32.30.00/23 MPD APPENDIX 7 OR
REMOVE NOSE LANDING GEAR FOR SPECIAL DETAILED MRB 32.50.00/02 20000 FC
INSPECTION IN SHOP MRB 322180-01-1
MRB 322181-01-1
NOTE:
PLANNING:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
- FOR THE PURPOSE OF THIS TASK, NLG LRU'S ARE:
DRAGSTAY, AND LEG AND DRESSING.
- INTERVAL CAN BE MANAGED SEPARATELY FOR LRU'S P/N
NON-10-XXXXXX (SUBJECT TO TASK 322111-01-1) AND
10-XXXXXX (SUBJECT TO TASK 322111-01-2).
2-32 322113-01-1 711 FNC NOSE LANDING GEAR SHOCK ABSORBER AF MRB 6 MRB 32.21.00/03 121232-610-002 24 MO APPL
OR
FUNCTIONAL CHECK OF NLG SHOCK ABSORBER CHARGE 5000 FC
PRESSURE AND FLUID LEVEL.
2-32 322127-01-1 711 FNC NOSE LANDING GEAR TORQUE LINK AF MRB 6 MRB 32.21.00/02 322100-200-003 5000 FC APPL
FUNCTIONAL CHECK OF NLG TORQUE LINKS FOR EXCESSIVE
PLAY
3-32 322141-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322141-01-1 322100-200-018 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, BARREL,
SLIDING TUBE AND TURNING TUBE EXTERNAL SURFACES,
EXCEPT WHERE COVERED BY DRESSINGS AND BUSH FLANGES.
3-32 322142-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322142-01-1 322100-200-013 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, TORQUE
LINKS - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS AND BUSH FLANGES.
3-32 322143-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322143-01-1 322100-200-014 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, FORESTAY
UPPER PANEL, LOWER LINK AND UNIVERSAL JOINT -
EXTERNAL SURFACES, EXCEPT WHERE COVERED BY DRESSINGS
AND BUSH FLANGES.
3-32 322144-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322144-01-1 322100-200-012 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, LOCK LINK
UPPER AND LOCK LINK LOWER - EXTERNAL SURFACES, EXCEPT
WHERE COVERED BY DRESSINGS AND BUSH FLANGES.
3-32 322145-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322145-01-1 322100-200-009 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, UPPER
BARREL HINGE PINS, FORESTAY BARREL PIN, ACTUATING
CYLINDER PINS, RETAINING NUT SHOCK ASSY, TORQUE LINK
PINS, TORQUE LINK APEX PIN AND NUT, UPPER PANEL TO
STRUCTURE PINS, UPPER PANEL TO UNIVERSAL JOINT PIN,
LOCK LINK CENTRE PIN, LOWER LOCK LINK PIN, LOWER LOCK
LINK TO UNIVERSAL JOINT PIN AND CROSS PIN - EXTERNAL
SURFACES, EXCEPT WHERE COVERED BY DRESSINGS AND BUSH
FLANGES.
APPENDIX A
AEG/AMP/A320 Page 50 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-32 322151-01-1 711 DET NOSE LANDING GEAR PARTS AF MRB CPCP MRB 322151-01-1 322100-200-015 6 YE 6 YE APPL
DETAILED INSPECTION OF NOSE LANDING GEAR, ACTUATING
CYLINDER - EXTERNAL SURFACES, EXCEPT WHERE COVERED BY
DRESSINGS AND BUSH FLANGES.
2-32 323000-01-1 711 VCK NORMAL EXTENSION AND RETRACTION AF MRB 8 MRB 32.30.00/01 323000-200-002 4 MO APPL
731 OR
741 VISUAL CHECK OF NLG AND MLG DOWNLOCK SPRINGS AND 750 FH
ATTACHMENTS.
2-32 323000-16-1 711 SDI NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.30.00/16 528100-220-002 20000 FC APPL
731 MRB 32.30.00/18
741 SPECIAL DETAILED INSPECTION OF MLG AND NLG DOOR HINGE
BEARINGS, ATTACHMENT LUG BUSHINGS AND PINS AND DOOR
ACTUATING CYLINDERS ATTACHMENT LUG BUSHINGS AND PINS.
2-32 323000-17-1 210 FNC NORMAL EXTENSION AND RETRACTION AV LUR MRB 32.30.00/17 323100-720-008 36 MO APPL
MRB 8 OR
FUNCTIONAL CHECK OF LGCIU POWER SUPPLY RELAYS. 4000 FH
2-32 323000-19-1 711 GVI NORMAL EXTENSION AND RETRACTION AF LUR MRB 32.30.00/19 323100-210-002 6 MO APPL
731 MRB 6 OR
741 GENERAL VISUAL INSPECTION OF L/G EXTENSION / 750 FH
RETRACTION SYSTEM COMPONENTS
2-32 323100-01-1 210 OPC NORMAL EXTENSION AND RETRACTION EL LUR MRB 32.30.00/02 326900-740-001 6 MO APPL
MRB 9 OR
BITE CHECK OF LANDING GEAR CONTROL INTERFACE UNIT 750 FH
(LGCIU) USING MCDU (TO ENSURE THAT CONTINUOUS BITE IS
OPERATIVE)
2-32 323100-02-1 711 DET NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.30.00/07 323100-200-001 24 MO APPL
731 OR
741 DETAILED INSPECTION OF GEAR UPLOCK AND DOOR UPLOCK 3500 FC
UNITS AND ROLLERS.
2-32 323100-03-1 210 OPC NORMAL EXTENSION AND RETRACTION AF MRB 9 MRB 32.30.00/11 323100-710-001 144 MO APPL
OR
OPERATIONAL CHECK OF RETRACTION INHIBITION BAULK 18000 FC
2-32 323100-04-1 210 OPC NORMAL EXTENSION AND RETRACTION AF MRB 8 MRB 32.30.00/12 323100-710-005 72 MO APPL
OR
OPERATIONAL CHECK TO ENSURE SAFETY VALVE CLOSES AT 15000 FH
260 KNOTS
2-32 323100-05-1 123 DET NORMAL EXTENSION AND RETRACTION AF MRB 5 MRB 32.30.00/06 323000-200-001 36 MO APPL
124 OR
DETAILED INSPECTION OF NOSE GEAR DOOR OPERATING 8000 FC
MECHANISM
2-32 323100-06-1 210 OPC NORMAL EXTENSION AND RETRACTION AF LUR MRB 32.30.00/05 326100-710-001 108 MO APPL
MRB 9 OR
BITE CHECK USING MCDU TO ENSURE "GEAR NOT DOWN FOR 12000 FH
LANDING" WARNINGS OPERATIVE
2-32 323100-08-1 711 SDI NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.21.00/09 323122-920-001 120 MO YES APPL
MRB CPCP MRB 32.30.00/21 MPD APPENDIX 7 OR
REMOVE NOSE LANDING GEAR ACTUATING CYLINDER AND MRB 322152-01-1 20000 FC
AIRFRAME ATTACHMENT PIN AND SLEEVE FOR SPECIAL MRB 322158-01-1
DETAILED INSPECTION IN SHOP
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
2-32 323100-08-2 711 SDI NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.21.00/09 323122-920-001 144 MO YES N/A
MRB CPCP MRB 32.30.00/21 MPD APPENDIX 7 OR
REMOVE NOSE LANDING GEAR ACTUATING CYLINDER AND MRB 322182-01-1 20000 FC
AIRFRAME ATTACHMENT PIN AND SLEEVE FOR SPECIAL MRB 322183-01-1
DETAILED INSPECTION IN SHOP
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
APPENDIX A
AEG/AMP/A320 Page 51 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-32 323100-09-1 731 SDI NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.11.00/20 323100-220-002 120 MO YES APPL
741 MRB CPCP MRB 32.30.00/20 MPD APPENDIX 7 OR
REMOVE MAIN LANDING GEAR RETRACTION ACTUATOR AND PINS MRB 321147-01-1 20000 FC
FOR SPECIAL DETAILED INSPECTION IN SHOP MRB 321171-01-1
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
2-32 323100-09-2 731 SDI NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.11.00/20 323100-220-002 144 MO YES APPL
741 MRB CPCP MRB 32.30.00/20 MPD APPENDIX 7 OR
REMOVE MAIN LANDING GEAR RETRACTION ACTUATOR AND PINS MRB 321184-01-1 20000 FC
FOR SPECIAL DETAILED INSPECTION IN SHOP MRB 321186-01-1
NOTE:
- TASK TO BE PERFORMED OFF AIRCRAFT IN ACCORDANCE
WITH RELEVANT CMM.
2-32 323105-04-1 731 FNC NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.30.00/24 323100-720-803 7500 FC APPL
741
FUNCTIONAL CHECK OF THE MLG DOOR ACTUATING CYLINDER.
2-32 323105-05-1 711 FNC NORMAL EXTENSION AND RETRACTION AF MRB 5,8 MRB 32.30.00/25 323100-720-804 7500 FC APPL
FUNCTIONAL CHECK OF THE NLG DOOR ACTUATING CYLINDER.
2-32 323300-01-1 100 DET LANDING GEAR FREE FALL EXTENSION AF MRB 8 MRB 32.30.00/09 323300-200-002 72 MO APPL
200
DETAILED INSPECTION OF FREE-FALL MECHANISM INCLUDING
CABLES
2-32 323300-03-1 700 FNC LANDING GEAR FREE FALL EXTENSION AF MRB 8 MRB 32.11.00/17 323300-720-003 80 MO APPL
MRB 32.21.00/08 OR
FUNCTIONAL CHECK OF FREE-FALL SYSTEM MRB 32.30.00/13 15000 FC
2-32 323300-04-1 100 FNC LANDING GEAR FREE FALL EXTENSION AF MRB 8 MRB 32.30.00/15 323300-200-001 72 MO APPL
FUNCTIONAL CHECK OF FREE-FALL MECHANISM CABLE TENSION
2-32 323300-05-2 210 OPC LANDING GEAR FREE FALL EXTENSION AF CMR* CMR 323000-00001-1-C 323300-710-001 NOTE 36 MO APPL
MRB 8 MRB 32.30.00/08 OR
OPERATIONAL CHECK OF FREE-FALL MECHANICAL CONTROL 7700 FH
NOTE
NOTE:
THRESHOLD/INTERVAL:
- FOR CEO AIRCRAFT, NEXT CMR 323000-00001-1-C
ACCOMPLISHMENT MUST BE CARRIED OUT NO LATER THAN:
- THE COMPLIANCE TIME PROVIDED IN THE EASA AD
MANDATING THE REV 05 OF A320FAM ALS PART 3, AND
ASSOCIATED VARIATION(S) (IF ANY),
OR
- WITHIN THE DUE THRESHOLD AND/OR INTERVAL (7700 FH
FROM A/C EIS, OR FROM LAST ACCOMPLISHMENT OF MPD
TASK 323300-05-1, WHICHEVER OCCURS LATER),
WHICHEVER OCCURS LATER.
2-32 324000-14-1 210 FNC WHEELS AND BRAKES AF MRB 8 MRB 32.40.00/14 324200-720-004 48 MO APPL
730 OR
744 FUNCTIONAL CHECK OF THE AUTOMATIC REACTIVATION OF THE 8000 FC
NORMAL BRAKING MODE (PARKING BRAKE APPLIED)
2-32 324000-15-1 148 FNC WHEELS AND BRAKES AF CMP CMP 32-2-0000-005 324400-720-002 14800 FH N/A
210
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF
BRAKING SYSTEM COMPONENTS.(PARK BRAKE SELECTOR VALVE,
PRESSURE RELIEF VALVE AND ALTERNATE BRAKE SELECTOR
VALVE)
2-32 324000-15-2 148 FNC WHEELS AND BRAKES AF CMR* CMR 324500-00002-1-C 324400-720-002 14800 FH N/A
210
FUNCTIONAL CHECK TO MONITOR INTERNAL LEAK RATE OF
BRAKING SYSTEM COMPONENTS.(PARK BRAKE SELECTOR VALVE,
PRESSURE RELIEF VALVE AND ALTERNATE BRAKE SELECTOR
VALVE)
NOTE:
FOR ETOPS: TASK COVERS 324000-15-1.
APPENDIX A
AEG/AMP/A320 Page 52 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-32 324000-16-1 731 GVI WHEELS AND BRAKES AF MRB 9 MRB 32.40.00/16 324000-210-801 100 FC APPL
741 Included into Weekly
GENERAL VISUAL INSPECTION OF L/G BRAKE UNITS Checklist
2-32 324000-17-1 210 FNC WHEELS AND BRAKES AF CMR* CMR 324000-00002-1-C 324400-720-002 108 MO APPL
730 LUR MRB 32.40.00/17 OR
740 FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM. MRB 9 8000 FC
OR
12000 FH
2-32 324100-01-1 700 FNC WHEELS AF MRB 6,9 MRB 32.40.00/01 324100-210-003 3 DY APPL
Included into Daily
FUNCTIONAL CHECK OF TIRE PRESSURES Checklist
2-32 324100-03-1 700 OPC WHEELS AF MRB 9 MRB 32.40.00/11 324100-210-004 4 MO N/A
FUNCTIONAL CHECK FOR CORRECT OPERATION OF WHEEL
MOUNTED TIRE PRESSURE INDICATORS
2-32 324100-04-1 730 SDI WHEELS AF VSB VSB C20452-32-3254 NOTE N/A
740
INSPECT INNER HALF WHEEL FOR CORROSION AND CRACKS.
NOTE:
TASK TO BE PERFORMED AT EACH TIRE CHANGE BUT TIME
BETWEEN TWO SUBSEQUENT INSPECTIONS NOT TO EXCEED 6
MO.
2-32 324200-02-1 730 FNC NORMAL BRAKING SYSTEM AF LUR MRB 32.40.00/15 324241-200-001 6 MO N/A
740 MRB 6 OR
FUNCTIONAL CHECK OF NORMAL BRAKE ACCUMULATOR BY 400 FH
READING THE CHARGE PRESSURE ON THE ACCUMULATOR GAUGE
2-32 324227-01-1 731 FNC MAIN LANDING GEAR BRAKES AF MRB 6 MRB 32.40.00/02 324227-210-003 100 FC APPL
741 Included into Weekly
FUNCTIONAL CHECK OF BRAKE HEAT PACK FOR WEAR BY USE Checklist
OF THE WEAR INDICATOR (PARKING BRAKE APPLIED)
2-32 324300-01-1 210 OPC ALTERNATE BRAKING SYSTEM AF CMR* CMR 324000-00001-1-C 324300-710-802 108 MO APPL
730 LUR MRB 32.40.00/08 OR
740 OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM MRB 9 11600 FH
NOTE:
TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE.
324300-01-2 ************** TASK DELETED ************** N/A
2-32 324300-01-3 210 OPC ALTERNATE BRAKING SYSTEM AF LUR MRB 32.40.00/08 324300-710-802 108 MO N/A
730 MRB 9 OR
740 OPERATIONAL CHECK OF ALTERNATE BRAKING SYSTEM 12000 FH
NOTE:
TASK MAY BE ACCOMPLISHED AT BRAKE CHANGE.
2-32 324300-02-1 210 OPC ALTERNATE BRAKING SYSTEM AF MRB 9 MRB 32.40.00/09 324200-710-003 24000 FC APPL
OPERATIONAL CHECK OF ANTISKID INHIBITION
2-32 324311-01-1 122 FNC LOW PRESSURE BRAKE RESERVOIR AF LUR MRB 32.40.00/06 324311-210-001 24 MO APPL
MRB 6 OR
FUNCTIONAL CHECK OF FLUID LEVEL OF LOW PRESSURE BRAKE 1500 FC
RESERVOIR
2-32 324314-01-1 148 RST ALTERNATE BRAKE DIST. - DUAL VALVE AF MRB 6 MRB 32.40.00/12 324314-200-002 13 MO APPL
DRAIN ACCUMULATED WATER FROM THE BRAKE DUAL
DISTRIBUTION VALVE (BDDV)
2-32 324411-01-1 148 FNC BRAKE ACCUMULATOR AF CMP CMP 32-2-0000-001 324411-200-001 4 MO APPL
210 MRB 6,9 MRB 32.40.00/05 OR
FUNCTIONAL CHECK OF PARKING/EMERGENCY BRAKE 750 FH
ACCUMULATOR BY READING THE CHARGE PRESSURE ON THE
ACCUMULATOR GAUGE
2-32 324500-01-1 210 OPC PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF MRB 9 MRB 32.40.00/13 324500-710-001 24 MO APPL
711 OR
730 OPERATIONAL CHECK OF THE PARKING BRAKE SYSTEM 2000 FC
740
2-32 324500-01-2 210 OPC PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF MRB 9 MRB 32.40.00/18 324500-710-001 48 MO N/A
711 OR
730 OPERATIONAL CHECK OF THE PARKING BRAKE SYSTEM 10000 FC
740
APPENDIX A
AEG/AMP/A320 Page 53 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-32 324500-02-1 148 FNC PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF CMP CMP 32-2-0000-002 324500-720-002 10000 FH N/A
210
FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM WITH THE
PARKING BRAKE APPLIED
2-32 324500-02-2 148 FNC PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF CMP CMP 32-2-0000-003 324500-720-002 9000 FH N/A
210
FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM WITH THE
PARKING BRAKE APPLIED
2-32 324500-03-1 210 FNC PARKING/ULTIMATE EMERGENCY BRAKING SYSTEM AF CMP CMP 32-2-0000-004 324400-720-002 3950 FH N/A
730
740 FUNCTIONAL CHECK OF BRAKE ACCUMULATOR SYSTEM WITH THE
PARKING BRAKE NOT APPLIED
2-32 324900-01-1 210 FNC TIRE PRESSURE INDICATING SYSTEM AF LUR MRB 32.40.00/03 324900-720-001 12 MO N/A
711 MRB 9 OR
730 FUNCTIONAL CHECK BY CROSSCHECK OF TPIS READING AND 750 FC
740 TIRE PRESSURE GAUGE
2-33 331400-01-1 210 OPC ANNUNCIATOR LIGHT TEST AND DIMMING EL LUR MRB 23.13.00/02 331400-710-001 24 MO APPL
MRB 9 MRB 27.90.00/01 OR
OPERATIONAL CHECK OF LIGHTS TEST SYSTEM MRB 31.50.00/07 2000 FH
MRB 33.14.00/01
MRB 34.48.00/03
2-33 334800-01-1 140 VCK ANTI-COLLISION/STROBE LIGHTING EL LUR MRB 33.48.00/01 334800-200-802 16600 FH 6 MO N/A
244 MRB 9 OR
VISUAL CHECK OF NEOL (NEAR END OF LIFE) ACTIVATION ON 750 FH
BEACON LIGHTS NOTE
NOTE:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-33 335100-01-1 210 OPC CABIN EMERGENCY LIGHTING EL MRB 8 MRB 33.51.00/01 335100-710-001 8 DY APPL
Included into Weekly
OPERATIONAL CHECK OF EMERGENCY POWER SUPPLY UNITS BY Checklist
BITE-CHECK
2-33 335100-02-1 220 OPC CABIN EMERGENCY LIGHTING EL LUR MRB 33.51.00/02 335100-710-002 12 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF EMERGENCY ESCAPE PATH MARKING 1000 FH
LIGHTS
2-33 335100-03-1 220 OPC CABIN EMERGENCY LIGHTING EL MRB 9 MRB 33.51.00/03 335100-710-003 6 MO APPL
NOTE
CHECK BATTERY CAPACITY
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-33 335100-04-1 200 RST CABIN EMERGENCY LIGHTING EL MRB 9 MRB 33.51.00/04 335139-920-001 18 MO YES N/A
NOTE
REMOVE POWER SUPPLY UNITS OF EMERGENCY ESCAPE PATH
MARKING LIGHTS AND RESTORE BATTERIES TO REQUIRED
STANDARD BY CAPACITY CHECK
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
335100-05-1 ************** TASK DELETED ************** N/A
2-33 335100-06-1 220 OPC CABIN EMERGENCY LIGHTING EL LUR MRB 33.51.00/06 335100-720-001 252 MO APPL
MRB 9 OR
CHECK OF DOOR SWITCH POWER SUPPLIED BY EMERGENCY 36000 FH
LIGHTS SYSTEM AND CHECK DOOR SWITCH OPERATION TO
ACTIVATE THE EXTERIOR LIGHTS
2-33 335100-10-1 220 OPC CABIN EMERGENCY LIGHTING EL LUR MRB 33.51.00/10 335100-710-805 12 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF EMERGENCY LIGHTING SYSTEM 1000 FH
INCLUDING CHECK OF ALL CABIN LIGHTS AND SIGNS
APPENDIX A
AEG/AMP/A320 Page 54 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-33 335100-11-1 220 OPC CABIN EMERGENCY LIGHTING EL LUR MRB 33.51.00/11 335100-710-804 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF MANUAL EMERGENCY LIGHTING 24000 FH
ACTIVATION
2-34 341300-01-1 210 OPC AIR DATA RA LUR MRB 34.13.00/01 341300-710-002 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF OVERSPEED WARNING VMO/MMO USING 24000 FH
CFDS.
2-34 341300-02-1 210 OPC AIR DATA RA LUR MRB 34.13.00/02 341300-710-001 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF AIR DATA SWITCHING FUNCTION 24000 FH
2-34 341300-03-1 210 OPC AIR DATA RA LUR MRB 34.13.00/01 341300-710-007 180 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF OVERSPEED WARNINGS VFE/VLE USING 24000 FH
CFDS.
2-34 341300-05-1 210 OPC AIR DATA AV LUR MRB 34.14.00/03 341000-710-009 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF THE 5-MINUTE TIME DELAY OF ADIRU 12000 FH
2 AND 3 POWER DISCONNECTION IN EMERGENCY
CONFIGURATION
2-34 341300-07-1 120 RST AIR DATA AV MRB 6 MRB 34.13.00/06 341000-170-001 20 MO APPL
OR
FLUSHING OF TOTAL PRESSURE LINES 6000 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-34 341300-09-1 210 OPC AIR DATA AV LUR MRB 34.13.00/07 341300-710-009 180 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF THE BACK UP SPEED SCALE DISPLAY 24000 FH
2-34 341300-11-1 120 RST AIR DATA AV LUR MRB 34.13.00/08 341000-170-004 6 MO APPL
MRB 6 OR
CLEANING OF 1 OUT OF 3 PITOT PROBES. 750 FH
NOTE:
TASK TO BE PERFORMED ALTERNATELY ON PITOT 1, 2 AND 3.
2-34 342000-03-1 210 OPC STANDBY NAVIGATION SYSTEMS (INCLUDING ISIS) AV LUR MRB 34.20.00/03 342225-710-001 180 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF ISIS DC HOT BUS SUPPLY 24000 FH
2-34 342100-01-1 120 FNC STANDBY ALTITUDE AND AIRSPEED AV LUR MRB 34.21.00/01 342100-790-001 108 MO APPL
MRB 6 OR
LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS 12000 FH
NOTE:
PLANNING:
- THIS TASK IS COVERED BY TASK 342100-02-1.
2-34 342100-02-1 120 SVC STANDBY ALTITUDE AND AIRSPEED AV MRB 6 MRB 34.21.00/02 341000-170-003 20 MO APPL
OR
DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITS 6000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- THIS TASK COVERS TASK 342100-01-1.
2-34 342200-01-1 210 OPC STANDBY COMPASS RA LUR MRB 34.22.00/01 342200-710-001 72 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF THE STANDBY COMPASS INCLUDING 7500 FH
LIGHT TEST AND VISUAL CHECK
APPENDIX A
AEG/AMP/A320 Page 55 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-34 342200-02-1 120 SVC STANDBY NAVIGATION SYSTEMS (INCLUDING ISIS) AV MRB 6 MRB 34.20.00/02 342225-170-001 20 MO N/A
OR
DRAINING AND FLUSHING OF STANDBY PNEUMATIC CIRCUITS 6000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- THIS TASK COVERS TASK 342200-05-1.
2-34 342200-05-1 120 FNC STANDBY NAVIGATION SYSTEMS (INCLUDING ISIS) AV LUR MRB 34.20.00/01 342225-790-001 108 MO N/A
MRB 6 OR
LOW RANGE LEAK TEST OF STANDBY PNEUMATIC CIRCUITS 12000 FH
NOTE:
PLANNING:
- THIS TASK IS COVERED BY TASK 342200-02-1.
2-34 344100-01-1 110 FNC WEATHER RADAR SYSTEM EL MRB 9 MRB 34.41.00/01 531511-760-002 30 MO N/A
RADIO ELECTRICAL TEST OF THE RADOME (FOR KEVLAR
RADOME WITH PWS ACTIVATED)
2-34 344200-01-1 152 DET RADIO ALTIMETER RA LUR MRB 34.42.00/01 344200-750-001 36 MO APPL
MRB 9 OR
OPERATIONAL CHECK AND DETAILED INSPECTION FOR 4000 FH
CONTAMINATION OF RADIO ALTIMETER FAN NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- TASK IS NOT APPLICABLE IF P/N 822-2365-022 IS
INSTALLED.
2-34 344800-01-1 210 OPC GROUND PROXIMITY WARNING SYSTEM RA LUR MRB 34.48.00/01 344800-710-001 108 MO APPL
MRB 9 OR
OPERATIONAL CHECK OF GROUND SELF TEST SYSTEM 12000 FH
2-34 344800-03-1 210 OPC TERRAIN AWARENESS WARNING SYSTEM RA LUR MRB 34.48.00/01 344300-740-004 108 MO N/A
MRB 9 OR
BITE TEST OF THE T2CAS 12000 FH
2-34 344800-04-1 210 OPC TERRAIN AWARENESS WARNING SYSTEM RA LUR MRB 34.48.00/01 347200-740-001 108 MO N/A
MRB 9 OR
BITE TEST OF THE T/TISS (TAWS PART) 12000 FH
345200-01-1 ************** TASK DELETED ************** N/A
2-34 345200-02-1 210 FNC ATC SYSTEM RA LUR MRB 34.52.00/02 345200-720-006 180 MO APPL
MRB 9 OR
FUNCTIONAL CHECK OF ATC ANTENNAS 24000 FH
345200-03-1 ************** TASK DELETED ************** N/A
2-34 345200-04-1 210 OPC ATC SYSTEM AF LUR MRB 34.52.00/03 345200-720-009 180 MO N/A
MRB 8 OR
OPERATIONAL CHECK OF REMOTE ATC CONTROL BOX 24000 FH
2-35 351000-01-1 210 OPC CREW OXYGEN SYSTEM AF MRB 8 MRB 35.10.00/01 351241-710-001 24 MO APPL
OPERATIONAL CHECK OF FLIGHT CREW OXYGEN SYSTEM
2-35 351000-08-1 210 FNC CREW OXYGEN AF MRB 8 MRB 35.10.00/08 351000-720-001 36 MO APPL
OR
FUNCTIONAL CHECK OF ECAM OXYGEN CYLINDER CONTENTS 6500 FH
INDICATION COMPARED WITH CYLINDER PRESSURE GAUGE
APPENDIX A
AEG/AMP/A320 Page 56 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-35 351000-09-1 122 DIS CREW OXYGEN AF MRB 6 MRB 35.10.00/09 351300-200-801 240 MO YES APPL
NOTE
DISCARD CREW OXYGEN LOW PRESSURE SUPPLY HOSE
(FLEXIBLE HOSE)
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 351000-10-1 122 FNC CREW OXYGEN AF MRB 8 MRB 35.10.00/10 351300-200-802 72 MO YES APPL
NOTE
REMOVE PRESSURE REGULATOR TRANSMITTER FOR IN SHOP
FUNCTIONAL CHECK
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 351141-01-1 125 FNC CREW OXYGEN CYLINDER AF MRB 5 MRB 35.10.00/05 351141-750-002 NOTE YES APPL
NOTE
REMOVE OXYGEN CYLINDER FOR IN SHOP HYDROSTATIC TEST
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 351241-01-1 210 DET CREW OXYGEN MASKS AF MRB 8 MRB 35.10.00/03 351241-200-001 24 MO APPL
DETAILED INSPECTION OF OXYGEN MASKS (OUT OF BOX) WITH
HARNESS INFLATED
2-35 351241-02-1 210 FNC CREW OXYGEN MASK REGULATORS AF MRB 9 MRB 35.10.00/04 351241-750-001 72 MO YES APPL
NOTE
REMOVE CREW OXYGEN MASK FOR IN SHOP FUNCTIONAL CHECK
OF MASK REGULATOR ASSEMBLY
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 351351-01-1 210 FNC OXYGEN SUPPLY VALVE EL MRB 9 MRB 35.10.00/02 351200-710-001 72 MO APPL
FUNCTIONAL CHECK OF LOW PRESSURE SWITCH
2-35 352000-01-1 200 OPC PASSENGER OXYGEN SYSTEM AF CMR** CMR 352000-00001-1-C 352300-710-001 72 MO APPL
LUR MRB 35.20.00/01 OR
OPERATIONAL CHECK OF MANUAL MASK RELEASE MRB 8 8500 FH
2-35 352000-02-1 200 FNC PASSENGER OXYGEN SYSTEM AF CMR** CMR 352000-00002-1-C 352300-720-003 72 MO APPL
MRB 8 MRB 35.20.00/02 OR
FUNCTIONAL CHECK OF AUTOMATIC MASK RELEASE, DETAILED 24000 FH
INSPECTION OF MASKS AND VISUAL CHECK OF CHEMICAL
OXYGEN GENERATORS
2-35 352000-04-1 200 DIS PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 8 MRB 35.20.00/04 352141-920-801 300 MO YES N/A
NOTE
DISCARD GASEOUS LAVATORY OXYGEN CONTAINER
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 57 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-35 352001-01-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 6 MRB 35.20.01/01 352100-750-001 60 MO YES N/A
200 NOTE
REMOVE OXYGEN CYLINDER FOR IN SHOP HYDROSTATIC TEST
NOTE:
INTERVAL:
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 352001-02-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 8 MRB 35.20.01/02 352300-720-006 72 MO N/A
200 OR
FUNCTIONAL CHECK OF ALTITUDE PRESSURE SWITCH AND 24000 FH
DETAILED INSPECTION OF OXYGEN MASK ASSEMBLY
2-35 352001-03-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 8 MRB 35.20.01/03 352300-720-007 72 MO N/A
200 OR
OPERATIONAL AND FUNCTIONAL CHECK OF PASSENGER OXYGEN 12000 FH
SYSTEM
2-35 352001-04-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF CMR** CMR 352000-00003-1-C 352300-720-004 72 MO YES N/A
200 LUR MRB 35.20.01/04 OR
REMOVE PRESSURE REGULATORS FOR IN SHOP FUNCTIONAL MRB 8 8000 FH
CHECK
2-35 352001-05-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 8 MRB 35.20.01/05 352300-720-005 60 MO YES N/A
200 MRB 35.20.01/07
REMOVE PRESSURE REDUCER, PRESSURE RELIEF VALVE, MAIN
DISTRIBUTION SHUTOFF VALVES, RISERLINE SHUTOFF VALVES
FOR IN SHOP FUNCTIONAL CHECK AND CHECK VALVES OF
ENGINE BURST PROTECTION SYSTEM FOR IN SHOP
OPERATIONAL CHECK
2-35 352001-06-1 162 OPC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 9 MRB 35.20.01/06 352300-710-004 160 MO N/A
210 OR
OPERATIONAL CHECK OF OXYGEN CYLINDER HANDVALVE 40000 FH
SWITCHES
2-35 352001-08-1 162 OPC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 8 MRB 35.20.01/08 352100-710-802 72 MO N/A
210
OPERATIONAL CHECK OF CHECK VALVES OF OXYGEN STORAGE
2-35 352001-09-1 162 FNC PASSENGER OXYGEN SYSTEM (GASEOUS) AF MRB 9 MRB 35.20.01/09 352100-720-802 180 MO YES N/A
200
REMOVE CHECK VALVES OF OXYGEN STORAGE FOR IN SHOP
FUNCTIONAL CHECK
2-35 352142-01-1 200 DIS PASSENGER OXYGEN SYSTEM (CHEMICAL) AF MRB 8 MRB 35.20.00/03 352100-920-001 NOTE YES APPL
NOTE
DISCARD CHEMICAL OXYGEN GENERATORS
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 353000-01-1 200 VCK PORTABLE OXYGEN CYLINDERS AF MRB 9 MRB 35.30.00/01 353242-210-002 4 MO APPL
CHECK CONNECTING HOSE, MASK AND PRESSURE ON CYLINDER
PRESSURE GAUGE.
2-35 353000-02-1 200 FNC PORTABLE OXYGEN AF MRB 9 MRB 35.30.00/02 353242-750-001 NOTE YES APPL
NOTE
REMOVE PORTABLE OXYGEN CYLINDER ASSEMBLY FOR IN SHOP
HYDROSTATIC TEST AND FUNCTIONAL CHECK OF REGULATOR
VALVE ASSEMBLY.
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
353000-04-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 58 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-35 353000-05-1 200 VCK PROTECT. BREATHING EQPT (CKPT & CABIN) AF MRB 8 MRB 35.30.00/04 353000-210-006 4 MO APPL
VISUAL CHECK OF THE TAMPER SEAL/SERVICEABILITY
INDICATION OF THE PROTECTIVE BREATHING EQUIPMENT
2-35 353000-06-1 200 DIS PROTECT. BREATHING EQPT (CKPT & CABIN) AF MRB 8 MRB 35.30.00/05 353000-920-001 NOTE YES APPL
NOTE
DISCARD PROTECTIVE BREATHING EQUIPMENT
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
- INTERVAL TO BE MANAGED AT COMPONENT LEVEL. REFER TO
SYSTEM SECTION INTRODUCTION FOR ADDITIONAL
GUIDANCE.
2-35 353000-07-1 200 DET PORTABLE OXYGEN AF MRB 9 MRB 35.30.00/06 353000-220-001 36 MO APPL
DETAILED INSPECTION OF PORTABLE OXYGEN MASK
2-36 361100-01-1 450 FNC ENGINE BLEED AIR SUPPLY SYSTEM AF MRB 9 MRB 36.11.00/03 361153-720-001 60 MO APPL
460 OR
FUNCTIONAL CHECK OF OVERPRESSURE VALVE 22000 FH
2-36 361100-02-1 450 FNC ENGINE BLEED AIR SUPPLY SYSTEM AF LUR MRB 36.11.01/01 180 MO N/A
460 MRB 9 OR
FUNCTIONAL CHECK OF OVERPRESSURE VALVE 25000 FH
2-36 361100-03-1 410 FNC ENGINE BLEED AIR SUPPLY SYSTEM AF LUR MRB 36.11.01/01 361153-720-803 180 MO N/A
420 MRB 9 OR
FUNCTIONAL CHECK OF OVERPRESSURE VALVE. 25000 FH
2-36 361100-05-1 191 DIS ENGINE BLEED AIR SUPPLY SYSTEM AF MRB 6 MRB 36.12.00/06 361241-920-001 48 MO N/A
192 OR
REMOVE AND REPLACE COMBO SEALS ON PACK INLET INCL. 12000 FH
ON SLEEVES DOWNSTREAM AND UPSTREAM OF FLOW CONTROL NOTE
VALVE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- TASK MAY BE COMBINED WITH TASK 215200-07-1.
2-36 361100-08-1 450 DET ENGINE BLEED AIR SUPPLY SYSTEM AF LUR 361149-200-004 24 MO N/A
460 VSB VSB RA32036-13 OR
DETAILED INSPECTION OF HIGH PRESSURE BLEED AIR DUCT 1800 FC
BEND RADIUS.
2-36 361100-08-2 450 DET ENGINE BLEED AIR SUPPLY SYSTEM AF LUR 361149-200-004 12 MO N/A
460 VSB VSB RA32036-13 OR
DETAILED INSPECTION OF HIGH PRESSURE BLEED AIR DUCT 750 FC
BEND RADIUS.
2-36 361101-01-1 410 DIS ENGINE BLEED AIR SUPPLY SYSTEM AF SEMR SEMR 361101-00001-1-E 545222-300-801 72 MO 72 MO N/A
420 OR OR
DISCARD PRE COOLER EXCHANGER (PCE) UPPER SEAL. 20000 FC 20000 FC
OR OR
40000 FH 40000 FH
2-36 361141-03-1 453 DET IP BLEED CHECK VALVE EN LUR MRB 36.11.00/04 361141-200-001 72 MO N/A
463 MRB 6 OR
CHECK OF IP BLEED CHECK VALVE FOR CONDITION 7500 FH
2-36 361141-04-1 450 DET IP BLEED CHECK VALVE EN LUR MRB 36.11.00/05 361141-200-010 108 MO APPL
460 MRB 6 OR
CHECK OF IP BLEED CHECK VALVE FOR CONDITION 12000 FH
2-36 361141-05-1 450 DET IP BLEED CHECK VALVE EN LUR MRB 36.11.00/05 361141-200-801 108 MO N/A
460 MRB 6 OR
CHECK OF IP BLEED CHECK VALVE FOR CONDITION 12000 FH
2-36 361141-06-1 450 DET IP BLEED CHECK VALVE EN LUR MRB 36.11.01/02 361141-200-802 108 MO N/A
460 MRB 6 OR
REMOVE INTERMEDIATE PRESSURE BLEED CHECK VALVE FOR 8000 FC
DETAILED INSPECTION OR
12000 FH
APPENDIX A
AEG/AMP/A320 Page 59 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-36 361141-07-1 450 DET IP BLEED CHECK VALVE EN LUR MRB 36.11.01/03 361141-200-803 108 MO N/A
460 MRB 6 OR
REMOVE INTERMEDIATE PRESSURE BLEED CHECK VALVE FOR 8000 FC
DETAILED INSPECTION. OR
12000 FH
2-36 361143-01-1 413 RST THERMOSTAT - FAN AIR VALVE CONTROL AF LUR MRB 36.11.00/02 361143-100-001 72 MO APPL
423 MRB 6 OR
REMOVE THE THERMOSTAT-FILTER OF THE FAN AIR 6000 FH
VALVE-CONTROL FOR CLEANING. NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-36 361148-01-1 500 FNC AIR BLEED DUCTS,WING EN LUR MRB 36.12.00/04 361148-790-001 180 MO APPL
600 MRB 6 OR
PERFORM LEAK CHECK ON BLEED AIR DUCTING IN WING AREA 22000 FH
BETWEEN BLEED AIR PRECOOLER, WING ANTI ICE VALVE AND NOTE
WING/FUSELAGE CONNECTION
NOTE:
PLANNING:
- TASK MAY BE COMBINED WITH TASKS 361200-02-1 AND
361200-03-1.
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-36 361200-01-1 210 OPC AIR BLEED AIR SUPPLY & CROSSBLEED SYST AF MRB 9 MRB 36.12.00/03 361200-710-002 72 MO APPL
OPERATIONAL CHECK OF CROSSBLEED VALVE IN MANUAL MODE
2-36 361200-02-1 150 FNC APU BLEED AIR SUPPLY & CROSSBLEED SYST EN LUR MRB 36.12.00/07 361200-790-002 180 MO APPL
160 MRB 6 OR
190 PERFORM LEAK CHECK ON APU BLEED AIR DUCTING (UPSTREAM 24000 FH
310 THE APU BLEED CHECK VALVE) NOTE
NOTE:
PLANNING:
- TASK MAY BE COMBINED WITH TASKS 361148-01-1 AND
361200-03-1.
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-36 361200-03-1 191 FNC APU BLEED AIR SUPPLY & CROSSBLEED SYST EN LUR MRB 36.12.00/05 361200-790-003 180 MO APPL
192 MRB 6 OR
LEAK CHECK OF BLEED AIR DUCTING IN FUSELAGE AREA 24000 FH
BETWEEN APU BLEED CHECK VALVE, AIR CONDITIONING PACK NOTE
AND WING/FUSELAGE CONNECTION
NOTE:
PLANNING:
- TASK MAY BE COMBINED WITH TASKS 361148-01-1 AND
361200-02-1.
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-36 361251-01-1 192 DET APU BLEED CHECK VALVE AF LUR MRB 36.12.00/02 361251-200-001 180 MO N/A
MRB 6,9 OR
REMOVE AND CHECK AUXILIARY POWER UNIT BLEED CHECK 24000 FH
VALVE FOR CONDITION
2-36 361251-01-2 192 DET APU BLEED CHECK VALVE AF CMR* CMR 361200-00001-1-C 361251-200-001 108 MO N/A
LUR MRB 36.12.00/01 OR
REMOVE AND CHECK AUXILIARY POWER UNIT BLEED CHECK MRB 6,9 11000 FH
VALVE FOR CONDITION
APPENDIX A
AEG/AMP/A320 Page 60 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-36 361251-01-3 192 DET APU BLEED CHECK VALVE AF CMR* CMR 361200-00001-1-C 361251-200-001 180 MO APPL
LUR MRB 36.12.00/02 OR
REMOVE AND CHECK AUXILIARY POWER UNIT BLEED CHECK MRB 6,9 13000 FH
VALVE FOR CONDITION
2-38 381000-01-1 171 RST POTABLE WATER SYSTEM CA MRB 6,9 MRB 38.10.00/01 381000-670-002 3 MO APPL
NOTE
STERILIZATION OF POTABLE WATER SYSTEM AND DISCARD OF
WATER FILTER ELEMENTS, IF INSTALLED
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-38 383100-02-1 170 DET VACUUM TOILET SYSTEM UT MRB 9 MRB 38.31.01/03 383167-610-001 24 MO APPL
OR
INSPECT WATER SEPARATOR AND ASSOCIATED FILTER 7500 FH
ELEMENT, AND CLEAN AS NECESSARY NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-38 383100-05-1 172 DET VACUUM TOILET SYSTEM UT MRB 6 MRB 38.31.01/06 383161-210-001 24 MO APPL
OR
DETAILED INSPECTION OF CLEANLINESS INSIDE WASTE TANK 7500 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-38 383100-06-1 200 RST VACUUM TOILET SYSTEM AF LUR MRB 38.31.01/05 383100-100-018 2 MO APPL
MRB 7 OR
CLEANING OF VACUUM WASTE LINES WITH CHEMICAL CLEANING 150 FH
AGENT AND CRUSHED ICE NOTE
Included into Weekly
NOTE: Checklist
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- THIS IS AN ALTERNATIVE TASK TO 383100-07-1.
2-38 383100-07-1 200 RST VACUUM TOILET SYSTEM AF MRB 7 MRB 38.31.01/07 383100-100-004 72 MO APPL
OR
CORRECTIVE VACUUM WASTE LINE CLEANING. 7500 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
PLANNING:
- THIS IS AN ALTERNATIVE TASK TO 383100-06-1.
2-38 383102-01-1 125 GVI TOILET SYSTEM (RECIRCULATION TYPE) UT LUR MRB 38.31.02/01 383174-210-801 72 MO N/A
171 MRB 9 OR
GENERAL VISUAL INSPECTION OF WASTE TANKS DRAIN PIPES. 6000 FH
2-38 383200-01-1 200 RST WASTE WATER DRAIN UT LUR MRB 38.32.00/02 383200-100-002 12 MO APPL
MRB 7 OR
CLEAN FILTER ELEMENT OF WASHBASIN DRAIN VALVES 1500 FH
NOTE
NOTE:
DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT INITIAL
INTERVAL MAY BE USED.
2-38 384142-01-1 137 DIS AIR FILTER CA MRB 6,9 MRB 38.40.00/01 384100-610-001 72 MO APPL
171 OR
DISCARD SYSTEM FILTER ELEMENT 24000 FH
APPENDIX A
AEG/AMP/A320 Page 61 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-38 384241-01-1 137 DET AIR SUPPLY CA LUR MRB 38.40.00/03 384200-210-001 144 MO N/A
172 MRB 9 OR
DETAILED INSPECTION OF COMPRESSOR INLET FILTER. 18000 FH
NOTE
NOTE:
INTERVAL:
- DEPENDING ON OPERATING ENVIRONMENT AND OPERATORS
EXPERIENCE, A LESS FREQUENT OR MORE FREQUENT
INITIAL INTERVAL MAY BE USED.
2-38 384241-02-1 137 DIS AIR SUPPLY CA LUR MRB 38.40.00/04 384200-610-002 108 MO N/A
163 MRB 9 OR
DISCARD COMPRESSOR INLET FILTER ELEMENT. 12000 FH
2-38 384242-01-1 137 DIS AIR SUPPLY CA MRB 9 MRB 38.40.00/02 384200-610-001 72 MO N/A
163 OR
171 DISCARD COMPRESSOR OUTLET FILTER ELEMENT. 24000 FH
2-44 443400-02-1 200 RST ON BOARD MOBILE TELEPHONY SYSTEM AV MRB 6 MRB 44.34.00/02 443400-820-001 24 MO YES N/A
CALIBRATION OF BASE TRANSCEIVER STATION
2-46 464000-02-1 200 RST CABIN INFORMATION SYSTEMS AV MRB 7 MRB 46.40.00/01 443400-820-802 NOTE YES N/A
NOTE
CALIBRATION OF BASE TRANSCEIVER STATION
NOTE:
INTERVAL:
- FOR INTERVAL SELECTED FOR THE VARIOUS PART NUMBERS
REFER TO VENDOR RECOMMENDATIONS.
2-47 470000-01-1 191 DIS INERT GAS GENERATION SYSTEM AF LUR MRB 47.00.00/01 471041-920-001 72 MO N/A
MRB 9 OR
D-ULPA FILTER ELEMENT REPLACEMENT 7000 FH
NOTE
NOTE:
INTERVAL:
- IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL REACTIVATION.
2-47 470000-02-1 191 DIS INERT GAS GENERATION SYSTEM AF LUR MRB 47.00.00/02 471043-920-001 180 MO N/A
MRB 6 OR
AIR SEPARATOR MODULE REPLACEMENT 27000 FH
NOTE
NOTE:
INTERVAL:
- IF SYSTEM IS DEACTIVATED WHEN TASK BECOMES DUE,
TASK MAY BE POSTPONED UNTIL REACTIVATION.
2-47 470000-05-1 191 OPC INERT GAS GENERATION SYSTEM AF FAL FAL 470000-00003-1-F 472143-700-002 12000 FH N/A
OPERATIONAL CHECK OF BOTH DUAL FLAPPER CHECK VALVES
(DFCV) FOR REVERSE FLOW AND NITROGEN ENRICHED AIR
(NEA) LINE FOR LEAKS.
NOTE:
TASK ONLY APPLICABLE TO AIRCRAFT ON WHICH IGGS
PROVISIONS MOD 38195 HAS BEEN EMBODIED BY SB AND THE
NEA LINE THROUGH THE MIXER UNIT BAY HAS BEEN ALSO
FITTED AS PART OF THE SB WITH MOD 150499, BUT THE
FTIS MOD 38062 IS NOT EMBODIED.
2-47 470000-06-1 191 OPC INERT GAS GENERATION SYSTEM AF FAL FAL 470000-00004-1-F 472143-700-004 12000 FH N/A
OPERATIONAL CHECK OF DUAL FLAPPER CHECK VALVES (DFCV)
FOR REVERSE FLOW.
NOTE:
TASK ONLY APPLICABLE TO AIRCRAFT ON WHICH IGGS
PROVISIONS MOD 38195 HAS BEEN EMBODIED IN PRODUCTION,
BUT THE FTIS MOD 38062 IS NOT EMBODIED.
491200-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 62 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-49 491200-02-1 315 GVI APU MOUNTS AF MRB 9 MRB 49.12.00/02-36 491200-210-002 36 MO N/A
316 OR
GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM 5200 FC
FOR CONDITION AND SECURITY. NOTE
NOTE:
INTERVAL:
- TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU
CHANGE.
491200-A1-1 ************** TASK DELETED ************** N/A
2-49 491200-A2-1 315 GVI APU MOUNTS AF MRB 9 MRB 49.12.00/01-32 491200-210-005 20 MO N/A
316
GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM
FOR CONDITION AND SECURITY.
491200-B1-1 ************** TASK DELETED ************** N/A
2-49 491200-B2-1 315 GVI APU MOUNTS AF MRB 9 MRB 49.12.00/01-13 491200-210-804 36 MO APPL
316 OR
GENERAL VISUAL INSPECTION OF APU SUSPENSION SYSTEM 5200 FC
FOR CONDITION AND SECURITY. NOTE
NOTE:
INTERVAL:
- TASK MAY BE ACCOMPLISHED AT OPPORTUNITY OF APU
CHANGE.
2-49 491300-01-1 310 GVI FIRE SEALS EN MRB 8 MRB 49.13.00/01-36 491300-200-001 36 MO N/A
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE
WALLS AND SEALS:
- COMPARTMENT DOORS
- FWD AND AFT FIRE WALLS
- SIDE FIRE WALLS
- UPPER FIRE WALL
2-49 491300-A1-1 310 GVI FIRE SEALS EN MRB 8 MRB 49.13.00/01-32 491300-200-002 36 MO N/A
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE
WALLS AND SEALS:
- COMPARTMENT DOORS
- FWD AND AFT FIRE WALLS
- SIDE FIRE WALLS
- UPPER FIRE WALL
2-49 491300-B1-1 310 GVI FIRE SEALS EN MRB 8 MRB 49.13.00/01-13 491300-200-003 36 MO APPL
GENERAL VISUAL INSPECTION OF ALL APU COMPARTMENT FIRE
WALLS AND SEALS:
- COMPARTMENT DOORS
- FWD AND AFT FIRE WALLS
- SIDE FIRE WALLS
- UPPER FIRE WALL
2-49 491600-01-1 310 DET AIR INTAKE SYSTEM AF MRB 9 MRB 49.16.00/02-36 491600-210-001 40 MO N/A
DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER
ELBOW, SEALS AND FELT METAL
2-49 491600-02-1 210 OPC AIR INTAKE SYSTEM AF MRB 9 MRB 49.16.00/03-36 491600-710-001 48 MO N/A
OPERATIONAL CHECK OF AIR INTAKE FLAP AND DIVERTER
2-49 491600-A1-1 310 DET AIR INTAKE SYSTEM EN MRB 9 MRB 49.16.00/03-32 491600-210-002 40 MO N/A
DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER
ELBOW, SEALS AND FELT METAL
2-49 491600-A2-1 310 OPC AIR INTAKE SYSTEM EN MRB 9 MRB 49.16.00/04-32 491600-710-002 48 MO N/A
OPERATIONAL CHECK OF AIR INTAKE FLAP AND DIVERTER
2-49 491600-B1-1 313 DET AIR INTAKE SYSTEM EN MRB 9 MRB 49.16.00/01-13 491600-200-002 40 MO APPL
315
DETAILED INSPECTION OF APU AIR INTAKE, DIFFUSER
ELBOW, SEALS AND FELT METAL
APPENDIX A
AEG/AMP/A320 Page 63 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-49 491600-B4-1 210 OPC AIR INTAKE SYSTEM EN MRB 9 MRB 49.16.00/04-13 491600-710-003 48 MO N/A
310
315 OPERATIONAL CHECK OF AIR INTAKE FLAP AND DIVERTER
492000-01-1 ************** TASK DELETED ************** N/A
2-49 492100-A1-1 315 DIS POWER SECTION EN MRB 7 MRB 49.21.00/01-32 VSB APS-49-320150 NOTE YES N/A
316 VSB
REMOVE APU FOR IN SHOP DISCARD OF POWER SECTION
IMPELLER, FIRST-STAGE TURBINE DISK AND SECOND-STAGE
TURBINE DISK.
NOTE:
INTERVAL:
- REFER TO ROTATING COMPONENTS LIFE LIMITS AS
SPECIFIED IN VSB APS-49-320150/ENGINE MANUAL (APU
HONEYWELL 131-9A) FOR INTERVAL.
2-49 492100-B5-1 315 DIS POWER SECTION EN MRB 7 MRB 49.21.00/05-13 492100-920-007 NOTE YES APPL
317
DISCARD LIFE LIMITED PARTS OF THE APU POWER SECTION
IN ACCORDANCE WITH OEM RECOMMENDATION
NOTE:
INTERVAL:
- REFER TO ROTATING GROUP LIFE LIMITED COMPONENTS
SECTION OF ENGINE MANUAL (APU HONEYWELL 131-9A) FOR
INTERVAL.
2-49 492300-A1-1 315 DIS LOAD COMPRESSOR EN MRB 7 MRB 49.23.00/01-32 VSB APS-49-320150 NOTE YES N/A
316 VSB
REMOVE APU FOR IN SHOP DISCARD OF LOAD COMPRESSOR
IMPELLER.
NOTE:
INTERVAL:
- REFER TO ROTATING COMPONENTS LIFE LIMITS AS
SPECIFIED IN VSB APS-49-320150/ENGINE MANUAL (APU
HONEYWELL 131-9A) FOR INTERVAL.
2-49 493000-B1-1 315 DIS ENGINE FUEL AND CONTROL EN LUR MRB 49.30.00/02-13 493241-920-001 72 MO APPL
MRB 9 OR
DISCARD FUEL INLET FILTER ELEMENT 8500 FH
2-49 493100-01-1 310 VCK FUEL DISTRIBUTION EN LUR MRB 49.31.00/01-36 493211-210-001 12 MO N/A
MRB 9 OR
VISUAL CHECK OF FUEL FILTER DIFFERENTIAL PRESSURE 1500 FH
INDICATOR.
493400-01-1 ************** TASK DELETED ************** N/A
493400-A1-1 ************** TASK DELETED ************** N/A
493400-B1-1 ************** TASK DELETED ************** N/A
2-49 494000-A1-1 316 DIS IGNITION AND STARTING EN LUR MRB 49.40.00/02-32 494141-920-001 24 MO N/A
MRB 9 OR
REMOVE AND DISCARD IGNITER PLUGS 2250 FH
2-49 494000-B2-1 315 DET IGNITION AND STARTING EN LUR MRB 49.40.00/02-13 494141-220-001 72 MO APPL
MRB 7 OR
DETAILED INSPECTION OF IGNITER PLUG 6000 FH
2-49 494141-01-1 316 DET IGNITER PLUG EN LUR MRB 49.40.00/03-36 494141-220-002 72 MO N/A
MRB 7 OR
DETAILED INSPECTION OF IGNITER PLUG 6000 FH
2-49 495100-01-1 315 RST LOAD COMPRESSOR SURGE/REVERSE FLOW PROTECTION AF LUR MRB 49.51.20/02-36 495152-600-001 24 MO N/A
MRB 7 OR
CLEAN SURGE VALVE FILTER 2250 FH
2-49 498000-A4-1 310 GVI EXHAUST EN MRB 9 MRB 49.80.00/04-32 498100-200-016 36 MO N/A
GENERAL VISUAL INSPECTION OF APU COMPARTMENT EXHAUST
MUFFLER INSULATION COVERS AND BELLOWS
2-49 498000-B1-1 310 GVI EXHAUST EN MRB 9 MRB 49.80.00/01-13 498100-200-017 36 MO APPL
GENERAL VISUAL INSPECTION OF APU COMPARTMENT EXHAUST
MUFFLER INSULATION COVERS AND BELLOWS
APPENDIX A
AEG/AMP/A320 Page 64 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-49 498100-04-1 310 GVI EXHAUST SYSTEM EN MRB 9 MRB 49.80.00/04-36 498100-200-015 36 MO N/A
GENERAL VISUAL INSPECTION OF APU COMPARTMENT EXHAUST
MUFFLER INSULATION COVERS AND BELLOWS
2-49 499000-A1-1 310 DIS OIL SYSTEM EN LUR MRB 49.90.00/02-32 499141-920-001 36 MO N/A
MRB 9 OR
DISCARD PRESSURE OIL FILTER ELEMENT 3000 FH
2-49 499141-01-1 310 DIS OIL FILTER EN LUR MRB 49.91.00/02-36 499145-200-002 12 MO N/A
MRB 9 OR
DISCARD LUBE AND ALTERNATOR SCAVENGE FILTER ELEMENTS 1500 FH
2-52 521000-01-1 831 FNC PASSENGER/CREW DOOR AF MRB 8 MRB 52.10.00/01 521000-210-004 14 DY APPL
832 Included into Weekly
841 CHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURE Checklist
842
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
2-52 521000-02-1 831 FNC PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/11 521000-720-001 36 MO APPL
832 OR
841 FUNCTIONAL CHECK OF DOOR SUSPENSION 8000 FC
842 OR
12000 FH
2-52 521000-03-1 831 DET PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/06 521000-220-006 48 MO APPL
832
841 DETAILED INSPECTION OF DOOR SEALS
842
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/
CREW DOORS.
2-52 521000-04-1 831 DET PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/12 521000-200-002 36 MO APPL
832 OR
841 DETAILED INSPECTION OF PASSENGER/CREW DOOR FOR 8000 FC
842 INTEGRITY AND GOOD ADJUSTMENT OF MECHANISMS OR
(INCLUDING GIRT BAR) 12000 FH
NOTE:
PLANNING:
- ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-05-1 831 FNC PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/13 521000-720-003 80 MO APPL
832 OR
841 FUNCTIONAL CHECK OF LOCKING MECHANISM 10000 FC
842 OR
15000 FH
2-52 521000-06-1 831 FNC PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/13 521000-720-005 80 MO APPL
832 OR
841 FUNCTIONAL CHECK OF ESCAPE SLIDE RELEASE MECHANISM 10000 FC
842 OR
NOTE: 15000 FH
PLANNING:
- ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-07-1 831 FNC PASSENGER/CREW DOOR AF LUR MRB 52.10.00/02 521000-200-001 216 MO APPL
832 MRB 6,9 OR
841 FUNCTIONAL CHECK OF DOOR STOPS ADJUSTMENT 16000 FC
842 OR
24000 FH
2-52 521000-07-2 831 FNC PASSENGER/CREW DOOR AF MRB 6,9 MRB 52.10.00/15 521000-200-001 80 MO N/A
832
841 FUNCTIONAL CHECK OF DOOR STOPS ADJUSTMENT
842
APPENDIX A
AEG/AMP/A320 Page 65 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-52 521000-08-1 831 OPC PASSENGER/CREW DOOR AF MRB 9 MRB 52.10.00/14 521000-710-002 80 MO APPL
832 OR
841 OPERATIONAL CHECK OF INTERLOCK MECHANISM TO ENSURE 16000 FC
842 THAT EMERGENCY ESCAPE HANDLE STAYS IN DISARMED OR
POSITION WHEN DOOR IS UP AND OUTSIDE OF FRAME 24000 FH
NOTE:
ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-09-1 831 FNC PASSENGER/CREW DOOR AF LUR MRB 52.10.00/02 521000-720-004 216 MO APPL
832 MRB 6,9 OR
841 FUNCTIONAL CHECK OF MECHANICAL LOCKING INDICATION 16000 FC
842 OR
24000 FH
2-52 521000-09-2 831 FNC PASSENGER/CREW DOOR AF MRB 6,9 MRB 52.10.00/15 521000-720-004 80 MO N/A
832
841 FUNCTIONAL CHECK OF MECHANICAL LOCKING INDICATION
842
2-52 521000-10-1 831 OPC PASSENGER/CREW DOOR AF MRB 9 MRB 52.10.00/14 521000-710-001 80 MO APPL
832 OR
841 OPERATIONAL CHECK OF DAMPING DURING OPENING/CLOSING 16000 FC
842 OR
NOTE: 24000 FH
PLANNING:
- ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-11-1 831 OPC PASSENGER/CREW DOOR AF MRB 9 MRB 52.10.00/14 521000-710-003 80 MO APPL
832 OR
841 OPERATIONAL CHECK OF STRIKER MECHANISM 16000 FC
842 OR
NOTE: 24000 FH
PLANNING:
- ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-12-1 831 OPC PASSENGER/CREW DOOR AF MRB 9 MRB 52.10.00/14 521000-720-002 80 MO APPL
832 OR
841 OPERATIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 16000 FC
842 IS OPENED FROM THE OUTSIDE OR
24000 FH
NOTE:
PLANNING:
- ONLY FWD DOORS FOR POST 37807 (IF AFT DOORS FULLY
DEACTIVATED).
2-52 521000-14-1 831 LUB PASSENGER/CREW DOOR AF MRB 9 MRB 52.10.00/05 122252-640-016 24 MO APPL
832
841 LUBRICATION OF HINGE ARM SUPPORT FITTING BEARINGS
842
NOTE:
PLANNING:
- TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/
CREW DOORS
2-52 521000-17-1 832 DET PASSENGER/CREW DOOR AF MRB 6 MRB 52.10.00/10 521000-220-009 80 MO N/A
842
DETAILED INSPECTION OF AFT DOOR SEALS
NOTE:
PLANNING:
- TASK IS ONLY APPLICABLE FOR DEACTIVATED PASSENGER/
CREW DOORS.
2-52 521000-18-1 831 FNC PASSENGER/CREW DOOR AF LUR MRB 52.10.00/02 521000-720-802 216 MO APPL
832 MRB 6,9 OR
841 FUNCTIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR 16000 FC
842 IS OPENED FROM OUTSIDE. OR
24000 FH
2-52 521000-19-1 831 FNC PASSENGER/CREW DOOR AF MRB 6,9 MRB 52.10.00/15 521000-720-803 80 MO N/A
841
FUNCTIONAL CHECK OF ESCAPE SLIDE DISARMING WHEN DOOR
IS OPENED FROM OUTSIDE.
APPENDIX A
AEG/AMP/A320 Page 66 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-52 521101-01-1 831 DET FWD PAX/CREW DOOR STOP ASSEMBLIES AF MRB CPCP MRB 521101-01-1 521100-200-001 12 YE 12 YE APPL
841
DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON
FORWARD PASSENGER/CREW DOOR, LH/RH
3-52 521103-01-1 831 GVI FWD PAX/CREW DOOR SKIN EXTERNAL SURFACE AF ALI ALI 521103-01-1 521100-210-002 27400 FC 27400 FC APPL
841
GENERAL VISUAL INSPECTION OF FORWARD PASSENGER/CREW
DOOR SKIN, EXTERNAL SURFACE, LH/RH
3-52 521104-01-1 831 DET FWD PAX/CREW DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 521104-01-1 521100-200-002 12 YE 6 YE APPL
841
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR,
INTERNAL STRUCTURE, LH/RH
3-52 521104-02-2 831 SDI FWD PAX/CREW DOOR INTERNAL STRUCTURE NDT MRB CPCP MRB 521104-02-2 521100-250-001 12 YE 6 YE N/A
841
SPECIAL DETAILED INSPECTION (LFEC) OF FORWARD
PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH.
NOTE:
TASK 521104-02-2 NEED TO BE PERFORMED AT SAME TIME AS
TASK 521104-01-1
2-52 521121-01-1 831 LUB PASSENGER / CREW DOOR AF MRB 6 MRB 52.10.00/03 122252-640-006 24 MO APPL
832
841 LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPIC
842 ARM
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
2-52 521121-02-1 831 LUB PASSENGER / CREW DOOR AF MRB 6 MRB 52.10.00/04 122252-640-014 36 MO APPL
832
841 LUBRICATION OF SAFETY PIN GUIDE FITTING AND DOOR
842 ARMING/DISARMING MECHANISM
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
3-52 521301-01-1 832 DET AFT PAX/CREW DOOR STOP ASSEMBLIES AF MRB CPCP MRB 521301-01-1 521300-200-001 12 YE 12 YE APPL
842
DETAILED INSPECTION OF DOOR STOP ASSEMBLIES ON AFT
PASSENGER/CREW DOOR, LH/RH
3-52 521303-01-1 832 GVI AFT PAX/CREW DOOR SKIN EXTERNAL SURFACE AF ALI ALI 521303-01-1 521300-210-002 27400 FC 27400 FC APPL
842
GENERAL VISUAL INSPECTION OF AFT PASSENGER/CREW DOOR
SKIN, EXTERNAL SURFACE, LH/RH
3-52 521304-01-1 832 DET AFT PAX/CREW DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 521304-01-1 521300-200-002 12 YE 6 YE APPL
842
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR,
INTERNAL STRUCTURE, LH/RH
3-52 521304-02-2 832 SDI AFT PAX/CREW DOOR INTERNAL STRUCTURE NDT MRB CPCP MRB 521304-02-2 521300-250-001 12 YE 6 YE N/A
842
SPECIAL DETAILED INSPECTION (LFEC) OF AFT
PASSENGER/CREW DOOR, INTERNAL STRUCTURE, LH/RH.
NOTE:
TASK 521304-02-2 NEED TO BE PERFORMED AT SAME TIME AS
TASK 521304-01-1
2-52 522100-01-1 151 OPC PASSENGER COMPARTMENT EMERGENCY EXIT AF LUR MRB 52.21.00/01 522100-710-003 108 MO APPL
152 MRB 8 OR
241 OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM 12000 FH
242 INSIDE IN ARMED MODE.
833
834
843
844
APPENDIX A
AEG/AMP/A320 Page 67 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-52 522100-02-5 151 FNC PASSENGER COMPARTMENT EMERGENCY EXIT AF LUR MRB 52.21.00/04 522100-720-001 180 MO APPL
152 MRB 8 OR
241 FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE 24000 FH
242 RELEASE SIGNAL.
833
834
843
844
2-52 522100-07-5 151 OPC PASSENGER COMPARTMENT EMERGENCY EXIT AF LUR MRB 52.21.00/04 522100-710-004 180 MO APPL
152 MRB 8 OR
241 OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM 24000 FH
242 OUTSIDE IN ARMED MODE.
833
834
843
844
2-52 522100-08-1 151 OPC PASSENGER COMPARTMENT EMERGENCY EXIT AF LUR MRB 52.21.00/03 522100-710-005 180 MO APPL
152 MRB 9 OR
241 - OPERATIONAL CHECK OF UNLOCKING AND OPENING FROM 24000 FH
242 INSIDE AND OUTSIDE IN DISARMED POSITION
833 - OPERATIONAL CHECK OF CLOSING AND LOCKING FROM
834 INSIDE
843 - OPERATIONAL CHECK OF ESCAPE SLIDE ARMING AND
844 DISARMING.
2-52 522101-01-1 833 OPC AUTOMATIC OVERWING EMERGENCY EXIT DOOR AF CMR* CMR 522101-00001-1-C 522200-710-803 36 MO N/A
834 MRB 8 MRB 52.21.01/01 OR
843 OPERATIONAL CHECK OF EMERGENCY OVERWING DOOR 16300 FH
844 MECHANISMS
2-52 522101-02-1 833 OPC AUTOMATIC OVERWING EMERGENCY EXIT DOOR AF CMR* CMR 522101-00002-1-C 522200-710-802 36 MO N/A
834 MRB 8 MRB 52.21.01/02 OR
843 OPERATIONAL CHECK OF ESCAPE SLIDE RELEASE MECHANISM 23800 FH
844
2-52 522101-02-2 833 OPC AUTOMATIC OVERWING EMERGENCY EXIT DOOR AF MRB 8 MRB 52.21.01/02 522200-710-802 36 MO N/A
834
843 OPERATIONAL CHECK OF ESCAPE SLIDE RELEASE MECHANISM
844
2-52 522101-03-1 833 FNC AUTOMATIC OVERWING EMERGENCY EXIT DOOR AF CMR* CMR 522101-00003-1-C 522200-720-802 36 MO N/A
834 MRB 6 MRB 52.21.01/03 OR
843 FUNCTIONAL CHECK OF FLIGHT LOCK MECHANISM 23800 FH
844
2-52 522101-04-1 833 FNC AUTOMATIC OVERWING EMERGENCY EXIT DOOR AF CMR* CMR 522101-00004-1-C 23800 FH N/A
834
843 FUNCTIONAL CHECK OF MANUAL AND AUTOMATIC SLIDE
844 RELEASE SIGNAL
3-52 522102-01-1 833 DET EMERGENCY EXITS STRUCTURE AF ALI ALI 522102-01-1 522100-200-001 12 YE 6 YE APPL
834 MRB CPCP MRB 522102-01-1 OR OR
843 DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL 39300 FC 11400 FC
844 STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
3-52 522102-01-2 834 DET EMERGENCY EXITS STRUCTURE AF ALI ALI 522102-01-2 522100-200-001 12 YE 6 YE N/A
844 MRB CPCP MRB 522102-01-2 OR OR
DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL 39300 FC 11400 FC
STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
3-52 522102-01-4 834 DET EMERGENCY EXITS STRUCTURE AF MRB CPCP MRB 522102-01-2 522100-200-001 12 YE 6 YE N/A
844
DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL
STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
3-52 522102-01-5 833 DET EMERGENCY EXITS STRUCTURE AF MRB CPCP MRB 522102-01-1 522100-200-001 12 YE 6 YE N/A
834
843 DETAILED INSPECTION OF EMERGENCY EXITS, INTERNAL
844 STRUCTURE AND LOAD TRANSMITTING PROFILE, LH/RH
522102-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 68 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-52 522200-01-1 833 FNC PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF LUR MRB 52.22.00/01 522200-710-001 72 MO N/A
834 MRB 8 OR
843 OPERATIONAL CHECK 8000 FH
844 - OF DOOR LOCKING/UNLOCKING AND DOOR OPENING/CLOSING
FROM INSIDE AND OUTSIDE AND DOOR LATCHING AND
UNLATCHING,
- TO ENSURE THAT DOOR CANNOT BE LOWERED AND LOCKED
WHEN OPEN,
- OF DOOR DAMPING MECHANISM,
- OF ESCAPE SLIDE DISARMING WHEN DOOR IS OPENED FROM
OUTSIDE,
- TO ENSURE THAT ESCAPE SLIDE ARMING LEVER IS LOCKED
IN "DISARMED" POSITION WHEN DOOR IS OPEN, AND
FUNCTIONAL CHECK
- OF LOCKING MECHANISM, HAND FORCE
2-52 522200-02-1 833 FNC PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF LUR MRB 52.22.00/02 522200-720-001 108 MO N/A
834 MRB 8 OR
843 OPERATIONAL CHECK 12000 FH
844 - OF DOOR UNLOCKING FROM INSIDE AND OUTSIDE IN
"ARMED" POSITION,
- OF ESCAPE SLIDE RELEASE MECHANISM
ARMING/DISARMING, AND FUNCTIONAL CHECK
- OF SLIDE RELEASE CABLE MOVEMENT
2-52 522200-03-1 833 LUB PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF MRB 8 MRB 52.22.00/03 122252-640-013 24 MO N/A
834
843 LUBRICATION OF EXTERIOR CONTROL HANDLE AND TELESCOPIC
844 ARM
2-52 522200-04-1 833 DET PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF LUR MRB 52.22.00/04 522211-200-004 72 MO N/A
834 MRB 8 OR
843 DETAILED INSPECTION OF CYLINDER ASSEMBLY 8000 FH
844
2-52 522200-08-1 833 VCK PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF MRB 8 MRB 52.22.00/06 522200-200-001 8 DY N/A
834 Included into Weekly
843 CHECK EMERGENCY CYLINDER/ACCUMULATOR PRESSURE ON Checklist
844 PRESSURE GAUGE
2-52 522200-10-1 833 VCK PASSENGER COMPARTMENT EMERGENCY EXIT DOOR AF MRB 9 MRB 52.22.00/07 522200-210-801 72 MO N/A
834
835 VISUAL CHECK OF DOOR SEAL
843
844
845
3-52 522202-01-1 833 DET FWD EMERGENCY EXISTS INTERNAL STRUCTURE AF MRB CPCP MRB 522202-01-1 522211-200-001 12 YE 6 YE N/A
843
DETAILED INSPECTION OF FORWARD EMERGENCY EXITS,
INTERNAL STRUCTURE, LH/RH
3-52 522203-01-1 833 GVI FWD EMERGENCY EXIT DOORS STOP ASSEMBLIES AF MRB MRB 522203-01-1 522211-200-006 24000 FC 4500 FC N/A
843
GENERAL VISUAL INSPECTION OF DOOR STOP ASSEMBLIES AND
LOCKING HOOK ON FORWARD EMERGENCY EXIT DOORS, LH/RH
3-52 522205-01-1 834 DET AFT EMERGENCY EXITS INTERNAL AF MRB CPCP MRB 522205-01-1 522211-200-002 12 YE 6 YE N/A
844
DETAILED INSPECTION OF AFT EMERGENCY EXITS, INTERNAL
STRUCTURE, LH/RH
3-52 522205-01-2 835 DET AFT EMERGENCY EXITS INTERNAL AF MRB CPCP MRB 522205-01-2 522211-200-002 12 YE 6 YE N/A
845
DETAILED INSPECTION OF AFT EMERGENCY EXITS, INTERNAL
STRUCTURE, LH/RH
3-52 522206-01-1 834 GVI AFT EMERGENCY EXIT DOORS STOP ASSEMBLIES AF MRB MRB 522206-01-1 522211-200-008 24000 FC 4500 FC N/A
844
GENERAL VISUAL INSPECTION OF DOOR STOP ASSEMBLIES AND
LOCKING HOOK ON AFT EMERGENCY EXIT DOORS, LH/RH
3-52 522206-01-2 835 GVI AFT EMERGENCY EXIT DOORS STOP ASSEMBLIES AF MRB MRB 522206-01-2 522211-200-008 24000 FC 4500 FC N/A
845
GENERAL VISUAL INSPECTION OF DOOR STOP ASSEMBLIES AND
LOCKING HOOK ON AFT EMERGENCY EXIT DOORS, LH/RH
2-52 523000-01-1 825 LUB CARGO COMPARTMENT DOOR, FWD AND AFT AF MRB 6,9 MRB 52.31.00/01 122252-640-002 24 MO APPL
826 OR
LUBRICATION OF CARGO DOOR 5000 FC
APPENDIX A
AEG/AMP/A320 Page 69 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-52 523000-03-1 825 LUB CARGO COMPARTMENT DOOR AF MRB 6,9 MRB 52.31.00/01 122252-640-009 24 MO APPL
826 OR
LUBRICATION OF EXTERIOR CARGO DOOR HANDLE 5000 FC
NOTE:
INTERVAL MAY NEED TO BE MORE FREQUENT WHEN OPERATING
IN HOSTILE ENVIRONMENTS
2-52 523100-01-1 825 FNC FORWARD CARGO COMPARTMENT DOOR AF MRB 6,9 MRB 52.31.00/02 523100-720-001 72 MO APPL
OR
FUNCTIONAL CHECK OF FORWARD CARGO COMPARTMENT DOOR, 18000 FC
COMPRISING FUNCTIONAL CHECKS OF:
- LOCKING MECHANISM
- INTERLOCK MECHANISM
- DRIFT PIN MECHANISM
- SAFETY MECHANISM
3-52 523103-01-1 825 DET FWD CARGO DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 523103-01-1 523111-200-001 12 YE 6 YE APPL
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, INTERNAL STRUCTURE
3-52 523106-01-1 825 SDI FWD CARGO DOOR UNDER HINGE FITTINGS NDT ALI WFD ALI 523106-01-1 523111-200-006 24 YE 12 YE N/A
MRB CPCP MRB 523106-01-1 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF FORWARD CARGO 48000 FC 13000 FC
COMPARTMENT DOOR SKIN, UNDERNEATH HINGE FITTINGS AT
SELECTED BOLT HOLES
3-52 523108-01-1 825 DET FWD CARGO DOOR FITTINGS EXTERNAL AREA AF ALI ALI 523108-01-1 523111-200-004 12 YE 12 YE APPL
MRB CPCP MRB 523108-01-1 OR OR
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT 51200 FC 14500 FC
DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
3-52 523108-01-3 825 DET FWD CARGO DOOR FITTINGS EXTERNAL AREA AF MRB CPCP MRB 523108-01-1 523111-200-004 12 YE 12 YE N/A
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
3-52 523109-01-1 825 DET FWD CARGO DOOR LOCKING HOOKS AF MRB CPCP MRB 523109-01-1 523111-200-005 12 YE 6 YE APPL
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL
FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523109-02-2 825 GVI FWD CARGO DOOR LOCKING HOOKS AF ALI ALI 523109-02-2 523111-200-013 10000 FC 10000 FC N/A
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL
FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523113-01-1 826 DET AFT CARGO DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 523113-01-1 523211-200-001 12 YE 6 YE APPL
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
3-52 523116-01-1 826 SDI AFT CARGO DOOR UNDER HINGE FITTINGS NDT ALI WFD ALI 523116-01-1 523211-200-003 24 YE 12 YE N/A
MRB CPCP MRB 523116-01-1 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF AFT CARGO 48000 FC 13000 FC
COMPARTMENT DOOR SKIN UNDERNEATH HINGE FITTINGS AT
SELECTED BOLT HOLES
3-52 523118-01-2 826 DET AFT CARGO DOOR FITTINGS EXTERNAL AREA AF ALI ALI 523118-01-2 523211-200-005 12 YE 12 YE APPL
MRB CPCP MRB 523118-01-2 OR OR
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR, 51200 FC 14500 FC
HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
APPENDIX A
AEG/AMP/A320 Page 70 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-52 523119-01-2 826 DET AFT CARGO DOOR LOCKING HOOKS AF MRB CPCP MRB 523119-01-2 523211-200-006 12 YE 6 YE APPL
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523119-02-2 826 GVI AFT CARGO DOOR LOCKING HOOKS AF MRB MRB 523119-02-2 523211-200-012 10300 FC 10300 FC APPL
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523123-01-1 825 DET FWD CARGO DOOR INTERNAL AF MRB CPCP MRB 523123-01-1 523111-200-019 12 YE 6 YE N/A
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, INTERNAL STRUCTURE
523127-01-1 ************** TASK DELETED ************** N/A
3-52 523128-01-1 825 DET FWD CARGO DOOR HINGE FITTINGS AND ATTACHMENT AREA AF MRB CPCP MRB 523128-01-1 523111-200-020 12 YE 12 YE N/A
EXTERNAL
DETAILED INSPECTION OF FORWARD CARGO COMPARTMENT
DOOR, HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
523128-01-2 ************** TASK DELETED ************** N/A
3-52 523129-01-1 825 DET FWD CARGO DOOR LOCKING HOOKS AND FORK FITTINGS AF MRB CPCP MRB 523129-01-1 523111-200-021 12 YE 6 YE N/A
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF FORWARD CARGO COMPARTMENT DOOR AT ALL
FRAMES, BETWEEN LONGERON 4 AND LONGERON 5 (4 PLACES)
523129-01-2 ************** TASK DELETED ************** N/A
2-52 523200-01-1 826 FNC AFT CARGO COMPARTMENT DOOR AF MRB 6,9 MRB 52.31.00/02 523200-720-001 72 MO APPL
OR
FUNCTIONAL CHECK OF AFT CARGO COMPARTMENT DOOR, 18000 FC
COMPRISING FUNCTIONAL CHECKS OF:
- LOCKING MECHANISM
- INTERLOCK MECHANISM
- DRIFT PIN MECHANISM
- SAFETY MECHANISM
3-52 523213-01-1 826 DET AFT CARGO DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 523213-01-1 523211-200-007 12 YE 6 YE N/A
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
3-52 523218-01-1 826 DET AFT CARGO DOOR FITTINGS EXTERNAL AREA AF MRB CPCP MRB 523218-01-1 523211-200-008 12 YE 12 YE N/A
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR
HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL.
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTING
3-52 523219-01-1 826 DET AFT CARGO DOOR FITTINGS EXTERNAL AREA AF MRB CPCP MRB 523219-01-1 523211-200-009 12 YE 6 YE N/A
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523219-02-2 826 GVI AFT CARGO DOOR LOCKING HOOKS AND FORK FITTINGS AF ALI ALI 523219-02-2 523211-200-015 10000 FC 10000 FC N/A
GENERAL VISUAL INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (6 PLACES)
3-52 523223-01-1 826 DET AFT CARGO DOOR INTERNAL AF MRB CPCP MRB 523223-01-1 523211-200-019 12 YE 6 YE N/A
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
523227-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 71 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-52 523228-01-1 826 DET AFT CARGO DOOR HINGE FITTINGS AND ATTACHMENT AREA AF MRB CPCP MRB 523228-01-1 523211-200-020 12 YE 12 YE N/A
DETAILED INSPECTION OF AFT CARGO COMPARTMENT DOOR
HINGE FITTINGS AND ATTACHMENT AREA, EXTERNAL
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTING
523228-01-2 ************** TASK DELETED ************** N/A
3-52 523229-01-1 826 DET AFT CARGO DOOR LOCKING HOOKS AND FORK FITTINGS AF MRB CPCP MRB 523229-01-1 523211-200-021 12 YE 6 YE N/A
DETAILED INSPECTION OF LOCKING HOOKS AND FORK
FITTINGS OF AFT CARGO COMPARTMENT DOOR AT ALL FRAMES,
BETWEEN LONGERON 4 AND LONGERON 5 (4 PLACES)
523229-01-2 ************** TASK DELETED ************** N/A
2-52 523300-01-1 827 LUB BULK CARGO COMPARTMENT DOOR AF MRB 6,9 MRB 52.33.00/01 122252-640-007 24 MO APPL
OR
LUBRICATION OF BULK CARGO COMPARTMENT DOOR HANDLE AND 5000 FC
HINGE ARM BEARINGS
3-52 523303-01-1 827 DET BULK CARGO DOOR INTERNAL AF MRB CPCP MRB 523303-01-1 523311-200-003 12 YE 6 YE APPL
DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR,
INTERNAL STRUCTURE
3-52 523305-01-1 827 DET BULK CARGO DOOR FITTINGS AREA AF MRB CPCP MRB 523305-01-1 523311-200-002 12 YE 12 YE APPL
DETAILED INSPECTION OF BULK CARGO COMPARTMENT DOOR
STOP FITTINGS AND ATTACHMENT AREA, EXTERNAL AND
INTERNAL
2-52 523500-01-1 100 OPC CARGO COMPARTMENT DOOR - ELECTRICAL CONTROL SYSTEM AF MRB 9 MRB 52.35.00/01 523500-710-001 72 MO APPL
AND HYDRAULIC SYSTEM OR
10000 FC
OPERATIONAL CHECK OF DOOR CLOSING INHIBITION BY DOOR
SILL LATCH SWITCH
2-52 523500-02-1 100 OPC CARGO COMPARTMENT DOOR - ELECTRICAL CONTROL SYSTEM AF MRB 9 MRB 52.35.00/01 523500-710-005 72 MO N/A
AND HYDRAULIC SYSTEM MRB 52.35.00/02 OR
10000 FC
OPERATIONAL CHECK OF FWD DOOR CLOSING INHIBITION BY
DOOR SILL LATCH SWITCH OPERATIONAL CHECK OF AFT CARGO
DOOR CLOSING INHIBITION BY ARO SWITCH, XZ-LATCH
PROXIMITY SENSORS AND ENTRANCE GUIDE PROXIMITY SENSOR
2-52 523500-03-1 100 OPC CARGO COMPARTMENT DOOR - ELECTRICAL CONTROL SYSTEM AF MRB 9 MRB 52.35.00/01 523500-710-004 72 MO N/A
AND HYDRAULIC SYSTEM MRB 52.35.00/02 OR
MRB 52.35.00/03 10000 FC
OPERATIONAL CHECK OF FWD DOOR CLOSING INHIBITION BY
DOOR SILL LATCH SWITCH OPERATIONAL CHECK OF AFT CARGO
DOOR CLOSING INHIBITION BY ARO SWITCH, XZ-LATCH
PROXIMITY SENSORS AND DOOR SILL ROLLER SWITCH
2-52 524100-01-1 811 DET ACCESS DOORS AF MRB 9 MRB 52.41.00/01 524100-210-001 72 MO APPL
812
822 DETAILED INSPECTION OF DOOR SEALS
824
2-52 524100-02-1 811 LUB ACCESS DOORS AF MRB 9 MRB 52.41.00/02 122252-640-008 36 MO APPL
812
822 LUBRICATION OF EXTERIOR AVIONIC COMPARTMENT DOOR
824 HANDLE
3-52 524111-01-1 811 DET FWD AVIONIC DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 524111-01-1 524111-200-001 12 YE 12 YE APPL
DETAILED INSPECTION OF FORWARD AVIONICS COMPARTMENT
ACCESS DOOR, INTERNAL STRUCTURE, INCLUDING HINGE ARMS
3-52 524121-01-1 824 DET AFT AVIONIC DOOR INTERNAL STRUCTURE AF MRB CPCP MRB 524121-01-1 524114-200-001 12 YE 6 YE APPL
DETAILED INSPECTION OF AFT AVIONICS COMPARTMENT
ACCESS DOOR, INTERNAL STRUCTURE
3-52 524131-01-1 822 DET LATERAL RIGHT AVIONIC DOOR AF MRB CPCP MRB 524131-01-1 524113-200-001 12 YE 6 YE APPL
DETAILED INSPECTION OF LATERAL RIGHT AVIONICS
COMPARTMENT ACCESS DOOR, INTERNAL STRUCTURE
APPENDIX A
AEG/AMP/A320 Page 72 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-52 524141-01-1 812 DET LATERAL LEFT AVIONIC DOOR AF MRB CPCP MRB 524141-01-1 524112-200-001 12 YE 6 YE APPL
DETAILED INSPECTION OF LATERAL LEFT AVIONICS
COMPARTMENT ACCESS DOOR, INTERNAL STRUCTURE
2-52 525111-01-1 220 DET COCKPIT DOOR AF LUR MRB 52.51.11/01 525100-220-001 180 MO APPL
MRB 6,9 OR
DETAILED INSPECTION OF MECHANICAL PARTS OF DOOR 24000 FH
LOCKING SYSTEMS
2-52 525111-02-1 220 OPC COCKPIT DOOR AF MRB 9 MRB 52.51.11/02 525100-720-002 72 MO APPL
OR
OPERATIONAL CHECK OF ALL PRESSURE SENSING CHANNELS 24000 FH
FOR RAPID DECOMPRESSION.
2-52 525111-03-1 220 OPC COCKPIT DOOR AF LUR MRB 52.51.11/03 525100-710-009 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF MANUAL SWITCH OVER 15000 FH
2-52 525111-04-1 220 OPC COCKPIT DOOR AF MRB 9 MRB 52.51.11/02 525100-710-005 72 MO APPL
OR
OPERATIONAL CHECK OF DOOR OPENING IN CASE OF POWER 24000 FH
OFF.
2-52 525111-05-1 220 OPC COCKPIT DOOR AF MRB 9 MRB 52.51.11/02 525100-710-006 72 MO APPL
OR
OPERATIONAL CHECK OF DOOR OPENING BY USING THE 24000 FH
EMERGENCY CODE.
2-52 525111-06-2 220 FNC COCKPIT DOOR AF MRB 6 MRB 52.51.11/06 525100-720-003 6 MO APPL
OR
FUNCTIONAL CHECK OF THE CORRECT ADJUSTMENT OF THE 2000 FH
COCKPIT DOOR, ELECTRICAL RELEASE STRIKES AND LATCH
MECHANISM
2-52 525111-07-1 220 OPC COCKPIT DOOR AF LUR MRB 52.51.11/04 525100-710-008 108 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF DEADBOLT 15000 FH
2-52 525111-08-1 220 OPC COCKPIT DOOR AF MRB 9 MRB 52.51.11/05 525100-710-010 108 MO APPL
OPERATIONAL CHECK OF MANUAL RELEASE OF PIP-PINS
2-52 526000-01-1 210 OPC ENTRANCE STAIRS AF LUR MRB 52.60.00/01 526100-710-001 72 MO N/A
MRB 9 OR
OPERATIONAL CHECK OF STAIRS DEPLOYMENT INHIBITION 5500 FH
CIRCUIT
2-52 526000-02-1 221 OPC ENTRANCE STAIRS AF MRB 9 MRB 52.60.00/02 526100-710-002 60 MO N/A
OPERATIONAL CHECK OF MANUAL RELEASE MECHANISM
2-52 526000-03-1 813 DET ENTRANCE STAIRS AF LUR MRB 52.60.00/03 526100-210-001 216 MO N/A
MRB 6 OR
DETAILED INSPECTION OF LOCKING MECHANISM 18000 FC
OR
22000 FH
2-52 526000-04-1 129 FNC ENTRANCE STAIRS AF MRB 6 MRB 52.60.00/04 526100-210-002 60 MO N/A
OR
CHECK OF CABLES FOR PRELOAD AND CONDITION 18000 FC
2-52 526000-05-1 129 GVI ENTRANCE STAIRS AF LUR MRB 52.60.00/05 526100-200-004 216 MO N/A
MRB 9 OR
GENERAL VISUAL INSPECTION OF CARRIER 18000 FC
OR
22000 FH
3-52 526101-01-1 813 DET ENTRANCE STAIRS DOOR AF MRB CPCP MRB 526101-01-1 526100-200-003 6 YE 6 YE N/A
DETAILED INSPECTION OF ENTRANCE STAIRS DOOR, INTERNAL
STRUCTURE
3-52 526102-01-1 813 DET ENTRANCE STAIRS DOOR SKIN AF ALI ALI 526102-01-1 526100-200-002 44100 FC 44100 FC N/A
DETAILED INSPECTION OF ENTRANCE STAIRS DOOR SKIN,
EXTERNAL SURFACE
2-52 526112-01-1 129 LUB ENTRANCE STAIRS AF MRB 6 MRB 52.60.00/06 526100-610-001 15 MO N/A
LUBRICATION OF ENTRANCE STAIRS DOOR SLIDES MECHANISM
END OF ROD
APPENDIX A
AEG/AMP/A320 Page 73 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-52 526112-01-2 129 LUB ENTRANCE STAIRS AF MRB 6,9 MRB 52.60.00/07 526100-610-001 60 MO N/A
LUBRICATION OF ENTRANCE STAIRS DOOR SLIDES MECHANISM
END OF ROD
2-52 527100-01-1 210 OPC DOOR WARNING EL MRB 9 MRB 52.71.00/01 527100-710-001 40 MO APPL
OR
OPERATIONAL CHECK OF DOOR WARNING SYSTEM 7500 FH
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS / EMERGENCY EXITS
2-52 527100-02-1 831 LUB DOOR WARNING AF MRB 9 MRB 52.71.00/02 122252-640-005 18 MO APPL
832
841 LUBRICATION OF DOOR WARNING PROXIMITY SWITCH
842 ACTUATING MECHANISM
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
2-52 527100-03-1 210 OPC DOOR WARNING EL MRB 9 MRB 52.71.00/03 527100-710-802 80 MO N/A
OPERATIONAL CHECK OF DOOR WARNING SYSTEM FOR AFT
PASSENGER/CREW DOORS
2-52 527300-01-1 210 OPC EMERGENCY ESCAPE SLIDE RELEASE AND OVERPRESSURE EL MRB 9 MRB 52.73.00/01 527300-710-003 40 MO APPL
WARNING SYSTEMS OR
7500 FH
OPERATIONAL CHECK OF EMERGENCY ESCAPE SLIDE RELEASE
WARNING
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS / EMERGENCY EXITS
2-52 527300-02-1 122 FNC EMERGENCY ESCAPE SLIDE RELEASE AND OVERPRESSURE AF MRB 9 MRB 52.73.00/02 527300-720-003 80 MO APPL
WARNING SYSTEMS OR
18000 FC
OPERATIONAL CHECK OF RESIDUAL CABIN PRESSURE WARNING
AND FUNCTIONAL CHECK OF DIFFERENTIAL PRESSURE SWITCH
NOTE:
TASK IS NOT APPLICABLE FOR DEACTIVATED PASSENGER/CREW
DOORS
3-52 528101-01-1 734 DET MLG DOOR FWD AND AFT FITTING AF MRB CPCP MRB 528101-01-1 528100-200-001 6 YE 6 YE N/A
744
DETAILED INSPECTION OF MLG DOOR, FORWARD AND AFT
FITTINGS, LH/RH
3-52 528103-01-1 734 DET MLG DOOR FWD, CTR AND AFT FITTING AF MRB CPCP MRB 528103-01-1 528100-200-002 6 YE 6 YE N/A
744
DETAILED INSPECTION OF MLG DOOR, FORWARD, CENTER AND
AFT FITTINGS, LH/RH
3-52 528104-01-1 734 DET MLG DOOR ACTUATOR FITTING AF MRB CPCP MRB 528104-01-1 528100-200-003 6 YE 6 YE N/A
744
DETAILED INSPECTION OF MLG DOOR, ACTUATOR FITTING,
LH/RH
3-52 528106-01-1 734 SDI MAIN GEAR DOORS NDT MRB MRB 528106-01-1 528100-280-801 48000 FC 4600 FC APPL
744
SPECIAL DETAILED INSPECTION (HFEC & US) OF MLG DOOR
ACTUATOR LUGS, LH/RH
NOTE:
FOR PRE 24903 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM SB 52-1073 EMBODIMENT
APPENDIX A
AEG/AMP/A320 Page 74 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-52 528107-01-1 730 DET MAIN GEAR DOORS AF ALI ALI 528107-01-1 528100-220-803 48000 FC 4400 FC APPL
740 NOTE
DETAILED INSPECTION OF MLG DOOR FWD FITTING JOINT TO
HINGE FITTING, LH/RH
NOTE:
THRESHOLD:
- FOR PRE 24903 AIRCRAFT RETROFITTED,THRESHOLD IS TO
BE COUNTED FROM SB 52-1073 EMBODIED.
3-52 528211-01-1 713 DET NLG MAIN DOOR HINGES AF MRB CPCP MRB 528211-01-1 528200-200-001 6 YE 6 YE APPL
714
DETAILED INSPECTION OF NLG, MAIN DOOR HINGES, LH/RH
3-52 528221-01-1 715 DET NLG SECONDARY DOOR HINGES AF MRB CPCP MRB 528221-01-1 528200-200-002 6 YE 6 YE APPL
716
DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGES,
LH/RH
3-52 528223-01-1 715 DET NOSE GEAR DOORS AF MRB MRB 528223-01-1 528200-220-801 26000 FC 7500 FC APPL
716
DETAILED INSPECTION OF NLG AFT DOOR AFT FITTINGS,
LH/RH
2-53 530000-01-1 100 DET FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/03 530000-210-001 72 MO APPL
REMOVE AND DETAILED INSPECTION OF PISTON TYPE DRAIN
VALVES IN LOWER FUSELAGE SHELL
3-53 531101-01-1 221 DET FWD PAX/CREW DOOR CUT OUT AF ALI ALI 531101-01-1 531100-220-802 35900 FC 9800 FC APPL
222
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUT
OUT, INTERCOSTALS FITTINGS NO 7 BETWEEN FR 15-16 AND
FR 20-21, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531101-02-1.
3-53 531101-02-1 221 SDI FWD PAX/CREW DOOR CUT OUT NDT ALI ALI 531101-02-1 531100-200-804 35900 FC 9800 FC APPL
222
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FWD
PASSENGER/CREW DOOR CUTOUT, INTERCOSTALS FITTINGS NO
7 BETWEEN FR 15-16 AND FR 20-21, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531101-01-1.
3-53 531101-03-1 221 DET FWD PAX/CREW DOOR CUT OUT AF ALI ALI 531101-03-1 531100-220-812 33900 FC 10000 FC N/A
222
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUT
OUT, INTERCOSTALS FITTINGS NO 1 BETWEEN FR 15-16 AND
FR 20-21, LH/RH
3-53 531102-01-1 220 DET FWD PAX/CREW DOOR AF ALI ALI 531102-01-1 531100-210-001 6 YE 6 YE APPL
MRB CPCP MRB 531102-01-1 OR OR
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR 18800 FC 15300 FC
FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH
3-53 531102-01-3 220 DET FWD PAX/CREW DOOR AF ALI ALI 531102-01-3 531100-210-001 6 YE 6 YE N/A
MRB CPCP MRB 531102-01-1 OR OR
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR 13700 FC 8500 FC
FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH
3-53 531102-01-5 220 DET FWD PAX/CREW DOOR AF MRB CPCP MRB 531102-01-1 531100-210-001 6 YE 6 YE N/A
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR
FRAME, UPPER CORNERS, EXTERNAL SURFACE, LH/RH
531103-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 75 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531103-01-2 221 SDI MAIN STRUCTURE NDT ALI ALI 531103-01-2 531100-250-805 30000 FC 16800 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF FWD
PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS HOLES ON FR
16 AND FR 20 AT POSITION 1 AND 7, LH/RH.
3-53 531103-01-3 221 SDI MAIN STRUCTURE NDT ALI ALI 531103-01-3 531100-250-805 53900 FC 16800 FC N/A
222 NOTE
SPECIAL DETAILED INSPECTION (ROTO) OF FWD
PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS HOLES ON FR
16 AND FR 20 AT POSITION 1 AND 7, LH/RH.
NOTE:
THRESHOLD:
- FOR AIRCRAFT POST 158422 THRESHOLD IS TO BE COUNTED
FROM SB 53-1330 EMBODIMENT.
3-53 531105-01-1 211 DET MAIN STRUCTURE AF ALI ALI 531105-01-1 531100-220-806 21100 FC 890 FC APPL
212
DETAILED INSPECTION OF LATERAL WINDOW FRAME
STIFFENER, UPPER AREA, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531105-02-1.
3-53 531105-01-2 211 DET MAIN STRUCTURE AF ALI ALI 531105-01-2 531100-220-806 38400 FC 890 FC N/A
212
DETAILED INSPECTION OF LATERAL WINDOW FRAME
STIFFENER, UPPER AREA, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531105-02-2.
3-53 531105-02-1 211 SDI MAIN STRUCTURE NDT ALI ALI 531105-02-1 531100-220-809 21100 FC 3100 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL WINDOW
FRAME STIFFENER, UPPER AREA, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531105-01-1.
3-53 531105-02-2 211 SDI MAIN STRUCTURE NDT ALI ALI 531105-02-2 531100-220-809 38400 FC 3100 FC N/A
212
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL WINDOW
FRAME STIFFENER, UPPER AREA, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531105-01-2.
3-53 531106-01-1 221 GVI FUSELAGE SKIN AND DOOR FRAME AROUND FORWARD AF ALI ALI 531106-01-1 531100-210-820 10700 FC 10700 FC APPL
222 PASSENGER/CREW DOOR
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND DOOR
FRAME AROUND FORWARD PASSENGER/CREW DOOR, BETWEEN FR
12 AND FR 24 AND BETWEEN UPPER AND LATERAL STRINGERS,
EXCEPT SCUFF PLATE AREA, EXTERNAL SURFACE, LH/RH
3-53 531106-01-2 221 GVI FUSELAGE SKIN AND DOOR FRAME AROUND FORWARD AF ALI ALI 531106-01-2 531100-210-820 9800 FC 9800 FC N/A
222 PASSENGER/CREW DOOR
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AND DOOR
FRAME AROUND FORWARD PASSENGER/CREW DOOR, BETWEEN FR
12 AND FR 24 AND BETWEEN UPPER AND LATERAL STRINGERS,
EXCEPT SCUFF PLATE AREA, EXTERNAL SURFACE, LH/RH
531107-01-1 ************** TASK DELETED ************** N/A
3-53 531108-01-1 123 SDI MAIN STRUCTURE NDT ALI ALI 531108-01-1 531100-220-804 54600 FC 19900 FC APPL
OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF HOLES AT FWD 109200 FH 39900 FH
CORNERS OF NLG BAY, FR 9
APPENDIX A
AEG/AMP/A320 Page 76 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
531108-01-2 ************** TASK DELETED ************** N/A
3-53 531109-03-1 100 DET ENTRANCE STAIRS DOOR SURROUND AF ALI ALI 531109-03-1 531100-220-007 5200 FC 5200 FC N/A
OR OR
DETAILED INSPECTION OF ENTRANCE STAIRS DOOR SURROUND, 16600 FH 16600 FH
UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH
3-53 531109-03-2 100 DET ENTRANCE STAIRS DOOR SURROUND AF ALI ALI 531109-03-2 531100-220-007 6300 FC 6300 FC N/A
OR OR
DETAILED INSPECTION OF ENTRANCE STAIRS DOOR SURROUND, 12700 FH 12700 FH
UPPER AND LOWER CORNERS, EXTERNAL SURFACE, LH
531111-01-1 ************** TASK DELETED ************** N/A
531111-01-2 ************** TASK DELETED ************** N/A
3-53 531111-02-1 100 DET AVIONICS DOORS SURROUND AF ALI ALI 531111-02-1 13200 FC 13200 FC APPL
DETAILED INSPECTION OF AVIONICS COMPARTMENT DOORS,
SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS)
3-53 531111-02-2 100 DET AVIONICS DOORS SURROUND AF ALI ALI 531111-02-2 10400 FC 10400 FC N/A
DETAILED INSPECTION OF AVIONICS COMPARTMENT DOORS,
SURROUND CORNERS, EXTERNAL SURFACE (4 DOORS)
3-53 531112-01-1 100 DET FUSELAGE LOWER PANEL EXTERNAL SURFACE AF ALI ALI 531112-01-1 531100-210-005 19800 FC 19800 FC APPL
OR OR
DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLG 39600 FH 39600 FH
BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH
3-53 531112-01-2 100 DET FUSELAGE LOWER PANEL EXTERNAL SURFACE AF ALI ALI 531112-01-2 531100-210-005 15400 FC 15400 FC N/A
DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLG
BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH
3-53 531112-01-3 100 DET FUSELAGE LOWER PANEL EXTERNAL SURFACE AF ALI ALI 531112-01-3 531100-210-005 16300 FC 16300 FC N/A
OR OR
DETAILED INSPECTION OF FUSELAGE LOWER PANEL AT NLG 32600 FH 32600 FH
BAY AFT CORNERS, EXTERNAL SURFACE, LH/RH
3-53 531113-01-1 200 GVI FUSELAGE SKIN ATTACHMENT AF ALI ALI 531113-01-1 531100-210-818 36500 FC 6500 FC APPL
GENERAL VISUAL INSPECTION OF ATTACHMENT TO SKIN
PANEL, FR 16, STRINGER 3 LH/RH
3-53 531114-02-1 200 GVI FUSELAGE SKIN EXTERNAL SURFACE AF ALI ALI 531114-02-1 531100-210-822 5700 FC 5700 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN ABOVE
WINDSHIELD BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE,
LH/RH.
3-53 531114-02-2 200 GVI FUSELAGE SKIN EXTERNAL SURFACE AF ALI ALI 531114-02-2 531100-210-822 5700 FC 5700 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN ABOVE
WINDSHIELD BETWEEN FR 4 AND FR 12, EXTERNAL SURFACE,
LH/RH.
3-53 531117-01-1 200 GVI FUSELAGE SIDE PANEL AF ALI ALI 531117-01-1 531100-210-810 14500 FC 14500 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE SIDE PANEL,
BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12,
EXTERNAL SURFACE, LH/RH
3-53 531117-01-3 200 GVI FUSELAGE SIDE PANEL AF ALI ALI 531117-01-3 531100-210-810 14000 FC 14000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE SIDE PANEL,
BELOW COCKPIT SIDE WINDOWS, BETWEEN FR 1 AND FR 12,
EXTERNAL SURFACE, LH/RH
3-53 531118-01-1 200 GVI FUSELAGE SIDE PANEL AF ALI ALI 531118-01-1 531100-210-811 10500 FC 10500 FC APPL
GENERAL VISUAL INSPECTION OF AREA FORWARD OF
WINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4,
EXTERNAL SURFACE, LH/RH
3-53 531118-01-3 200 GVI FUSELAGE SIDE PANEL AF ALI ALI 531118-01-3 531100-210-811 9400 FC 9400 FC N/A
GENERAL VISUAL INSPECTION OF AREA FORWARD OF
WINDSHIELD, ABOVE SIDE PANEL, FROM FR 0 TO FR 4,
EXTERNAL SURFACE, LH/RH
APPENDIX A
AEG/AMP/A320 Page 77 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531119-01-1 100 DET LOWER LAP JOINT EXTERNAL SURFACE AF ALI ALI 531119-01-1 531100-210-007 48600 FC 11800 FC APPL
OR OR
DETAILED INSPECTION OF UPPER SKIN OF LOWER 97200 FH 23600 FH
LONGITUDINAL LAP JOINT, BETWEEN FR 9 AND FR 20,
EXTERNAL SURFACE, LH/RH
531119-01-3 ************** TASK DELETED ************** N/A
531119-01-4 ************** TASK DELETED ************** N/A
531120-01-1 ************** TASK DELETED ************** N/A
531121-01-1 ************** TASK DELETED ************** N/A
3-53 531123-01-1 100 DET LAT LAP JOINT FR 01-24 AF MRB CPCP MRB 531123-01-1 531100-210-010 6 YE 6 YE 24 YE 6 YE APPL
DETAILED INSPECTION OF OUTER SKIN OF LATERAL
LONGITUDINAL LAP JOINT, BETWEEN FR 1 AND FR 24, LH/RH
3-53 531124-01-1 127 DET SPLICE AT FR 20 AF ALI ALI 531124-01-1 531100-210-011 33600 FC 7900 FC APPL
128 OR OR
DETAILED INSPECTION OF FR 20 SPLICE, BETWEEN STRINGER 67200 FH 15800 FH
30 AND STRINGER 32, LH/RH
531124-01-4 ************** TASK DELETED ************** N/A
3-53 531125-02-1 211 DET NOSE FORWARD FUSELAGE AF ALI ALI 531125-02-1 531100-220-805 48000 FC 29800 FC APPL
212
DETAILED INSPECTION OF CENTRAL/LATERAL WINDOW FRAME
JUNCTION UPPER AREA AROUND FASTENER HOLE LHS/RHS
531126-01-1 ************** TASK DELETED ************** N/A
3-53 531126-01-2 211 SDI LATERAL SPLICING FR 8 NDT ALI ALI 531126-01-2 531100-220-810 25500 FC 4800 FC N/A
212 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL 51000 FH 9700 FH
SPLICING, FR 8, LH/RH
NOTE:
PLANNING:
- AFTER SB 53-1039 EMBODIMENT AIRCRAFT REMAIN IN PRE
22112 CONFIGURATION.
3-53 531126-09-1 211 SDI LATERAL SPLICING FR 8 NDT MRB FMP MRB 531126-09-1 18 YE 6 YE APPL
212 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL
SPLICING, FR 8, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-53 531127-01-1 211 SDI MAIN STRUCTURE NDT ALI ALI 531127-01-1 531100-220-807 31400 FC 7200 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL
SPLICING, FR 11, LH/RH
531127-01-2 ************** TASK DELETED ************** N/A
3-53 531127-09-2 211 SDI LATERAL SPLICING FR 11 NDT MRB FMP MRB 531127-09-2 12 YE 6 YE N/A
212 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL
SPLICING, FR 11, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 78 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531129-02-1 211 SDI WINDSHIELD CTR POST LWR ATTACHMENT NDT ALI ALI 531129-02-1 531100-220-001 36000 FC 8300 FC N/A
212
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD
CENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDE
3-53 531129-02-2 211 SDI WINDSHIELD CTR POST LWR ATTACHMENT NDT ALI ALI 531129-02-2 531100-220-001 30600 FC 8800 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD
CENTER POST, LOWER ATTACHMENT AREA, INTERNAL SIDE
3-53 531130-02-1 211 SDI NOSE FORWARD FUSELAGE NDT ALI ALI 531130-02-1 531100-220-808 48000 FC 13800 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF WINDOW FRAME AT
FR 4 LOWER FORWARD CORNERS, INTERNAL SIDE, LH/RH
3-53 531131-02-1 211 SDI NOSE FORWARD FUSELAGE NDT ALI ALI 531131-02-1 531100-200-803 31100 FC 12600 FC APPL
212
SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD
CENTER POST, 2 FASTENER HOLES, UPPER ATTACHMENT AREA,
INTERNAL, LH/RH
3-53 531133-01-1 211 DET WINDSHIELD SIDE POST LWR ATTACHMENT AF ALI ALI 531133-01-1 531100-210-014 23100 FC 1100 FC APPL
212
DETAILED INSPECTION OF WINDSHIELD SIDE POST AT FR 4,
LOWER ATTACHMENT, INTERNAL SIDE, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531133-02-1
531133-01-3 ************** TASK DELETED ************** N/A
3-53 531133-02-1 211 SDI WINDSHIELD SIDE POST LWR ATTACHMENT NDT ALI ALI 531133-02-1 531100-210-029 23100 FC 3300 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE
POST AT FR 4, LOWER ATTACHMENT, INTERNAL SIDE, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 531133-01-1
531133-02-3 ************** TASK DELETED ************** N/A
3-53 531134-01-1 211 SDI WINDSHIELD SIDE POST LOWER CORNER NDT ALI ALI 531134-01-1 531100-250-806 48000 FC 10800 FC APPL
212
SPECIAL DETAILED INSPECTION (HFEC) OF WINDSHIELD SIDE
POST AT FR4, LOWER CORNER, LH/RH
3-53 531135-01-2 211 SDI WINDSHIELD SIDE POST UPR ATTACHMENT NDT ALI ALI 531135-01-2 531100-210-026 28800 FC 11000 FC APPL
212
SPECIAL DETAILED INSPECTION (ROTO) OF WINDSHIELD SIDE
POST AT FR 4, UPPER ATTACHMENT, INTERNAL SIDE, LH/RH
531135-01-3 ************** TASK DELETED ************** N/A
3-53 531142-01-1 221 DET RAIN GUTTER AREA OVER FORWARD PAX DOOR AF ALI ALI 531142-01-1 531100-220-814 37800 FC 4500 FC APPL
222 OR OR
DETAILED INSPECTION OF RAIN GUTTER AREA OVER FORWARD 75600 FH 9100 FH
PAX DOOR, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531142-02-1.
APPENDIX A
AEG/AMP/A320 Page 79 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531142-02-1 221 SDI RAIN GUTTER AREA OVER FORWARD PAX DOOR NDT ALI ALI 531142-02-1 531100-250-807 37800 FC 37800 FC APPL
222 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF RAIN GUTTER 75600 FH 75600 FH
AREA OVER FORWARD PAX DOOR, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531142-01-1.
3-53 531151-01-1 221 DET DOOR STOP FITTINGS AF MRB CPCP MRB 531151-01-1 531100-210-017 12 YE 12 YE APPL
222
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 16
AND FR 20, LH/RH
3-53 531153-02-1 221 SDI DOOR STOPS AT FR 16 NDT ALI ALI 531153-02-1 531100-210-025 30200 FC 6800 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF DOOR FR 16, AT
DOUBLE JOGGLE AREA IN OUTER FLANGE OF FR, AT DOOR
STOPS NUMBER 1 AND 7 LOCATION, LH
3-53 531153-02-2 221 SDI DOOR STOPS AT FR 16 NDT ALI ALI 531153-02-2 531100-210-025 30200 FC 6800 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF DOOR FR 16, AT
DOUBLE JOGGLE AREA IN OUTER FLANGE OF FR, AT DOOR
STOPS NUMBER 1 AND 7 LOCATION, RH
3-53 531154-01-1 221 SDI MAIN STRUCTURE NDT ALI ALI 531154-01-1 531100-250-804 48000 FC 16800 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF FWD
PASSENGER/CREW DOOR CUTOUT, STOP FITTINGS HOLES ON FR
16 AND FR 20 AT POSITION 2 TO 6, LH/RH.
3-53 531155-02-1 221 SDI DOOR STOPS AT FR 20 NDT ALI ALI 531155-02-1 531100-210-027 31800 FC 8900 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF DOOR FR 20, AT
DOUBLE JOGGLE AREA IN OUTER FLANGE OF FRAME, AT DOOR
STOPS NUMBER 1 AND 7 LOCATION, LH
3-53 531155-02-2 221 SDI DOOR STOPS AT FR 20 NDT ALI ALI 531155-02-2 531100-210-027 31800 FC 8900 FC APPL
222
SPECIAL DETAILED INSPECTION (ROTO) OF DOOR FR 20, AT
DOUBLE JOGGLE AREA IN OUTER FLANGE OF FRAME, AT DOOR
STOPS NUMBER 1 AND 7 LOCATION, RH
3-53 531156-01-1 221 DET FUSELAGE SKIN JUNCTION TO FR 13 AND FR 14 AF ALI ALI 531156-01-1 531100-220-815 30000 FC 3100 FC APPL
222
DETAILED INSPECTION OF FUSELAGE SKIN JUNCTION TO FR
13 AND FR 14, BETWEEN Z+475 AND Z+950, EXTERNAL
SURFACE, LH/RH.
3-53 531157-01-2 127 DET CONTINUITY AND ANGLE FITTINGS AF ALI ALI 531157-01-2 531100-210-021 24000 FC 7000 FC APPL
128
DETAILED INSPECTION OF CONTINUITY FITTING BETWEEN FR
20 AND FR 21, AND ANGLE FITTING, BOTH SIDES OF FR 21,
AT STRINGER 41 LOCATION, LH/RH
531157-01-3 ************** TASK DELETED ************** N/A
3-53 531161-01-1 123 GVI NLG BAY ALL PANELS AF MRB CPCP MRB 531161-01-1 531100-210-803 12 YE 12 YE APPL
124
GENERAL VISUAL INSPECTION OF NLG BAY, ALL PANELS,
LH/RH
531162-01-1 ************** TASK DELETED ************** N/A
531162-01-2 ************** TASK DELETED ************** N/A
531162-01-3 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 80 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531163-01-1 221 DET FWD PAX/CREW DOOR SURROUND AF MRB CPCP MRB 531163-01-1 531100-210-019 6 YE 6 YE APPL
222
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
FORWARD PASSENGER/CREW DOOR, ABOVE CABIN FLOOR LEVEL,
BETWEEN FR 15 AND FR 21 AND BETWEEN STRINGER 8 AND
STRINGER 23, LH/RH, EXCLUDING THE LOWER CORNERS OF
THE DOOR ENTRANCE AREA AT FR 16 AND FR 20, BETWEEN
STRINGER 22 AND 23, LH/RH
NOTE:
EXCLUDED AREA COVERED BY TASKS 531166-01-1 AND
531166-01-2.
3-53 531164-01-1 125 DET FUSELAGE FR 15-21 AF MRB CPCP MRB 531164-01-1 531100-210-801 6 YE 6 YE APPL
126
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW FORWARD PASSENGER/CREW DOOR AND CABIN FLOOR
LEVEL, FROM FR 15 TO FR 21 AND BETWEEN STRINGER 28 LH
AND STRINGER 28 RH.
3-53 531166-01-1 221 DET FUSELAGE FR 16-20 AF MRB CPCP MRB 531166-01-1 531100-220-006 5 YE 5 YE N/A
222
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE ABOVE CABIN FLOOR
LEVEL, AT FR 16 AND FR 20 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH.
3-53 531166-01-2 221 DET FUSELAGE FR 16-20 AF MRB CPCP MRB 531166-01-2 531100-220-006 6 YE 6 YE APPL
222
DETAILED INSPECTION OF FWD PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE ABOVE CABIN FLOOR
LEVEL, AT FR 16 AND FR 20 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH.
3-53 531167-01-1 126 DET AREA BELOW BATTERIES AF MRB CPCP MRB 531167-01-1 531100-210-036 6 YE 6 YE APPL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW BATTERIES, BETWEEN FR 10 AND FR 16, RH
3-53 531169-01-1 123 GVI FUSELAGE FR 12-15 AF MRB CPCP MRB 531169-01-1 531100-210-804 6 YE 6 YE APPL
124
125 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
126 STRUCTURE, BELOW GALLEY AND TOILET, BETWEEN FR 12 AND
FR 15 AND BETWEEN STRINGER 23 LH AND STRINGER 23 RH,
EXCLUDING STRUCTURE FROM FR 12 TO FR 14 UNDER HEAT
EXCHANGER PANELS.
3-53 531170-01-1 200 DET COCKPIT WINDSHIELD LOWER FRONT FTG AF ALI ALI 531170-01-1 531100-210-038 30000 FC 4000 FC N/A
DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER
FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL
SURFACE, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-1
3-53 531170-01-2 200 DET COCKPIT WINDSHIELD LOWER FRONT FTG AF ALI ALI 531170-01-2 531100-210-038 48000 FC 4000 FC APPL
DETAILED INSPECTION OF COCKPIT WINDSHIELD, LOWER
FRONT FITTING AT FR 4, LOWER ATTACHMENT, EXTERNAL
SURFACE, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531170-02-2
531170-01-3 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 81 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531170-02-1 200 SDI COCKPIT WINDSHIELD LOWER FRONT FTG NDT ALI ALI 531170-02-1 531100-210-039 30000 FC 15500 FC N/A
SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT
WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER
ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-1.
3-53 531170-02-2 200 SDI COCKPIT WINDSHIELD LOWER FRONT FTG NDT ALI ALI 531170-02-2 531100-210-039 48000 FC 15500 FC APPL
SPECIAL DETAILED INSPECTION (HFEC) OF COCKPIT
WINDSHIELD, LOWER FRONT FITTING AT FR 4, LOWER
ATTACHMENT, EXTERNAL SURFACE, LH/RH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 531170-01-2.
531170-02-3 ************** TASK DELETED ************** N/A
3-53 531171-01-1 123 DET NLG SECONDARY DOOR HINGE SUPPORTS AF MRB CPCP MRB 531171-01-1 531100-210-020 6 YE 6 YE APPL
124
DETAILED INSPECTION OF NLG, SECONDARY DOOR HINGE
SUPPORTS ON FUSELAGE, LH/RH
3-53 531172-01-1 100 DET SKIN FR 21-23 AND FR 17-18 FROM STRINGER 31-36 AF ALI ALI 531172-01-1 531100-210-032 40400 FC 23300 FC APPL
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 21
AND FR 23 LH AND FR 17 AND FR 18 RH, FROM STRINGER 31
TO STRINGER 36
3-53 531175-01-1 110 DET FWD FACE OF FRONT PRESSURE BULKHEAD AF MRB CPCP MRB 531175-01-1 531100-210-040 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF FORWARD FACE OF FRONT PRESSURE
BULKHEAD ATTACHED TO FR 1
3-53 531176-01-1 200 DET COCKPIT SIDE WINDOWS FRAMEWORK AF MRB CPCP MRB 531176-01-1 531100-210-041 6 YE 6 YE APPL
DETAILED INSPECTION OF COCKPIT SIDE WINDOWS, EXTERNAL
VISIBLE PORTION OF FRAMEWORK, BETWEEN FR 4 AND FR 12,
LH/RH
3-53 531177-01-1 200 DET COCKPIT WINDSHIELD FRAME AF MRB CPCP MRB 531177-01-1 531100-210-042 12 YE 12 YE APPL
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
PORTION OF FRAMEWORK COVERED BY RETAINERS
3-53 531178-01-1 200 DET COCKPIT WINDSHIELD RETAINERS AF MRB CPCP MRB 531178-01-1 531100-210-043 6 YE 6 YE APPL
DETAILED INSPECTION OF COCKPIT WINDSHIELD, EXTERNAL
VISIBLE PORTION OF RETAINERS
3-53 531180-01-1 100 DET FWD PAX/CREW DOOR UNDER SCUFF-PLATE AF MRB CPCP MRB 531180-01-1 531100-210-044 12 YE 12 YE APPL
DETAILED INSPECTION OF FORWARD PASSENGER/CREW DOOR
CUTOUT, UNDERNEATH THE SCUFF-PLATE, LH/RH
3-53 531181-01-1 129 DET FUSELAGE INTL STRUCT FR 15-21, STRINGER 23-28 AF MRB CPCP MRB 531181-01-1 531100-210-035 6 YE 6 YE APPL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AND LOWER SURFACE OF CABIN FLOOR STRUCTURE FROM FR 15
TO FR 21, BETWEEN STRINGER 23 AND STRINGER 28 LH/RH
NOTE:
TII TPS MAY BE LIMITED TO LOWER SURFACE OF CABIN
FLOOR STRUCTURE BETWEEN FR 15 AND FR 21
3-53 531184-01-2 211 DET FWD PRESSURE BULKHEAD VERTICAL POSTS AF ALI ALI 531184-01-2 531100-210-045 28700 FC 11900 FC APPL
212
DETAILED INSPECTION OF CENTRAL AND ADJACENT VERTICAL
POSTS OF FORWARD PRESSURE BULKHEAD AND WEB ASSEMBLY,
UPPER PORTION
APPENDIX A
AEG/AMP/A320 Page 82 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531185-01-1 211 GVI FUSELAGE INTERNAL STRUCTURE AF MRB CPCP MRB 531185-01-1 531100-210-814 12 YE 12 YE 24 YE 12 YE APPL
212
221 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
222 STRUCTURE, FROM FR 1 TO FR 24, ABOVE CABIN FLOOR
223 LEVEL, EXCLUDING STRUCTURE FROM FR 12 TO FR 14 UNDER
224 HEAT EXCHANGER PANELS.
231
232
233
234
3-53 531186-01-1 211 DET AFT FACE OF FWD PRESSURE BULKHEAD AF MRB CPCP MRB 531186-01-1 531100-210-046 12 YE 12 YE 24 YE 12 YE APPL
212
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD, ABOVE COCKPIT FLOOR LEVEL, INCLUDING FR 1,
AS FAR AS VISIBLE
3-53 531187-01-1 211 DET COCKPIT WINDOW FRAMES AF MRB CPCP MRB 531187-01-1 531100-210-047 12 YE 12 YE 24 YE 12 YE APPL
212
DETAILED INSPECTION OF COCKPIT WINDOW FRAMES AND
CLOSING PANELS, INTERNAL STRUCTURE (FR 12 AND
FORWARD).
3-53 531188-01-1 211 DET COCKPIT FLOOR STRUCTURE AF MRB CPCP MRB 531188-01-1 531100-210-048 12 YE 12 YE APPL
212
DETAILED INSPECTION OF COCKPIT FLOOR STRUCTURE,
BETWEEN FR 1 AND FR 12
3-53 531189-01-1 211 DET FLOOR STRUCTURE FR 12 TO 21 AF MRB CPCP MRB 531189-01-1 531100-210-049 5 YE 5 YE N/A
212
221 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BETWEEN
222 FR 12 AND FR 21
231
232
3-53 531189-01-2 211 DET FLOOR STRUCTURE FR 12 TO 21 AF MRB CPCP MRB 531189-01-2 531100-210-049 6 YE 6 YE APPL
212
221 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE BETWEEN
222 FR 12 AND FR 21
231
232
3-53 531190-01-1 221 GVI FLOOR STRUCTURE FR 21 TO FR 24 AF MRB CPCP MRB 531190-01-1 531100-210-805 10 YE 10 YE N/A
222
231 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
232 EXCLUDING AREAS BELOW GALLEYS AND TOILETS, BETWEEN FR
21 AND FR 24
3-53 531190-01-2 221 GVI FLOOR STRUCTURE FR 21 TO FR 24 AF MRB CPCP MRB 531190-01-2 531100-210-805 12 YE 12 YE APPL
222
231 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
232 EXCLUDING AREAS BELOW GALLEYS AND TOILETS, BETWEEN FR
21 AND FR 24
3-53 531191-01-1 121 DET AFT FACE OF FWD PRESSURE BULKHEAD AF MRB CPCP MRB 531191-01-1 531100-220-002 12 YE 12 YE APPL
122
DETAILED INSPECTION OF AFT FACE OF FORWARD PRESSURE
BULKHEAD, BELOW COCKPIT FLOOR LEVEL, INCLUDING FR 1
AND STRINGER CONNECTIONS.
NOTE:
IF CORROSION IS FOUND ON THE PRESSURE BULKHEAD ABOVE
THE AVIONICS FLOOR PANELS THE COMPLETE AFT FACE
(UPPER AND LOWER AREAS) OF THE PRESSURE BULKHEAD IS
TO BE INSPECTED.
APPENDIX A
AEG/AMP/A320 Page 83 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 531192-01-1 121 GVI FUSELAGE FR 1 TO 12 AF MRB CPCP MRB 531192-01-1 531100-210-806 12 YE 12 YE APPL
122
125 GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
126 STRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAY
PANELS, BETWEEN FR 1 AND FR 12, BELOW COCKPIT FLOOR
PANELS
NOTE:
TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE
BETWEEN FR 1 AND FR 12 AND AFT FACE OF PRESSURE
BULKHEAD, FROM STRINGER 32, LH/RH TO BOTTOM
CENTERLINE
3-53 531193-01-1 127 GVI FUSELAGE FR 21 TO 24 AF MRB CPCP MRB 531193-01-1 531100-210-807 12 YE 12 YE APPL
128
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE AND FLOOR STRUCTURE, INCLUDING NLG BAY AFT
FACE, BETWEEN FR 21 AND FR 24, BELOW CABIN FLOOR
PANELS
NOTE:
TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE
BETWEEN FR 21 AND FR 24, FROM STRINGER 32, LH/RH TO
BOTTOM CENTERLINE
3-53 531194-01-1 221 DET FLOOR STRUCTURE FR 21 TO 24 AF MRB CPCP MRB 531194-01-1 531100-220-003 5 YE 5 YE N/A
222
231 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
232 AND 0.5M AROUND GALLEYS AND TOILETS, BETWEEN FR 21
AND FR 24
3-53 531194-01-2 221 DET FLOOR STRUCTURE FR 21 TO 24 AF MRB CPCP MRB 531194-01-2 531100-220-003 6 YE 6 YE N/A
222
231 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
232 AND 0.5M AROUND GALLEYS AND TOILETS, BETWEEN FR 21
AND FR 24
3-53 531198-01-1 125 SDI NOSE FORWARD FUSELAGE NDT MRB CPCP MRB 531198-01-1 531100-200-802 12 YE 12 YE 24 YE 12 YE APPL
126
221 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF FUSELAGE
222 INTERNAL STRUCTURE, FROM FR 12 TO FR 14, UNDER HEAT
223 EXCHANGER PANELS.
224
3-53 531201-01-1 211 SDI NOSE FORWARD FUSELAGE NDT ALI ALI 531201-01-1 531100-250-802 15200 FC 12500 FC N/A
212 NOTE
SPECIAL DETAILED INSPECTION (ROTO) OF WINDOW FRAME AT
TABLET BRACKET LOCATION, INTERNAL SIDE, LH/RH.
NOTE:
THRESHOLD:
- FOR AIRCRAFT POST 155989 THRESHOLD IS TO BE COUNTED
FROM SB 53-1321 EMBODIMENT.
3-53 531259-02-1 140 DET TI-ANGLE CONNECTION BETWEEN BELLY FAIRING AND KEEL AF ALI ALI 531259-02-1 533100-220-810 30000 FC 5000 FC N/A
BEAM SIDE PANEL OR OR
60000 FH 10000 FH
DETAILED INSPECTION OF TI-ANGLE CONNECTION BETWEEN
BELLY FAIRING AND KEEL BEAM SIDE PANEL FR 40 - FR 42,
LH/RH.
2-53 531900-01-1 220 DET FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/06 531900-210-001 4 MO APPL
INSPECTION OF THE COCKPIT GRID COLLECTOR ASSY
2-53 531900-02-1 120 OPC FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/07 531900-710-001 72 MO APPL
OPERATIONAL CHECK OF THE COCKPIT DRAINAGE PIPE
2-53 531900-03-1 120 OPC FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/08 531900-710-003 36 MO APPL
130 OR
150 OPERATIONAL CHECK OF PISTON TYPE DRAIN VALVES IN 8000 FC
LOWER FUSELAGE SHELL FROM OUTSIDE
APPENDIX A
AEG/AMP/A320 Page 84 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532102-01-1 231 GVI FLOOR STRUCTURE FR 24-35 AF MRB CPCP MRB 532102-01-1 532100-210-001 12 YE 12 YE APPL
232
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IF
INSTALLED), BETWEEN FR 24 AND FR 35
3-53 532102-01-2 231 GVI FLOOR STRUCTURE FR 24-35.8 AF MRB CPCP MRB 532102-01-2 532100-210-001 12 YE 12 YE N/A
232
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IF
INSTALLED) AND EMERGENCY EXIT ENTRANCE AREA, BETWEEN
FR 24 AND FR 35.8
3-53 532102-01-3 231 GVI FLOOR STRUCTURE FR 24-35.8 AF MRB CPCP MRB 532102-01-3 532100-210-001 12 YE 12 YE N/A
232
GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
EXCLUDING AREAS BELOW GALLEYS AND TOILETS (IF
INSTALLED), BETWEEN FR 24 AND FR 35.8.
3-53 532104-01-1 131 SDI FLOOR STRUCTURE NDT ALI WFD ALI 532104-01-1 532100-220-802 43400 FC 35600 FC APPL
132 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF ATTACHMENT AREA 86900 FH 71200 FH
OF FR 25 LH TO FR 34 LH AND FR 29 RH TO FR 34 RH TO
CABIN FLOOR BEAMS, INTERNAL STRUCTURE
3-53 532105-01-1 231 DET FLOOR STRUCTURE FR 24 TO FR 35 AF MRB CPCP MRB 532105-01-1 532100-220-001 6 YE 6 YE N/A
232
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
AND 0.5M AROUND GALLEYS AND TOILETS, BETWEEN FR 24
AND FR 35
3-53 532105-02-1 231 DET FORWARD FUSELAGE AF MRB CPCP MRB 532105-02-1 532100-220-804 6 YE 6 YE N/A
232
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
AND 0.5M AROUND GALLEYS AND TOILETS (IF INSTALLED)
AND EMERGENCY EXIT ENTRANCE AREA, BETWEEN FR 24 AND
FR 35.8.
3-53 532105-02-2 231 DET FORWARD FUSELAGE AF MRB CPCP MRB 532105-02-2 532100-220-804 6 YE 6 YE N/A
232
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
AND 0.5M AROUND GALLEYS AND TOILETS (IF INSTALLED),
BETWEEN FR 24 AND FR 35.8.
3-53 532106-01-1 131 SDI FORWARD FUSELAGE NDT ALI ALI 532106-01-1 532100-250-805 43400 FC 35600 FC N/A
132 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF ATTACHMENT AREA 86900 FH 71200 FH
OF FR 35.4 TO FR 35.7 TO CABIN FLOOR BEAMS, INTERNAL
STRUCTURE, LH/RH.
3-53 532113-01-1 231 DET FWD EMERGENCY EXIT CUTOUT SURROUNDS AF MRB CPCP MRB 532113-01-1 532100-200-018 6 YE 6 YE N/A
232
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
FORWARD EMERGENCY EXIT CUTOUTS, BETWEEN FR 35 AND FR
35.3 FROM STRINGER 23 LH TO STRINGER 7 LH AND FROM
STRINGER 23 RH TO STRINGER 10 RH
3-53 532114-01-1 231 DET DOOR STOP FITTINGS AF MRB CPCP MRB 532114-01-1 532100-200-019 12 YE 12 YE N/A
232
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 35.1
AND FR 35.2A, LH/RH
532115-01-2 ************** TASK DELETED ************** N/A
3-53 532117-01-1 131 DET ESCAPE CHUTE SLIDE COMPARTMENT AF MRB CPCP MRB 532117-01-1 532100-200-020 6 YE 6 YE N/A
132
DETAILED INSPECTION OF ESCAPE CHUTE SLIDE
COMPARTMENT, INTERNAL STRUCTURE, BETWEEN FR 35.1 AND
FR 35.2A, FROM STRINGER 24 TO STRINGER 28, LH/RH
APPENDIX A
AEG/AMP/A320 Page 85 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532119-01-2 100 DET FWD EMER EXIT CUTOUT UNDER SCUFF-PLATE AF MRB CPCP MRB 532119-01-2 532100-200-021 12 YE 12 YE N/A
DETAILED INSPECTION OF FORWARD EMERGENCY EXIT CUT OUT
UNDERNEATH THE SCUFF-PLATE, LH/RH
532120-01-1 ************** TASK DELETED ************** N/A
532120-02-1 ************** TASK DELETED ************** N/A
532120-02-2 ************** TASK DELETED ************** N/A
532120-03-1 ************** TASK DELETED ************** N/A
532125-01-1 ************** TASK DELETED ************** N/A
532125-02-1 ************** TASK DELETED ************** N/A
3-53 532132-01-1 100 DET FWD CARGO DOOR HINGE FITTING AF ALI ALI 532132-01-1 532100-200-027 12 YE 12 YE APPL
132 MRB CPCP MRB 532132-01-3 OR OR
DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOOR 28000 FC 9300 FC
HINGE FITTING AND EXTERNAL ATTACHMENT AREA OR OR
56000 FH 18600 FH
3-53 532132-01-3 100 DET FWD CARGO DOOR HINGE FITTING AF MRB CPCP MRB 532132-01-3 532100-200-027 12 YE 12 YE N/A
132
DETAILED INSPECTION OF FUSELAGE FORWARD CARGO DOOR
HINGE FITTING AND EXTERNAL ATTACHMENT AREA
NOTE:
TPS APPLICATION IS LIMITED TO THE INNER SIDE OF THE
HINGE FITTINGS
3-53 532135-01-2 132 GVI FWD CARGO DOOR CUTOUT LATERAL FRAMES AF MRB CPCP MRB 532135-01-1 532100-210-002 6 YE 6 YE APPL
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
CUTOUT, VISIBLE PART OF LATERAL FR 24A AND FR 28
3-53 532135-02-1 132 DET FWD CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 532135-02-1 532100-220-808 1200 FC 1200 FC APPL
OR OR
DETAILED INSPECTION OF FORWARD CARGO DOOR CUTOUT, 2400 FH 2400 FH
VISIBLE PART OF LATERAL FR 24A AND FR 28
3-53 532137-01-1 100 DET FWD CARGO DOOR CUTOUT PANELS AF ALI ALI 532137-01-1 532100-200-004 9700 FC 9700 FC APPL
132 OR OR
DETAILED INSPECTION OF FORWARD CARGO DOOR CUTOUT 19400 FH 19400 FH
PANELS, UPPER AND LOWER CORNERS, EXTERNAL SURFACE
3-53 532137-01-2 100 DET FWD CARGO DOOR CUTOUT PANELS AF ALI ALI 532137-01-2 532100-200-004 9000 FC 9000 FC N/A
132
DETAILED INSPECTION OF FORWARD CARGO DOOR CUTOUT
PANELS, UPPER AND LOWER CORNERS, EXTERNAL SURFACE
532140-01-1 ************** TASK DELETED ************** N/A
532140-01-2 ************** TASK DELETED ************** N/A
532140-01-3 ************** TASK DELETED ************** N/A
532140-02-1 ************** TASK DELETED ************** N/A
532140-02-2 ************** TASK DELETED ************** N/A
532140-02-3 ************** TASK DELETED ************** N/A
532145-01-2 ************** TASK DELETED ************** N/A
532145-01-3 ************** TASK DELETED ************** N/A
3-53 532147-01-1 131 DET CABIN FLOOR BEAM JUNCTION AT FR 35.1 AND FR 35.2 AF ALI ALI 532147-01-1 532100-220-811 36900 FC 15300 FC N/A
132 OR OR
DETAILED INSPECTION OF CABIN FLOOR BEAM JUNCTION AT 73900 FH 30600 FH
FR 35.1 AND FR 35.2, LH/RH.
3-53 532150-01-2 231 DET FWD EMERGENCY EXIT CUTOUT UPR CORNERS AF ALI ALI 532150-01-2 532100-200-022 6 YE 6 YE N/A
MRB CPCP MRB 532150-01-2 OR OR
DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKIN 18000 FC 18000 FC
CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, LH OR OR
36000 FH 36000 FH
APPENDIX A
AEG/AMP/A320 Page 86 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532151-01-1 232 DET FWD EMERG. EXIT SKIN CUTOUT AF ALI ALI 532151-01-1 532100-220-004 6 YE 6 YE N/A
MRB CPCP MRB 532151-01-1 OR OR
DETAILED INSPECTION OF FORWARD EMERGENCY EXIT SKIN 18000 FC 18000 FC
CUT OUT, UPPER CORNERS, EXTERNAL SURFACE, RH OR OR
36000 FH 36000 FH
3-53 532152-02-1 231 DET FWD EMERG. EXIT SKIN CUTOUT AF ALI ALI 532152-02-1 532100-220-809 18300 FC 18300 FC N/A
OR OR
DETAILED INSPECTION OF FUSELAGE SKIN AROUND FORWARD 36700 FH 36700 FH
EMERGENCY EXIT SKIN CUT OUT BETWEEN FR 35 AND FR 35.3
AND FROM STRINGER 8 TO STRINGER 23, EXTERNAL SURFACE,
LH/RH.
532153-01-1 ************** TASK DELETED ************** N/A
532155-01-1 ************** TASK DELETED ************** N/A
3-53 532155-02-1 131 SDI FRAME SPLICES FR 24-34 NDT ALI ALI 532155-02-1 532100-250-809 48500 FC 25900 FC APPL
SPECIAL DETAILED INSPECTION (ROTO) OF FRAME SPLICES
AT STRINGER 35 LH, FROM FR 24 TO FR 34.
532160-01-1 ************** TASK DELETED ************** N/A
3-53 532164-01-3 200 GVI FORWARD FUSELAGE AF MRB MRB 532164-01-3 532100-210-802 30000 FC 3300 FC N/A
OR OR
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 60000 FH 6700 FH
SURFACE, FROM STRINGER 23 LH/RH TO CROWN CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
3-53 532164-01-5 200 GVI FORWARD FUSELAGE AF MRB MRB 532164-01-5 532100-210-802 30000 FC 3500 FC APPL
OR OR
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 60000 FH 7000 FH
SURFACE, FROM STRINGER 23 LH/RH TO CROWN CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
3-53 532164-01-6 200 GVI FORWARD FUSELAGE AF MRB MRB 532164-01-6 532100-210-802 30000 FC 2900 FC N/A
OR OR
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL 60000 FH 5800 FH
SURFACE, FROM STRINGER 23 LH/RH TO CROWN CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.8.
3-53 532165-01-1 100 GVI FUSELAGE SKIN BETWEEN FR 24 AND 35 AF ALI ALI 532165-01-1 532100-210-005 4300 FC 4300 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
3-53 532165-01-3 100 GVI FUSELAGE SKIN BETWEEN FR 24 AND 35.8 AF ALI ALI 532165-01-3 532100-210-005 4400 FC 4400 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.8.
3-53 532165-01-4 100 GVI FUSELAGE SKIN BETWEEN FR 24 AND 35 AF ALI ALI 532165-01-4 532100-210-005 4000 FC 4000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
APPENDIX A
AEG/AMP/A320 Page 87 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532165-01-7 100 GVI FUSELAGE SKIN BETWEEN FR 24 AND 35 AF ALI ALI 532165-01-7 532100-210-005 3900 FC 3900 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
3-53 532165-01-8 100 GVI FUSELAGE SKIN BETWEEN FR 24 AND 35 AF ALI ALI 532165-01-8 532100-210-005 3200 FC 3200 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, FROM STRINGER 23 LH/RH TO BOTTOM CENTERLINE,
EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
532165-02-5 ************** TASK DELETED ************** N/A
3-53 532166-01-1 137 DET FUSELAGE SKIN AT FR 35 AF ALI ALI 532166-01-1 532100-200-023 44500 FC 6500 FC APPL
138
DETAILED INSPECTION OF FUSELAGE SKIN AT FR 35 AND 10
CM FORWARD, AT LEVEL OF STRINGER 30, INTERNAL SIDE,
LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-02-1
3-53 532166-02-1 137 SDI FORWARD FUSELAGE NDT ALI ALI 532166-02-1 532100-220-803 44500 FC 20000 FC APPL
138
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE SKIN
AT FR 35 AND 10 CM FORWARD, AT LEVEL OF STRINGER 30,
INTERNAL SIDE, LH/RH
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 532166-01-1.
3-53 532170-01-1 132 GVI FWD CARGO DOOR LOCK FITTINGS AND SURROUNDING AF ALI ALI 532170-01-1 532100-210-006 6 YE 6 YE APPL
STRUCTURE MRB CPCP MRB 532170-01-4 OR OR
9100 FC 9100 FC
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCK
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION
NOTE:
INSPECTION BETWEEN FR 25 AND FR 27A (6 PLACES).
3-53 532170-01-3 132 GVI FWD CARGO DOOR LOCK FITTINGS AND SURROUNDING AF ALI ALI 532170-01-3 532100-210-006 6 YE 6 YE N/A
STRUCTURE MRB CPCP MRB 532170-01-5 OR OR
9100 FC 9100 FC
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCK
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION
NOTE:
INSPECTION BETWEEN FR 25 AND FR 26A (4 PLACES).
3-53 532170-01-6 132 GVI FWD CARGO DOOR LOCK FITTINGS AND SURROUNDING AF ALI ALI 532170-01-6 532100-210-006 6 YE 6 YE N/A
STRUCTURE MRB CPCP MRB 532170-01-4 OR OR
MRB 532170-01-5 8400 FC 8400 FC
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR LOCK
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION
NOTE:
- A318: INSPECTION BETWEEN FR 25 AND FR 26A (4
PLACES).
- A319: INSPECTION BETWEEN FR 25 AND FR 27A (6
PLACES).
3-53 532175-01-1 132 DET FWD CARGO DOOR CUT OUT AF MRB CPCP MRB 532175-01-1 532100-200-011 12 YE 6 YE APPL
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
FORWARD CARGO DOOR CUTOUT, FROM FR 24 TO FR 29 AND
BETWEEN STRINGER 23 AND STRINGER 38, RH
APPENDIX A
AEG/AMP/A320 Page 88 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532180-01-1 133 DET FUSELAGE FR 24-35 AF MRB CPCP MRB 532180-01-1 532100-200-013 5 YE 5 YE N/A
134
137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
138 INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM
STRINGER 38 LH/RH TO BOTTOM CENTERLINE
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
TYPE 2 TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE FROM FR 34 TO FR 35, AND FORWARD FACE OF
PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO BOTTOM
CENTERLINE.
3-53 532180-01-2 133 DET FUSELAGE FR 24-35 AF MRB CPCP MRB 532180-01-2 532100-200-013 6 YE 6 YE APPL
134
137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
138 INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM
STRINGER 38 LH/RH TO BOTTOM CENTERLINE
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.
TYPE 2 TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE FROM FR 34 TO FR 35, AND FORWARD FACE OF
PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO BOTTOM
CENTERLINE.
3-53 532180-01-3 133 DET FUSELAGE FR 24-35.8 AF MRB CPCP MRB 532180-01-3 532100-200-013 5 YE 5 YE N/A
134
137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
138 INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM
STRINGER 38 LH/RH TO BOTTOM CENTERLINE
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.8.
TYPE 2 TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE FROM FR 35.7 TO FR 35.8, AND FORWARD FACE
OF PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO
BOTTOM CENTERLINE.
3-53 532180-01-4 133 DET FUSELAGE FR 24-35.8 AF MRB CPCP MRB 532180-01-4 532100-200-013 6 YE 6 YE N/A
134
137 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
138 INCLUDING FORWARD FACE OF PRESSURE BULKHEAD, FROM
STRINGER 38 LH/RH TO BOTTOM CENTERLINE
NOTE:
INSPECTION BETWEEN FR 24 AND FR 35.8.
TYPE 2 TPS MAY BE LIMITED TO FUSELAGE INTERNAL
STRUCTURE FROM FR 35.7 TO FR 35.8, AND FORWARD FACE
OF PRESSURE BULKHEAD, FROM STRINGER 38, LH/RH TO
BOTTOM CENTERLINE.
3-53 532186-02-1 230 SDI CIRCUMFERENTIAL JOINT AT FR 35 NDT ALI ALI 532186-02-1 532100-250-803 48000 FC 13300 FC APPL
240 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CIRCUMFERENTIAL 96000 FH 26600 FH
JOINT AT FR 35, BETWEEN STRINGER 4 AND STRINGER 7,
LH/RH, EXTERNAL SIDE.
3-53 532187-02-1 230 SDI CIRCUMFERENTIAL JOINT AT FR 35.8 NDT ALI ALI 532187-02-1 532100-250-804 38000 FC 11900 FC N/A
240 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CIRCUMFERENTIAL 76100 FH 23900 FH
JOINT AT FR 35.8, BETWEEN STRINGER 4 AND STRINGER 7,
LH/RH, EXTERNAL SIDE.
3-53 532190-02-1 100 DET FUSELAGE SKIN BETWEEN FR 28 AND FR 29 AF ALI ALI 532190-02-1 532100-220-806 48000 FC 8100 FC APPL
DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE
AROUND WATER DRAIN PANEL CUTOUT AND RADIUS INSIDE
WATER DRAIN BOX, BETWEEN FR 28 AND FR 29 AT STRINGER
43 LH.
APPENDIX A
AEG/AMP/A320 Page 89 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532190-02-2 100 DET FUSELAGE SKIN BETWEEN FR 28 AND FR 29 AF ALI ALI 532190-02-2 532100-220-806 39300 FC 7600 FC N/A
DETAILED INSPECTION OF FUSELAGE EXTERNAL SURFACE
AROUND WATER DRAIN PANEL CUTOUT AND RADIUS INSIDE
WATER DRAIN BOX, BETWEEN FR 28 AND FR 29 AT STRINGER
43 LH.
532190-02-3 ************** TASK DELETED ************** N/A
532190-02-4 ************** TASK DELETED ************** N/A
3-53 532195-01-1 132 GVI FWD CARGO DOOR ACTUATOR AF MRB MRB 532195-01-1 532100-210-008 16700 FC 16700 FC APPL
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
ACTUATOR ATTACH BRACKETS
NOTE:
INSPECTION BETWEEN CABIN FLOOR BEAMS, FROM FR 25 TO
FR 27.
3-53 532195-01-2 132 GVI FWD CARGO DOOR ACTUATOR AF MRB MRB 532195-01-2 532100-210-008 16700 FC 16700 FC N/A
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
ACTUATOR ATTACH BRACKETS
NOTE:
INSPECTION BETWEEN CABIN FLOOR BEAMS, FROM FR 25 TO
FR 28.
3-53 532195-01-3 132 GVI FWD CARGO DOOR ACTUATOR AF MRB MRB 532195-01-3 532100-210-008 11400 FC 11400 FC N/A
GENERAL VISUAL INSPECTION OF FORWARD CARGO DOOR
ACTUATOR ATTACH BRACKETS
NOTE:
INSPECTOIN BETWEEN CABIN FLOOR BEAMS, FROM FR 25 TO
FR 27.
3-53 532196-01-1 132 DET FWD CARGO DOOR ECCENTRIC BOLTS AF MRB CPCP MRB 532196-01-1 532100-200-005 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF FORWARD CARGO DOOR ECCENTRIC
BOLTS OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN
FR 24A AND FR 28.
532196-01-4 ************** TASK DELETED ************** N/A
532196-01-5 ************** TASK DELETED ************** N/A
3-53 532199-01-1 131 SDI FASTENER HOLES OF FR 35.1 UNDER SLIDEBOX AND TRIFORM NDT ALI ALI 532199-01-1 532100-250-806 18300 FC 5300 FC N/A
132 FITTING
SPECIAL DETAILED INSPECTION (ROTO) OF FASTENER HOLES
OF FR 35.1 UNDER SLIDEBOX AND TRIFORM FITTING, LH/RH.
3-53 532199-02-1 131 SDI TRIFORM FITTING AT FR 35.2 NDT ALI ALI 532199-02-1 532100-250-807 18300 FC 5300 FC N/A
132
SPECIAL DETAILED INSPECTION (ROTO) OF TRIFORM FITTING
AT FR 35.2, LH/RH.
3-53 532201-01-1 231 SDI HOLES AT FR 35.2A BETWEEN STRINGER 22 AND 23 NDT ALI ALI 532201-01-1 532100-250-808 25400 FC 21500 FC N/A
232 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF HOLES AT FR 50900 FH 43100 FH
35.2A BETWEEN STRINGER 22 AND STRINGER 23, LH/RH.
3-53 532209-01-1 133 SDI BAY UNDER FWD CARGO COMPARTMENT NDT ALI WFD ALI 532209-01-1 532100-250-802 40500 FC 5000 FC APPL
134 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF HOLES AT FR 24 81100 FH 10000 FH
- FR 34 BETWEEN STRINGER 33 AND STRINGER 39 (LH
ONLY)
IN CARGO FLOOR AREA.
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 532209-02-1.
APPENDIX A
AEG/AMP/A320 Page 90 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 532209-02-1 133 SDI BAY UNDER FWD CARGO COMPARTMENT NDT ALI WFD ALI 532209-02-1 532100-250-801 40500 FC 1800 FC APPL
134 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF HOLES AT FR 24 81100 FH 3600 FH
- FR 34 BETWEEN STRINGER 33 AND STRINGER 39 (LH
ONLY)
IN CARGO FLOOR AREA.
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 532209-01-1.
3-53 532210-01-1 131 DET FWD CARGO COMPARTMENT FLOOR LEVEL AREA AF ALI ALI 532210-01-1 532100-220-810 43400 FC 12300 FC APPL
132 OR OR
DETAILED INSPECTION OF HOLES BETWEEN FR 25 LH TO FR 86900 FH 24700 FH
34 LH AND FR 29 RH TO FR 34 RH BETWEEN STRINGER 23
AND STRINGER 24
533101-01-1 ************** TASK DELETED ************** N/A
533101-01-3 ************** TASK DELETED ************** N/A
3-53 533103-01-1 151 DET AFT PRESSURE BULKHEAD AFT FACE AF MRB CPCP MRB 533103-01-1 533100-210-008 12 YE 12 YE APPL
152
DETAILED INSPECTION OF PRESSURE BULKHEAD AT FR 46,
AFT FACE, INCLUDING VERTICAL BEAMS, ABOVE CARGO FLOOR
LEVEL
533103-01-4 ************** TASK DELETED ************** N/A
533103-01-5 ************** TASK DELETED ************** N/A
533105-01-1 ************** TASK DELETED ************** N/A
3-53 533105-01-2 147 DET MLG BAY SIDE PANELS AF MRB CPCP MRB 533105-01-2 533100-210-003 12 YE 6 YE 24 YE 6 YE APPL
148
DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS
INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING
SLANTED FRAMES AND SIDE BOX, LH/RH
3-53 533105-01-6 147 DET MLG BAY SIDE PANELS AF ALI ALI 533105-01-6 533100-210-003 12 YE 6 YE 24 YE 6 YE N/A
148 MRB CPCP MRB 533105-01-2 OR OR OR OR
DETAILED INSPECTION OF MLG BAY FUSELAGE SIDE PANELS 13100 FC 9000 FC 13100 FC 9000 FC
INSIDE MLG BAY, BETWEEN FR 42 AND FR 46, INCLUDING OR OR OR OR
SLANTED FRAMES AND SIDE BOX, LH/RH 56400 FH 38700 FH 56400 FH 38700 FH
533105-01-7 ************** TASK DELETED ************** N/A
533105-01-8 ************** TASK DELETED ************** N/A
533105-01-9 ************** TASK DELETED ************** N/A
533107-01-1 ************** TASK DELETED ************** N/A
3-53 533109-01-3 145 DET PRESSURE DECK MEMBRANES UPR SURFACE AF ALI ALI 533109-01-3 533100-210-005 13100 FC 9000 FC N/A
146 OR OR
DETAILED INSPECTION OF UPPER SURFACES OF PRESSURE 56400 FH 38700 FH
DECK MEMBRANES AND SIDE BOXES, BETWEEN FR 42 AND FR
46, INCLUDING CONNECTIONS TO LONGITUDINAL BEAMS AND
SUPPORT RIBS, LH/RH
533110-01-1 ************** TASK DELETED ************** N/A
533110-01-2 ************** TASK DELETED ************** N/A
3-53 533110-09-2 145 SDI LONGITUDINAL FLOOR BEAMS NDT MRB FMP MRB 533110-09-2 18 YE 6 YE N/A
146 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF UPPER FLANGE OF
LONGITUDINAL FLOOR BEAMS AT FR 42 AND FR 46, AS FAR
AS VISIBLE
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 91 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533110-09-3 145 SDI LONGITUDINAL FLOOR BEAMS NDT MRB FMP MRB 533110-09-3 18 YE 6 YE N/A
146 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF UPPER FLANGE OF
LONGITUDINAL FLOOR BEAMS AT FR 42 AND FR 46, AS FAR
AS VISIBLE
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-53 533111-01-1 147 DET PRESSURE DECK MEMBRANES LWR SURFACE AF ALI ALI 533111-01-1 533100-210-006 12 YE 6 YE 24 YE 6 YE APPL
148 MRB CPCP MRB 533111-01-1 OR OR OR OR
DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECK 24000 FC 8400 FC 24000 FC 8400 FC
MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING OR OR OR OR
CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES, 48000 FH 16800 FH 48000 FH 16800 FH
SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND
PRESSURE BULKHEAD, LH/RH
3-53 533111-01-2 147 DET PRESSURE DECK MEMBRANES LWR SURFACE AF ALI ALI 533111-01-2 533100-210-006 12 YE 6 YE 24 YE 6 YE N/A
148 MRB CPCP MRB 533111-01-1 OR OR OR OR
DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECK 33900 FC 10900 FC 33900 FC 10900 FC
MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING OR OR OR OR
CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES, 67800 FH 21900 FH 67800 FH 21900 FH
SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND
PRESSURE BULKHEAD, LH/RH
3-53 533111-01-3 147 DET PRESSURE DECK MEMBRANES LWR SURFACE AF ALI ALI 533111-01-3 533100-210-006 12 YE 6 YE 24 YE 6 YE N/A
148 MRB CPCP MRB 533111-01-1 OR OR OR OR
DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECK 21100 FC 6800 FC 21100 FC 6800 FC
MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING OR OR OR OR
CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES, 42200 FH 13600 FH 42200 FH 13600 FH
SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND
PRESSURE BULKHEAD, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533111-01-5 147 DET PRESSURE DECK MEMBRANES LWR SURFACE AF MRB CPCP MRB 533111-01-1 533100-210-006 12 YE 6 YE 24 YE 6 YE N/A
148
DETAILED INSPECTION OF LOWER SURFACE OF PRESSURE DECK
MEMBRANES, BETWEEN FR 42 AND FR 46, INCLUDING
CONNECTIONS TO LONGITUDINAL BEAMS, SIDE BOXES,
SUPPORT RIBS, REAR SPAR OF CENTER WING BOX AND
PRESSURE BULKHEAD, LH/RH
533121-01-1 ************** TASK DELETED ************** N/A
533121-01-2 ************** TASK DELETED ************** N/A
533122-01-5 ************** TASK DELETED ************** N/A
3-53 533127-01-6 200 SDI LOWER SKIN OF LONGITUDINAL LAP JOINTS NDT ALI WFD ALI 533127-01-6 60000 FC 9100 FC N/A
SPECIAL DETAILED INSPECTION (LFEC) OF LOWER SKIN OF
LONGITUDINAL LAP JOINTS AT STRINGER 18, BETWEEN FR
35.8 AND FR 47, EXTERNAL SURFACE, LH/RH.
3-53 533128-01-2 200 DET EMERGENCY EXIT SKIN CUTOUTS AF ALI ALI 533128-01-2 533100-210-016 31100 FC 10900 FC APPL
OR OR
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, 62200 FH 21900 FH
UPPER AND LOWER CORNERS, LH/RH
3-53 533128-01-3 200 DET EMERGENCY EXIT SKIN CUTOUTS AF ALI ALI 533128-01-3 533100-210-016 31100 FC 10900 FC N/A
OR OR
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, 62200 FH 21900 FH
UPPER AND LOWER CORNERS, LH/RH
APPENDIX A
AEG/AMP/A320 Page 92 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533128-01-4 200 DET EMERGENCY EXIT SKIN CUTOUTS AF ALI ALI 533128-01-4 533100-210-016 28800 FC 9100 FC N/A
OR OR
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, 57700 FH 18300 FH
UPPER AND LOWER CORNERS, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533128-01-5 200 DET EMERGENCY EXIT SKIN CUTOUTS AF ALI ALI 533128-01-5 533100-210-016 24000 FC 7600 FC N/A
OR OR
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, 60000 FH 19000 FH
UPPER AND LOWER CORNERS, LH/RH
3-53 533128-01-7 200 DET EMERGENCY EXIT SKIN CUTOUTS AF ALI ALI 533128-01-7 533100-210-016 28800 FC 9100 FC N/A
OR OR
DETAILED INSPECTION OF EMERGENCY EXIT SKIN CUTOUTS, 57700 FH 18300 FH
UPPER AND LOWER CORNERS, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533128-02-3 200 GVI EMERGENCY EXIT SKIN CUTOUTS AF MRB CPCP MRB 533128-02-3 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF EMERGENCY EXITS SKIN
CUTOUTS, UPPER AND LOWER CORNERS, LH/RH
3-53 533129-01-1 241 DET EMERGENCY EXIT CUTOUTS AF ALI ALI 533129-01-1 533100-210-009 12 YE 6 YE N/A
242 MRB CPCP MRB 533129-01-1 OR OR
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND 28400 FC 28400 FC
EMERGENCY EXIT CUTOUTS, BETWEEN FR 37 AND FR 41, BOTH OR OR
SIDES, FROM STRINGER 10 TO STRINGER 23, LH/RH 56800 FH 56800 FH
3-53 533129-01-2 241 DET EMERGENCY EXIT CUTOUTS AF MRB CPCP MRB 533129-01-2 533100-210-009 12 YE 6 YE N/A
242
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
EMERGENCY EXIT CUTOUTS, BETWEEN FR 39 AND FR 41,
BOTH SIDES, FROM STRINGER 10 TO STRINGER 23, LH/RH
3-53 533129-01-3 241 DET EMERGENCY EXIT CUTOUTS AF MRB CPCP MRB 533129-01-1 533100-210-009 12 YE 6 YE APPL
242
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND
EMERGENCY EXIT CUTOUTS, BETWEEN FR 37 AND FR 41, BOTH
SIDES, FROM STRINGER 10 TO STRINGER 23, LH/RH
3-53 533129-02-1 241 SDI EMERGENCY EXIT CUTOUTS NDT ALI ALI 533129-02-1 18100 FC 1700 FC N/A
242 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF INTERNAL 36200 FH 3500 FH
STRUCTURE AROUND EMERGENCY EXIT CUTOUTS, BETWEEN FR
37 AND FR 41, FROM STRINGER 10 TO STRINGER 23, LH/RH.
3-53 533130-01-1 200 DET ANTI COLLISION LIGHT SKIN CUTOUT AF MRB CPCP MRB 533130-01-1 533100-210-010 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION
LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
3-53 533130-01-2 200 DET ANTI COLLISION LIGHT SKIN CUTOUT AF ALI ALI 533130-01-2 533100-210-010 12 YE 12 YE 24 YE 12 YE N/A
MRB CPCP MRB 533130-01-1 OR OR OR OR
DETAILED INSPECTION OF SKIN AROUND ANTI COLLISION 30500 FC 17000 FC 30500 FC 17000 FC
LIGHT CUTOUT, BETWEEN FR 40 AND FR 41 AND BETWEEN
STRINGER 1, LH/RH, EXTERNAL SURFACE
533130-01-4 ************** TASK DELETED ************** N/A
533130-01-5 ************** TASK DELETED ************** N/A
533130-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 93 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533131-01-1 200 DET ADF1 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 533131-01-1 533100-210-011 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNA
CUTOUT, BETWEEN FR 44 AND FR 45 AND BETWEEN STRINGER
1, LH/RH, EXTERNAL SURFACE
533131-01-4 ************** TASK DELETED ************** N/A
3-53 533131-01-5 200 DET ADF1 ANTENNA SKIN CUTOUT AF ALI ALI 533131-01-5 533100-210-011 12 YE 12 YE 24 YE 12 YE N/A
MRB CPCP MRB 533131-01-1 OR OR OR OR
DETAILED INSPECTION OF SKIN AROUND ADF 1 ANTENNA 26300 FC 15700 FC 26300 FC 15700 FC
CUTOUT, BETWEEN FR 44 AND FR 45 AND BETWEEN STRINGER
1, LH/RH, EXTERNAL SURFACE
533132-01-2 ************** TASK DELETED ************** N/A
3-53 533132-01-4 200 DET WINDOW FORGINGS FR 35 - FR 47/54 AF ALI ALI 533132-01-4 533100-210-020 36300 FC 9300 FC N/A
DETAILED INSPECTION OF VISIBLE PART OF WINDOW
FORGINGS AND FUSELAGE SKIN IN WINDOW FORGING AREA,
LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 35 AND FR 47/54.
3-53 533133-01-5 200 GVI CENTER FUSELAGE AF MRB MRB 533133-01-5 533100-210-038 30000 FC 5000 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE, EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECT FROM FR 35 TO FR 47.
3-53 533133-01-6 200 GVI CENTER FUSELAGE AF MRB MRB 533133-01-6 533100-210-038 30000 FC 5000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE, EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECT FROM FR 35.8 TO FR 47.
3-53 533133-01-7 200 GVI CENTER FUSELAGE AF MRB MRB 533133-01-7 533100-210-038 30000 FC 5000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE, EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECT FROM FR 35 TO FR 47/51.
3-53 533133-01-8 200 GVI CENTER FUSELAGE AF MRB MRB 533133-01-8 533100-210-038 30000 FC 5000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE, EXCEPT AREAS COVERED BY BELLY FAIRING
NOTE:
INSPECT FROM FR 35 TO FR 47/54.
3-53 533135-01-1 145 GVI FUSELAGE FR 36-46 AF MRB CPCP MRB 533135-01-1 533100-210-031 12 YE 12 YE APPL
146
GENERAL VISUAL INSPECTION OF FUSELAGE INTERNAL
STRUCTURE BELOW CABIN FLOOR PANELS, INCLUDING CABIN
FLOOR STRUCTURE BETWEEN FR 36 AND FR 46
NOTE:
CAN BE PERFORMED AT SAME TIME AS TASK 571157-01-1
3-53 533136-01-1 147 GVI MAIN LANDING GEAR BAY AF MRB CPCP MRB 533136-01-1 533100-210-023 6 YE 6 YE APPL
148
GENERAL VISUAL INSPECTION OF MLG BAY, INCLUDING MLG
DOOR HINGES
APPENDIX A
AEG/AMP/A320 Page 94 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533138-01-1 241 DET LONGITUDINAL LAP JOINT AT FR 42 AF ALI ALI 533138-01-1 533100-210-027 40000 FC 17400 FC APPL
242 OR OR
DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP 80000 FH 34900 FH
JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT
AREA AT FR 42, INTERNAL
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533138-02-1
3-53 533138-01-2 241 DET LONGITUDINAL LAP JOINT AT FR 42 AF ALI ALI 533138-01-2 533100-210-027 40900 FC 10000 FC N/A
242 OR OR
DETAILED INSPECTION OF LOWER SKIN OF LONGITUDINAL LAP 81800 FH 20000 FH
JOINT AT STRINGER 18 LH AND STRINGER 18 RH, IN RUNOUT
AREA AT FR 42, INTERNAL
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533138-02-2
3-53 533138-02-1 241 SDI LONGITUDINAL LAP JOINT AT FR 42 NDT ALI ALI 533138-02-1 533100-220-004 40000 FC 31400 FC APPL
242 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF 80000 FH 62800 FH
LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER
18 RH, IN RUNOUT AREA AT FR 42, INTERNAL
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533138-01-1
3-53 533138-02-2 241 SDI LONGITUDINAL LAP JOINT AT FR 42 NDT ALI ALI 533138-02-2 533100-220-004 40900 FC 12000 FC N/A
242 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER SKIN OF 81800 FH 24000 FH
LONGITUDINAL LAP JOINT AT STRINGER 18 LH AND STRINGER
18 RH, IN RUNOUT AREA AT FR 42, INTERNAL
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 533138-01-2
3-53 533139-01-1 241 DET FRAME FLANGES AT FR 38, 39, 40 AND 41 AF ALI ALI 533139-01-1 533100-210-028 27400 FC 7400 FC APPL
242 OR OR
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL 54800 FH 14900 FH
BEAM FLANGE
NOTE:
INSPECTION OF FRAME FLANGES AT FR 38 AND FR 39, AND
AT FR 40 AND FR 41 BETWEEN STRINGER 12 AND STRINGER
21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER
20A LH AND STRINGER 20A RH, BETWEEN FR 38 AND FR 39
AND BETWEEN FR 40 AND FR 41.
3-53 533139-01-2 241 DET FRAME FLANGES AT FR 40 AND 41 AF ALI ALI 533139-01-2 533100-210-028 27400 FC 7400 FC N/A
242 OR OR
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL 54800 FH 14900 FH
BEAM FLANGE
NOTE:
INSPECTION OF FRAME FLANGES AT FR 40 AND FR 41,
BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND
LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND
STRINGER 20A RH, BETWEEN FR 40 AND FR 41.
3-53 533139-01-4 241 DET FRAME FLANGES AT FR 38, 39, 40 AND 41 AF ALI ALI 533139-01-4 533100-210-028 30300 FC 15000 FC N/A
242
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL
BEAM FLANGE
NOTE:
INSPECTION OF FRAME FLANGES AT FR 38 AND FR 39, AND
AT FR 40 AND FR 41 BETWEEN STRINGER 12 AND STRINGER
21, LH/RH, AND LONGITUDINAL BEAM FLANGE AT STRINGER
20A LH AND STRINGER 20A RH, BETWEEN FR 38 AND FR 39
AND BETWEEN FR 40 AND FR 41
FOR AIRCRAFT POST 153069 THRESHOLD IS TO BE COUNTED
FROM SB 53-1265 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 95 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533139-01-5 241 DET FRAME FLANGES AT FR 40 AND 41 AF ALI ALI 533139-01-5 533100-210-028 30300 FC 15000 FC N/A
242
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL
BEAM FLANGE
NOTE:
INSPECTION OF FRAME FLANGES AT FR 40 AND FR 41,
BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND
LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND
STRINGER 20A RH, BETWEEN FR 40 AND FR 41.
FOR AIRCRAFT POST 153069 THRESHOLD IS TO BE COUNTED
FROM SB 53-1265 EMBODIMENT.
3-53 533139-01-6 241 DET FRAME FLANGES AT FR 40 AND 41 AF ALI ALI 533139-01-6 533100-210-028 26400 FC 7400 FC N/A
242 OR OR
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL 52900 FH 14900 FH
BEAM FLANGE
NOTE:
- INSPECTION OF FRAME FLANGES AT FR 40 AND FR 41,
BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND
LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND
STRINGER 20A RH, BETWEEN FR 40 AND FR 41.
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533139-01-7 241 DET FRAME FLANGES AT FR 40 AND 41 AF ALI ALI 533139-01-7 533100-210-028 26400 FC 7400 FC N/A
242 OR OR
DETAILED INSPECTION OF FRAME FLANGES AND LONGITUDINAL 52900 FH 14900 FH
BEAM FLANGE
NOTE:
- INSPECTION OF FRAME FLANGES AT FR 40 AND FR 41,
BETWEEN STRINGER 12 AND STRINGER 21, LH/RH, AND
LONGITUDINAL BEAM FLANGE AT STRINGER 20A LH AND
STRINGER 20A RH, BETWEEN FR 40 AND FR 41.
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533140-01-10 200 SDI SPLICE PLATE AT FR 47 NDT ALI ALI 533140-01-10 533100-220-006 40300 FC 7200 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT 80700 FH 14400 FH
CIRCUMFERENTIAL SKIN SPLICE
NOTE:
- INSPECTION AT FR 47, FROM STRINGER 10, LH/RH, TO
CROWN CENTER LINE, EXTERNAL SURFACE.
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
533140-01-2 ************** TASK DELETED ************** N/A
3-53 533140-01-3 200 SDI SPLICE PLATE AT FR 47 NDT ALI WFD ALI 533140-01-3 533100-220-006 54600 FC 10100 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT 109300 FH 20300 FH
CIRCUMFERENTIAL SKIN SPLICE
NOTE:
INSPECTION AT FR 47, FROM STRINGER 10, LH/RH, TO
CROWN CENTER LINE, EXTERNAL SURFACE.
533140-01-4 ************** TASK DELETED ************** N/A
533140-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 96 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533140-01-8 200 SDI SPLICE PLATE AT FR 47 NDT ALI WFD ALI 533140-01-8 533100-220-006 40300 FC 7200 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT 80700 FH 14400 FH
CIRCUMFERENTIAL SKIN SPLICE
NOTE:
INSPECTION AT FR 47, FROM STRINGER 10, TO CROWN
CENTER LINE, EXTERNAL SURFACE, LH/RH.
3-53 533141-01-1 190 DET FUSELAGE SKIN BETWEEN FR 35 AND 36 AF ALI ALI 533141-01-1 533100-210-025 38600 FC 9800 FC APPL
OR OR
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35 77200 FH 19600 FH
AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30,
LH/RH, EXTERNAL SURFACE
3-53 533141-01-2 190 DET FUSELAGE SKIN BETWEEN FR 35.8 AND 36 AF ALI ALI 533141-01-2 533100-210-025 38600 FC 9800 FC N/A
OR OR
DETAILED INSPECTION OF FUSELAGE SKIN, BETWEEN FR 35.8 77200 FH 19600 FH
AND FR 36 AND BETWEEN STRINGER 25 AND STRINGER 30,
LH/RH, EXTERNAL SURFACE
3-53 533143-01-1 147 DET SIDE BOX BEAM IN AREA OF FR 46 AF ALI ALI 533143-01-1 533100-210-029 40000 FC 10600 FC N/A
148 OR OR
DETAILED INSPECTION OF SIDE BOX BEAM IN AREA OF 80000 FH 21200 FH
ATTACHMENT TO FR 46, LH/RH
3-53 533144-01-1 145 DET FRAME ATTACHMENTS TO PRESSURE FLOOR AF ALI ALI 533144-01-1 533100-210-030 33100 FC 12800 FC N/A
146 OR OR
DETAILED INSPECTION OF FRAME ATTACHMENTS TO PRESSURE 66200 FH 25600 FH
FLOOR FROM FR 42 TO FR 46, LH/RH
3-53 533151-01-1 147 DET KEELBEAM BOX AF MRB CPCP MRB 533151-01-1 533100-210-007 6 YE 6 YE APPL
148
191 DETAILED INSPECTION OF KEELBEAM BOX
192
195 NOTE:
196 INSPECTION BETWEEN FR 35 AND FR 47.
3-53 533151-01-2 147 DET KEELBEAM BOX AF MRB CPCP MRB 533151-01-2 533100-210-007 6 YE 6 YE N/A
148
191 DETAILED INSPECTION OF KEELBEAM BOX
192
195 NOTE:
196 INSPECTION BETWEEN FR 35.8 AND FR 47.
3-53 533151-01-3 147 DET KEELBEAM BOX AF MRB CPCP MRB 533151-01-3 533100-210-007 6 YE 6 YE N/A
148
191 DETAILED INSPECTION OF KEELBEAM BOX
192
195 NOTE:
196 INSPECTION BETWEEN FR 35 AND FR 47/51.
3-53 533151-01-4 147 DET KEELBEAM BOX AF MRB CPCP MRB 533151-01-4 533100-210-007 6 YE 6 YE N/A
148
191 DETAILED INSPECTION OF KEELBEAM BOX
192
195 NOTE:
196 INSPECTION BETWEEN FR 35 AND FR 47/54.
533151-01-5 ************** TASK DELETED ************** N/A
3-53 533152-01-1 137 DET PRESSURE BULKHEAD AT FR 35 FWD FACE AF MRB CPCP MRB 533152-01-1 533100-210-012 12 YE 6 YE N/A
138
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
NOTE:
INSPECTION AT FR 35 AND PRESSURE DECK UPPER SURFACE,
BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO
CENTER WING BOX AT FR 35 AND FR 36.
533152-01-11 ************** TASK DELETED ************** N/A
3-53 533152-01-3 137 DET PRESSURE BULKHEAD AT FR 35.8 FWD FACE AF MRB CPCP MRB 533152-01-3 533100-210-012 12 YE 6 YE N/A
138
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
NOTE:
INSPECTION AT FR 35.8 AND PRESSURE DECK UPPER
SURFACE, BETWEEN FR 35.8 AND FR 36, INCLUDING
CONNECTIONS TO CENTER WING BOX AT FR 35.8 AND FR 36.
APPENDIX A
AEG/AMP/A320 Page 97 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
533152-01-5 ************** TASK DELETED ************** N/A
533152-01-6 ************** TASK DELETED ************** N/A
3-53 533152-01-7 137 DET PRESSURE BULKHEAD AT FR 35 FWD FACE AF MRB CPCP MRB 533152-01-7 533100-210-012 12 YE 6 YE APPL
138
DETAILED INSPECTION OF PRESSURE BULKHEAD FORWARD FACE
NOTE:
INSPECTION AT FR 35 AND PRESSURE DECK UPPER SURFACE,
BETWEEN FR 35 AND FR 36, INCLUDING CONNECTIONS TO
CENTER WING BOX AT FR 35 AND FR 36.
533152-01-8 ************** TASK DELETED ************** N/A
533153-01-4 ************** TASK DELETED ************** N/A
3-53 533153-02-1 191 GVI PRESSURE BULKHEAD AT FR 35 AFT FACE AF MRB CPCP MRB 533153-02-1 533100-210-807 6 YE 6 YE APPL
192
GENERAL VISUAL INSPECTION OF PRESSURE BULKHEAD AFT
FACE AND LOWER SKIN OF PRESSURE DECK LOWER SURFACE
NOTE:
INSPECTION AT FR 35 AND LOWER SKIN OF PRESSURE DECK
LOWER SURFACE, BETWEEN FR 35 AND FR 36.
3-53 533153-02-2 191 GVI PRESSURE BULKHEAD AT FR 35.8 AFT FACE AF MRB CPCP MRB 533153-02-2 533100-210-807 6 YE 6 YE N/A
192
GENERAL VISUAL INSPECTION OF PRESSURE BULKHEAD AFT
FACE AND LOWER SKIN OF PRESSURE DECK LOWER SURFACE
NOTE:
INSPECTION AT FR 35.8 AND LOWER SKIN OF PRESSURE DECK
LOWER SURFACE, BETWEEN FR 35.8 AND FR 36.
3-53 533154-01-1 147 DET MLG DOORS FITTINGS AF MRB CPCP MRB 533154-01-1 533100-210-014 6 YE 6 YE APPL
148
DETAILED INSPECTION OF HINGE AND ACTUATOR FITTINGS
FOR MLG DOORS AT KEELBEAM
3-53 533154-03-2 147 SDI MLG DOORS FITTINGS NDT ALI ALI 533154-03-2 533100-220-001 3000 FC 2250 FC N/A
148
734 SPECIAL DETAILED INSPECTION (US AND HFEC) OF ACTUATOR
744 FITTING FOR MLG DOORS AT KEEL BEAM, LH/RH.
3-53 533154-04-2 147 SDI MLG DOORS FITTINGS NDT ALI ALI 533154-04-2 533100-220-813 3000 FC 3000 FC N/A
148
734 SPECIAL DETAILED INSPECTION (HFEC) OF THE KEEL BEAM
744 MLG DOOR FWD HINGE FITTING, LH/RH.
3-53 533155-03-1 147 SDI KEEL BEAM BOX ELLIPTICAL CUTOUT NDT ALI ALI 533155-03-1 533100-220-007 38400 FC 17500 FC N/A
148 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF KEELBEAM BOX 60000 FH 39300 FH
ELLIPTICAL CUTOUT AT FR 46, LH/RH
3-53 533157-01-1 200 DET SKIN AROUND AINS ANTENNA CUTOUT AT FR 35/36 AF MRB CPCP MRB 533157-01-1 533100-210-046 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND AINS ANTENNA
CUTOUT AT FR 35/36, BETWEEN STRINGER 1, LH/RH AND
RIVETED AREA AROUND AINS ANTENNA CUTOUT DOUBLER,
BETWEEN FR 35/36 AND STRINGER 1, LH/RH.
533157-01-2 ************** TASK DELETED ************** N/A
3-53 533180-01-1 145 SDI UPPER SURFACES OF PRESSURE DECK MEMBRANES AND SIDE NDT ALI WFD ALI 533180-01-1 533100-220-803 48100 FC 6100 FC APPL
146 BOXES, BETWEEN FR 42 AND FR 46 OR OR
96300 FH 12200 FH
SPECIAL DETAILED INSPECTION (HFEC) OF UPPER SURFACE
OF PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR
42 AND FR 46, AT CONNECTIONS TO LONGITUDINAL BEAMS
AND SUPPORT RIBS (INCLUDING LATERAL OUTER PART OF
CONNECTION PLATES AT FR 43) AT Y=+/- 254 MM, Y=+/-
765 MM, Y=+/- 1292 MM AND Y=+/- 1650 MM
APPENDIX A
AEG/AMP/A320 Page 98 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533180-01-2 145 SDI UPPER SURFACES OF PRESSURE DECK MEMBRANES AND SIDE NDT ALI WFD ALI 533180-01-2 533100-220-803 34000 FC 4500 FC N/A
146 BOXES, BETWEEN FR 42 AND FR 46 OR OR
68100 FH 9000 FH
SPECIAL DETAILED INSPECTION (HFEC) OF UPPER SURFACE
OF PRESSURE DECK MEMBRANES AND SIDE BOXES, BETWEEN FR
42 AND FR 46, AT CONNECTIONS TO LONGITUDINAL BEAMS
AND SUPPORT RIBS (INCLUDING LATERAL OUTER PART OF
CONNECTION PLATES AT FR 43) AT Y=+/- 254 MM, Y=+/-
765 MM, Y=+/- 1292 MM AND Y=+/- 1650 MM
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533181-01-1 147 SDI LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO NDT ALI WFD ALI 533181-01-1 533100-220-802 48500 FC 12500 FC APPL
148 PRESSURE DECK MEMBRANE BETWEEN FR 42 AND FR 46 OR OR
97100 FH 25100 FH
SPECIAL DETAILED INSPECTION (LFEC) OF LONGITUDINAL
BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK
MEMBRANE BETWEEN FR 42 AND FR 46 AT Y=+/- 254 MM,
Y=+/- 765MM, Y=+/- 1292 MM AND SIDE BOX FLANGE AT
Y=+/- 1650 MM
3-53 533181-01-2 147 SDI LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO NDT ALI WFD ALI 533181-01-2 533100-220-802 33300 FC 7500 FC N/A
148 PRESSURE DECK MEMBRANE BETWEEN FR 42 AND FR 46 OR OR
66700 FH 15100 FH
SPECIAL DETAILED INSPECTION (LFEC) OF LONGITUDINAL
BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK
MEMBRANE BETWEEN FR 42 AND FR 46 AT Y=+/- 254 MM,
Y=+/- 765MM, Y=+/- 1292 MM AND SIDE BOX FLANGE AT
Y=+/- 1650 MM
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533181-01-3 147 SDI LONGITUDINAL BEAMS FLANGES AT ATTACHMENT AREA TO NDT ALI WFD ALI 533181-01-3 533100-220-802 46400 FC 9100 FC N/A
148 PRESSURE DECK MEMBRANE BETWEEN FR 42 AND FR 46 OR OR
92900 FH 18300 FH
SPECIAL DETAILED INSPECTION (LFEC) OF LONGITUDINAL
BEAMS FLANGES AT ATTACHMENT AREA TO PRESSURE DECK
MEMBRANE BETWEEN FR 42 AND FR 46 AT Y=+/- 254 MM,
Y=+/- 765MM, Y=+/- 1292 MM AND SIDE BOX FLANGE AT
Y=+/- 1650 MM
3-53 533182-01-1 145 DET CENTER FUSELAGE AF MRB MRB 533182-01-1 533100-210-802 48000 FC 20000 FC APPL
146 OR OR
DETAILED INSPECTION OF CONNECTION PLATES AT FR 43, 96000 FH 40000 FH
(EXCLUDING LATERAL OUTER PART OF CONNECTION PLATES)
BETWEEN Y=+/- 254 MM, AND BETWEEN Y=+ 765 MM AND Y=+
1292 MM, AND BETWEEN Y=- 765 MM AND Y=- 1292 MM (3
PLACES)
3-53 533185-01-1 137 SDI PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING NDT ALI ALI 533185-01-1 533100-220-804 48000 FC 31200 FC N/A
138 BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER OR OR
BRACKETS AT FR 36 96000 FH 62500 FH
SPECIAL DETAILED INSPECTION (LFEC AND ROTO) OF
PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING
BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER
BRACKETS AT FR 36
APPENDIX A
AEG/AMP/A320 Page 99 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533185-01-2 137 SDI PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING NDT ALI ALI 533185-01-2 533100-220-804 48000 FC 31200 FC APPL
138 BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER OR OR
BRACKETS AT FR 36 96000 FH 62500 FH
SPECIAL DETAILED INSPECTION (LFEC AND ROTO) OF
PRESSURE DECK MEMBRANE UPPER SURFACE TO CENTER WING
BOX, UNDER TITANIUM ANGLE CONNECTION AND CORNER
BRACKETS AT FR 36
3-53 533186-01-1 137 SDI FR 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENTS NDT ALI ALI 533186-01-1 533100-220-805 40000 FC 15000 FC APPL
138 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF FRAME FORWARD 80000 FH 30000 FH
FACE TO PRESSURE BULKHEAD ATTACHMENTS, AROUND RIVETS
AND HOLES BETWEEN STRINGER 28 AND STRINGER 31, LH/RH
NOTE:
INSPECTION OF FR 35 FORWARD FACE.
3-53 533186-01-2 137 SDI FR 35 FORWARD FACE TO PRESSURE BULKHEAD ATTACHMENTS NDT ALI ALI 533186-01-2 533100-220-805 40000 FC 15000 FC N/A
138 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF FRAME FORWARD 80000 FH 30000 FH
FACE TO PRESSURE BULKHEAD ATTACHMENTS, AROUND RIVETS
AND HOLES BETWEEN STRINGER 28 AND STRINGER 31, LH/RH
NOTE:
INSPECTION OF FR 35.8 FORWARD FACE.
3-53 533188-01-1 191 DET PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL AF ALI ALI 533188-01-1 533100-220-806 30300 FC 8400 FC APPL
192 STRUTS
DETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE,
LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT
Y= +/-765 MM (2 PLACES)
NOTE:
PRESSURE BULKHEAD FR 35.
3-53 533188-01-2 191 DET PRESSURE BULKHEAD, AFT FACE, LOWER PART OF VERTICAL AF ALI ALI 533188-01-2 533100-220-806 30300 FC 8400 FC N/A
192 STRUTS
DETAILED INSPECTION OF PRESSURE BULKHEAD, AFT FACE,
LOWER PART OF VERTICAL STRUTS (200 MM FROM BOTTOM) AT
Y= +/-765 MM (2 PLACES)
NOTE:
PRESSURE BULKHEAD FR 35.8.
3-53 533189-01-1 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-1 533100-220-807 26900 FC 21500 FC APPL
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 53800 FH 43000 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
3-53 533189-01-3 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-3 533100-220-807 50100 FC 32600 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 100200 FH 65200 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
3-53 533189-01-4 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-4 533100-220-807 16900 FC 16500 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 33900 FH 33000 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 100 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 533189-01-5 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-5 533100-220-807 38500 FC 16500 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 77000 FH 33000 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533189-01-6 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-6 533100-220-807 31700 FC 25000 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 63400 FH 50000 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533189-01-7 191 SDI ANGLE FITTING ATTACHMENT AT FR 36 AT STRINGER 30 NDT ALI ALI 533189-01-7 533100-220-807 10500 FC 10500 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF ANGLE FITTING 45200 FH 45200 FH
FORWARD ATTACHMENT, AT FR 36 AT STRINGER 30, LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 533191-01-1 200 SDI STRINGER COUPLING AREA AT FR 47 NDT ALI WFD ALI 533191-01-1 533100-220-809 40300 FC 6700 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (HFEC AND US) OF STRINGER 80700 FH 13400 FH
COUPLING FROM STRINGER 10 LH/RH TO CROWN CENTER LINE,
FWD AND AFT FR 47, INTERNAL SURFACE.
2-53 533900-01-1 140 OPC FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/01 533900-210-001 36 MO APPL
OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE HOLES IN
PRESSURE FLOOR FROM MLG BAY
534103-01-1 ************** TASK DELETED ************** N/A
534103-01-2 ************** TASK DELETED ************** N/A
534103-01-3 ************** TASK DELETED ************** N/A
534103-01-4 ************** TASK DELETED ************** N/A
3-53 534106-01-1 252 DET FRAME SPLICES FR 53-56 AF ALI ALI 534106-01-1 534100-210-840 51300 FC 12900 FC APPL
OR OR
DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT 102700 FH 25800 FH
AREA LOCATED ABOVE STRINGER 18 RH
NOTE:
INSPECT AREA FROM FR 53 TO FR 56.
534106-01-3 ************** TASK DELETED ************** N/A
3-53 534106-01-4 252 DET FRAME SPLICES FR 53-56 AF ALI ALI 534106-01-4 534100-210-840 12000 FC 4000 FC N/A
OR OR
DETAILED INSPECTION OF FRAME SPLICES AND ADJACENT 69000 FH 23000 FH
AREA LOCATED ABOVE STRINGER 18 RH
NOTE:
INSPECT AREA FROM FR 53 TO FR 56.
THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534106-02-4.
534106-01-5 ************** TASK DELETED ************** N/A
534106-02-1 ************** TASK DELETED ************** N/A
534106-02-3 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 101 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534106-02-4 252 SDI FRAME SPLICES FR 53-56 NDT ALI ALI 534106-02-4 534100-220-004 12000 FC 9100 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (US) OF FRAME SPLICES AND 69000 FH 52500 FH
ADJACENT AREA LOCATED ABOVE STRINGER 18
NOTE:
INSPECT AREA FROM FR 53 TO FR 56.
THIS TASK IS AN ALTERNATIVE INSPECTION TO TASK
534106-01-4.
3-53 534107-01-1 153 DET FUSELAGE INTERNAL STRUCTURE FR 46-65 AF MRB CPCP MRB 534107-01-1 534100-210-014 6 YE 6 YE APPL
154
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BETWEEN FR 46 AND FR 65, INCLUDING AFT FACE OF
PRESSURE BULKHEAD FROM STRINGER 38, LH/RH TO BOTTOM
CENTER LINE.
3-53 534108-01-2 100 GVI FUSELAGE EXTERNAL SURFACE FR 47-70 AF ALI ALI 534108-01-2 534100-210-810 3000 FC 3000 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47 AND FR 70, FROM STRINGER 23,
LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED BY
BELLY FAIRING
3-53 534108-01-4 100 GVI FUSELAGE EXTERNAL SURFACE FR 47/51-70 AF ALI ALI 534108-01-4 534100-210-810 3000 FC 3000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47/51 AND FR 70, FROM STRINGER
23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED
BY BELLY FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 534108-01-6 100 GVI FUSELAGE EXTERNAL SURFACE FR 47/54-70 AF ALI ALI 534108-01-6 534100-210-810 3000 FC 3000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47/54 AND FR 70, FROM STRINGER
23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED
BY BELLY FAIRING
3-53 534108-01-8 100 GVI FUSELAGE EXTERNAL SURFACE FR 47/51-70 AF ALI ALI 534108-01-8 534100-210-810 1300 FC 1300 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN FR 47/54 AND FR 70, FROM STRINGER
23, LH/RH TO BOTTOM CENTERLINE, EXCEPT AREA COVERED
BY BELLY FAIRING
534109-01-1 ************** TASK DELETED ************** N/A
534110-01-1 ************** TASK DELETED ************** N/A
534110-01-2 ************** TASK DELETED ************** N/A
3-53 534111-01-1 200 DET ADF2 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534111-01-1 534100-210-002 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 48 AND FR 49.
FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM EMBODIMENT OF MOD 20053 VIA SB.
3-53 534111-01-2 200 DET ADF2 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534111-01-2 534100-210-002 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 47.1 AND FR 47.2.
FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM EMBODIMENT OF MOD 20053 VIA SB.
APPENDIX A
AEG/AMP/A320 Page 102 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534111-01-4 200 DET ADF2 ANTENNA SKIN CUTOUT AF ALI ALI 534111-01-4 534100-210-002 12 YE 12 YE 24 YE 12 YE N/A
MRB CPCP MRB 534111-01-4 OR OR OR OR
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA 28800 FC 16700 FC 28800 FC 16700 FC
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE OR OR OR OR
60000 FH 41700 FH 60000 FH 41700 FH
NOTE:
INSPECTION BETWEEN FR 55 AND FR 56.
FOR PRE 20053 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM EMBODIMENT OF MOD 20053 VIA SB.
534111-01-5 ************** TASK DELETED ************** N/A
3-53 534111-01-6 200 DET ADF2 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534111-01-4 534100-210-002 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 55 AND FR 56.
3-53 534111-01-8 200 DET ADF2 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534111-01-8 534100-210-002 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND ADF2 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 52 AND FR 53.
3-53 534112-01-1 200 DET VHF3 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534112-01-1 534100-210-019 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 52 AND FR 53.
3-53 534112-01-4 200 DET VHF3 ANTENNA SKIN CUTOUT AF ALI ALI 534112-01-4 534100-210-019 12 YE 12 YE 24 YE 12 YE N/A
MRB CPCP MRB 534112-01-4 OR OR OR OR
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA 31200 FC 18700 FC 31200 FC 18700 FC
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE OR OR OR OR
60000 FH 56100 FH 60000 FH 56100 FH
NOTE:
INSPECTION BETWEEN FR 60 AND FR 61.
3-53 534112-01-5 200 DET VHF3 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534112-01-5 534100-210-019 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE
NOTE:
INSPECTION BETWEEN FR 56 AND FR 57.
3-53 534112-01-6 200 DET VHF3 ANTENNA SKIN CUTOUT AF MRB CPCP MRB 534112-01-4 534100-210-019 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF SKIN AROUND VHF 3 ANTENNA
CUTOUT, BETWEEN STRINGER 1, LH/RH, EXTERNAL SURFACE.
NOTE:
INSPECTION BETWEEN FR 60 AND FR 61.
534112-01-7 ************** TASK DELETED ************** N/A
3-53 534113-01-3 200 DET CIRCUMFERENTIAL SKIN SPLICE AT FR 64 AF ALI ALI 534113-01-3 534100-210-020 12500 FC 10500 FC N/A
OR OR
DETAILED INSPECTION OF SKIN IN CIRCUMFERENTIAL SPLICE 56600 FH 47600 FH
AND STRINGER COUPLING AREAS AT FR 64, FROM STRINGER
10, LH/RH TO CROWN CENTER LINE, EXTERNAL SURFACE
3-53 534118-01-4 200 GVI REAR FUSELAGE AF MRB MRB 534118-01-4 534100-210-823 30000 FC 3000 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE
NOTE:
INSPECTION FROM FR 47 TO FR 70.
APPENDIX A
AEG/AMP/A320 Page 103 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534118-01-5 200 GVI REAR FUSELAGE AF MRB MRB 534118-01-5 534100-210-823 30000 FC 3000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE
NOTE:
INSPECTION FROM FR 47/51 TO FR 70.
3-53 534118-01-6 200 GVI REAR FUSELAGE AF MRB MRB 534118-01-6 534100-210-823 30000 FC 3000 FC N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, BETWEEN STRINGER 23, LH/RH TO CROWN CENTER
LINE
NOTE:
INSPECTION FROM FR 47/54 TO FR 70.
3-53 534120-01-1 151 DET REAR FUSELAGE AF ALI ALI 534120-01-1 534100-210-825 42700 FC 8200 FC N/A
152 OR OR
161 DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE, 85400 FH 16400 FH
162 BETWEEN CABIN FLOOR PANELS AND CARGO COMPARTMENT
FLOOR, INCLUDING CABIN FLOOR STRUCTURE, FROM FR 47 TO
FR 65
534121-01-1 ************** TASK DELETED ************** N/A
3-53 534121-01-3 200 SDI CIRCUMFERENTIAL SKIN SPLICE AT FR 64 NDT ALI ALI 534121-01-3 534100-220-010 12500 FC 10500 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT 56500 FH 47600 FH
CIRCUMFERENTIAL SKIN SPLICE AT FR 64, FROM STRINGER
10, LH/RH TO CROWN CENTERLINE, EXTERNAL SURFACE
534121-01-4 ************** TASK DELETED ************** N/A
3-53 534122-01-1 250 SDI REAR FUSELAGE NDT ALI WFD ALI 534122-01-1 534100-220-816 36200 FC 8700 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 72500 FH 17400 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE SATCOM ANTENNA, IN THE AREA OF FR 58 TO FR 61,
STRINGER 2 LH AND STRINGER 2 RH, EXCEPT RIVETS AT
STRINGER OR FRAME JUNCTIONS
534122-01-2 ************** TASK DELETED ************** N/A
3-53 534122-01-3 200 SDI REAR FUSELAGE NDT ALI WFD ALI 534122-01-3 534100-220-816 41300 FC 7800 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 82600 FH 15600 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE SATCOM ANTENNA, IN THE AREA OF FR 58 TO FR 61,
STRINGER 2 LH AND STRINGER 2 RH, EXCEPT RIVETS AT
STRINGER OR FRAME JUNCTIONS
3-53 534122-01-5 200 SDI REAR FUSELAGE NDT ALI WFD ALI 534122-01-5 534100-220-816 60000 FC 10500 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 120000 FH 21100 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE SATCOM ANTENNA, IN THE AREA OF FR 58 TO FR 61,
STRINGER 2 LH AND STRINGER 2 RH, EXCEPT RIVETS AT
STRINGER OR FRAME JUNCTIONS
534122-02-4 ************** TASK DELETED ************** N/A
534123-01-1 ************** TASK DELETED ************** N/A
3-53 534123-01-2 261 SDI REAR FUSELAGE NDT ALI ALI 534123-01-2 534100-220-802 21400 FC 8600 FC N/A
262 OR OR
263 SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE 42900 FH 17300 FH
264 INTERNAL STRUCTURE, FR 66 AND FR 68 INNER CAP JOINT
TO GUSSETS PLATE FROM STRINGER 10 TO STRINGER 16,
LH/RH
3-53 534123-01-3 261 SDI REAR FUSELAGE NDT ALI ALI 534123-01-3 534100-220-802 26400 FC 10100 FC APPL
262 OR OR
263 SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE 52900 FH 20300 FH
264 INTERNAL STRUCTURE, FR 66 AND FR 68 INNER CAP JOINT
TO GUSSETS PLATE FROM STRINGER 10 TO STRINGER 16,
LH/RH
APPENDIX A
AEG/AMP/A320 Page 104 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
534123-01-4 ************** TASK DELETED ************** N/A
534123-01-5 ************** TASK DELETED ************** N/A
534123-01-6 ************** TASK DELETED ************** N/A
534123-01-9 ************** TASK DELETED ************** N/A
3-53 534124-01-1 263 SDI REAR FUSELAGE NDT ALI ALI 534124-01-1 534100-220-808 22100 FC 5400 FC N/A
264
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
3-53 534124-01-2 263 SDI REAR FUSELAGE NDT ALI ALI 534124-01-2 534100-220-808 33600 FC 5900 FC N/A
264
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
3-53 534124-01-3 263 SDI REAR FUSELAGE NDT ALI ALI 534124-01-3 534100-220-808 38700 FC 6800 FC APPL
264
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
534124-01-4 ************** TASK DELETED ************** N/A
534124-01-5 ************** TASK DELETED ************** N/A
534124-01-6 ************** TASK DELETED ************** N/A
534124-01-7 ************** TASK DELETED ************** N/A
3-53 534124-01-8 263 SDI REAR FUSELAGE NDT ALI ALI 534124-01-8 534100-220-808 42200 FC 7100 FC N/A
264
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
3-53 534124-01-9 263 SDI REAR FUSELAGE NDT ALI ALI 534124-01-9 534100-220-808 45400 FC 7600 FC N/A
264
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
3-53 534124-09-4 263 SDI REAR FUSELAGE NDT MRB FMP MRB 534124-09-4 18 YE NOTE N/A
264 NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF AFT PASSENGER/
CREW DOOR CUTOUT, AFT UPPER CORNER BETWEEN STRINGER 8
AND STRINGER 10, FR 68 WEB JOINT TO DOOR FRAME, AFT
FACE, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-53 534125-01-2 100 SDI REAR FUSELAGE NDT ALI WFD ALI 534125-01-2 534100-220-809 32000 FC 3400 FC N/A
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT,
BETWEEN FR 65 AND FR 66 AT AND BELOW STRINGER 37, TWO
UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH
3-53 534125-01-3 100 SDI REAR FUSELAGE NDT ALI WFD ALI 534125-01-3 534100-220-809 42000 FC 4500 FC APPL
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
EXTERNAL SURFACE AT WATER SERVICE PANEL CUTOUT,
BETWEEN FR 65 AND FR 66 AT AND BELOW STRINGER 37, TWO
UPPER RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, LH
534125-01-4 ************** TASK DELETED ************** N/A
534125-01-5 ************** TASK DELETED ************** N/A
534125-01-6 ************** TASK DELETED ************** N/A
534125-01-7 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 105 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534126-01-2 100 SDI REAR FUSELAGE NDT ALI WFD ALI 534126-01-2 534100-220-810 29000 FC 2100 FC N/A
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT,
BETWEEN FR 65 AND FR 66 BELOW STRINGER 33, TWO UPPER
RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH
3-53 534126-01-3 100 SDI REAR FUSELAGE NDT ALI WFD ALI 534126-01-3 534100-220-810 35100 FC 2800 FC APPL
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN
EXTERNAL SURFACE AT WASTE SERVICE PANEL CUTOUT,
BETWEEN FR 65 AND FR 66 BELOW STRINGER 33, TWO UPPER
RIVET ROWS AT SKIN TO REINFORCEMENT JOINT, RH
534126-01-4 ************** TASK DELETED ************** N/A
534126-01-5 ************** TASK DELETED ************** N/A
534126-01-6 ************** TASK DELETED ************** N/A
534126-01-7 ************** TASK DELETED ************** N/A
3-53 534127-01-1 263 SDI REAR FUSELAGE NDT ALI ALI 534127-01-1 534100-220-811 26800 FC 10700 FC N/A
264
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, LATERAL FR 68 JOINT TO UPPER FR
68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH
534127-01-2 ************** TASK DELETED ************** N/A
3-53 534127-01-3 263 SDI REAR FUSELAGE NDT ALI ALI 534127-01-3 534100-220-811 28300 FC 11000 FC APPL
264
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, LATERAL FR 68 JOINT TO UPPER FR
68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH
534127-01-4 ************** TASK DELETED ************** N/A
534127-01-5 ************** TASK DELETED ************** N/A
534127-01-8 ************** TASK DELETED ************** N/A
3-53 534127-09-5 263 SDI REAR FUSELAGE NDT MRB FMP MRB 534127-09-5 18 YE 6 YE N/A
264 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE
INTERNAL STRUCTURE, LATERAL FR 68 JOINT TO UPPER FR
68 BETWEEN STRINGER 4 AND STRINGER 5, LH/RH
NOTE:
THRESHOLD:
- FOR PRE 154905 AIRCRAFT RETROFITTED, THRESHOLD TO
BE COUNTED FROM SB 53-1279 EMBODIMENT.
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
534128-01-3 ************** TASK DELETED ************** N/A
534128-01-4 ************** TASK DELETED ************** N/A
534128-01-6 ************** TASK DELETED ************** N/A
3-53 534131-01-1 100 GVI FUSELAGE SKIN BETWEEN FR 65 AND 70 AF ALI ALI 534131-01-1 534100-210-814 37900 FC 37900 FC APPL
200
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND AFT
PASSENGER/CREW DOOR CUTOUTS, BETWEEN FR 65 AND FR 70
AND FROM STRINGER 6 TO STRINGER 26, EXTERNAL SURFACE
(EXCEPT AREA UNDER SCUFF PLATE), LH/RH
534131-01-10 ************** TASK DELETED ************** N/A
534131-01-11 ************** TASK DELETED ************** N/A
534131-01-3 ************** TASK DELETED ************** N/A
534131-01-4 ************** TASK DELETED ************** N/A
534131-01-6 ************** TASK DELETED ************** N/A
534131-01-7 ************** TASK DELETED ************** N/A
534131-01-8 ************** TASK DELETED ************** N/A
534131-01-9 ************** TASK DELETED ************** N/A
534132-01-10 ************** TASK DELETED ************** N/A
534132-01-11 ************** TASK DELETED ************** N/A
534132-01-12 ************** TASK DELETED ************** N/A
534132-01-13 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 106 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534132-01-4 260 DET AFT PAX/CREW DOOR CUTOUT UPR CORNER AF ALI ALI 534132-01-4 534100-210-010 15100 FC 10000 FC APPL
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY
THE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RH
534132-01-5 ************** TASK DELETED ************** N/A
534132-01-6 ************** TASK DELETED ************** N/A
534132-01-7 ************** TASK DELETED ************** N/A
3-53 534132-01-8 260 DET AFT PAX/CREW DOOR CUTOUT UPR CORNER AF ALI ALI 534132-01-8 534100-210-010 11700 FC 7600 FC N/A
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY
THE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RH
3-53 534132-01-9 260 DET AFT PAX/CREW DOOR CUTOUT UPR CORNER AF ALI ALI 534132-01-9 534100-210-010 12000 FC 8000 FC N/A
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UPPER CORNERS, INCLUDING SKIN AND INTERNALLY
THE VISIBLE PORTION OF THE INTERNAL DOUBLER, LH/RH
3-53 534134-01-1 261 DET DOOR STOP FITTINGS FR 66 AND 68 AF MRB CPCP MRB 534134-01-1 534100-210-029 12 YE 12 YE APPL
262
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 66
AND FR 68, LH/RH
3-53 534135-01-4 261 DET AFT PAX/CREW DOOR CUTOUT AF MRB CPCP MRB 534135-01-4 534100-210-003 6 YE 6 YE APPL
262
263 DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT
264 PASSENGER/CREW DOOR CUTOUT, ABOVE CABIN FLOOR LEVEL,
BETWEEN FR 65 AND FR 69 AND FROM STRINGER 6 TO
STRINGER 23, LH/RH, EXCLUDING THE LOWER CORNERS OF
THE DOOR ENTRANCE AREA AT FR 66 AND FR 68, BETWEEN
STRINGER 22 AND 23, LH/RH
NOTE:
EXCLUDED AREA COVERED BY TASKS 534143-01-1 OR
534143-01-3.
3-53 534136-01-1 100 DET AFT PAX/CREW DOOR UNDER SCUFF-PLATE AF MRB CPCP MRB 534136-01-1 534100-210-041 12 YE 12 YE APPL
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR
CUTOUT, UNDERNEATH THE SCUFF PLATE, LH/RH
534137-01-2 ************** TASK DELETED ************** N/A
534139-01-3 ************** TASK DELETED ************** N/A
534140-01-10 ************** TASK DELETED ************** N/A
534140-01-11 ************** TASK DELETED ************** N/A
534140-01-12 ************** TASK DELETED ************** N/A
534140-01-6 ************** TASK DELETED ************** N/A
534140-01-7 ************** TASK DELETED ************** N/A
3-53 534140-01-8 100 GVI FUSELAGE SKIN AROUND OUTFLOW VALVE CUTOUT AF ALI ALI 534140-01-8 534100-210-815 53400 FC 7800 FC APPL
GENERAL VISUAL INSPECTION OF FUSELAGE SKIN AROUND
OUTFLOW VALVE CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 26 TO STRINGER 31, RH, EXTERNAL SURFACE
534141-01-11 ************** TASK DELETED ************** N/A
534141-01-12 ************** TASK DELETED ************** N/A
534141-01-13 ************** TASK DELETED ************** N/A
3-53 534141-01-14 100 DET FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT AF ALI ALI 534141-01-14 534100-210-816 31200 FC 31200 FC N/A
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE
3-53 534141-01-5 100 DET FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT AF ALI ALI 534141-01-5 534100-210-816 37500 FC 37300 FC APPL
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE
534141-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 107 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534141-01-8 100 DET FUSELAGE SKIN AROUND WATER SERVICE PANEL CUTOUT AF ALI ALI 534141-01-8 534100-210-816 23600 FC 23600 FC N/A
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WATER
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 37 TO STRINGER 43, LH, EXTERNAL SURFACE
534141-01-9 ************** TASK DELETED ************** N/A
534142-01-10 ************** TASK DELETED ************** N/A
534142-01-12 ************** TASK DELETED ************** N/A
534142-01-13 ************** TASK DELETED ************** N/A
3-53 534142-01-14 100 DET FUSELAGE SKIN AROUND WASTE SERVICE PANEL CUTOUT AF ALI ALI 534142-01-14 534100-210-817 31700 FC 31700 FC N/A
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTE
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE
534142-01-2 ************** TASK DELETED ************** N/A
534142-01-6 ************** TASK DELETED ************** N/A
534142-01-8 ************** TASK DELETED ************** N/A
3-53 534142-01-9 100 DET FUSELAGE SKIN AROUND WASTE SERVICE PANEL CUTOUT AF ALI ALI 534142-01-9 534100-210-817 26500 FC 26500 FC APPL
DETAILED INSPECTION OF FUSELAGE SKIN AROUND WASTE
SERVICE PANEL CUTOUT, BETWEEN FR 65 AND FR 66 AND
FROM STRINGER 33 TO STRINGER 40, RH, EXTERNAL SURFACE
3-53 534143-01-1 261 DET FUSELAGE INTERNAL STRUCTURE FR 66-68 AF MRB CPCP MRB 534143-01-1 534100-210-834 5 YE 5 YE APPL
262
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOOR
LEVEL, AT FR 66 AND FR 68 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH
3-53 534143-01-3 261 DET FUSELAGE INTERNAL STRUCTURE FR 66-68 AF MRB CPCP MRB 534143-01-3 534100-210-834 6 YE 6 YE N/A
262
DETAILED INSPECTION OF AFT PASSENGER/CREW DOOR CUTOUT
LOWER CORNERS INTERNAL STRUCTURE, ABOVE CABIN FLOOR
LEVEL, AT FR 66 AND FR 68 FROM STRINGER 22 TO
STRINGER 23 AND AROUND GIRT BAR FITTINGS, LH/RH
3-53 534144-01-1 171 DET FUSELAGE INTERNAL STRUCTURE FR 65-70 AF MRB CPCP MRB 534144-01-1 534100-210-030 6 YE 6 YE APPL
172
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE,
BELOW CABIN FLOOR PANELS INCLUDING FLOOR STRUCTURE,
FROM FR 65 TO FR 70
3-53 534145-01-1 200 SDI SPLICE PLATE AT FR 47.5 NDT ALI WFD ALI 534145-01-1 534100-220-012 51300 FC 4500 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF SPLICE PLATE AT 102600 FH 9100 FH
CIRCUMFERENTIAL SKIN SPLICE AT FR 47.5, FROM STRINGER
16, LH/RH, TO CROWN CENTER LINE, EXTERNAL SURFACE
3-53 534146-01-1 251 GVI CABIN FLOOR STRUCTURE FR 47 TO FR 70 AF MRB CPCP MRB 534146-01-1 534100-210-801 12 YE 12 YE APPL
252
261 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
262 EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOOR
ENTRANCE AREA, FROM FR 47 TO FR 70
3-53 534146-01-2 251 GVI CABIN FLOOR STRUCTURE FR 47/51 TO FR 70 AF MRB CPCP MRB 534146-01-2 534100-210-801 12 YE 12 YE N/A
252
261 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
262 EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOOR
ENTRANCE AREA, FROM FR 47/51 TO FR 70
3-53 534146-01-3 251 GVI CABIN FLOOR STRUCTURE FR 47/54 TO FR 70 AF MRB CPCP MRB 534146-01-3 534100-210-801 12 YE 12 YE N/A
252
261 GENERAL VISUAL INSPECTION OF CABIN FLOOR STRUCTURE,
262 EXCLUDING AREAS BELOW GALLEYS AND TOILETS AND DOOR
ENTRANCE AREA, FROM FR 47/54 TO FR 70
APPENDIX A
AEG/AMP/A320 Page 108 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534147-01-1 251 DET FLOOR STRUCTURE FR 47 TO 70 AF MRB CPCP MRB 534147-01-1 534100-210-037 6 YE 6 YE APPL
252
261 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
262 AND 0.5M AROUND GALLEYS AND TOILETS
NOTE:
- INSPECTION FROM FR 47 TO FR 70, EXCEPT AREA BETWEEN
FR 66 AND FR 68 AND LATERAL SHEAR PLATES BETWEEN FR
68 AND FR 70.
3-53 534147-01-2 251 DET FLOOR STRUCTURE FR 47/51 TO 70 AF MRB CPCP MRB 534147-01-2 534100-210-037 6 YE 6 YE N/A
252
261 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
262 AND 0.5M AROUND GALLEYS AND TOILETS
NOTE:
- INSPECTION FROM FR 47/51 TO FR 70, EXCEPT AREA
BETWEEN FR 66 AND FR 68 AND LATERAL SHEAR PLATES
BETWEEN FR 68 AND FR 70.
3-53 534147-01-3 251 DET FLOOR STRUCTURE FR 47/54 TO 70 AF MRB CPCP MRB 534147-01-3 534100-210-037 6 YE 6 YE N/A
252
261 DETAILED INSPECTION OF CABIN FLOOR STRUCTURE, BELOW
262 AND 0.5M AROUND GALLEYS AND TOILETS
NOTE:
- INSPECTION FROM FR 47/54 TO FR 70, EXCEPT AREA
BETWEEN FR 66 AND FR 68 AND LATERAL SHEARPLATES
BETWEEN FR 68 AND FR 70.
3-53 534148-01-1 190 GVI FUSELAGE UNDER BELLY FAIRING AF MRB CPCP MRB 534148-01-1 534100-210-802 6 YE 6 YE APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE BETWEEN
FR 30 AND FR 53, UNDER THE BELLY FAIRING
3-53 534148-01-2 190 GVI FUSELAGE UNDER BELLY FAIRING AF MRB CPCP MRB 534148-01-2 534100-210-802 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE BETWEEN
FR 35.3 AND FR 48, UNDER THE BELLY FAIRING
3-53 534148-01-3 190 GVI FUSELAGE UNDER BELLY FAIRING AF MRB CPCP MRB 534148-01-3 534100-210-802 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE (AND
PORTION OF AFT CARGO DOOR COVERED BY BELLY FAIRING)
BETWEEN FR 27 AND FR 57, UNDER THE BELLY FAIRING
3-53 534148-01-4 190 GVI FUSELAGE UNDER BELLY FAIRING AF MRB CPCP MRB 534148-01-4 534100-210-802 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE, AND BELLY FAIRING SUPPORT STRUCTURE (AND
PORTION OF AFT CARGO DOOR COVERED BY BELLY FAIRING)
BETWEEN FR 27 AND FR 59, UNDER THE BELLY FAIRING
3-53 534150-01-1 152 DET AFT CARGO DOOR CUTOUT AF MRB CPCP MRB 534150-01-1 534100-210-004 12 YE 6 YE APPL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND AFT CARGO DOOR CUTOUT
NOTE:
INSPECTION FROM FR 52 TO FR 57 AND BETWEEN STRINGER
23 AND STRINGER 38.
3-53 534150-01-2 152 DET AFT CARGO DOOR CUTOUT AF MRB CPCP MRB 534150-01-2 534100-210-004 12 YE 6 YE N/A
162
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND AFT CARGO DOOR CUTOUT
NOTE:
INSPECTION FROM FR 55 TO FR 60 AND BETWEEN STRINGER
23 AND STRINGER 38.
APPENDIX A
AEG/AMP/A320 Page 109 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534152-01-2 252 DET AFT CARGO DOOR HINGE FITTINGS INTERNAL AF MRB CPCP MRB 534152-01-2 534100-210-005 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
INTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGE
FITTINGS, FROM FR 52 TO FR 57, BETWEEN STRINGER 22
AND STRINGER 23
534152-01-3 ************** TASK DELETED ************** N/A
3-53 534152-01-4 252 DET AFT CARGO DOOR HINGE FITTINGS INTERNAL AF MRB CPCP MRB 534152-01-4 534100-210-005 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
INTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGE
FITTINGS, FROM FR 55 TO FR 60, BETWEEN STRINGER 22
AND STRINGER 23
534152-01-5 ************** TASK DELETED ************** N/A
534153-01-1 ************** TASK DELETED ************** N/A
3-53 534153-01-2 152 DET AFT CARGO DOOR HINGE FITTINGS EXTERNAL AF MRB CPCP MRB 534153-01-2 534100-210-006 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF FUSELAGE AFT CARGO DOOR HINGE
FITTINGS AND EXTERNAL ATTACHMENT AREA
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
534153-01-3 ************** TASK DELETED ************** N/A
534153-01-5 ************** TASK DELETED ************** N/A
3-53 534154-01-1 152 SDI REAR FUSELAGE NDT ALI ALI 534154-01-1 534100-220-815 48000 FC 38600 FC APPL
OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE 96000 FH 77200 FH
STRUCTURE AT ATTACHMENT AREA UNDER AFT CARGO DOOR
OUTER HINGE FITTINGS FROM FR 55 TO FR 56 BETWEEN
STRINGER 22 AND STRINGER 23
3-53 534154-01-2 152 SDI REAR FUSELAGE NDT ALI ALI 534154-01-2 534100-220-815 48000 FC 38600 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF FUSELAGE 96000 FH 77200 FH
STRUCTURE AT ATTACHMENT AREA UNDER AFT CARGO DOOR
OUTER HINGE FITTINGS FROM FR 55 TO FR 56 BETWEEN
STRINGER 22 AND STRINGER 23
3-53 534155-01-2 154 DET AFT CARGO DOOR ECCENTRIC BOLTS AF MRB CPCP MRB 534155-01-2 534100-210-025 12 YE 12 YE 24 YE 12 YE APPL
DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTS
OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 53
AND FR 55A (6 PLACES)
534155-01-3 ************** TASK DELETED ************** N/A
3-53 534155-01-4 154 DET AFT CARGO DOOR ECCENTRIC BOLTS AF MRB CPCP MRB 534155-01-4 534100-210-025 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTS
OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 56
AND FR 58A (6 PLACES)
534155-01-5 ************** TASK DELETED ************** N/A
534156-01-1 ************** TASK DELETED ************** N/A
534156-01-2 ************** TASK DELETED ************** N/A
534156-02-1 ************** TASK DELETED ************** N/A
534156-02-2 ************** TASK DELETED ************** N/A
3-53 534157-01-4 152 GVI AFT CARGO DOOR LOCK FITTING AF ALI ALI 534157-01-4 534100-210-038 6 YE 6 YE APPL
MRB CPCP MRB 534157-01-1 OR OR
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK 13800 FC 13800 FC
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION OR OR
(6 PLACES) 27600 FH 27600 FH
NOTE:
- BETWEEN FR 53 AND FR 55A
APPENDIX A
AEG/AMP/A320 Page 110 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534157-01-5 152 GVI AFT CARGO DOOR LOCK FITTING AF ALI ALI 534157-01-5 534100-210-038 6 YE 6 YE N/A
MRB CPCP MRB 534157-01-2 OR OR
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK 13800 FC 13800 FC
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION OR OR
(6 PLACES) 27600 FH 27600 FH
NOTE:
- BETWEEN FR 56 AND FR 58A
3-53 534157-01-7 152 GVI AFT CARGO DOOR LOCK FITTING AF ALI ALI 534157-01-7 534100-210-038 6 YE 6 YE N/A
MRB CPCP MRB 534157-01-2 OR OR
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK 7500 FC 7500 FC
FITTINGS AND SURROUNDING STRUCTURE, EXTERNAL PORTION OR OR
(6 PLACES) 32300 FH 32300 FH
NOTE:
- BETWEEN FR 56 AND FR 58A
3-53 534159-01-1 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-1 534100-210-031 13400 FC 13400 FC APPL
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 26800 FH 26800 FH
AND LOWER CORNERS, EXTERNAL SURFACE
3-53 534159-01-2 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-2 534100-210-031 12000 FC 12000 FC N/A
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 51600 FH 51600 FH
AND LOWER CORNERS, EXTERNAL SURFACE
3-53 534159-01-3 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-3 534100-210-031 15500 FC 15500 FC N/A
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 31100 FH 31100 FH
AND LOWER CORNERS, EXTERNAL SURFACE
3-53 534159-01-4 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-4 534100-210-031 11300 FC 11300 FC N/A
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 22600 FH 22600 FH
AND LOWER CORNERS, EXTERNAL SURFACE
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 534159-01-5 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-5 534100-210-031 10000 FC 10000 FC N/A
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 43400 FH 43400 FH
AND LOWER CORNERS, EXTERNAL SURFACE
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 534159-01-6 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-6 534100-210-031 14800 FC 14800 FC N/A
154 OR OR
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER 29700 FH 29700 FH
AND LOWER CORNERS, EXTERNAL SURFACE
3-53 534159-01-7 152 DET AFT CARGO DOOR CUTOUT UPR/LWR CORNERS AF ALI ALI 534159-01-7 534100-210-031 12000 FC 12000 FC N/A
154
252 DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, UPPER
AND LOWER CORNERS, EXTERNAL SURFACE
3-53 534160-01-3 152 GVI AFT CARGO DOOR CUTOUT LATERAL FRAMES AF MRB CPCP MRB 534160-01-1 534100-210-803 6 YE 6 YE APPL
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT,
VISIBLE PART OF LATERAL FRAMES.
NOTE:
INSPECTION OF FR 52A AND FR 56.
APPENDIX A
AEG/AMP/A320 Page 111 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534160-01-4 152 GVI AFT CARGO DOOR CUTOUT LATERAL FRAMES AF MRB CPCP MRB 534160-01-2 534100-210-803 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT,
VISIBLE PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 55A AND FR 59.
3-53 534160-02-1 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-1 534100-220-803 1400 FC 1400 FC APPL
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 2800 FH 2800 FH
PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 52A AND FR 56.
3-53 534160-02-2 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-2 534100-220-803 1100 FC 1100 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 2300 FH 2300 FH
PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 55A AND FR 59.
3-53 534160-02-3 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-3 534100-220-803 1100 FC 1100 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 2200 FH 2200 FH
PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 52A AND FR 56.
3-53 534160-02-4 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-4 534100-220-803 1000 FC 1000 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 2100 FH 2100 FH
PART OF LATERAL FRAMES
NOTE:
- INSPECTION OF FR 55A AND FR 59.
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-53 534160-02-5 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-5 534100-220-803 800 FC 800 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 3500 FH 3500 FH
PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 55A AND FR 59.
3-53 534160-02-6 152 DET AFT CARGO DOOR CUTOUT LATERAL FRAMES AF ALI ALI 534160-02-6 534100-220-803 700 FC 700 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, VISIBLE 1400 FH 1400 FH
PART OF LATERAL FRAMES
NOTE:
INSPECTION OF FR 52A AND FR 56.
3-53 534163-01-1 152 GVI AFT CARGO DOOR ACTUATOR ATTACH BRACKET AF MRB MRB 534163-01-1 534100-210-819 16700 FC 16700 FC APPL
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR
ATTACH BRACKET
NOTE:
INSPECTION BETWEEN FLOOR BEAMS AT FR 53, FR 54 AND FR
55.
APPENDIX A
AEG/AMP/A320 Page 112 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534163-01-2 152 GVI AFT CARGO DOOR ACTUATOR ATTACH BRACKET AF MRB MRB 534163-01-2 534100-210-819 16700 FC 16700 FC N/A
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR
ATTACH BRACKET
NOTE:
INSPECTION BETWEEN FLOOR BEAMS AT FR 56, FR 57 AND FR
58.
3-53 534163-01-3 152 GVI AFT CARGO DOOR ACTUATOR ATTACH BRACKET AF MRB MRB 534163-01-3 534100-210-819 16700 FC 16700 FC N/A
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR
ATTACH BRACKET
NOTE:
INSPECTION BETWEEN FLOOR BEAMS AT FR 58, FR 59 AND FR
60.
3-53 534163-01-4 152 GVI AFT CARGO DOOR ACTUATOR ATTACH BRACKET AF ALI ALI 534163-01-4 534100-210-819 11400 FC 11400 FC N/A
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR ACTUATOR
ATTACH BRACKET
NOTE:
INSPECTION BETWEEN FLOOR BEAMS AT FR 56, FR 57 AND FR
58.
3-53 534164-01-1 162 DET BULK CARGO DOOR CUTOUT AF MRB CPCP MRB 534164-01-1 534100-210-028 12 YE 6 YE APPL
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND BULK CARGO COMPARTMENT DOOR, FROM FR 59 TO FR
63 AND BETWEEN STRINGER 23 AND STRINGER 38.
3-53 534167-02-1 162 GVI BULK CARGO DOOR STOP FITTING AF MRB CPCP MRB 534167-02-1 534100-210-805 6 YE 6 YE APPL
GENERAL VISUAL INSPECTION OF BULK CARGO DOOR STOP
FITTINGS INCLUDING VISIBLE PART OF LATERAL FR 60 AND
FR 62.
NOTE:
TPS APPLICATION IS LIMITED TO THE VISIBLE PART OF THE
LATERAL BULK CARGO DOOR FRAMES.
3-53 534169-01-1 162 DET FUSELAGE SKIN UNDER SCUFF PLATE AF MRB CPCP MRB 534169-01-1 534100-210-007 12 YE 12 YE 24 YE 12 YE APPL
164
DETAILED INSPECTION OF FUSELAGE SKIN UNDER BULK CARGO
DOOR SCUFF PLATE.
3-53 534171-01-2 162 SDI BULK CARGO DOOR CUTOUT UPR CORNERS NDT ALI ALI 534171-01-2 534100-210-008 19900 FC 19900 FC APPL
OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN 39800 FH 39800 FH
OF BULK CARGO DOOR CUTOUT AT UPPER CORNERS
3-53 534171-01-5 162 SDI BULK CARGO DOOR CUTOUT UPR CORNERS NDT ALI ALI 534171-01-5 534100-210-008 18800 FC 18800 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF FUSELAGE SKIN 37600 FH 37600 FH
OF BULK CARGO DOOR CUTOUT AT UPPER CORNERS
3-53 534172-01-2 162 GVI BULK CARGO DOOR CUTOUT SEALING PROFILE AF ALI ALI 534172-01-2 534100-210-804 6 YE 6 YE APPL
MRB CPCP MRB 534172-01-1 OR OR
GENERAL VISUAL INSPECTION OF SEALING PROFILE OF BULK 13600 FC 13600 FC
CARGO DOOR CUTOUT AT UPPER CORNERS OR OR
27200 FH 27200 FH
NOTE:
TPS TO BE APPLIED AT THRESHOLD/INTERVAL NOT EXCEEDING
6 YE.
3-53 534172-01-4 162 GVI BULK CARGO DOOR CUTOUT SEALING PROFILE AF ALI ALI 534172-01-4 534100-210-804 6 YE 6 YE N/A
MRB CPCP MRB 534172-01-4 OR OR
GENERAL VISUAL INSPECTION OF SEALING PROFILE OF BULK 14500 FC 14500 FC
CARGO DOOR CUTOUT AT UPPER CORNERS OR OR
29100 FH 29100 FH
NOTE:
TPS TO BE APPLIED AT THRESHOLD/INTERVAL NOT EXCEEDING
6 YE.
534176-01-1 ************** TASK DELETED ************** N/A
534177-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 113 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534178-01-1 200 DET EXTERNAL SKIN COVERED BY KU-BAND ANTENNA AF MRB CPCP MRB 534178-01-1 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF EXTERNAL SKIN COVERED BY
KU-BAND ANTENNA, FROM FR 58 TO FR 63, BETWEEN
STRINGER 4 LH AND STRINGER 4 RH.
3-53 534182-01-1 151 SDI FLOOR CROSS BEAM ATTACHMENT TO FR C47.3 AND C47.4 NDT ALI ALI 534182-01-1 534100-220-819 50000 FC 14000 FC N/A
152
SPECIAL DETAILED INSPECTION (HFEC) OF RIVET HOLES IN
FLOOR CROSS BEAM ATTACHMENT TO FR C47.3 AND C47.4
BETWEEN STRINGER POSITION P23 AND P24 (LH/RH).
3-53 534184-01-1 251 SDI BUTT JOINT SPLICE PLATE FR C47.3 NDT ALI ALI 534184-01-1 534100-220-820 53600 FC 13000 FC N/A
252 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF RIVET HOLES IN 107300 FH 26000 FH
BUTT JOINT SPLICE PLATE FR C47.3 FROM STRINGER 10 TO
STRINGER 12, INTERNAL SURFACE, LH/RH.
534185-01-1 ************** TASK DELETED ************** N/A
3-53 534185-01-2 100 SDI WASTE SERVICE PANEL CUTOUT NDT ALI ALI 534185-01-2 534100-220-818 40300 FC 39600 FC APPL
SPECIAL DETAILED INSPECTION (ROTO) OF INTERNAL
DOUBLER, WASTE SERVICE PANEL CUTOUT, FIVE RIVETS FROM
THE CORNERS JOINING DOUBLER AND CAP ALONG STRINGER 35
AND STRINGER 39, RH.
3-53 534186-01-1 151 SDI FRAME COUPLING RUN-OUT C47.3 BELOW EMERGENCY EXIT NDT ALI ALI 534186-01-1 534100-220-821 41000 FC 16200 FC N/A
152
SPECIAL DETAILED INSPECTION (ROTO) OF RIVET HOLE AT
FRAME COUPLING RUN-OUT C47.3 BELOW EMERGENCY EXIT
ESCAPE CHUTE COMPARTMENT BETWEEN STRINGER POSITION
P29 AND P30 (LH/RH).
3-53 534187-01-1 151 DET ESCAPE CHUTE SLIDE COMPARTMENT AF MRB CPCP MRB 534187-01-1 534100-210-049 6 YE 6 YE N/A
152
DETAILED INSPECTION OF ESCAPE CHUTE SLIDE COMPARTMENT
INTERNAL STRUCTURE, BETWEEN FR 47.2A AND FR 47.4 AND
FROM STRINGER 24 TO STRINGER 28, LH/RH
3-53 534187-01-2 151 DET ESCAPE CHUTE SLIDE COMPARTMENT AF MRB CPCP MRB 534187-01-2 534100-210-049 6 YE 6 YE N/A
152
DETAILED INSPECTION OF ESCAPE CHUTE SLIDE COMPARTMENT
INTERNAL STRUCTURE, BETWEEN FR 48A AND FR 50 AND FROM
STRINGER 24 TO STRINGER 28, LH/RH.
3-53 534188-01-1 251 SDI RUN-OUT OF UPPER INTERNAL SEALING PROFILE IN FR 47.4 NDT ALI ALI 534188-01-1 534100-220-822 50000 FC 15900 FC N/A
252
SPECIAL DETAILED INSPECTION (HFEC) OF FASTENER HOLE
AT RUN-OUT OF UPPER INTERNAL SEALING PROFILE IN FR
47.4 AT STRINGER 13 (LH/RH).
3-53 534189-01-1 251 SDI DOOR STOP FITTING FASTENER HOLES IN FR 47.4 NDT ALI ALI 534189-01-1 534100-220-823 50000 FC 26600 FC N/A
252
SPECIAL DETAILED INSPECTION (ROTO) OF DOOR STOP
FITTING FASTENER HOLES IN FR 47.4 AT STRINGER 13
(LH/RH) AND AT STRINGER 22 (LH/RH).
3-53 534190-01-1 251 DET DOOR STOP FITTINGS ON FR 47.2A & 47.4 AF MRB CPCP MRB 534190-01-1 534100-210-048 12 YE 12 YE N/A
252
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 47.2A
AND FR 47.4, LH/RH
3-53 534190-01-2 251 DET DOOR STOP FITTINGS ON FR 48A & 50 AF MRB CPCP MRB 534190-01-2 534100-210-048 12 YE 12 YE N/A
252
DETAILED INSPECTION OF DOOR STOP FITTINGS ON FR 48A
AND FR 50, LH/RH.
534191-01-1 ************** TASK DELETED ************** N/A
3-53 534192-01-1 251 DET INTL STRUCT AROUND EMERG EXIT CUTOUTS AF MRB CPCP MRB 534192-01-1 534100-210-047 12 YE 6 YE N/A
252
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT
EMERGENCY EXIT CUTOUTS, ABOVE CABIN FLOOR LEVEL,
BETWEEN FR 47.2 AND FR 47.5 AND FROM STRINGER 10 TO
STRINGER 23, LH/RH
APPENDIX A
AEG/AMP/A320 Page 114 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534192-01-2 251 DET INTL STRUCT AROUND EMERG EXIT CUTOUTS AF MRB CPCP MRB 534192-01-2 534100-210-047 12 YE 6 YE N/A
252
DETAILED INSPECTION OF INTERNAL STRUCTURE AROUND AFT
EMERGENCY EXIT CUTOUTS, ABOVE CABIN FLOOR LEVEL,
BETWEEN FR 48 AND FR 51 AND FROM STRINGER 10 TO
STRINGER 23, LH/RH.
3-53 534195-01-1 261 DET CABIN FLOOR STRUCTURE AFT ENTRANCE AREA AF MRB CPCP MRB 534195-01-1 534100-210-835 5 YE 5 YE APPL
262
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE AND
STRUCTURE BELOW AFT ENTRANCE AREA; BETWEEN FR 66 AND
FR 68 AND LATERAL SHEAR PLATES BETWEEN FR 68 AND FR
70.
NOTE:
IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS
NOT POSSIBLE DUE TO GALLEY CONFIGURATION, THE GALLEY
MUST BE REMOVED TO GET ACCESS TO THE INSPECTION AREA.
3-53 534195-01-2 261 DET CABIN FLOOR STRUCTURE AFT ENTRANCE AREA AF MRB CPCP MRB 534195-01-2 534100-210-835 6 YE 6 YE N/A
262
DETAILED INSPECTION OF CABIN FLOOR STRUCTURE AND
STRUCTURE BELOW AFT ENTRANCE AREA; BETWEEN FR 66 AND
FR 68 AND LATERAL SHEAR PLATES BETWEEN FR 68 AND FR
70.
NOTE:
- IN CASE SUFFICIENT ACCESS TO LATERAL SHEAR WEBS IS
NOT POSSIBLE DUE TO GALLEY CONFIGURATION, THE
GALLEY MUST BE REMOVED TO GET ACCESS TO THE
INSPECTION AREA.
THRESHOLD:
- FOR PRE 35792 OR PRE 35882 OR PRE 36309 PRE SB
53-1194 OR PRE 36309 PRE 53-1207 AIRCRAFT
RETROFITTED, THRESHOLD IS TO BE COUNTED FROM SB
53-1194 AND SB 53-1207 EMBODIMENT.
534197-01-1 ************** TASK DELETED ************** N/A
534197-01-2 ************** TASK DELETED ************** N/A
3-53 534198-01-1 200 DET EXTERNAL SKIN UNDER THE CABIN SWIFT BROADBAND ANTENNA AF MRB CPCP MRB 534198-01-1 534100-220-020 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF EXTERNAL SKIN UNDER THE CABIN
SWIFT BROADBAND ANTENNA, BETWEEN STRINGER 2 LH AND
STRINGER 2 RH, INCLUDING ANTENNA CABLE CUTOUT AND
ANTENNA ATTACHMENT POINTS.
NOTE:
INSPECTION FROM FR 57 TO FR 59.
534198-01-2 ************** TASK DELETED ************** N/A
3-53 534198-01-3 200 DET EXTERNAL SKIN UNDER THE CABIN SWIFT BROADBAND ANTENNA AF MRB CPCP MRB 534198-01-3 534100-220-020 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF EXTERNAL SKIN UNDER THE CABIN
SWIFT BROADBAND ANTENNA, BETWEEN STRINGER 2 LH AND
STRINGER 2 RH, INCLUDING ANTENNA CABLE CUTOUT AND
ANTENNA ATTACHMENT POINTS.
NOTE:
INSPECTION FROM FR 59 TO FR 61.
534198-01-4 ************** TASK DELETED ************** N/A
534198-01-5 ************** TASK DELETED ************** N/A
534198-01-6 ************** TASK DELETED ************** N/A
534199-01-1 ************** TASK DELETED ************** N/A
534199-01-2 ************** TASK DELETED ************** N/A
534199-01-3 ************** TASK DELETED ************** N/A
534199-01-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 115 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534199-02-1 200 SDI INTERNAL SKIN UNDER THE CABIN SWIFT BROADBAND ANTENNA NDT ALI WFD ALI 534199-02-1 534100-220-805 45600 FC 9900 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 60000 FH 19800 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE CABIN SWIFT BROADBAND ANTENNA, STRINGER 2 LH AND
STRINGER 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME
JUNCTIONS.
NOTE:
- INSPECTION IN THE AREA OF FR 57 TO FR 59.
THRESHOLD:
- FOR PRE 36590 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM SB 53-1211 OR SB 53-1219
EMBODIMENT.
3-53 534199-02-2 200 SDI INTERNAL SKIN UNDER THE CABIN SWIFT BROADBAND ANTENNA NDT ALI WFD ALI 534199-02-2 534100-220-805 33600 FC 7600 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 67200 FH 15200 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE CABIN SWIFT BROADBAND ANTENNA, STRINGER 2 LH AND
STRINGER 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME
JUNCTIONS.
NOTE:
- INSPECTION IN THE AREA OF FR 59 TO FR 61.
THRESHOLD:
- FOR PRE 36590 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM SB 53-1211 OR SB 53-1219
EMBODIMENT.
534199-02-3 ************** TASK DELETED ************** N/A
3-53 534199-02-4 200 SDI INTERNAL SKIN UNDER THE CABIN SWIFT BROADBAND ANTENNA NDT ALI WFD ALI 534199-02-4 534100-220-805 44800 FC 7800 FC N/A
OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF FUSELAGE SKIN 89600 FH 15600 FH
UNDER THE COMPLETE OUTER RIVET ROW OF THE DOUBLER OF
THE CABIN SWIFT BROADBAND ANTENNA, STRINGER 2 LH AND
STRINGER 2 RH, EXCEPT RIVETS AT STRINGER OR FRAME
JUNCTIONS.
NOTE:
- INSPECTION IN THE AREA OF FR 59 TO FR 61.
THRESHOLD:
- FOR PRE 36590 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM SB 53-1211 OR SB 53-1219
EMBODIMENT.
3-53 534250-01-2 152 DET FUSELAGE INTL STRUCT AROUND AFT CARGO DOOR CUTOUT AF MRB CPCP MRB 534250-01-2 534100-210-828 12 YE 6 YE N/A
162
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE
AROUND AFT CARGO DOOR CUTOUT, FROM FR 57 TO FR 61 AND
BETWEEN STRINGER 23 AND STRINGER 38
3-53 534252-01-1 252 DET FUSELAGE INTL STRUCT AT AFT CARGO DOOR HINGE FITTING AF MRB CPCP MRB 534252-01-1 534100-210-829 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF FUSELAGE INTERNAL STRUCTURE AT
INTERNAL ATTACHMENT AREA OF AFT CARGO DOOR HINGE
FITTINGS, FROM FR 57 TO FR 61, BETWEEN STRINGER 22
AND STRINGER 23
3-53 534253-01-1 152 DET FUSELAGE INTL STRUCT AT AFT CARGO DOOR HINGE FITTING AF MRB CPCP MRB 534253-01-1 534100-210-830 12 YE 12 YE N/A
DETAILED INSPECTION OF FUSELAGE AFT CARGO DOOR HINGE
FITTINGS AND EXTERNAL ATTACHMENT AREA
NOTE:
APPLICATION OF TPS IS LIMITED TO THE INNER SIDE OF
HINGE FITTINGS
3-53 534255-01-1 154 DET AFT CARGO DOOR ECCENTRIC BOLTS AF MRB CPCP MRB 534255-01-1 534100-210-831 12 YE 12 YE 24 YE 12 YE N/A
DETAILED INSPECTION OF AFT CARGO DOOR ECCENTRIC BOLTS
OF LOCKING MECHANISM AT LOCK FITTINGS, BETWEEN FR 58
AND FR 59A (4 PLACES)
534255-01-2 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 116 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 534257-01-2 152 GVI AFT CARGO DOOR LOCK FITTINGS AND SURROUNDING AF ALI ALI 534257-01-2 534100-210-821 6 YE 6 YE N/A
STRUCTURE MRB CPCP MRB 534257-01-1 OR OR
13800 FC 13800 FC
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK OR OR
FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 58 AND 27700 FH 27700 FH
FR 59A, EXTERNAL PORTION (4 PLACES)
3-53 534257-01-3 152 GVI AFT CARGO DOOR LOCK FITTINGS AND SURROUNDING AF ALI ALI 534257-01-3 534100-210-821 6 YE 6 YE N/A
STRUCTURE MRB CPCP MRB 534257-01-1 OR OR
7500 FC 7500 FC
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR LOCK OR OR
FITTINGS AND SURROUNDING STRUCTURE, BETWEEN FR 58 AND 22500 FH 22500 FH
FR 59A, EXTERNAL PORTION (4 PLACES)
3-53 534260-01-2 152 GVI AFT CARGO DOOR CUTOUT AF MRB CPCP MRB 534260-01-1 534100-210-822 6 YE 6 YE N/A
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT,
VISIBLE PART OF LATERAL FR 57A AND FR 60
3-53 534260-01-3 152 GVI AFT CARGO DOOR CUTOUT AF ALI ALI 534260-01-3 534100-210-822 6 YE 6 YE N/A
MRB CPCP MRB 534260-01-1 OR OR
GENERAL VISUAL INSPECTION OF AFT CARGO DOOR CUTOUT, 1000 FC 1000 FC
VISIBLE PART OF LATERAL FR 57A AND FR 60 OR OR
3000 FH 3000 FH
3-53 534260-02-1 152 DET AFT CARGO DOOR CUTOUT AF ALI ALI 534260-02-1 534100-220-814 1400 FC 1400 FC N/A
OR OR
DETAILED INSPECTION OF AFT CARGO DOOR CUTOUT, 2800 FH 2800 FH
VISIBLE PART OF LATERAL FR 57A AND FR 60
3-53 535101-01-1 311 DET REAR PRESSURE BULKHEAD AFT FACE AF MRB CPCP MRB 535101-01-1 535100-210-001 6 YE 6 YE APPL
312
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD
COMPLETE AFT FACE, AND FUSELAGE INTERNAL STRUCTURE,
BETWEEN FR 70 AND FR 71, FROM STRINGER 26, LH/RH TO
BOTTOM CENTER LINE
NOTE:
TPS MAY BE LIMITED TO FUSELAGE INTERNAL STRUCTURE
FROM FR 70 TO FR 71, AND AFT FACE OF PRESSURE
BULKHEAD, FROM STRINGER 26, LH/RH TO BOTTOM
CENTERLINE
535105-01-2 ************** TASK DELETED ************** N/A
535105-01-3 ************** TASK DELETED ************** N/A
535105-01-4 ************** TASK DELETED ************** N/A
535105-01-5 ************** TASK DELETED ************** N/A
535107-01-1 ************** TASK DELETED ************** N/A
535107-01-2 ************** TASK DELETED ************** N/A
535107-01-3 ************** TASK DELETED ************** N/A
535107-01-4 ************** TASK DELETED ************** N/A
3-53 535107-02-2 311 SDI CIRCUMFERENTIAL JOINT AT FR 70 NDT ALI WFD ALI 535107-02-2 60000 FC 19400 FC N/A
312 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF RING FRAME AT 120000 FH 38800 FH
CIRCUMFERENTIAL JOINT OF REAR PRESSURE BULKHEAD SKIN
AT FR 70, AFT FACE.
3-53 535113-01-1 311 DET FUSELAGE SKIN AT THS CUTOUT AF MRB CPCP MRB 535113-01-1 535100-210-004 12 YE 12 YE APPL
312
DETAILED INSPECTION OF FUSELAGE SKIN AT HORIZONTAL
STABILIZER CUTOUT AT FORWARD, UPPER AND LOWER
CORNERS, LH/RH
535113-01-3 ************** TASK DELETED ************** N/A
535113-01-5 ************** TASK DELETED ************** N/A
3-53 535115-01-1 311 DET FR 74 SPLICES AF MRB CPCP MRB 535115-01-1 535100-210-005 12 YE 12 YE APPL
312
DETAILED INSPECTION OF FR 74, SPLICES AT STRINGER 12
AND STRINGER 19, LH/RH, INTERNAL STRUCTURE
3-53 535117-01-1 311 DET HORIZONTAL STABILIZER ATTACHMENT AF MRB CPCP MRB 535117-01-1 535100-210-007 12 YE 12 YE APPL
312
DETAILED INSPECTION OF HORIZONTAL STABILIZER
ATTACHMENT AND BACK UP STRUCTURE AT FR 77, FROM
STRINGER 8 TO STRINGER 21, LH/RH
535117-01-5 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 117 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-53 535119-01-1 311 DET SHEAR TIES/FRAME CLIPS AT FR 72 AND 74 AF ALI WFD ALI 535119-01-1 535100-210-017 33100 FC 9500 FC N/A
312 OR OR
DETAILED INSPECTION OF SHEAR TIES AND FRAME CLIPS AT 66200 FH 19100 FH
FR 72 AND FR 74, BETWEEN STRINGER 3 AND STRINGER 9, NOTE
LH/RH, INTERNAL STRUCTURE
NOTE:
FOR PRE 153833 AIRCRAFT RETROFITTED, THRESHOLD IS TO
BE COUNTED FROM SB 53-1266 EMBODIMENT.
3-53 535121-01-1 171 DET REAR PRESSURE BULKHEAD BLW CABIN FLOOR AF MRB CPCP MRB 535121-01-1 535100-210-002 6 YE 6 YE APPL
172
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,
FORWARD FACE, BELOW CABIN FLOOR LEVEL
3-53 535123-01-1 261 DET REAR PRESSURE BULKHEAD ABV CABIN FLOOR AF MRB CPCP MRB 535123-01-1 535100-210-008 12 YE 12 YE APPL
262
DETAILED INSPECTION OF REAR PRESSURE BULKHEAD,
FORWARD FACE, ABOVE CABIN FLOOR LEVEL
3-53 535126-01-1 323 GVI FUSELAGE AND VERT STAB ATTACH FITTINGS AF MRB CPCP MRB 535126-01-1 535100-210-018 12 YE 12 YE APPL
GENERAL VISUAL INSPECTION OF FUSELAGE EXTERNAL
SURFACE AND VERTICAL STABILIZER ATTACHMENT FITTING,
UNDERNEATH VERTICAL STABILIZER/FUSELAGE FAIRINGS
3-53 535151-01-1 311 DET TAIL CONE ATTACH FITTINGS AF MRB CPCP MRB 535151-01-1 535100-210-009 12 YE 12 YE 24 YE 12 YE APPL
312
313 DETAILED INSPECTION OF TAIL CONE ATTACHMENT FITTINGS
314 AT FR 77 AND FR 78
535162-01-1 ************** TASK DELETED ************** N/A
3-53 535162-01-2 323 DET FIN/FUSELAGE ATTACH FITTINGS OUTSIDE AF ALI ALI 535162-01-2 535100-210-012 40500 FC 29600 FC N/A
OR OR
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID 81000 FH 59300 FH
AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
535162-01-3 ************** TASK DELETED ************** N/A
3-53 535162-01-4 323 DET FIN/FUSELAGE ATTACH FITTINGS OUTSIDE AF ALI ALI 535162-01-4 535100-210-012 34100 FC 14400 FC N/A
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID
AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
3-53 535162-09-1 323 DET FIN/FUSELAGE ATTACH FITTINGS OUTSIDE AF MRB FMP MRB 535162-09-1 24 YE 6 YE APPL
NOTE NOTE
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID
AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-53 535162-09-2 323 DET FIN/FUSELAGE ATTACH FITTINGS OUTSIDE AF MRB FMP MRB 535162-09-2 18 YE NOTE N/A
NOTE
DETAILED INSPECTION OF FIN TO FUSELAGE, FORWARD, MID
AND AFT ATTACH FITTINGS, OUTSIDE FUSELAGE, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-53 535163-01-1 311 SDI LOWER FLANGES FR 72 AND FR 74 NDT ALI ALI 535163-01-1 535100-220-802 45800 FC 15900 FC N/A
312 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER FLANGES 91700 FH 31800 FH
OF FR 72 AND FR 74, BETWEEN STRINGER 10 LH AND
STRINGER 10 RH.
3-53 535163-01-2 311 SDI LOWER FLANGES FR 72 AND FR 74 NDT ALI ALI 535163-01-2 535100-220-802 28200 FC 7700 FC N/A
312 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF LOWER FLANGES 56500 FH 15400 FH
OF FR 72 AND FR 74, BETWEEN STRINGER 10 LH AND
STRINGER 10 RH.
APPENDIX A
AEG/AMP/A320 Page 118 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-53 535900-01-1 310 OPC FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/02 535900-210-001 8 MO APPL
OPERATIONAL CHECK OF SINGLE DRAIN PIPE AFT OF FR 70
FROM OUTSIDE
2-53 535900-02-1 827 OPC FUSELAGE DRAINAGE AF MRB 9 MRB 53.19.00/05 535900-210-002 36 MO APPL
OPERATIONAL CHECK OF RUBBER FLAP DRAIN VALVE AT BULK
CARGO COMPARTMENT DOOR FROM OUTSIDE
2-54 545000-01-1 410 GVI PYLONS AF MRB 8 MRB 54.50.00/01 545000-200-001 36 MO APPL
420
GENERAL VISUAL INSPECTION OF COMPARTMENT A AND F
PYLON DRAIN SYSTEM
2-54 545000-02-1 410 FNC PYLONS AF MRB 8 MRB 54.50.00/02 545000-200-002 108 MO APPL
420
FLOW CHECK OF INDIVIDUAL DRAIN LINES OF PYLON SYSTEM
2-54 545000-04-1 410 DET PYLONS AF LUR MRB 54.50.00/03 545000-220-002 108 MO APPL
420 MRB 8 OR
DETAILED INSPECTION OF PYLON COMPARTMENT C DRAIN 12000 FH
SYSTEM.
2-54 545000-05-1 413 DET PYLONS AF LUR MRB 54.50.00/04 545000-220-807 108 MO APPL
414 MRB 8 OR
415 DETAILED INSPECTION OF PYLON FIRE SEALS 12000 FH
423
424
425
473
483
2-54 545000-06-1 410 DET PYLONS AF MRB 9 MRB 54.50.00/05 36 MO APPL
420
DETAILED INSPECTION OF THE CAF 4 SEALANT IN PYLON
CANTILEVER ZONE A.
3-54 545102-01-12 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-01-12 545100-200-002 45700 FC 45700 FC APPL
425 OR OR
SPECIAL DETAILED INSPECTION (US) OF PYLON FORWARD 91400 FH 91400 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545102-02-1 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-02-1 545100-200-802 48000 FC 22500 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD 96000 FH 45000 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545102-02-2 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-02-2 545100-200-802 39600 FC 17700 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD 79300 FH 35400 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545102-02-3 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-02-3 545100-200-802 41000 FC 18500 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD 82100 FH 37000 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545102-02-4 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-02-4 545100-200-802 31500 FC 14200 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD 63100 FH 28400 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545102-02-6 415 SDI PYLON FWD MOUNT FITTING NDT ALI ALI 545102-02-6 545100-200-802 48000 FC 24200 FC APPL
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON FORWARD 96000 FH 48400 FH
MOUNT FITTING, END OF LOWER ARMS, AFT OF RIB 1,
FORWARD ATTACHMENT, BOLT HOLES
3-54 545103-01-10 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-10 545100-200-003 15700 FC 15700 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING, 31400 FH 31400 FH
FORWARD OF RIB 1
APPENDIX A
AEG/AMP/A320 Page 119 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545103-01-2 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-2 545100-200-003 10800 FC 10800 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING, 21700 FH 21700 FH
FORWARD OF RIB 1
3-54 545103-01-4 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-4 545100-200-003 20000 FC 20000 FC N/A
425
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,
FORWARD OF RIB 1
3-54 545103-01-6 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-6 545100-200-003 9400 FC 9400 FC N/A
425
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,
FORWARD OF RIB 1
3-54 545103-01-7 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-7 545100-200-003 11800 FC 11800 FC N/A
425
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,
FORWARD OF RIB 1
3-54 545103-01-8 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-8 545100-200-003 11900 FC 11900 FC N/A
425
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING,
FORWARD OF RIB 1
3-54 545103-01-9 415 DET PYLON FWD MOUNT FITTING AF ALI ALI 545103-01-9 545100-200-003 23200 FC 23200 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON FORWARD MOUNT FITTING, 46400 FH 46400 FH
FORWARD OF RIB 1
3-54 545104-01-1 415 DET PYLON LOWER SPAR UPPER SURFACE AF MRB CPCP MRB 545104-01-1 545100-200-027 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON, LOWER SPAR, UPPER
SURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545104-02-1
3-54 545104-02-1 415 SDI PYLON LOWER SPAR UPPER SURFACE NDT MRB CPCP MRB 545104-02-1 545100-200-028 12 YE 12 YE 24 YE 12 YE APPL
425
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,
LOWER SPAR, UPPER SURFACE, BETWEEN RIB 1 AND RIB 2,
AND RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545104-01-1
3-54 545106-01-1 415 DET PYLON LWR SPAR AF MRB CPCP MRB 545106-01-1 545100-200-004 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON, LOWER SPAR, BETWEEN RIB
1 AND RIB 10, LOWER SURFACE
3-54 545107-01-1 415 DET ENGINE AFT ATTACH BEAM AF ALI ALI 545107-01-1 545100-200-005 12 YE 12 YE 24 YE 12 YE APPL
425 MRB CPCP MRB 545107-01-1 OR OR OR OR
DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM 48000 FC 8500 FC 48000 FC 8500 FC
OR OR OR OR
96000 FH 17000 FH 96000 FH 17000 FH
3-54 545107-01-3 415 DET ENGINE AFT ATTACH BEAM AF MRB CPCP MRB 545107-01-1 545100-200-005 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM
3-54 545107-01-5 415 DET ENGINE AFT ATTACH BEAM AF ALI ALI 545107-01-5 545100-200-005 12 YE 12 YE 24 YE 12 YE N/A
425 MRB CPCP MRB 545107-01-1 OR OR OR OR
DETAILED INSPECTION OF ENGINE AFT ATTACHMENT BEAM. 48000 FC 8900 FC 48000 FC 8900 FC
OR OR OR OR
96000 FH 17900 FH 96000 FH 17900 FH
545107-01-6 ************** TASK DELETED ************** N/A
3-54 545114-01-1 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-1 545100-200-006 48000 FC 8100 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 16300 FH
LUGS AT RIB 4
545114-01-10 ************** TASK DELETED ************** N/A
545114-01-11 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 120 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545114-01-2 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-2 545100-200-006 48000 FC 4600 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 9200 FH
LUGS AT RIB 4
3-54 545114-01-3 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-3 545100-200-006 48000 FC 7300 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 14600 FH
LUGS AT RIB 4
3-54 545114-01-4 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-4 545100-200-006 48000 FC 8100 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 16300 FH
LUGS AT RIB 4
3-54 545114-01-5 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-5 545100-200-006 48000 FC 4600 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 9200 FH
LUGS AT RIB 4
3-54 545114-01-6 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 4 AF ALI ALI 545114-01-6 545100-200-006 48000 FC 7300 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 96000 FH 14600 FH
LUGS AT RIB 4
545114-01-7 ************** TASK DELETED ************** N/A
3-54 545115-01-1 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-1 545100-200-008 48000 FC 8100 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 16300 FH
ATTACHMENT SHACKLES AT RIB 4
545115-01-10 ************** TASK DELETED ************** N/A
545115-01-11 ************** TASK DELETED ************** N/A
3-54 545115-01-2 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-2 545100-200-008 48000 FC 4600 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 9200 FH
ATTACHMENT SHACKLES AT RIB 4
3-54 545115-01-3 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-3 545100-200-008 48000 FC 7300 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 14600 FH
ATTACHMENT SHACKLES AT RIB 4
3-54 545115-01-4 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-4 545100-200-008 48000 FC 8100 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 16300 FH
ATTACHMENT SHACKLES AT RIB 4
3-54 545115-01-5 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-5 545100-200-008 48000 FC 4600 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 9200 FH
ATTACHMENT SHACKLES AT RIB 4
3-54 545115-01-6 415 DET PYLON/WING RIB 4 AF ALI ALI 545115-01-6 545100-200-008 48000 FC 7300 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 96000 FH 14600 FH
ATTACHMENT SHACKLES AT RIB 4
3-54 545116-01-1 415 DET PYLON/WING ATTACH FITTING RIB 4 AF MRB CPCP MRB 545116-01-1 545100-200-009 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF SHACKLES, SLEEVES AND BOLTS OF
PYLON TO WING ATTACHMENT FITTINGS AT RIB 4
3-54 545117-01-1 415 DET PYLON SPIGOT AF MRB CPCP MRB 545117-01-1 545100-200-010 12 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR
SURROUNDING SURFACE
3-54 545117-01-2 415 DET PYLON SPIGOT AF MRB CPCP MRB 545117-01-2 545100-200-010 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR
SURROUNDING SURFACE
3-54 545117-01-3 415 DET PYLON SPIGOT AF MRB CPCP MRB 545117-01-3 545100-200-010 12 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR
SURROUNDING SURFACE
APPENDIX A
AEG/AMP/A320 Page 121 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545117-01-4 415 DET PYLON SPIGOT AF MRB CPCP MRB 545117-01-4 545100-200-010 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, INCLUDING FITTING BORE, AND UPPER SPAR
SURROUNDING SURFACE
3-54 545120-01-1 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-1 545100-200-011 40600 FC 11400 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 81300 FH 22900 FH
LUGS AT RIB 10
3-54 545120-01-10 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-10 545100-200-011 21400 FC 6000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 42800 FH 12000 FH
LUGS AT RIB 10.
545120-01-11 ************** TASK DELETED ************** N/A
545120-01-12 ************** TASK DELETED ************** N/A
3-54 545120-01-2 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-2 545100-200-011 41000 FC 10700 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 82100 FH 21500 FH
LUGS AT RIB 10
3-54 545120-01-4 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-4 545100-200-011 40600 FC 11400 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 81300 FH 22900 FH
LUGS AT RIB 10
3-54 545120-01-5 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-5 545100-200-011 41000 FC 10700 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 82100 FH 21500 FH
LUGS AT RIB 10
3-54 545120-01-9 415 DET PYLON/WING ATTACH FITTINGS LUGS RIB 10 AF ALI ALI 545120-01-9 545100-200-011 21400 FC 6000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING ATTACH FITTING 42800 FH 12000 FH
LUGS AT RIB 10.
3-54 545123-02-1 415 DET PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10 AF ALI ALI 545123-02-1 545100-220-807 40600 FC 10700 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT 81300 FH 21500 FH
SHACKLES AT RIB 10.
3-54 545123-02-2 415 DET PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10 AF ALI ALI 545123-02-2 545100-220-807 40600 FC 10700 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT 81300 FH 21500 FH
SHACKLES AT RIB 10.
3-54 545123-02-3 415 DET PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10 AF ALI ALI 545123-02-3 545100-220-807 21400 FC 6000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT 42800 FH 12000 FH
SHACKLES AT RIB 10.
3-54 545123-02-4 415 DET PYLON/WING AFT ATTACHMENT SHACKLES AT RIB 10 AF ALI ALI 545123-02-4 545100-220-807 21400 FC 6000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT 42800 FH 12000 FH
SHACKLES AT RIB 10.
545123-02-5 ************** TASK DELETED ************** N/A
545123-02-6 ************** TASK DELETED ************** N/A
3-54 545124-01-1 415 DET PYLON/WING AFT ATTACH FITTING SLEEVES AF MRB CPCP MRB 545124-01-1 545100-200-014 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT
FITTING, SLEEVES AND BOLTS
3-54 545130-01-1 415 DET PYLON LATERAL PANELS EDGE OF CUTOUTS AF ALI ALI 545130-01-1 545100-200-016 20000 FC 20000 FC APPL
425
DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE
EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 5 AND RIB 6,
LH/RH
545133-01-1 ************** TASK DELETED ************** N/A
545133-01-2 ************** TASK DELETED ************** N/A
3-54 545134-01-1 415 DET PYLON UPR SPAR RIB 4 AND 10 AF ALI ALI 545134-01-1 545100-200-019 53600 FC 11800 FC APPL
425 OR OR
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF 107300 FH 23700 FH
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
APPENDIX A
AEG/AMP/A320 Page 122 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545134-01-10 415 DET PYLON UPR SPAR RIB 4 AND 10 AF ALI ALI 545134-01-10 545100-200-019 53600 FC 11800 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF 107300 FH 23700 FH
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
545134-01-11 ************** TASK DELETED ************** N/A
545134-01-12 ************** TASK DELETED ************** N/A
545134-01-2 ************** TASK DELETED ************** N/A
545134-01-5 ************** TASK DELETED ************** N/A
545134-01-6 ************** TASK DELETED ************** N/A
545134-01-9 ************** TASK DELETED ************** N/A
3-54 545134-09-2 415 DET PYLON UPR SPAR RIB 4 AND 10 AF MRB FMP MRB 545134-09-2 18 YE 6 YE N/A
425 NOTE NOTE
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-54 545134-09-6 415 DET PYLON UPR SPAR RIB 4 AND 10 AF MRB FMP MRB 545134-09-6 18 YE 6 YE N/A
425 NOTE NOTE
DETAILED INSPECTION OF PYLON, UPPER SPAR, IN AREAS OF
FASTENERS AT JUNCTION WITH LATERAL PANEL, BETWEEN RIB
4 AND RIB 10, LH/RH
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-54 545156-01-1 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-1 545100-200-021 10 YE 10 YE APPL
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545156-01-2 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-2 545100-200-021 10 YE 10 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545156-01-3 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-3 545100-200-021 12 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545156-01-4 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-4 545100-200-021 12 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545156-01-5 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-5 545100-200-021 10 YE 10 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545156-01-6 415 DET PYLON UPPER SPARS UPPER SURFACE AF MRB CPCP MRB 545156-01-6 545100-200-021 12 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPARS, UPPER
SURFACE, FROM FORWARD OF RIB 1 TO RIB 10
3-54 545161-01-1 415 DET PYLON UPPER SPAR LOWER SURFACE AF MRB CPCP MRB 545161-01-1 545100-200-022 10 YE 10 YE APPL
425
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, FORWARD OF RIB 1
3-54 545161-01-2 415 DET PYLON UPPER SPAR LOWER SURFACE AF MRB CPCP MRB 545161-01-2 545100-200-022 12 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, FORWARD OF RIB 1
APPENDIX A
AEG/AMP/A320 Page 123 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545162-01-1 415 DET PYLON UPPER SPAR LOWER SURFACE AF MRB CPCP MRB 545162-01-1 545100-200-023 10 YE 10 YE 24 YE 10 YE APPL
425
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545162-02-1
3-54 545162-01-2 415 DET PYLON UPPER SPAR LOWER SURFACE AF MRB CPCP MRB 545162-01-2 545100-200-023 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON, UPPER SPAR, LOWER
SURFACE, BETWEEN RIB 2 AND RIB 3, AND RIB 4 AND RIB 8
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545162-02-2
3-54 545162-02-1 415 SDI PYLON UPPER SPAR LOWER SURFACE NDT MRB CPCP MRB 545162-02-1 545100-200-024 10 YE 10 YE 24 YE 10 YE APPL
425
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,
UPPER SPAR, LOWER SURFACE, BETWEEN RIB 1 AND RIB 2,
RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545162-01-1.
3-54 545162-02-2 415 SDI PYLON UPPER SPAR LOWER SURFACE NDT MRB CPCP MRB 545162-02-2 545100-200-024 12 YE 12 YE 24 YE 12 YE N/A
425
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON,
UPPER SPAR, LOWER SURFACE, BETWEEN RIB 1 AND RIB 2,
RIB 3 AND RIB 4, AND RIB 8 AND RIB 10.
NOTE:
THIS TASK MUST BE PERFORMED AT THE SAME TIME AS TASK
545162-01-2.
3-54 545170-01-1 415 DET PYLON PYRAMID MATING FACE AF MRB CPCP MRB 545170-01-1 545100-200-025 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON, PYRAMID MATING FACE
WITH THE ENGINE FORWARD MOUNT FITTING
3-54 545171-01-1 415 DET PYLON ENGINE AFT ATTACHMENT BEAM AF MRB CPCP MRB 545171-01-1 545100-200-026 12 YE 12 YE 24 YE 12 YE APPL
425
DETAILED INSPECTION OF PYLON, ENGINE AFT ATTACHMENT
BEAM MATING FACE WITH THE ENGINE AFT MOUNT FITTING
3-54 545201-01-1 415 DET PYLON FORWARD LATERAL SPARS AF ALI ALI 545201-01-1 545100-220-808 15000 FC 15000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON, FORWARD LATERAL SPARS, 30000 FH 30000 FH
FORWARD STIFFENERS, LH/RH.
3-54 545202-01-1 415 SDI PYLON FORWARD LATERAL SPARS NDT ALI ALI 545202-01-1 545100-250-805 35200 FC 17700 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, FORWARD 70400 FH 35500 FH
LATERAL SPARS, AT JUNCTION WITH LOWER SPAR, BETWEEN
RIB 1 AND RIB 3, ATTACHMENT BOLT HOLES, LH/RH.
3-54 545204-01-1 415 SDI PYLON LATERAL PANELS NDT ALI ALI 545204-01-1 545100-250-803 28100 FC 16300 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LATERAL 56300 FH 32600 FH
PANELS, AT JUNCTION WITH FORWARD LATERAL SPARS,
BETWEEN RIB 2 AND RIB 3, ATTACHMENT BOLTS HOLES,
LH/RH.
545205-01-1 ************** TASK DELETED ************** N/A
3-54 545205-01-2 415 SDI PYLON FORWARD LATERAL SPARS NDT ALI ALI 545205-01-2 545100-250-802 18500 FC 8500 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF PYLON, FORWARD 37100 FH 17100 FH
LATERAL SPARS, LOWER RADIUS FORWARD OF RIB 1.
3-54 545207-01-1 415 DET PYLON ENGINE AFT ATTACHMENT FITTINGS AF MRB CPCP MRB 545207-01-1 545100-220-802 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO ENGINE AFT ATTACHMENT
FITTINGS.
APPENDIX A
AEG/AMP/A320 Page 124 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545216-01-1 415 DET PYLON TO WING FORWARD ATTACHMENT AF MRB CPCP MRB 545216-01-1 545100-220-803 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO WING FORWARD
ATTACHMENT, SLEEVES AND BOLTS AT RIB 5.
3-54 545217-01-1 415 DET PYLON SPIGOT RECEPTACLE UPPER SURFACE AF MRB CPCP MRB 545217-01-1 545100-220-805 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE AND UPPER SPAR SURROUNDING STRUCTURE.
3-54 545217-02-1 415 SDI PYLON SPIGOT RECEPTACLE NDT MRB CPCP MRB 545217-02-1 545100-270-802 12 YE 12 YE 24 YE 12 YE N/A
425
SPECIAL DETAILED INSPECTION (US) OF PYLON SPIGOT
RECEPTACLE, MATING FACE WITH REAR UPPER SPAR.
3-54 545218-01-1 415 DET PYLON TO WING FORWARD ATTACHMENT AF ALI ALI 545218-01-1 545100-220-809 24000 FC 10900 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 48000 FH 21900 FH
ATTACHMENTS.
3-54 545224-01-1 415 DET PYLON TO WING AFT ATTACHMENT AF MRB CPCP MRB 545224-01-1 545100-220-804 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT,
SLEEVES AND BOLTS AT RIB 10.
3-54 545225-01-1 415 DET PYLON TO WING AFT ATTACHMENT AF ALI ALI 545225-01-1 545100-220-810 24000 FC 15000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENTS. 48000 FH 30000 FH
3-54 545228-01-1 451 GVI PYLON REVERSER FITTINGS AF MRB MRB 545228-01-1 545100-210-802 6500 FC 6500 FC N/A
452 OR OR
461 GENERAL VISUAL INSPECTION OF PYLON, REVERSER 13100 FH 13100 FH
462 FITTINGS.
3-54 545230-01-1 415 DET PYLON LATERAL PANELS AF ALI ALI 545230-01-1 545100-220-811 6900 FC 6900 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE 13900 FH 13900 FH
EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 7 AND RIB 8
(RH) AND RIB 6 AND RIB 7 (LH).
3-54 545272-01-1 415 DET PYLON TO ENGINE AFT MOUNT FITTINGS AF ALI ALI 545272-01-1 545100-220-812 15000 FC 15000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO ENGINE AFT MOUNT 30000 FH 30000 FH
FITTINGS STIFFENERS.
3-54 545301-01-1 415 DET PYLON FORWARD LATERAL SPARS AF ALI ALI 545301-01-1 545100-220-817 14000 FC 14000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON, FORWARD LATERAL SPARS, 28100 FH 28100 FH
STIFFENERS FORWARD RIB 0, LH/RH.
3-54 545305-01-1 415 SDI PYLON FORWARD LATERAL SPARS NDT ALI ALI 545305-01-1 545100-250-806 45600 FC 21200 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF PYLON, FORWARD 91300 FH 42400 FH
LATERAL SPARS, LOWER RADIUS FORWARD OF RIB 1.
3-54 545307-01-1 415 DET PYLON TO ENGINE AFT ATTACHMENT FITTINGS AF MRB CPCP MRB 545307-01-1 545100-220-813 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO ENGINE AFT ATTACHMENT
FITTINGS.
3-54 545308-01-1 415 SDI PYLON FRONT UPPER SPAR NDT ALI ALI 545308-01-1 545100-250-807 45000 FC 21500 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, FRONT 90000 FH 43000 FH
UPPER SPAR, SPLICING BETWEEN RIB 2 AND RIB 3,
ATTACHMENT BOLTS HOLES, LH/RH.
3-54 545309-01-1 415 SDI PYLON LATERAL PANEL NDT ALI ALI 545309-01-1 545100-250-808 43200 FC 12200 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LATERAL 86400 FH 24500 FH
PANEL SPLICING BETWEEN RIB 6 AND RIB 7, ATTACHMENT
BOLTS HOLES, LH/RH.
3-54 545309-01-2 415 SDI PYLON LATERAL PANEL NDT ALI ALI 545309-01-2 545100-250-808 34400 FC 9700 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LATERAL 68800 FH 19500 FH
PANEL SPLICING BETWEEN RIB 6 AND RIB 7, ATTACHMENT
BOLTS HOLES, LH/RH.
3-54 545310-01-1 415 SDI PYLON LOWER SPAR NDT ALI ALI 545310-01-1 545100-290-801 39800 FC 10800 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF PYLON, 79700 FH 21700 FH
LOWER SPAR, AT JUNCTION WITH LATERAL PANEL, BETWEEN
RIB 3 AND RIB 4, LH/RH.
APPENDIX A
AEG/AMP/A320 Page 125 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-54 545311-01-1 415 SDI PYLON LOWER SPAR AND LATERAL PANEL NDT ALI ALI 545311-01-1 545100-250-809 33700 FC 14600 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LOWER 67500 FH 29200 FH
SPAR AND LATERAL PANEL, AT JUNCTION WITH FORWARD
LATERAL SPAR, BETWEEN RIB 2 AND RIB 3, ATTACHMENT
BOLTS HOLES, LH/RH.
3-54 545311-01-2 415 SDI PYLON LOWER SPAR AND LATERAL PANEL NDT ALI ALI 545311-01-2 545100-250-809 26700 FC 11500 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LOWER 53400 FH 23100 FH
SPAR AND LATERAL PANEL, AT JUNCTION WITH FORWARD
LATERAL SPAR, BETWEEN RIB 2 AND RIB 3, ATTACHMENT
BOLTS HOLES, LH/RH.
3-54 545316-01-1 415 DET PYLON TO ENGINE FORWARD ATTACHMENT AF MRB CPCP MRB 545316-01-1 545100-220-814 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO WING FORWARD
ATTACHMENT, SLEEVES AND BOLTS AT RIB 5.
3-54 545317-01-1 415 DET PYLON SPIGOT RECEPTACLE UPPER SURFACE AF MRB CPCP MRB 545317-01-1 545100-220-815 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON SPIGOT RECEPTACLE UPPER
SURFACE, AND UPPER SPAR SURROUNDING STRUCTURE.
3-54 545317-02-1 415 SDI PYLON SPIGOT RECEPTACLE NDT MRB CPCP MRB 545317-02-1 545100-270-801 12 YE 12 YE 24 YE 12 YE N/A
425
SPECIAL DETAILED INSPECTION (US) OF PYLON SPIGOT
RECEPTACLE, MATING FACE WITH REAR UPPER SPAR.
3-54 545318-01-1 415 DET PYLON TO WING FORWARD ATTACHMENT AF ALI ALI 545318-01-1 545100-220-818 24000 FC 7600 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING FORWARD 48000 FH 15200 FH
ATTACHMENTS, LH/RH.
3-54 545324-01-1 415 DET PYLON TO ENGINE AFT ATTACHMENT AF MRB CPCP MRB 545324-01-1 545100-220-816 12 YE 12 YE 24 YE 12 YE N/A
425
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENT,
SLEEVES AND BOLTS AT RIB 10.
3-54 545325-01-1 415 DET PYLON TO WING AFT ATTACHMENT AF ALI ALI 545325-01-1 545100-220-819 24000 FC 15000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO WING AFT ATTACHMENTS 48000 FH 30000 FH
3-54 545329-01-1 451 GVI PYLON REVERSER FITTINGS AF MRB MRB 545329-01-1 545100-210-803 7500 FC 7500 FC N/A
452 OR OR
461 GENERAL VISUAL INSPECTION OF PYLON, REVERSER 15000 FH 15000 FH
462 FITTINGS, LH/RH
3-54 545330-01-1 415 DET PYLON LATERAL PANELS AF ALI ALI 545330-01-1 545100-220-820 2300 FC 2300 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON, LATERAL PANELS, AT THE 4700 FH 4700 FH
EDGE OF ACCESS DOOR CUTOUTS, BETWEEN RIB 7 AND RIB 8
(RH) AND RIB 6 AND RIB 7 (LH).
3-54 545330-02-1 415 SDI PYLON LATERAL PANELS NDT ALI ALI 545330-02-1 545100-250-810 37300 FC 14000 FC N/A
425 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF PYLON, LATERAL 74600 FH 28000 FH
PANELS, AT THE EDGE OF ACCESS DOOR CUTOUTS, BETWEEN
RIB 7 AND RIB 8 (RH) AND RIB 6 AND RIB 7 (LH).
3-54 545372-01-1 415 DET PYLON TO ENGINE AFT MOUNT FITTINGS AF ALI ALI 545372-01-1 545100-220-821 15000 FC 15000 FC N/A
425 OR OR
DETAILED INSPECTION OF PYLON TO ENGINE AFT MOUNT 30000 FH 30000 FH
FITTINGS STIFFENERS, LH/RH
2-54 545900-L1-1 413 OPC PYLON DRAINAGE AF MRB 8 MRB 54.59.00/01-CL 545000-200-805 72 MO N/A
415
423 OPERATIONAL CHECK OF PYLON DRAIN LINES IN ZONES C, G
425 AND D.
471
472
481
482
APPENDIX A
AEG/AMP/A320 Page 126 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
2-54 545900-L2-1 413 DET PYLON DRAINAGE AF LUR MRB 54.59.00/02-CL 545000-220-806 108 MO N/A
414 MRB 8 OR
415 DETAILED INSPECTION OF RMF FINGER SEALS, BLOCK, 12000 FH
423 KARMAN FAIRING AND NOSE FIRE SEALS.
424
425
471
472
481
482
2-54 545900-L3-1 435 DET PYLON DRAINAGE AF LUR MRB 54.59.00/03-CL 545000-220-805 288 MO N/A
436 MRB 8 OR
445 DETAILED INSPECTION OF FORWARD SECONDARY STRUCTURE 40000 FH
446 FIRE SEAL. NOTE
NOTE:
INTERVAL:
- TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED.
2-54 545900-W1-1 415 VCK PYLON DRAINAGE AF MRB 8 MRB 54.59.00/01-P1 545000-200-802 48 MO N/A
425
VISUAL CHECK OF PYLON DRAINAGE SYSTEM IN ZONE C.
2-54 545900-W2-1 415 OPC PYLON DRAINAGE AF MRB 8 MRB 54.59.00/02-P1 545000-200-803 72 MO N/A
425
OPERATIONAL CHECK OF PYLON DRAINAGE SYSTEM IN ZONE C.
2-54 545900-W3-1 470 DET PYLON DRAINAGE AF LUR MRB 54.59.00/03-P1 545000-220-802 108 MO N/A
480 MRB 8 OR
DETAILED INSPECTION OF KARMAN FAIRING FIRE SEALS. 12000 FH
2-54 545900-W4-1 415 DET PYLON DRAINAGE AF MRB 8 MRB 54.59.00/04-P1 545000-220-803 40000 FH N/A
425 NOTE
DETAILED INSPECTION OF NOSE FIRE SEAL.
NOTE:
- TASK MAY BE PERFORMED AT OPPORTUNITY OF ENGINE
REMOVAL PROVIDED INTERVAL NOT EXCEEDED.
2-54 545900-W5-1 415 DET PYLON DRAINAGE AF LUR MRB 54.59.00/05-P1 545000-220-804 108 MO N/A
425 MRB 8 OR
DETAILED INSPECTION OF RMF BLOCK SEAL AND RMF FIRE 12000 FH
FINGER SEAL.
3-55 551001-01-1 333 DET THS JACK FITTING AF MRB MRB 551001-01-1 551634-200-001 6 YE 6 YE APPL
343
DETAILED INSPECTION OF HORIZONTAL STABILIZER, JACK
FITTING AND SURROUNDING EXTERNAL STRUCTURE
551002-01-2 ************** TASK DELETED ************** N/A
3-55 551003-01-2 333 GVI THS UPR AND LWR JOINT FITTINGS AF MRB CPCP MRB 551003-01-2 551600-200-003 6 YE 6 YE N/A
343
GENERAL VISUAL INSPECTION OF HORIZONTAL STABILIZER,
UPPER AND LOWER JOINT FITTINGS, EXTERNAL SURFACE
3-55 551010-01-1 333 DET THS SUPPORT AND ATTACH FITTINGS AF MRB MRB 551010-01-1 551600-200-001 6 YE 6 YE APPL
343
DETAILED INSPECTION OF HORIZONTAL STABILIZER, REAR
SUPPORT FITTINGS, UPPER AND LOWER ATTACH FITTINGS AND
SURROUNDING EXTERNAL STRUCTURE, LH/RH
3-55 551012-01-1 333 DET THS SPARBOX INTERNAL STRUCTURE AF MRB MRB 551012-01-1 551000-210-001 12 YE 12 YE APPL
343
DETAILED INSPECTION OF HORIZONTAL STABILIZER,
INTERNAL STRUCTURE OF TORQUE BOX, INBOARD OF FUSELAGE
FAIRINGS
3-55 551019-01-1 333 DET THS TORQUE BOX INTERNAL STRUCTURE AF MRB MRB 551019-01-1 551000-210-002 12 YE 12 YE APPL
343
DETAILED INSPECTION OF HORIZONTAL STABILIZER,
INTERNAL STRUCTURE OF TORQUE BOX, OUTBOARD OF
FUSELAGE FAIRINGS, LH/RH
APPENDIX A
AEG/AMP/A320 Page 127 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-55 551020-01-1 334 DET ELEVATOR HINGE SUPPORTS AND FITTINGS AF MRB CPCP MRB 551020-01-1 551600-200-004 6 YE 6 YE APPL
344
DETAILED INSPECTION OF HORIZONTAL STABILIZER, HINGE
FITTINGS AND SUPPORT RIBS AND ACTUATOR FITTINGS FOR
THE ELEVATOR, LH/RH
3-55 551021-01-1 332 DET HORIZONTAL STABILIZER OUTBOARD END RIB (RIB 14) AF MRB CPCP MRB 551021-01-1 551000-220-801 12 YE 12 YE N/A
342
DETAILED INSPECTION OF HORIZONTAL STABILIZER, END RIB
(RIB 14), EXTERNAL SURFACE, LH/RH
3-55 552002-01-1 335 DET ELEVATOR HINGE SUPPORT AND ACT. FTG. AF MRB CPCP MRB 552002-01-1 552000-200-003 6 YE 6 YE APPL
345
DETAILED INSPECTION OF ELEVATOR, HINGE FITTINGS AND
ACTUATOR FITTINGS, LH/RH
3-55 552004-01-1 300 SDI ELEVATOR SKIN PANELS NDT MRB MRB 552004-01-1 552000-200-001 6 YE 6 YE APPL
SPECIAL DETAILED INSPECTION (TAP TEST) OF ELEVATOR,
TOP AND BOTTOM SKIN PANELS IN AREA OF HINGE SUPPORTS
2, 3 AND 4 AND ACTUATOR FITTINGS 1 AND 2, LH/RH
3-55 552005-01-1 335 DET ELEVATOR PANELS INTERNAL STRUCTURE AF MRB MRB 552005-01-1 552000-200-002 12 YE 12 YE APPL
345
DETAILED INSPECTION OF ELEVATOR PANELS, INTERNAL
STRUCTURE AS FAR AS VISIBLE, LH/RH
3-55 552006-01-1 335 DET ELEVATOR OUTBOARD RIB AF MRB CPCP MRB 552006-01-1 552000-200-005 10 YE 10 YE N/A
345
DETAILED INSPECTION OF ELEVATOR OUTBOARD RIB,
EXTERNAL SURFACE, LH/RH
3-55 552006-01-2 335 DET ELEVATOR OUTBOARD RIB AF MRB CPCP MRB 552006-01-2 552000-200-005 12 YE 12 YE APPL
345
DETAILED INSPECTION OF ELEVATOR OUTBOARD RIB,
EXTERNAL SURFACE, LH/RH
3-55 553003-01-1 321 DET VERT STABILIZER CENTER BOX AF MRB MRB 553003-01-1 553000-200-001 12 YE 12 YE APPL
322
323 DETAILED INSPECTION OF VERTICAL STABILIZER, CENTER
324 BOX, INTERNAL STRUCTURE AS FAR AS VISIBLE, FRONT SPAR
FORWARD FACE AND UPPER CLOSING RIB, UPPER SURFACE
3-55 553004-01-1 323 DET VERT STABILIZER ATTACH FITTINGS AF MRB MRB 553004-01-1 553600-210-001 6 YE 6 YE APPL
DETAILED INSPECTION OF VERTICAL STABILIZER, ATTACH
FITTINGS, INCLUDING LOAD INTRODUCTION AREA AT SKIN
PANELS
3-55 553005-01-1 325 DET RUDDER HINGE ARMS AND ACTUATOR AF MRB CPCP MRB 553005-01-1 553000-210-001 6 YE 6 YE APPL
DETAILED INSPECTION OF RUDDER HINGE ARM 1,2,3,4 AND 5
AND FIN ACTUATOR FITTINGS (ACTUATOR 1, 2 AND 3)
3-55 553006-01-1 325 DET RUDDER HINGE ARM 6 AND 7 AF MRB CPCP MRB 553006-01-1 553000-210-002 6 YE 6 YE N/A
DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7
3-55 553006-01-2 325 DET RUDDER HINGE ARM 6 AND 7 AF MRB CPCP MRB 553006-01-2 553000-210-002 6 YE 6 YE APPL
DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7
3-55 553006-01-3 325 DET RUDDER HINGE ARM 6 AND 7 AF MRB CPCP MRB 553006-01-3 553000-210-002 6 YE 6 YE N/A
DETAILED INSPECTION OF RUDDER HINGE ARM 6 AND 7
3-55 553008-01-1 321 DET VERTICAL STABILIZER AF MRB MRB 553008-01-1 553000-210-003 12 YE 12 YE N/A
322
323 DETAILED INSPECTION OF VERTICAL STABILIZER, CENTER
324 BOX AND ADAPTATION BOX, INTERNAL STRUCTURE AS FAR AS
VISIBLE, FRONT SPAR FORWARD FACE AND UPPER CLOSING
RIB (RIB 12), UPPER SURFACE, AND UPPER SURFACE OF RIB
11
APPENDIX A
AEG/AMP/A320 Page 128 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-55 554003-01-1 300 SDI RUDDER SIDE PANELS NDT MRB MRB 554003-01-1 554000-210-001 6 YE 6 YE APPL
SPECIAL DETAILED INSPECTION (US) OF RUDDER SIDE
PANELS, IN AREA OF RUDDER BEARINGS, IN THE BOOSTER
AREA AND AROUND TRAILING EDGE FASTENERS AND HOISTING
POINTS, LH/RH.
3-55 554004-01-1 326 DET RUDDER SIDE PANELS INTERNAL SURFACES AF MRB MRB 554004-01-1 554000-210-003 12 YE 12 YE APPL
DETAILED INSPECTION OF RUDDER SIDE PANELS, INTERNAL
SURFACES
NOTE:
ALTERNATIVE ACCESS: 325AR 325BR 325CR 325DR 325ER
326AT
3-55 554004-01-2 326 DET RUDDER SIDE PANELS INTERNAL SURFACES AF MRB MRB 554004-01-2 554000-210-003 12 YE 12 YE N/A
DETAILED INSPECTION OF RUDDER SIDE PANELS, INTERNAL
SURFACES
NOTE:
ALTERNATIVE ACCESS: 325AR 325BR 325CR 325DR 325ER
326BT
3-55 554005-01-1 326 DET RUDDER FITTINGS,ACT. ATTACH FITTINGS AF MRB CPCP MRB 554005-01-1 554000-210-004 6 YE 6 YE APPL
DETAILED INSPECTION OF RUDDER ATTACH FITTING 1,2,3,4
AND 5 AND RUDDER ACTUATOR ATTACH FITTINGS (ACTUATOR
1, 2 AND 3)
NOTE:
ON A/C POST SB 55-1030 ONLY RUDDER ACTUATOR ATTACH
FITTINGS (ACTUATOR 1, 2 AND 3) TO BE INSPECTED.
3-55 554006-01-1 326 DET RUDDER ATTACH FITTING 6 AND 7 AF MRB CPCP MRB 554006-01-1 554000-210-005 6 YE 6 YE APPL
DETAILED INSPECTION OF RUDDER ATTACH FITTING 6 AND 7
3-55 554006-01-2 326 DET RUDDER ATTACH FITTING 6 AND 7 AF MRB CPCP MRB 554006-01-2 554000-210-005 6 YE 6 YE N/A
DETAILED INSPECTION OF RUDDER ATTACH FITTING 6 AND 7
3-55 554008-01-1 300 SDI RUDDER SIDE PANELS NDT MRB MRB 554008-01-1 554000-220-001 6 YE 6 YE APPL
SPECIAL DETAILED INSPECTION (THERMOGRAPHIC) OF THE
HONEYCOMB CORE OF THE RUDDER SIDE PANELS, LH / RH.
3-55 554009-01-1 300 SDI RUDDER SIDE PANELS NDT MRB MRB 554009-01-1 554000-210-006 6 YE 6 YE APPL
SPECIAL DETAILED INSPECTION (ELCH TEST) OF THE
BONDING LAYERS BETWEEN RUDDER SIDE PANEL HONEYCOMB
STRUCTURE AND EXTERNAL SKINS OF THE RUDDER SIDE
PANELS, LH / RH.
2-56 561200-01-1 210 DET SLIDING WINDOWS AF MRB 9 MRB 56.12.00/02 561200-220-001 48 MO APPL
DETAILED INSPECTION OF WINDOW SEALS
2-56 561200-02-1 210 LUB SLIDING WINDOWS AF MRB 6,9 MRB 56.12.00/01 122256-600-001 36 MO APPL
LUBRICATION OF COCKPIT SLIDING WINDOW TRACKS
3-56 562101-01-1 221 DET WINDOW PANES AF MRB MRB 562101-01-1 562113-200-001 6 YE 6 YE APPL
222
231 DETAILED INSPECTION OF CABIN WINDOW PANES, INCLUDING
232 WINDOW PANES IN DOORS
241
242
251
252
261
262
3-57 571101-02-1 147 SDI MAIN STRUCTURE NDT ALI ALI 571101-02-1 571000-220-802 37200 FC 20300 FC APPL
148 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 74400 FH 40600 FH
BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES
APPENDIX A
AEG/AMP/A320 Page 129 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 571101-02-4 147 SDI MAIN STRUCTURE NDT ALI ALI 571101-02-4 571000-220-802 43000 FC 23700 FC N/A
148 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 86000 FH 47400 FH
BOX, REAR SPAR, SYSTEM HOLES NEAR MAN HOLES
571106-01-2 ************** TASK DELETED ************** N/A
571106-01-3 ************** TASK DELETED ************** N/A
571106-01-4 ************** TASK DELETED ************** N/A
571106-01-7 ************** TASK DELETED ************** N/A
3-57 571106-09-2 141 SDI CENTER WING BOX LWR SKIN NDT MRB FMP MRB 571106-09-2 24 YE 6 YE APPL
142 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX
AT ENDS OF LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 571106-09-3 141 SDI CENTER WING BOX LWR SKIN NDT MRB FMP MRB 571106-09-3 18 YE 6 YE N/A
142 NOTE NOTE
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING BOX
AT ENDS OF LOWER SKIN STIFFENERS, 8 TO 15, LH/RH.
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 571109-01-1 147 DET CENTER WING BOX REAR SPAR AF MRB CPCP MRB 571109-01-1 571000-200-004 12 YE 12 YE APPL
148
DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR,
AROUND ACCESS DOOR CUTOUTS
3-57 571122-01-1 147 DET CENTER WING BOX REAR SPAR AF MRB CPCP MRB 571122-01-1 571000-200-012 6 YE 6 YE APPL
148
DETAILED INSPECTION OF CENTER WING BOX, REAR SPAR AFT
FACE
3-57 571134-01-1 191 DET CENTER WING BOX SKIN STRINGER 11-15 AF ALI ALI 571134-01-1 571000-200-013 32800 FC 7200 FC APPL
192 OR OR
195 DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN 65600 FH 14500 FH
196 LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,
BETWEEN Y=+/-1292, AS FAR AS VISIBLE
571134-01-3 ************** TASK DELETED ************** N/A
571134-01-4 ************** TASK DELETED ************** N/A
571134-01-5 ************** TASK DELETED ************** N/A
571134-01-7 ************** TASK DELETED ************** N/A
3-57 571134-01-9 191 DET CENTER WING BOX SKIN STRINGER 11-15 AF ALI ALI 571134-01-9 571000-200-013 32800 FC 6500 FC N/A
192 OR OR
195 DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN 65600 FH 13100 FH
196 LOWER SURFACE, FROM STRINGER 11 TO STRINGER 15,
BETWEEN Y=+/-1292, AS FAR AS VISIBLE
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571135-01-1 141 DET CENTER WING BOX SKIN STRINGER 6-11, 11-15 AF ALI ALI 571135-01-1 571000-200-014 32800 FC 9500 FC APPL
142 OR OR
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN 65600 FH 19000 FH
UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6
TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11
TO STRINGER 15, BETWEEN Y=+/-1292
571135-01-2 ************** TASK DELETED ************** N/A
571135-01-4 ************** TASK DELETED ************** N/A
571135-01-5 ************** TASK DELETED ************** N/A
571135-01-7 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 130 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 571135-01-9 141 DET CENTER WING BOX SKIN STRINGER 6-11, 11-15 AF ALI ALI 571135-01-9 571000-200-014 32800 FC 8400 FC N/A
142 OR OR
DETAILED INSPECTION OF CENTER WING BOX, BOTTOM SKIN 65600 FH 16800 FH
UPPER SURFACE, INCLUDING STRINGERS, FROM STRINGER 6
TO STRINGER 11, BETWEEN Y=+/-765 AND FROM STRINGER 11
TO STRINGER 15, BETWEEN Y=+/-1292
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571136-01-1 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-1 571000-220-003 41400 FC 7800 FC APPL
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 82800 FH 15600 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
3-57 571136-01-2 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-2 571000-220-003 49100 FC 9100 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 98300 FH 18200 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
3-57 571136-01-3 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-3 571000-220-003 20000 FC 8600 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 49100 FH 23700 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
3-57 571136-01-4 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-4 571000-220-003 16500 FC 8800 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 71200 FH 38000 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
3-57 571136-01-6 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-6 571000-220-003 34700 FC 7100 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 69400 FH 14200 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571136-01-7 141 SDI CENTER WING BOX DRAIN HOLES NDT ALI ALI 571136-01-7 571000-220-003 42700 FC 9300 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (ROTO) OF CENTER WING 85500 FH 18600 FH
BOX, DRAIN HOLES ON STRINGER 13 AND STRINGER 14 ON
BOTTOM SKIN, UPPER SURFACE (12 PLACES)
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571154-01-1 191 DET CENTER WING BOX LOWER SKIN AF MRB CPCP MRB 571154-01-1 571000-200-019 6 YE 6 YE APPL
192
195 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN
196 LOWER SURFACE, FROM FR 36 TO FR 42, BETWEEN RIB 1 LH
AND RIB 1 RH, INCLUDING LOWER SPLICE AT RIB 1, AS FAR
AS VISIBLE
3-57 571155-01-1 191 DET CENTER WING BOX LOWER SKIN AF MRB CPCP MRB 571155-01-1 571000-200-016 12 YE 12 YE 24 YE 12 YE APPL
192
195 DETAILED INSPECTION OF CENTER WING BOX, LOWER SKIN
196 LOWER SURFACE, FROM FR 36 TO FR 42 BETWEEN RIB 1 LH
AND RIB 1 RH, COVERED BY VAPOR SEAL
APPENDIX A
AEG/AMP/A320 Page 131 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 571156-01-1 137 DET CENTER WING BOX FRONT SPAR AF MRB CPCP MRB 571156-01-1 571000-200-020 12 YE 12 YE 24 YE 12 YE APPL
138
DETAILED INSPECTION OF CENTER WING BOX, FRONT SPAR,
FORWARD FACE
3-57 571157-01-1 145 DET CENTER WING BOX UPPER SKIN AF MRB CPCP MRB 571157-01-1 571000-200-021 12 YE 12 YE APPL
146
DETAILED INSPECTION OF CENTER WING BOX, UPPER SKIN
UPPER SURFACE AND BEAMS, INCLUDING FRAME FEET BETWEEN
FR 36 AND FR 42.
NOTE:
- CAN BE PERFORMED AT SAME TIME AS 533135-01-1
- TPS MAY BE LIMITED TO CENTER WING BOX, UPPER SKIN
BEAMS, BETWEEN FR 36 AND FR 42
3-57 571164-01-1 145 DET CENTER WING BOX UPPER PANEL AF ALI ALI 571164-01-1 571000-200-015 26400 FC 11700 FC N/A
146 OR OR
DETAILED INSPECTION OF CENTER WING BOX, UPPER PANEL, 52900 FH 23500 FH
ENDS OF FLOOR BEAM, AFT FLANGE (6 PLACES)
3-57 571164-02-1 145 SDI CENTER WING BOX UPPER PANEL NDT ALI WFD ALI 571164-02-1 571000-220-803 54400 FC 14400 FC N/A
146 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 108900 FH 28900 FH
BOX, UPPER PANEL, ENDS OF FLOOR BEAM, AFT FLANGE (6
PLACES).
3-57 571170-01-1 191 SDI INSPECTION OF CENTER WING BOX NDT ALI ALI 571170-01-1 571000-220-006 34000 FC 9800 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, 68000 FH 19600 FH
CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FR 42,
LH/RH
3-57 571170-01-2 191 SDI INSPECTION OF CENTER WING BOX NDT ALI ALI 571170-01-2 571000-220-006 21000 FC 9800 FC APPL
192 OR OR
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, 42000 FH 19600 FH
CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FR 42,
LH/RH
3-57 571170-01-5 191 SDI INSPECTION OF CENTER WING BOX NDT ALI ALI 571170-01-5 571000-220-006 10100 FC 4200 FC N/A
192 OR OR
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, 43600 FH 18000 FH
CRUCIFORM FITTING, REAR SPAR AT THE LEVEL OF FR 42,
LH/RH
3-57 571181-01-10 141 SDI CENTER WING BOX TRIFORM FITTING NDT ALI ALI 571181-01-10 571000-200-023 48000 FC 39100 FC APPL
142 OR OR
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, 96000 FH 78200 FH
UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF
FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42,
LH/RH
3-57 571181-01-11 141 SDI CENTER WING BOX TRIFORM FITTING NDT ALI ALI 571181-01-11 571000-200-023 45600 FC 40500 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (US) OF CENTER WING BOX, 91300 FH 81000 FH
UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF
FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42,
LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571182-01-10 540 SDI OUTER WING TRIFORM FITTING NDT ALI ALI 571182-01-10 571000-200-024 48000 FC 14800 FC APPL
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX, 96000 FH 29700 FH
UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF
FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42,
LH/RH
APPENDIX A
AEG/AMP/A320 Page 132 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 571182-01-11 540 SDI OUTER WING TRIFORM FITTING NDT ALI ALI 571182-01-11 571000-200-024 48000 FC 9700 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX, 96000 FH 19400 FH
UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF
FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42,
LH/RH
3-57 571182-01-12 540 SDI OUTER WING TRIFORM FITTING NDT ALI ALI 571182-01-12 571000-200-024 39900 FC 15500 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX, 79900 FH 31100 FH
UPPER SURFACE OF TRIFORM FITTING (ON FIRST ROW OF
FASTENERS FROM RIB 1), BETWEEN STRINGER 8 AND FR 42,
LH/RH.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571183-01-10 191 SDI CENTER WING BOX LOWER SPLICE AT RIB 1 NDT ALI ALI 571183-01-10 571000-200-025 51700 FC 19500 FC N/A
192 OR OR
195 SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE 103400 FH 39100 FH
196 ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
3-57 571183-01-11 191 SDI CENTER WING BOX LOWER SPLICE AT RIB 1 NDT ALI ALI 571183-01-11 571000-200-025 46700 FC 21400 FC APPL
192 OR OR
195 SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE 93400 FH 42800 FH
196 ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
3-57 571183-01-12 191 SDI CENTER WING BOX LOWER SPLICE AT RIB 1 NDT ALI ALI 571183-01-12 571000-200-025 48000 FC 20600 FC N/A
192 OR OR
195 SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE 96000 FH 41200 FH
196 ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
3-57 571183-01-13 191 SDI CENTER WING BOX LOWER SPLICE AT RIB 1 NDT ALI ALI 571183-01-13 571000-200-025 38600 FC 21400 FC N/A
192 OR OR
195 SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE 77200 FH 42800 FH
196 ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571183-01-14 191 SDI CENTER WING BOX LOWER SPLICE AT RIB 1 NDT ALI ALI 571183-01-14 571000-200-025 42500 FC 18500 FC N/A
192 OR OR
195 SPECIAL DETAILED INSPECTION (US) OF CWB, LOWER SPLICE 85000 FH 37100 FH
196 ON LOWER SKIN LOWER SURFACE AT RIB 1 (AT TWO CENTRAL
ROWS OF FASTENERS), BETWEEN STRINGER 8 AND FR 42,
LH/RH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 571185-01-1 540 SDI OUTER WING UPPER HALF OF VERTICAL TEE NDT ALI ALI 571185-01-1 571000-200-026 29000 FC 11200 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX 60000 FH 33000 FH
(HOLES ON) UPPER HALF OF VERTICAL TEE FITTING AT
JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH
571185-01-10 ************** TASK DELETED ************** N/A
571185-01-11 ************** TASK DELETED ************** N/A
571185-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 133 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
571185-01-8 ************** TASK DELETED ************** N/A
3-57 571185-01-9 540 SDI OUTER WING UPPER HALF OF VERTICAL TEE NDT ALI ALI 571185-01-9 571000-200-026 24000 FC 4600 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING BOX 48000 FH 9300 FH
(HOLES ON) UPPER HALF OF VERTICAL TEE FITTING AT
JUNCTION WITH RIB 1 AND REAR SPAR, LH/RH
571189-01-3 ************** TASK DELETED ************** N/A
3-57 571189-01-5 141 DET CENTER WING BOX STRINGER WEB AF ALI ALI 571189-01-5 571000-200-017 30100 FC 27200 FC N/A
142 OR OR
DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB 60300 FH 54400 FH
AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER
STRINGERS 2, 3, 8, 9, 15, 16
571189-01-6 ************** TASK DELETED ************** N/A
571189-01-8 ************** TASK DELETED ************** N/A
3-57 571189-09-8 141 DET CENTER WING BOX STRINGER WEB AF MRB FMP MRB 571189-09-8 24 YE 6 YE APPL
142 NOTE NOTE
DETAILED INSPECTION OF CENTER WING BOX, STRINGER WEB
AT JUNCTION WITH STRUT ATTACH FITTINGS ON UPPER
STRINGERS 2, 3, 8, 9, 15, 16.
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 571190-01-1 141 SDI CENTER WING BOX, FRAME FEET NDT ALI ALI 571190-01-1 571000-200-018 29900 FC 9700 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 59800 FH 19500 FH
BOX, FRAME FEET, UPPER FLANGE AT JUNCTION WITH CROWN
FITTING ON FR 37 TO FR 41
3-57 571191-01-1 141 SDI CENTER WING BOX NDT ALI ALI 571191-01-1 571000-250-802 42400 FC 40600 FC APPL
142
SPECIAL DETAILED INSPECTION (HFEC) OF FLOOR BEAM
ELLIPTICAL HOLES IN CURRENT AREA, Y+/-254, Y+/-765
BETWEEN STIFFENER 12 AND STIFFENER 15.
3-57 571191-01-2 141 SDI CENTER WING BOX NDT ALI ALI 571191-01-2 571000-250-802 48000 FC 46900 FC N/A
142
SPECIAL DETAILED INSPECTION (HFEC) OF FLOOR BEAM
ELLIPTICAL HOLES IN CURRENT AREA, Y+/-254, Y+/-765
BETWEEN STIFFENER 12 AND STIFFENER 15.
3-57 571192-01-1 141 SDI CENTER WING BOX REAR SPAR NDT ALI ALI 571192-01-1 571000-220-005 21900 FC 10600 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 43900 FH 21300 FH
BOX, REAR SPAR, EDGE OF LOWER FLANGE AT CORNER
FITTING, LH/RH
3-57 571192-01-2 141 SDI CENTER WING BOX REAR SPAR NDT ALI ALI 571192-01-2 571000-220-005 25200 FC 12100 FC N/A
142 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF CENTER WING 50400 FH 24300 FH
BOX, REAR SPAR, EDGE OF LOWER FLANGE AT CORNER
FITTING, LH/RH
3-57 571199-01-1 540 DET OUTER WING BOX EXTERNAL SURFACE AF MRB CPCP MRB 571199-01-1 571000-200-022 12 YE 12 YE APPL
640
DETAILED INSPECTION OF OUTER WING BOX, OUTBOARD
SURFACE OF RIB 1 AND UPPER SURFACE OF TRIFORM
FITTING, BETWEEN FRONT SPAR AND REAR SPAR
3-57 572001-01-1 521 DET OUTER WING FRONT SPAR FWD FACE AF MRB CPCP MRB 572001-01-1 572000-220-004 12 YE 6 YE APPL
621
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING VICINITY OF
CUTOUTS FOR SLAT TRACKS 1,2,3 AND 4
3-57 572002-01-1 540 DET OUTER WING FRONT SPAR ROOT JOINT FTG AF MRB CPCP MRB 572002-01-1 572000-200-003 12 YE 12 YE 24 YE 12 YE APPL
640
DETAILED INSPECTION OF OUTER WING, FRONT SPAR, AFT
FACE, UPPER AND LOWER ROOT JOINT FITTINGS
572002-01-2 ************** TASK DELETED ************** N/A
572002-01-5 ************** TASK DELETED ************** N/A
572002-01-6 ************** TASK DELETED ************** N/A
572002-01-7 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 134 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572004-01-1 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-1 572000-200-004 57000 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 114000 FH 30000 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-10 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-10 572000-200-004 36300 FC 7800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 72600 FH 15600 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-11 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-11 572000-200-004 41700 FC 6600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 83500 FH 13300 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-12 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-12 572000-200-004 33600 FC 7400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 67200 FH 14800 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572004-01-13 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-13 572000-200-004 29600 FC 7400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 59200 FH 14800 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572004-01-14 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-14 572000-200-004 44000 FC 13200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 88000 FH 26400 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-15 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-15 572000-200-004 33400 FC 7700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 66900 FH 15400 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-2 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-2 572000-200-004 44000 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 88000 FH 30000 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
572004-01-3 ************** TASK DELETED ************** N/A
3-57 572004-01-4 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-4 572000-200-004 39800 FC 14700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 60000 FH 24300 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-5 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-5 572000-200-004 34200 FC 9900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 68400 FH 19800 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-6 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-6 572000-200-004 27500 FC 9900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 55000 FH 19800 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
APPENDIX A
AEG/AMP/A320 Page 135 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572004-01-7 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-7 572000-200-004 38200 FC 8500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 76400 FH 17000 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-8 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-8 572000-200-004 23900 FC 8500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 47800 FH 17000 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572004-01-9 540 DET OUTER WING FRONT SPAR AFT FACE AF ALI ALI 572004-01-9 572000-200-004 22700 FC 7800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 45400 FH 15600 FH
FACE, BETWEEN RIB 1 AND RIB 8, EXCLUDING THE AREA
INSIDE THE DRY BAY
3-57 572007-01-10 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-10 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 8100 FC 8100 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 16200 FH 16200 FH
3-57 572007-01-11 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-11 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 7100 FC 7100 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 30500 FH 30500 FH
3-57 572007-01-13 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-13 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 11200 FC 11200 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 22400 FH 22400 FH
3-57 572007-01-14 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-14 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 7100 FC 7100 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 14200 FH 14200 FH
3-57 572007-01-15 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-15 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 5100 FC 5100 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 10200 FH 10200 FH
3-57 572007-01-16 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-16 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 5400 FC 5400 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 23400 FH 23400 FH
3-57 572007-01-17 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-17 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 10100 FC 10100 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 20300 FH 20300 FH
3-57 572007-01-18 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-18 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 8400 FC 8400 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 16800 FH 16800 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 136 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572007-01-19 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-19 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 5500 FC 5500 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 23600 FH 23600 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572007-01-2 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-2 572000-200-005 12 YE 6 YE APPL
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 11900 FC 11900 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 23800 FH 23800 FH
3-57 572007-01-20 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-20 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 5800 FC 5800 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 11600 FH 11600 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572007-01-21 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-21 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 14800 FC 14800 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE. 29700 FH 29700 FH
3-57 572007-01-3 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-3 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 11200 FC 11200 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 18400 FH 18400 FH
3-57 572007-01-4 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-4 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 11200 FC 11200 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 22400 FH 22400 FH
3-57 572007-01-6 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-6 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 10600 FC 10600 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 45500 FH 45500 FH
3-57 572007-01-7 571 DET OUTER WING REAR SPAR AFT FACE AF MRB CPCP MRB 572007-01-2 572000-200-005 12 YE 6 YE N/A
671
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING
REAR SPAR ANGLE
3-57 572007-01-8 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-8 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR, AFT 8000 FC 8000 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 16000 FH 16000 FH
3-57 572007-01-9 571 DET OUTER WING REAR SPAR AFT FACE AF ALI ALI 572007-01-9 572000-200-005 12 YE 6 YE N/A
671 MRB CPCP MRB 572007-01-2 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 10500 FC 10500 FC
FACE, BETWEEN RIB 1 AND GEAR SUPPORT RIB 5, INCLUDING OR OR
REAR SPAR ANGLE 21000 FH 21000 FH
572008-01-1 ************** TASK DELETED ************** N/A
3-57 572008-01-10 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-10 572000-200-006 34700 FC 8500 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 69500 FH 17000 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
APPENDIX A
AEG/AMP/A320 Page 137 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572008-01-11 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-11 572000-200-006 24700 FC 6200 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 49400 FH 12400 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572008-01-12 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-12 572000-200-006 8500 FC 4100 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 36500 FH 17600 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572008-01-13 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-13 572000-200-006 21900 FC 4200 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 43800 FH 8400 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572008-01-14 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-14 572000-200-006 27300 FC 6500 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 54600 FH 13100 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
572008-01-2 ************** TASK DELETED ************** N/A
572008-01-3 ************** TASK DELETED ************** N/A
3-57 572008-01-4 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-4 572000-200-006 21300 FC 7800 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 42600 FH 15600 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6.
3-57 572008-01-5 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-5 572000-200-006 26000 FC 7100 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 52000 FH 14200 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6.
3-57 572008-01-6 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-6 572000-200-006 7100 FC 5200 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 30700 FH 22300 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
3-57 572008-01-7 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-7 572000-200-006 18800 FC 5200 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 37600 FH 10400 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
3-57 572008-01-8 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-8 572000-200-006 23000 FC 4400 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 46000 FH 8800 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
3-57 572008-01-9 574 SDI OUTER WING REAR SPAR JOINT PLATE NDT ALI ALI 572008-01-9 572000-200-006 5900 FC 4000 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 25700 FH 17200 FH
WING, REAR SPAR AFT FACE SPAR JOINT PLATE AT RIB 6
3-57 572009-01-1 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-1 572000-280-801 48000 FC 12000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 96000 FH 24000 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
APPENDIX A
AEG/AMP/A320 Page 138 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572009-01-10 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-10 572000-280-801 36400 FC 9200 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 72900 FH 18500 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-3 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-3 572000-280-801 46700 FC 4700 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 93400 FH 9400 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-4 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-4 572000-280-801 42500 FC 8100 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 85000 FH 16200 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-5 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-5 572000-280-801 41400 FC 3000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 82800 FH 6000 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-6 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-6 572000-280-801 33000 FC 17000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 66000 FH 34000 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-7 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-7 572000-280-801 43700 FC 6300 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 87400 FH 12700 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-8 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-8 572000-280-801 48000 FC 12000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 96000 FH 24000 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572009-01-9 540 SDI OUTER WING REAR SPAR NDT ALI ALI 572009-01-9 572000-280-801 24000 FC 3600 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 39400 FH 5600 FH
SPAR FORWARD FACE, AT THE ATTACHMENT HOLES OF GEAR
SUPPORT RIB 5, MLG FORWARD PINTLE FITTING AND
RETRACTION JACK FITTING
3-57 572010-01-10 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-10 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 41700 FC 14300 FC 41700 FC 14300 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS OR OR OR OR
83400 FH 28600 FH 83400 FH 28600 FH
572010-01-11 ************** TASK DELETED ************** N/A
3-57 572010-01-12 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-12 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 39300 FC 9700 FC 39300 FC 9700 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS OR OR OR OR
78600 FH 19400 FH 78600 FH 19400 FH
3-57 572010-01-13 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-13 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 38400 FC 14300 FC 38400 FC 14300 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS OR OR OR OR
76800 FH 28600 FH 76800 FH 28600 FH
APPENDIX A
AEG/AMP/A320 Page 139 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572010-01-14 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-14 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 17400 FC 10100 FC 17400 FC 10100 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS OR OR OR OR
74900 FH 43500 FH 74900 FH 43500 FH
572010-01-15 ************** TASK DELETED ************** N/A
3-57 572010-01-2 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF MRB CPCP MRB 572010-01-4 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD
FACE, UPPER AND LOWER ROOT JOINT FITTINGS.
3-57 572010-01-4 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-4 572000-200-007 12 YE 12 YE 24 YE 12 YE APPL
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 58600 FC 15000 FC 58600 FC 15000 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS OR OR OR OR
117200 FH 30000 FH 117200 FH 30000 FH
3-57 572010-01-5 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-5 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 36200 FC 11400 FC 36200 FC 11400 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS. OR OR OR OR
72400 FH 22800 FH 72400 FH 22800 FH
3-57 572010-01-6 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-6 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 34100 FC 11400 FC 34100 FC 11400 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS. OR OR OR OR
60000 FH 23600 FH 60000 FH 23600 FH
3-57 572010-01-7 540 DET OUTER WING REAR SPAR ROOT JOINT FTG AF ALI ALI 572010-01-7 572000-200-007 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572010-01-4 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 35200 FC 11400 FC 35200 FC 11400 FC
FACE, UPPER AND LOWER ROOT JOINT FITTINGS. OR OR OR OR
70400 FH 22800 FH 70400 FH 22800 FH
572010-01-8 ************** TASK DELETED ************** N/A
572010-01-9 ************** TASK DELETED ************** N/A
3-57 572011-01-10 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-10 572000-200-008 18300 FC 5700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 36600 FH 11400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-11 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-11 572000-200-008 12200 FC 5700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 24400 FH 11400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-12 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-12 572000-200-008 13300 FC 4200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 57100 FH 18000 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-13 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-13 572000-200-008 17900 FC 5700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 35800 FH 11400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-14 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-14 572000-200-008 32900 FC 9400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 60000 FH 15300 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-15 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-15 572000-200-008 26800 FC 6600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 53600 FH 13300 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-16 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-16 572000-200-008 17400 FC 4300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 34800 FH 8600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
APPENDIX A
AEG/AMP/A320 Page 140 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572011-01-17 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-17 572000-200-008 16400 FC 4300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 32800 FH 8600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-18 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-18 572000-200-008 10800 FC 3500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 21600 FH 7000 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-19 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-19 572000-200-008 16300 FC 3500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 32600 FH 7000 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-2 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-2 572000-200-008 32400 FC 9300 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 64800 FH 18600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-20 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-20 572000-200-008 27900 FC 8800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 55800 FH 17600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-21 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-21 572000-200-008 9000 FC 5400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 38700 FH 23400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-22 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-22 572000-200-008 11100 FC 3200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 48000 FH 14000 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-23 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-23 572000-200-008 27600 FC 6100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 55300 FH 12300 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-24 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-24 572000-200-008 23800 FC 4600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 47600 FH 9200 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572011-01-25 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-25 572000-200-008 10900 FC 3100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 46800 FH 13300 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 141 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572011-01-26 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-26 572000-200-008 21100 FC 3200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 42200 FH 6400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572011-01-27 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-27 572000-200-008 31500 FC 7300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 63100 FH 14700 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-4 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-4 572000-200-008 30000 FC 10500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 60000 FH 21000 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-5 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-5 572000-200-008 30300 FC 8800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 60600 FH 17600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-6 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-6 572000-200-008 28700 FC 6300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 57500 FH 12600 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-7 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-7 572000-200-008 9000 FC 9000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 38700 FH 38700 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-8 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-8 572000-200-008 19600 FC 6200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 39200 FH 12400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
3-57 572011-01-9 540 DET OUTER WING REAR SPAR FWD FACE AF ALI ALI 572011-01-9 572000-200-008 18600 FC 6200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 37200 FH 12400 FH
FACE, BETWEEN RIB 1 AND RIB 8, INCLUDING THE REGION
OF THE JOINT AT RIB 6 AND TOP AND BOTTOM FLANGES
572011-03-10 ************** TASK DELETED ************** N/A
572011-03-11 ************** TASK DELETED ************** N/A
572011-03-13 ************** TASK DELETED ************** N/A
572011-03-16 ************** TASK DELETED ************** N/A
572011-03-17 ************** TASK DELETED ************** N/A
572011-03-18 ************** TASK DELETED ************** N/A
572011-03-19 ************** TASK DELETED ************** N/A
572011-03-24 ************** TASK DELETED ************** N/A
572011-03-8 ************** TASK DELETED ************** N/A
572011-03-9 ************** TASK DELETED ************** N/A
3-57 572012-01-1 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-1 572000-220-001 59600 FC 15000 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 119200 FH 30000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
3-57 572012-01-2 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-2 572000-220-001 26000 FC 13400 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 52000 FH 26800 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
572012-01-3 ************** TASK DELETED ************** N/A
572012-01-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 142 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572012-01-5 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-5 572000-220-001 56000 FC 15000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 112000 FH 30000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8.
3-57 572012-01-6 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-6 572000-220-001 41000 FC 14100 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 82000 FH 28200 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572012-01-7 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-7 572000-220-001 38400 FC 11200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 76800 FH 22400 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572012-01-8 500 DET OUTER WING TOP SKIN UPR SURFACE AF ALI ALI 572012-01-8 572000-220-001 22500 FC 9800 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN UPPER 45100 FH 19600 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 1 AND RIB 8
3-57 572014-01-11 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-11 572000-210-802 30700 FC 3400 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 61400 FH 6800 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572014-02-2.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572014-01-12 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-12 572000-210-802 28800 FC 2700 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 57600 FH 5400 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572014-02-14.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572014-01-13 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-13 572000-210-802 30700 FC 3400 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 61400 FH 6800 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572014-02-15.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 143 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572014-01-3 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-3 572000-210-802 48300 FC 15000 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 96600 FH 30000 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
3-57 572014-01-4 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-4 572000-210-802 42700 FC 8000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 60000 FH 12600 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
3-57 572014-01-7 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-7 572000-210-802 42800 FC 10000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 85600 FH 20000 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
3-57 572014-01-8 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-8 572000-210-802 45400 FC 15000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 90800 FH 30000 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
3-57 572014-01-9 500 GVI OUTER WING TOP SKIN AF ALI ALI 572014-01-9 572000-210-802 36700 FC 7700 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 73500 FH 15400 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR
3-57 572014-02-1 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-1 572000-220-807 57400 FC 13000 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 114800 FH 26000 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
3-57 572014-02-14 500 DET OUTER WING TOP SKIN AF ALI ALI 572014-02-14 572000-220-807 28800 FC 10500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 57600 FH 21000 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
NOTE:
PLANNING:
- THIS TASK IS ALTERNATIVE TO TASK 572014-01-12.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572014-02-15 500 DET OUTER WING TOP SKIN AF ALI ALI 572014-02-15 572000-220-807 30700 FC 13200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 61400 FH 26400 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572014-01-13.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572014-02-2 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-2 572000-220-807 30700 FC 7600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 61400 FH 15300 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572014-01-11.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 144 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572014-02-3 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-3 572000-220-807 50200 FC 10600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 100400 FH 21200 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
3-57 572014-02-4 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-4 572000-220-807 53900 FC 10200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 107800 FH 20500 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
3-57 572014-02-5 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-5 572000-220-807 43500 FC 6600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 87000 FH 13200 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
3-57 572014-02-7 500 DET OUTER WING TOP SKIN AF ALI WFD ALI 572014-02-7 572000-220-807 37900 FC 6400 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 75800 FH 12800 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 1 AND RIB 8 FROM FRONT SPAR TO REAR SPAR.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572019-01-1 ************** TASK DELETED ************** N/A
572019-01-2 ************** TASK DELETED ************** N/A
572019-01-3 ************** TASK DELETED ************** N/A
572019-01-4 ************** TASK DELETED ************** N/A
3-57 572020-01-1 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-1 572000-200-010 33900 FC 11700 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 67800 FH 23400 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT
STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE
DRY BAY
3-57 572020-01-10 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-10 572000-200-010 36700 FC 36700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 73400 FH 73400 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT
STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE
DRY BAY
3-57 572020-01-11 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-11 572000-200-010 36700 FC 36700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 73400 FH 73400 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-13 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI WFD ALI 572020-01-13 572000-200-010 33000 FC 6900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 66000 FH 13800 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-14 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-14 572000-200-010 34500 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 69000 FH 30000 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT
STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE
DRY BAY
APPENDIX A
AEG/AMP/A320 Page 145 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572020-01-15 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-15 572000-200-010 39800 FC 11600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS 79700 FH 23200 FH
BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR
TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-16 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-16 572000-200-010 34500 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 69000 FH 30000 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-17 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-17 572000-200-010 33000 FC 9200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 66000 FH 18400 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-18 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-18 572000-200-010 34400 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS 68800 FH 30000 FH
BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR
TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572020-01-19 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-19 572000-200-010 34400 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS 68800 FH 30000 FH
BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR
TRANSFER HOLES AND BUTT STRAP, AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572020-01-25 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-25 572000-200-010 32300 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS 64600 FH 30000 FH
BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR
TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572020-01-26 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-26 572000-200-010 40600 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN STRINGERS 81200 FH 30000 FH
BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS AND AIR
TRANSFER HOLES, STRINGER JOINTS, AND BUTT STRAP, AT
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-3 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-3 572000-200-010 33900 FC 11700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 67800 FH 23400 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
APPENDIX A
AEG/AMP/A320 Page 146 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572020-01-4 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-4 572000-200-010 38400 FC 11900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 76800 FH 23800 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-6 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-6 572000-200-010 33000 FC 12000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 66000 FH 24000 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572020-01-7 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-7 572000-200-010 32000 FC 10600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 60000 FH 20500 FH
STRINGERS BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, AND BUTTSTRAP AT STRINGER 11,
EXCLUDING THE AREA INSIDE THE DRY BAY
572020-01-8 ************** TASK DELETED ************** N/A
3-57 572020-01-9 540 DET OUTER WING TOP SKIN RIB 1 AND 8 AF ALI ALI 572020-01-9 572000-200-010 33000 FC 9200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 66000 FH 18400 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGER JOINTS, AND BUTT
STRAP, AT STRINGER 11, EXCLUDING THE AREA INSIDE THE
DRY BAY
3-57 572021-01-1 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-1 572000-220-806 53000 FC 14500 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 106000 FH 29000 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572021-01-10 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-10 572000-220-806 41800 FC 11400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 83700 FH 22900 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572021-01-11 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-11 572000-220-806 31100 FC 6900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 62200 FH 13800 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572021-01-2 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-2 572000-220-806 49400 FC 11000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 98800 FH 22000 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572021-01-4 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-4 572000-220-806 33800 FC 8800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 67600 FH 17600 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 147 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572021-01-7 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-7 572000-220-806 37600 FC 7100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 75200 FH 14300 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572021-01-8 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-8 572000-220-806 26700 FC 6900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 53400 FH 13800 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572021-01-9 540 DET OUTER WING TOP SKIN RIBS 4, 5 AND 6 AF ALI WFD ALI 572021-01-9 572000-220-806 23600 FC 4500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN 47200 FH 9000 FH
STRINGERS, INBOARD AND OUTBOARD OF RIBS 4, 5 AND 6 AT
ATTACHMENT TO CLEATS INCLUDING AFT WEB FACE, FORWARD
WEB FACE AND CROWN. INCLUDING ANY ATTACHMENTS HOLE IN
THE STRINGER WEB BETWEEN RIB 4 TO 6.
3-57 572022-01-1 521 DET OUTER WING TOP SKIN LWR SURFACE AF MRB CPCP MRB 572022-01-1 572000-200-011 12 YE 12 YE 24 YE 12 YE APPL
540
621 DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
640 SURFACE PYLON REINFORCING PLATE
572024-01-1 ************** TASK DELETED ************** N/A
572024-01-2 ************** TASK DELETED ************** N/A
572024-01-3 ************** TASK DELETED ************** N/A
572024-01-4 ************** TASK DELETED ************** N/A
572024-01-5 ************** TASK DELETED ************** N/A
572026-01-1 ************** TASK DELETED ************** N/A
572026-01-2 ************** TASK DELETED ************** N/A
572026-01-4 ************** TASK DELETED ************** N/A
572026-01-5 ************** TASK DELETED ************** N/A
572026-01-6 ************** TASK DELETED ************** N/A
3-57 572026-01-7 540 DET OUTER WING BOLTED PANEL AF ALI ALI 572026-01-7 572000-200-014 38300 FC 10800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF 60000 FH 25300 FH
BOLTED PANEL
3-57 572026-01-8 540 DET OUTER WING BOLTED PANEL AF ALI ALI 572026-01-8 572000-200-014 38300 FC 10800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, RIB 5, AFT OF 76600 FH 21600 FH
BOLTED PANEL
572027-01-1 ************** TASK DELETED ************** N/A
572027-01-2 ************** TASK DELETED ************** N/A
572027-01-3 ************** TASK DELETED ************** N/A
572027-01-4 ************** TASK DELETED ************** N/A
3-57 572027-01-5 540 DET OUTER WING RIB 5 AND RIB 6 AF ALI ALI 572027-01-5 572000-200-015 30100 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 AT 60200 FH 30000 FH
SKIN ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS,
ACCESS CUTOUT SURROUNDS AND IN REGION OF STRINGER
CUTOUTS, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572027-01-6 540 DET OUTER WING RIB 5 AND RIB 6 AF ALI ALI 572027-01-6 572000-200-015 26600 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, RIB 5 AND RIB 6 AT 53200 FH 30000 FH
SKIN ATTACHMENTS (INCLUDING CLEATS) SPAR ATTACHMENTS,
ACCESS CUTOUT SURROUNDS AND IN REGION OF STRINGER
CUTOUTS, EXCLUDING THE AREA INSIDE THE DRY BAY
572028-01-1 ************** TASK DELETED ************** N/A
572028-01-2 ************** TASK DELETED ************** N/A
572029-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 148 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
572029-01-2 ************** TASK DELETED ************** N/A
572029-01-3 ************** TASK DELETED ************** N/A
572029-01-4 ************** TASK DELETED ************** N/A
572029-01-5 ************** TASK DELETED ************** N/A
572029-01-6 ************** TASK DELETED ************** N/A
3-57 572029-01-7 500 DET OUTER WING BOTTOM SKIN RIB 1-7 AF ALI ALI 572029-01-7 572000-200-017 25400 FC 11800 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 50800 FH 23600 FH
SURFACE AT ATTACHMENT TO FRONT SPAR, BETWEEN RIB 1
AND RIB 7, EXCLUDING AREA COVERED BY PYLON FAIRING
AND PYLON REINFORCING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572029-01-8 500 DET OUTER WING BOTTOM SKIN RIB 1-7 AF ALI ALI 572029-01-8 572000-200-017 24000 FC 11000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 22000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR, BETWEEN RIB 1
AND RIB 7, EXCLUDING AREA COVERED BY PYLON FAIRING
AND PYLON REINFORCING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572030-01-1 500 SDI OUTER WING BOTTOM SKIN NDT ALI WFD ALI 572030-01-1 572000-280-804 52800 FC 5800 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 105700 FH 11700 FH
BOTTOM SKIN MASKED BY PYLON REINFORCING PLATE.
572031-01-1 ************** TASK DELETED ************** N/A
572031-01-2 ************** TASK DELETED ************** N/A
3-57 572032-01-1 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-1 572000-200-020 60000 FC 7500 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 120000 FH 15000 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
3-57 572032-01-2 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-2 572000-200-020 24000 FC 6800 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 13600 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
3-57 572032-01-4 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-4 572000-200-020 16800 FC 4400 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 72300 FH 19000 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
3-57 572032-01-5 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-5 572000-200-020 24000 FC 6500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 42000 FH 11300 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
3-57 572032-01-7 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-7 572000-200-020 24000 FC 6500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 13000 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
APPENDIX A
AEG/AMP/A320 Page 149 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572032-01-8 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-8 572000-200-020 31700 FC 10700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 63400 FH 21400 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572032-01-9 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 572032-01-9 572000-200-020 29900 FC 9900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 59800 FH 19800 FH
SURFACE AT ATTACHMENT TO REAR SPAR, BETWEEN RIB 1 AND
RIB 8, EXCLUDING AREAS COVERED BY MLG REINFORCING
PLATE, FLAP TRACK 2 FAIRING AND PYLON FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572033-01-1 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-1 572000-200-021 48000 FC 8800 FC APPL
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 96000 FH 17700 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
3-57 572033-01-11 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-11 572000-200-021 31900 FC 8200 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 63800 FH 16500 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572033-01-12 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI ALI 572033-01-12 572000-200-021 33800 FC 15000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 67600 FH 30000 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572033-01-2 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-2 572000-200-021 48000 FC 8200 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 96000 FH 16400 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
572033-01-4 ************** TASK DELETED ************** N/A
3-57 572033-01-5 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-5 572000-200-021 48000 FC 8400 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 96000 FH 16800 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
APPENDIX A
AEG/AMP/A320 Page 150 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572033-01-6 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-6 572000-200-021 45200 FC 8500 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 90400 FH 17000 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
3-57 572033-01-7 540 SDI OUTER WING BOTTOM SKIN LDG PLATE NDT ALI WFD ALI 572033-01-7 572000-200-021 33800 FC 8500 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 67600 FH 17100 FH
BOTTOM SKIN, FORWARD OF REAR SPAR IN AREA MASKED BY
MLG REINFORCING PLATE INCLUDING ATTACHMENT TO REAR
SPAR.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572034-01-1 500 GVI OUTER WING BOTTOM SKIN LDG PLATE AF ALI ALI 572034-01-1 572000-210-003 31700 FC 10100 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 51400 FH 16300 FH
LOWER SURFACE MLG REINFORCING PLATE
3-57 572034-01-3 500 GVI OUTER WING BOTTOM SKIN LDG PLATE AF ALI ALI 572034-01-3 572000-210-003 32700 FC 10200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 65400 FH 20400 FH
LOWER SURFACE MLG REINFORCING PLATE
3-57 572034-01-6 500 GVI OUTER WING BOTTOM SKIN LDG PLATE AF ALI ALI 572034-01-6 572000-210-003 15400 FC 5300 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 66300 FH 23000 FH
LOWER SURFACE MLG REINFORCING PLATE
3-57 572034-01-8 500 GVI OUTER WING BOTTOM SKIN LDG PLATE AF ALI ALI 572034-01-8 572000-210-003 36900 FC 9000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 73900 FH 18000 FH
LOWER SURFACE MLG REINFORCING PLATE
3-57 572036-01-2 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-2 572000-200-022 60000 FC 10300 FC APPL
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 120000 FH 20600 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
3-57 572036-01-3 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-3 572000-200-022 35800 FC 10600 FC N/A
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 71600 FH 21200 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
3-57 572036-01-4 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-4 572000-200-022 28700 FC 10600 FC N/A
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 57400 FH 21200 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
3-57 572036-01-5 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-5 572000-200-022 36500 FC 10200 FC N/A
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 60000 FH 17700 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
572036-01-6 ************** TASK DELETED ************** N/A
3-57 572036-01-8 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-8 572000-200-022 37400 FC 14500 FC N/A
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 74800 FH 29100 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 151 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572036-01-9 531 DET OUTER WING BOTTOM SKIN FLAP TRACK 2 AF ALI ALI 572036-01-9 572000-200-022 35200 FC 13500 FC N/A
631 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 70400 FH 27100 FH
SURFACE, FORWARD OF REAR SPAR IN AREA COVERED BY FLAP
TRACK 2 FAIRINGS, INCLUDING ATTACHMENT TO REAR SPAR
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572037-02-4 ************** TASK DELETED ************** N/A
572037-02-5 ************** TASK DELETED ************** N/A
572037-02-6 ************** TASK DELETED ************** N/A
3-57 572038-01-1 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572038-01-1 572000-200-023 54600 FC 5600 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 109200 FH 11200 FH
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB
BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
3-57 572038-01-2 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572038-01-2 572000-200-023 24000 FC 4100 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 8200 FH
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB
BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
572038-01-3 ************** TASK DELETED ************** N/A
572038-01-4 ************** TASK DELETED ************** N/A
3-57 572038-01-5 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572038-01-5 572000-200-023 51500 FC 5300 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 103000 FH 10600 FH
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB
BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
3-57 572038-01-6 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572038-01-6 572000-200-023 24400 FC 8200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48800 FH 16400 FH
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB
BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572038-01-7 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572038-01-7 572000-200-023 23000 FC 7900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 46000 FH 15800 FH
SURFACE AT RUNOUTS OF STRINGER 2 (RIB BAY 5-6),
STRINGER 9 (RIB BAYS 2-3 AND 6-7), STRINGER 10 (RIB
BAYS 2-3 AND 6-7), STRINGER 14 (RIB BAY 3-4) AND
STRINGER 15 (RIB BAY 2-3)
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572040-01-1 540 DET OUTER WING BOTTOM SKIN CUTOUTS AF MRB CPCP MRB 572040-01-1 572000-200-001 10 YE 5 YE N/A
640
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER
AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB
BAY 2-3 AND RIB BAY 6-7
APPENDIX A
AEG/AMP/A320 Page 152 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572040-01-2 540 DET OUTER WING BOTTOM SKIN CUTOUTS AF MRB CPCP MRB 572040-01-2 572000-200-001 12 YE 6 YE APPL
640
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER
AND LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN RIB
BAY 2-3 AND RIB BAY 6-7
3-57 572040-03-1 540 SDI OUTER WING BOTTOM SKIN CUTOUTS NDT ALI ALI 572040-03-1 572000-200-032 41600 FC 15000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 83200 FH 30000 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS
DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7
572040-03-2 ************** TASK DELETED ************** N/A
572040-03-3 ************** TASK DELETED ************** N/A
3-57 572040-03-4 540 SDI OUTER WING BOTTOM SKIN CUTOUTS NDT ALI ALI 572040-03-4 572000-200-032 51900 FC 15000 FC APPL
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 103800 FH 30000 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS
DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7
572040-03-5 ************** TASK DELETED ************** N/A
3-57 572040-03-6 540 SDI OUTER WING NDT ALI ALI 572040-03-6 572000-200-032 49000 FC 15000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 98000 FH 30000 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES, AROUND ACCESS
DOOR CUTOUTS IN RIB BAY 2-3 AND RIB BAY 6-7
3-57 572041-02-11 500 DET OUTER WING AF ALI ALI 572041-02-11 572000-220-802 36500 FC 2800 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 73000 FH 5600 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572041-02-12 500 DET OUTER WING AF ALI ALI 572041-02-12 572000-220-802 34400 FC 2600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 68800 FH 5200 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572041-02-4 500 DET OUTER WING AF ALI ALI 572041-02-4 572000-220-802 31200 FC 4900 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 62400 FH 9800 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
3-57 572041-02-5 500 DET OUTER WING AF ALI ALI 572041-02-5 572000-220-802 29400 FC 4700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 58800 FH 9400 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
APPENDIX A
AEG/AMP/A320 Page 153 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572041-02-6 500 DET OUTER WING AF ALI ALI 572041-02-6 572000-220-802 42800 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 60000 FH 7900 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
3-57 572041-02-7 500 DET OUTER WING AF ALI ALI 572041-02-7 572000-220-802 36200 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 72400 FH 9800 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
3-57 572041-02-9 500 DET OUTER WING AF ALI ALI 572041-02-9 572000-220-802 42400 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 84800 FH 9800 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
(EXCLUDING STRINGERS 8 AND 11) BETWEEN RIB 1 AND RIB
8 FROM FRONT SPAR TO REAR SPAR EXCLUDING AREAS
COVERED BY FAIRINGS AND REINFORCING PLATES.
3-57 572042-01-10 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-10 572000-210-005 30900 FC 5500 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 61800 FH 11000 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572042-01-11 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-11 572000-210-005 29100 FC 5100 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 58200 FH 10200 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572042-01-2 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-2 572000-210-005 37300 FC 5300 FC APPL
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 74600 FH 10600 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
3-57 572042-01-3 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-3 572000-210-005 22500 FC 4000 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 45000 FH 8000 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
3-57 572042-01-4 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-4 572000-210-005 24000 FC 4000 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 8000 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
3-57 572042-01-6 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-6 572000-210-005 14800 FC 3800 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 63400 FH 16300 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
3-57 572042-01-7 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-7 572000-210-005 24000 FC 3800 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42000 FH 6200 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
APPENDIX A
AEG/AMP/A320 Page 154 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572042-01-8 471 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572042-01-8 572000-210-005 24000 FC 3800 FC N/A
481 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 7600 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, IN
AREA COVERED BY PYLON FAIRING
3-57 572044-01-2 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-2 572000-210-004 38000 FC 5800 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 76000 FH 11600 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-01-3 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-3 572000-210-004 26300 FC 3800 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42800 FH 6200 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-01-4 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-4 572000-210-004 19100 FC 4600 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 38200 FH 9200 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-01-5 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-5 572000-210-004 29000 FC 4600 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 58000 FH 9200 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-01-6 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-6 572000-210-004 12700 FC 3800 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 54600 FH 16300 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-01-7 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-01-7 572000-210-004 22600 FC 3800 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 45200 FH 7600 FH
LOWER SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
3-57 572044-02-1 500 DET OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-02-1 572000-220-812 32200 FC 3000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 64400 FH 6000 FH
SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572044-02-2 500 DET OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572044-02-2 572000-220-812 30400 FC 2700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 60800 FH 5400 FH
SURFACE SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 1 AND RIB 8, EXCLUDING AREAS
COVERED BY REINFORCING PLATES AND FAIRINGS
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572047-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 155 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572047-01-2 471 SDI OUTER BOTTOM SKIN LOWER SURFACE NDT ALI ALI 572047-01-2 572000-200-024 42500 FC 14000 FC N/A
481 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 85000 FH 28000 FH
BOTTOM SKIN, LOWER SURFACE AROUND AFT PYLON
ATTACHMENT FITTING CUTOUT
572047-01-3 ************** TASK DELETED ************** N/A
572047-01-4 ************** TASK DELETED ************** N/A
572047-01-5 ************** TASK DELETED ************** N/A
3-57 572049-01-3 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF MRB CPCP MRB 572049-01-3 574100-200-003 6 YE 6 YE N/A
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB
BAYS 1-2, 2-3, 4-5, 5-6); MAGNETIC LEVEL INDICATOR
HOLE ADJACENT TO RIB 6; MLG PICK UP RAIL HOLE FORWARD
OF REAR SPAR INBOARD OF RIB 5
3-57 572049-01-6 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF ALI ALI 572049-01-6 574100-200-003 6 YE 6 YE N/A
600 MRB CPCP MRB 572049-01-3 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 30100 FC 3000 FC
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB OR OR
BAYS 1-2, 2-3, 4-5, 5-6); MAGNETIC LEVEL INDICATOR 60200 FH 6000 FH
HOLE ADJACENT TO RIB 6; MLG PICK UP RAIL HOLE FORWARD
OF REAR SPAR INBOARD OF RIB 5
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572049-04-1.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572049-01-7 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF ALI ALI 572049-01-7 574100-200-003 6 YE 6 YE N/A
600 MRB CPCP MRB 572049-01-3 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 28400 FC 2700 FC
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB OR OR
BAYS 1-2, 2-3, 4-5, 5-6); MAGNETIC LEVEL INDICATOR 56800 FH 5400 FH
HOLE ADJACENT TO RIB 6; MLG PICK UP RAIL HOLE FORWARD
OF REAR SPAR INBOARD OF RIB 5
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572049-03-1 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF MRB CPCP MRB 572049-03-1 574100-200-802 6 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB
BAYS 1-2, 2-3, 4-5, 5-6); DRY BAY DRAIN HOLE IN RIB
BAY 6-7; MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO
RIB 6; MLG PICK UP RAIL HOLE FORWARD OF REAR SPAR
INBOARD OF RIB 5
3-57 572049-03-2 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF ALI ALI 572049-03-2 574100-200-802 6 YE 6 YE N/A
600 MRB CPCP MRB 572049-03-1 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 30100 FC 3000 FC
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB OR OR
BAYS 1-2, 2-3, 4-5, 5-6); DRY BAY DRAIN HOLE IN RIB 60200 FH 6000 FH
BAY 6-7; MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO
RIB 6; MLG PICK UP RAIL HOLE FORWARD OF REAR SPAR
INBOARD OF RIB 5
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572049-05-1.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 156 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572049-03-3 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF ALI ALI 572049-03-3 574100-200-802 6 YE 6 YE N/A
600 MRB CPCP MRB 572049-03-1 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 28400 FC 2700 FC
SURFACE AT DRAIN HOLES FOR TRACK CANS, 1,2,3,& 4 (RIB OR OR
BAYS 1-2, 2-3, 4-5, 5-6); DRY BAY DRAIN HOLE IN RIB 56800 FH 5400 FH
BAY 6-7; MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO
RIB 6; MLG PICK UP RAIL HOLE FORWARD OF REAR SPAR
INBOARD OF RIB 5
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572049-04-1 500 SDI OUTER WING BOTTOM SKIN DRAIN HOLES NDT ALI ALI 572049-04-1 574100-280-801 30100 FC 6000 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, 60200 FH 12000 FH
BOTTOM SKIN, LOWER SURFACE AT DRAIN HOLES FOR TRACK
CANS, 1,2,3,& 4 (RIB BAYS 1-2, 2-3, 4-5, 5-6);
MAGNETIC LEVEL INDICATOR HOLE ADJACENT TO RIB 6; MLG
PICK UP RAIL HOLE FORWARD OF REAR SPAR INBOARD OF RIB
5
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572049-01-6.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572049-05-1 500 SDI OUTER WING BOTTOM SKIN DRAIN HOLES NDT ALI ALI 572049-05-1 574100-280-802 30100 FC 6000 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, 60200 FH 12000 FH
BOTTOM SKIN, LOWER SURFACE AT DRAIN HOLES FOR TRACK
CANS, 1,2,3,& 4 (RIB BAYS 1-2, 2-3, 4-5, 5-6); DRY
BAY DRAIN HOLE IN RIB BAY 6-7; MAGNETIC LEVEL
INDICATOR HOLE ADJACENT TO RIB 6; MLG PICK UP RAIL
HOLE FORWARD OF REAR SPAR INBOARD OF RIB 5
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572049-03-2.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572050-01-1 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-1 572000-200-034 25000 FC 10600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 44800 FH 20500 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-1.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-01-2 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-2 572000-200-034 12700 FC 5700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 54600 FH 24300 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-2.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
APPENDIX A
AEG/AMP/A320 Page 157 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572050-01-4 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-4 572000-200-034 29800 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 59600 FH 30000 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-4.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS OF
SSI 572004 OR 572020 OR 572027 OR 572053. FROM THAT
TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF THIS
TASK.
3-57 572050-01-5 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-5 572000-200-034 28700 FC 12000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 57400 FH 24000 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-5.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-01-6 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-6 572000-200-034 28700 FC 12000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 57400 FH 24000 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-6.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-01-8 540 DET OUTER WING, DRY BAY AREA AF ALI ALI 572050-01-8 572000-200-034 25000 FC 11700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, DRY BAY AREA 50000 FH 23400 FH
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-02-8.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-02-1 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-1 572000-220-011 25000 FC 10600 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 44800 FH 20500 FH
WING, DRY BAY AREA
NOTE:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-1.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
APPENDIX A
AEG/AMP/A320 Page 158 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572050-02-10 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-10 572000-220-011 33600 FC 7400 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 67200 FH 14800 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572050-02-11 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-11 572000-220-011 29100 FC 7400 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 58200 FH 14800 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572050-02-12 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-12 572000-220-011 36000 FC 7700 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 72000 FH 15400 FH
WING, DRY BAY AREA
3-57 572050-02-2 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-2 572000-220-011 12700 FC 5700 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 54600 FH 24300 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-2.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-02-4 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-4 572000-220-011 29800 FC 15000 FC APPL
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 59600 FH 30000 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-4.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-02-5 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-5 572000-220-011 28700 FC 12000 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 57400 FH 24000 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-5.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
APPENDIX A
AEG/AMP/A320 Page 159 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572050-02-6 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-6 572000-220-011 28700 FC 12000 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 57400 FH 24000 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-6.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-02-8 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-8 572000-220-011 25000 FC 11700 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 50000 FH 23400 FH
WING, DRY BAY AREA
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572050-01-8.
- IF AN A/C HAS ALREADY EXCEEDED THE INSPECTION
THRESHOLD OF THIS TASK, THE INSPECTION SHOULD BE
PERFORMED AT THE NEXT DUE OF ANY APPLICABLE TASKS
OF SSI 572004 OR 572020 OR 572027 OR 572053. FROM
THAT TIME ONWARDS, APPLY THE INSPECTION INTERVAL OF
THIS TASK.
3-57 572050-02-9 521 SDI OUTER WING, DRY BAY AREA NDT ALI ALI 572050-02-9 572000-220-011 33200 FC 6600 FC N/A
621 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTER 66500 FH 13300 FH
WING, DRY BAY AREA
3-57 572052-01-1 540 DET OUTER WING BOTTOM SKIN ROOT JOINT FTG AF MRB CPCP MRB 572052-01-1 572000-200-025 12 YE 12 YE 24 YE 12 YE APPL
640
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT
JOINT FITTINGS ON STRINGER 8 AND STRINGER 11
3-57 572052-01-10 540 DET OUTER WING AF ALI ALI 572052-01-10 572000-200-025 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572052-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT 44700 FC 15000 FC 44700 FC 15000 FC
JOINT FITTINGS ON STRINGER 8 AND STRINGER 11 OR OR OR OR
89500 FH 30000 FH 89500 FH 30000 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572052-01-11 540 DET OUTER WING AF ALI ALI 572052-01-11 572000-200-025 12 YE 12 YE 24 YE 12 YE N/A
640 MRB CPCP MRB 572052-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN ROOT 42200 FC 15000 FC 42200 FC 15000 FC
JOINT FITTINGS ON STRINGER 8 AND STRINGER 11 OR OR OR OR
84400 FH 30000 FH 84400 FH 30000 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572052-01-2 ************** TASK DELETED ************** N/A
572052-01-5 ************** TASK DELETED ************** N/A
572052-01-6 ************** TASK DELETED ************** N/A
572052-01-8 ************** TASK DELETED ************** N/A
572052-01-9 ************** TASK DELETED ************** N/A
3-57 572053-01-2 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-2 572000-200-026 37300 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 74600 FH 30000 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
APPENDIX A
AEG/AMP/A320 Page 160 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572053-01-3 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-3 572000-200-026 28700 FC 12300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 57400 FH 24600 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572053-01-4 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-4 572000-200-026 12700 FC 11800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 54600 FH 50900 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572053-01-5 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-5 572000-200-026 25000 FC 11800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 44800 FH 21100 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572053-01-6 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-6 572000-200-026 25000 FC 11800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 50000 FH 23600 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
3-57 572053-01-7 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-7 572000-200-026 24400 FC 9700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 48800 FH 19400 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572053-01-8 540 DET OUTER WING BOTTOM SKIN STRINGERS AF ALI ALI 572053-01-8 572000-200-026 23000 FC 9000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 46000 FH 18000 FH
STRINGERS, BETWEEN RIB 1 AND RIB 8, INCLUDING DRAIN
HOLES IN STRINGERS AND BUTT STRAP AT STRINGER 8 AND
STRINGER 11, EXCLUDING THE AREA INSIDE THE DRY BAY
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572054-01-1 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-1 572000-200-002 12 YE 12 YE 24 YE 12 YE APPL
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 49700 FC 15000 FC 49700 FC 15000 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 99400 FH 30000 FH 99400 FH 30000 FH
3-57 572054-01-10 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-10 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 23200 FC 7000 FC 23200 FC 7000 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 46400 FH 14000 FH 46400 FH 14000 FH
3-57 572054-01-11 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-11 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 34200 FC 6800 FC 34200 FC 6800 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 68500 FH 13700 FH 68500 FH 13700 FH
APPENDIX A
AEG/AMP/A320 Page 161 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572054-01-12 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-12 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 30100 FC 3000 FC 30100 FC 3000 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 60200 FH 6000 FH 60200 FH 6000 FH
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572054-03-1.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572054-01-13 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-13 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 28400 FC 2700 FC 28400 FC 2700 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 56800 FH 5400 FH 56800 FH 5400 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572054-01-2 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF MRB CPCP MRB 572054-01-1 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES
BETWEEN RIB 1 AND RIB 2
572054-01-4 ************** TASK DELETED ************** N/A
572054-01-5 ************** TASK DELETED ************** N/A
572054-01-6 ************** TASK DELETED ************** N/A
572054-01-7 ************** TASK DELETED ************** N/A
3-57 572054-01-8 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-8 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 24700 FC 7500 FC 24700 FC 7500 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 49400 FH 15000 FH 49400 FH 15000 FH
3-57 572054-01-9 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF ALI ALI 572054-01-9 572000-200-002 12 YE 12 YE 24 YE 12 YE N/A
600 MRB CPCP MRB 572054-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 46800 FC 15000 FC 46800 FC 15000 FC
SURFACE AT FUEL PUMP APERTURES AND ADJACENT HOLES OR OR OR OR
BETWEEN RIB 1 AND RIB 2 93600 FH 30000 FH 93600 FH 30000 FH
3-57 572054-02-1 500 DET OUTER WING BOTTOM SKIN PUMP APERTURES AF MRB CPCP MRB 572054-02-1 572000-220-805 6 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE AT HOLES ADJACENT TO FUEL PUMP APERTURES
BETWEEN RIB 1 AND RIB 2
3-57 572054-03-1 500 SDI OUTER WING BOTTOM SKIN LOWER SURFACE NDT ALI ALI 572054-03-1 572000-280-803 30100 FC 6000 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (US) OF OUTER WING, 60200 FH 12000 FH
BOTTOM SKIN LOWER SURFACE AT FUEL PUMP APERTURES AND
ADJACENT HOLES BETWEEN RIB 1 AND RIB 2
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572054-01-12.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572057-01-1 ************** TASK DELETED ************** N/A
572057-01-2 ************** TASK DELETED ************** N/A
3-57 572062-01-1 571 DET OUTER WING FIXED TRAILING EDGE AF MRB CPCP MRB 572062-01-1 572000-220-003 12 YE 6 YE APPL
574
671 DETAILED INSPECTION OF OUTER WING, FIXED TRAILING
674 EDGE, REAR SPAR AFT FACE, BETWEEN GEAR SUPPORT RIB 5
AND RIB 8
APPENDIX A
AEG/AMP/A320 Page 162 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572063-01-1 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF MRB CPCP MRB 572063-01-1 572000-200-031 6 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE, AREA COVERED BY FUEL PUMP WIRING HARNESS
FAIRINGS.
3-57 572064-01-1 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-1 572000-220-810 31200 FC 4900 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 62400 FH 9800 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
3-57 572064-01-2 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-2 572000-220-810 36200 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 72400 FH 9800 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
3-57 572064-01-3 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-3 572000-220-810 42800 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 69600 FH 7900 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
3-57 572064-01-4 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-4 572000-220-810 29400 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 58800 FH 9800 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
3-57 572064-01-5 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-5 572000-220-810 20200 FC 5000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 40500 FH 10000 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572064-01-6 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-6 572000-220-810 12300 FC 3000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 53100 FH 13100 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572064-01-7 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572064-01-7 572000-220-810 19100 FC 5000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 38200 FH 10000 FH
SURFACE AT ATTACHMENT TO RIB 2 BETWEEN STRINGERS 8
AND 11.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572065-01-1 571 DET OUTER WING TOP SKIN LOWER SURFACE AF MRB CPCP MRB 572065-01-1 572100-220-809 6 YE 6 YE APPL
671
DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
SURFACE, OVERHANG FROM RIB 1 TO GEAR SUPPORT RIB 5
3-57 572066-01-1 571 DET OUTER WING TOP SKIN LOWER SURFACE AF MRB CPCP MRB 572066-01-1 572100-220-810 6 YE 6 YE APPL
574
671 DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
674 SURFACE, OVERHANG FROM GEAR SUPPORT RIB 5 TO RIB 8
APPENDIX A
AEG/AMP/A320 Page 163 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572101-01-1 522 DET OUTER WING FRT SPAR FWD FACE RIB 8-22 AF ALI ALI 572101-01-1 572100-200-006 12 YE 12 YE 24 YE 12 YE APPL
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 43000 FC 15000 FC 43000 FC 15000 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
86000 FH 30000 FH 86000 FH 30000 FH
3-57 572101-01-10 522 DET OUTER WING FRT SPAR FWD FACE RIB 8-22 AF ALI ALI 572101-01-10 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 37500 FC 6900 FC 37500 FC 6900 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
75100 FH 13800 FH 75100 FH 13800 FH
3-57 572101-01-11 522 DET OUTER WING FRT SPAR FWD FACE RIB 8-22 AF ALI ALI 572101-01-11 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 47700 FC 15000 FC 47700 FC 15000 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
95400 FH 30000 FH 95400 FH 30000 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572101-01-2 522 DET OUTER WING FRT SPAR FWD FACE RIB 8-22 AF MRB CPCP MRB 572101-01-1 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS
572101-01-5 ************** TASK DELETED ************** N/A
572101-01-6 ************** TASK DELETED ************** N/A
3-57 572101-01-7 522 DET MAIN STRUCTURE AF ALI ALI 572101-01-7 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 33300 FC 11600 FC 33300 FC 11600 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
55100 FH 19100 FH 55100 FH 19100 FH
3-57 572101-01-8 522 DET MAIN STRUCTURE AF ALI ALI 572101-01-8 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 30500 FC 4700 FC 30500 FC 4700 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
61000 FH 9400 FH 61000 FH 9400 FH
3-57 572101-01-9 522 DET MAIN STRUCTURE AF ALI ALI 572101-01-9 572100-200-006 12 YE 12 YE 24 YE 12 YE N/A
622 MRB CPCP MRB 572101-01-1 OR OR OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR FORWARD 16800 FC 3200 FC 16800 FC 3200 FC
FACE, BETWEEN RIB 8 AND RIB 22, INCLUDING ALL CUTOUTS OR OR OR OR
72200 FH 13700 FH 72200 FH 13700 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572106-01-1 522 DET OUTER WING FRT SPAR FWD FACE RIB 22-27 AF MRB CPCP MRB 572106-01-1 572100-200-007 12 YE 12 YE 24 YE 12 YE APPL
622
DETAILED INSPECTION OF OUTER WING, FRONT SPAR,
FORWARD FACE BETWEEN RIB 22 AND RIB 27, INCLUDING ALL
CUTOUTS.
572106-01-2 ************** TASK DELETED ************** N/A
572106-01-4 ************** TASK DELETED ************** N/A
572106-01-5 ************** TASK DELETED ************** N/A
572106-01-6 ************** TASK DELETED ************** N/A
572106-01-7 ************** TASK DELETED ************** N/A
572106-01-8 ************** TASK DELETED ************** N/A
3-57 572108-01-10 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-10 572100-200-008 38100 FC 3500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 76200 FH 7000 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
APPENDIX A
AEG/AMP/A320 Page 164 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572108-01-11 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-11 572100-200-008 15400 FC 3500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 30800 FH 7000 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-12 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-12 572100-200-008 11200 FC 4300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 48100 FH 18700 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572108-01-13 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-13 572100-200-008 37600 FC 3500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 75200 FH 7000 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-14 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-14 572100-200-008 26900 FC 8300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 53800 FH 16600 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-15 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-15 572100-200-008 33000 FC 6100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 66100 FH 12300 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-16 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-16 572100-200-008 36500 FC 8100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 73000 FH 16200 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572108-01-17 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-17 572100-200-008 33700 FC 5900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 67400 FH 11800 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-2 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-2 572100-200-008 35700 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 71500 FH 30000 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
572108-01-3 ************** TASK DELETED ************** N/A
3-57 572108-01-6 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-6 572100-200-008 29500 FC 8000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 48700 FH 13100 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
APPENDIX A
AEG/AMP/A320 Page 165 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572108-01-7 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-7 572100-200-008 17200 FC 5000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 73800 FH 21500 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-8 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-8 572100-200-008 30300 FC 8300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 60600 FH 16600 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
3-57 572108-01-9 540 DET OUTER WING FRT SPAR AFT FACE RIB 8-22 AF ALI ALI 572108-01-9 572100-200-008 24200 FC 8300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 48400 FH 16600 FH
FACE BETWEEN RIB 8 AND RIB 22 INCLUDING REINFORCING
STRAP
572108-03-10 ************** TASK DELETED ************** N/A
572108-03-11 ************** TASK DELETED ************** N/A
572108-03-13 ************** TASK DELETED ************** N/A
572109-01-1 ************** TASK DELETED ************** N/A
3-57 572109-01-10 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-10 572100-200-009 35700 FC 11700 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 71400 FH 23400 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
3-57 572109-01-11 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-11 572100-200-009 32000 FC 3800 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 64000 FH 7600 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572109-01-12 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-12 572100-200-009 32500 FC 6100 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 65000 FH 12300 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
572109-01-2 ************** TASK DELETED ************** N/A
572109-01-4 ************** TASK DELETED ************** N/A
3-57 572109-01-5 550 DET MAIN STRUCTURE AF ALI ALI 572109-01-5 572100-200-009 33900 FC 3100 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 67800 FH 6200 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
3-57 572109-01-6 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-6 572100-200-009 30800 FC 2900 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 61600 FH 5800 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
3-57 572109-01-7 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-7 572100-200-009 29800 FC 4200 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 59600 FH 8400 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
3-57 572109-01-8 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-8 572100-200-009 37200 FC 4200 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 74400 FH 8400 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
3-57 572109-01-9 550 DET OUTER WING FRT SPAR AFT FACE RIB 22-27 AF ALI ALI 572109-01-9 572100-200-009 36000 FC 4200 FC N/A
560 OR OR
650 DETAILED INSPECTION OF OUTER WING, FRONT SPAR AFT 72100 FH 8400 FH
660 FACE, BETWEEN RIB 22 AND RIB 27
572109-03-10 ************** TASK DELETED ************** N/A
572109-03-11 ************** TASK DELETED ************** N/A
572109-03-5 ************** TASK DELETED ************** N/A
572109-03-6 ************** TASK DELETED ************** N/A
572109-03-7 ************** TASK DELETED ************** N/A
572109-03-8 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 166 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
572109-03-9 ************** TASK DELETED ************** N/A
3-57 572111-01-1 574 DET OUTER WING REAR SPAR AFT FACE RIB 8-11 AF MRB CPCP MRB 572111-01-1 572100-200-002 12 YE 6 YE APPL
575
674 DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
675 FACE, FROM RIB 8 TO RIB 11
3-57 572111-01-2 574 DET OUTER WING REAR SPAR AFT FACE RIB 8-11 AF ALI ALI 572111-01-2 572100-200-002 12 YE 6 YE N/A
575 MRB CPCP MRB 572111-01-1 OR OR
674 DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 21800 FC 11600 FC
675 FACE, FROM RIB 8 TO RIB 11 OR OR
35800 FH 19000 FH
3-57 572111-01-3 574 DET OUTER WING REAR SPAR AFT FACE RIB 8-11 AF ALI ALI 572111-01-3 572100-200-002 12 YE 6 YE N/A
575 MRB CPCP MRB 572111-01-1 OR OR
674 DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 24000 FC 14000 FC
675 FACE, FROM RIB 8 TO RIB 11 OR OR
48000 FH 28000 FH
3-57 572111-01-4 574 DET OUTER WING REAR SPAR AFT FACE RIB 8-11 AF ALI ALI 572111-01-4 572100-200-002 12 YE 6 YE N/A
575 MRB CPCP MRB 572111-01-1 OR OR
674 DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 15900 FC 9600 FC
675 FACE, FROM RIB 8 TO RIB 11 OR OR
68300 FH 41400 FH
572111-01-5 ************** TASK DELETED ************** N/A
572111-01-7 ************** TASK DELETED ************** N/A
3-57 572112-01-1 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF ALI ALI 572112-01-1 572100-200-003 12 YE 6 YE APPL
675 MRB CPCP MRB 572112-01-1 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 22800 FC 15000 FC
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT OR OR
PLATE AT RIB 22. 45600 FH 30000 FH
3-57 572112-01-2 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF ALI ALI 572112-01-2 572100-200-003 12 YE 6 YE N/A
675 MRB CPCP MRB 572112-01-1 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 22800 FC 12500 FC
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT OR OR
PLATE AT RIB 22. 40300 FH 22100 FH
3-57 572112-01-3 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF ALI ALI 572112-01-3 572100-200-003 12 YE 6 YE N/A
675 MRB CPCP MRB 572112-01-1 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 24000 FC 15100 FC
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT OR OR
PLATE AT RIB 22. 48000 FH 30200 FH
3-57 572112-01-4 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF MRB CPCP MRB 572112-01-1 572100-200-003 12 YE 6 YE N/A
675
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT
PLATE AT RIB 22.
572112-01-5 ************** TASK DELETED ************** N/A
3-57 572112-01-6 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF ALI ALI 572112-01-6 572100-200-003 12 YE 6 YE N/A
675 MRB CPCP MRB 572112-01-1 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 21000 FC 11900 FC
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT OR OR
PLATE AT RIB 22. 42000 FH 23800 FH
572112-01-7 ************** TASK DELETED ************** N/A
572112-01-8 ************** TASK DELETED ************** N/A
3-57 572112-01-9 575 DET OUTER WING REAR SPAR AFT FACE RIB 11-27 AF ALI ALI 572112-01-9 572100-200-003 12 YE 6 YE N/A
675 MRB CPCP MRB 572112-01-1 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT 24000 FC 12500 FC
FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT OR OR
PLATE AT RIB 22. 48000 FH 25000 FH
3-57 572114-01-10 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-10 572100-200-010 35200 FC 6400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 70400 FH 12800 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-11 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-11 572100-200-010 32500 FC 6800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 65000 FH 13600 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
APPENDIX A
AEG/AMP/A320 Page 167 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572114-01-12 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-12 572100-200-010 21100 FC 6800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 42200 FH 13600 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-13 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-13 572100-200-010 31200 FC 3900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 62400 FH 7800 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-14 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-14 572100-200-010 33100 FC 6000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 66300 FH 12000 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-15 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-15 572100-200-010 38600 FC 5200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 77200 FH 10400 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572114-01-16 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-16 572100-200-010 38600 FC 5000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 77200 FH 10000 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572114-01-17 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-17 572100-200-010 39300 FC 6300 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 78700 FH 12600 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-3 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-3 572100-200-010 30100 FC 9600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 49400 FH 15800 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-4 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-4 572100-200-010 30100 FC 10100 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 60200 FH 20200 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-5 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-5 572100-200-010 38900 FC 9200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 77800 FH 18400 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
3-57 572114-01-6 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-6 572100-200-010 30100 FC 8500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 60200 FH 17000 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
572114-01-7 ************** TASK DELETED ************** N/A
3-57 572114-01-8 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-8 572100-200-010 32500 FC 7100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 65000 FH 14200 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
APPENDIX A
AEG/AMP/A320 Page 168 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572114-01-9 540 DET OUTER WING REAR SPAR FWD FACE RIB 8-11 AF ALI ALI 572114-01-9 572100-200-010 21100 FC 7100 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 42200 FH 14200 FH
FACE, BETWEEN RIB 8 AND RIB 11, INCLUDING TOP AND
BOTTOM FLANGES
572114-03-10 ************** TASK DELETED ************** N/A
572114-03-11 ************** TASK DELETED ************** N/A
572114-03-12 ************** TASK DELETED ************** N/A
572114-03-13 ************** TASK DELETED ************** N/A
572114-03-14 ************** TASK DELETED ************** N/A
572114-03-15 ************** TASK DELETED ************** N/A
572114-03-8 ************** TASK DELETED ************** N/A
572114-03-9 ************** TASK DELETED ************** N/A
3-57 572115-01-10 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-10 572100-200-011 37300 FC 4700 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 74600 FH 9400 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-03-10.
3-57 572115-01-11 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-11 572100-200-011 17200 FC 4700 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 34400 FH 9400 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-03-11.
3-57 572115-01-12 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-12 572100-200-011 12500 FC 5800 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 53700 FH 24900 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572115-01-13 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-13 572100-200-011 32500 FC 6800 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 65000 FH 13600 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-01-14 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-14 572100-200-011 33500 FC 6500 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 67000 FH 13000 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
APPENDIX A
AEG/AMP/A320 Page 169 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572115-01-15 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-15 572100-200-011 11100 FC 6500 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 22200 FH 13000 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-01-16 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-16 572100-200-011 15200 FC 2900 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 30400 FH 5800 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-03-16.
3-57 572115-01-17 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-17 572100-200-011 33000 FC 2900 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 66000 FH 5800 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-03-17.
3-57 572115-01-18 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-18 572100-200-011 37500 FC 6400 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 75100 FH 12900 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-01-19 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-19 572100-200-011 32400 FC 5200 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 64800 FH 10400 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572115-01-2 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-2 572100-200-011 43200 FC 15000 FC APPL
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 86400 FH 30000 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
APPENDIX A
AEG/AMP/A320 Page 170 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572115-01-20 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-20 572100-200-011 32400 FC 5000 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 64800 FH 10000 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572115-01-3 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-3 572100-200-011 35600 FC 12400 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 71200 FH 24800 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-01-4 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-4 572100-200-011 34600 FC 12400 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 69200 FH 24800 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
572115-01-5 ************** TASK DELETED ************** N/A
572115-01-7 ************** TASK DELETED ************** N/A
3-57 572115-01-8 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-8 572100-200-011 11100 FC 6800 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 22200 FH 13600 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-01-9 540 DET OUTER WING REAR SPAR FWD FACE RIB 11-27 AF ALI ALI 572115-01-9 572100-200-011 33500 FC 6800 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, REAR SPAR FORWARD 67000 FH 13600 FH
640 FACE, BETWEEN RIB 11 AND RIB 27, INCLUDING JOINT AT
650 RIB 22 AND TOP AND BOTTOM FLANGES, REINFORCING ANGLE
660 AT RIB 20 AND JOINT ANGLES BETWEEN RIB 24 AND RIB 25.
3-57 572115-03-10 540 SDI OUTER WING REAR SPAR FWD FACE RIB 11-27 NDT ALI ALI 572115-03-10 572100-280-803 37300 FC 7200 FC N/A
550 OR OR
560 SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 74600 FH 14400 FH
640 SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27,
650 INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES,
660 REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN
RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-01-10.
APPENDIX A
AEG/AMP/A320 Page 171 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572115-03-11 540 SDI OUTER WING REAR SPAR FWD FACE RIB 11-27 NDT ALI ALI 572115-03-11 572100-280-803 17200 FC 7200 FC N/A
550 OR OR
560 SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 34400 FH 14400 FH
640 SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27,
650 INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES,
660 REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN
RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-01-11.
572115-03-13 ************** TASK DELETED ************** N/A
572115-03-14 ************** TASK DELETED ************** N/A
572115-03-15 ************** TASK DELETED ************** N/A
3-57 572115-03-16 540 SDI OUTER WING REAR SPAR FWD FACE RIB 11-27 NDT ALI ALI 572115-03-16 572100-280-803 15200 FC 4500 FC N/A
550 OR OR
560 SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 30400 FH 9000 FH
640 SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27,
650 INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES,
660 REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN
RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-01-16.
3-57 572115-03-17 540 SDI OUTER WING REAR SPAR FWD FACE RIB 11-27 NDT ALI ALI 572115-03-17 572100-280-803 33000 FC 4500 FC N/A
550 OR OR
560 SPECIAL DETAILED INSPECTION (US) OF OUTER WING, REAR 66000 FH 9000 FH
640 SPAR FORWARD FACE, BETWEEN RIB 11 AND RIB 27,
650 INCLUDING JOINT AT RIB 22 AND TOP AND BOTTOM FLANGES,
660 REINFORCING ANGLE AT RIB 20 AND JOINT ANGLES BETWEEN
RIB 24 AND RIB 25.
NOTE:
THIS TASK IS AN ALTERNATIVE TO TASK 572115-01-17.
572115-03-19 ************** TASK DELETED ************** N/A
572115-03-8 ************** TASK DELETED ************** N/A
572115-03-9 ************** TASK DELETED ************** N/A
3-57 572116-02-1 500 DET MAIN STRUCTURE AF ALI ALI 572116-02-1 572100-220-801 58800 FC 15000 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 117600 FH 30000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR
BETWEEN RIB 8 AND RIB 22
572116-02-2 ************** TASK DELETED ************** N/A
3-57 572116-02-3 500 DET MAIN STRUCTURE AF ALI ALI 572116-02-3 572100-220-801 31500 FC 15000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 63000 FH 30000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR
BETWEEN RIB 8 AND RIB 22
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572116-02-4 500 DET MAIN STRUCTURE AF ALI ALI 572116-02-4 572100-220-801 31500 FC 15000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 63000 FH 30000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR
BETWEEN RIB 8 AND RIB 22
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 172 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572116-02-5 500 DET MAIN STRUCTURE AF ALI ALI 572116-02-5 572100-220-801 56800 FC 10600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 113600 FH 21200 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR
BETWEEN RIB 8 AND RIB 22
3-57 572120-01-3 500 GVI OUTER WING TOP SKIN AF ALI ALI 572120-01-3 572100-210-804 51700 FC 15000 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 103400 FH 30000 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR
3-57 572120-01-4 500 GVI OUTER WING TOP SKIN AF ALI ALI 572120-01-4 572100-210-804 34300 FC 3400 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 68600 FH 6800 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572120-02-1.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572120-01-5 500 GVI OUTER WING TOP SKIN AF ALI ALI 572120-01-5 572100-210-804 34300 FC 3200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 68600 FH 6400 FH
UPPER SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS
BETWEEN RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572120-02-2.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572120-02-1 500 DET OUTER WING TOP SKIN UPPER SURFACE AF ALI ALI 572120-02-1 572100-220-806 34300 FC 13200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 68600 FH 26400 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572120-01-4.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572120-02-2 500 DET OUTER WING TOP SKIN UPPER SURFACE AF ALI ALI 572120-02-2 572100-220-806 34300 FC 12600 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, UPPER 68600 FH 25200 FH
SURFACE AT ATTACHMENTS TO RIBS AND STRINGERS BETWEEN
RIB 8 AND RIB 27 FROM FRONT SPAR TO REAR SPAR
NOTE:
PLANNING:
- THIS TASK IS AN ALTERNATIVE TO TASK 572120-01-5.
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 173 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572121-01-3 500 GVI OUTER WING TOP SKIN AF ALI ALI 572121-01-3 572100-210-805 34600 FC 9200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 69200 FH 18400 FH
UPPER SURFACE SKIN JOINT AT STRINGER 11 BETWEEN RIB 8
AND RIB 18.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572121-01-4 500 GVI OUTER WING TOP SKIN AF ALI ALI 572121-01-4 572100-210-805 34600 FC 8700 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN, 69200 FH 17400 FH
UPPER SURFACE SKIN JOINT AT STRINGER 11 BETWEEN RIB 8
AND RIB 18.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572122-01-1 ************** TASK DELETED ************** N/A
572122-01-4 ************** TASK DELETED ************** N/A
3-57 572122-02-1 500 DET OUTER WING TOP SKIN RIB 19-20 AF MRB CPCP MRB 572122-02-1 572100-200-032 6 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING TOP SKIN, UPPER
SURFACE AROUND MANUAL REFUELLING APERTURE BETWEEN RIB
19 AND RIB 20
3-57 572123-01-1 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-1 572100-200-012 53200 FC 20000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 106400 FH 40000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
3-57 572123-01-14 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-14 572100-200-012 40400 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 80900 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
572123-01-3 ************** TASK DELETED ************** N/A
3-57 572123-01-4 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-4 572100-200-012 37500 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 75000 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
3-57 572123-01-5 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-5 572100-200-012 34300 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 68600 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
3-57 572123-01-6 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-6 572100-200-012 30600 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 61200 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
3-57 572123-01-7 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-7 572100-200-012 39000 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 78100 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
APPENDIX A
AEG/AMP/A320 Page 174 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572123-01-8 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-8 572100-200-012 38200 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 76400 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572123-01-9 540 DET OUTER WING TOP SKIN STRINGER RIB 8-13 AF ALI ALI 572123-01-9 572100-200-012 38200 FC 15000 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, TOP SKIN, 76400 FH 30000 FH
STRINGERS BETWEEN RIB 8 AND RIB 13, INCLUDING RUNOUTS
AND AIR TRANSFER HOLES, STRINGERS JOINT BETWEEN RIB 8
AND RIB 9 AND BUTT STRAP AT STRINGER 11
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572124-01-10 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-10 572100-200-013 34000 FC 15000 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 68000 FH 30000 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572124-01-2 ************** TASK DELETED ************** N/A
3-57 572124-01-3 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-3 572100-200-013 53300 FC 17300 FC APPL
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 106600 FH 34600 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
3-57 572124-01-5 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-5 572100-200-013 42900 FC 17300 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 60000 FH 30500 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
3-57 572124-01-6 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-6 572100-200-013 17800 FC 14400 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 76600 FH 62100 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
APPENDIX A
AEG/AMP/A320 Page 175 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572124-01-7 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-7 572100-200-013 43000 FC 17300 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 60000 FH 34600 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
3-57 572124-01-8 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-8 572100-200-013 40300 FC 29400 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 80600 FH 58800 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
3-57 572124-01-9 540 DET OUTER WING TOP SKIN STRINGER RIB 13-27 AF ALI ALI 572124-01-9 572100-200-013 43900 FC 38100 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, TOP SKIN 87800 FH 76200 FH
640 STRINGERS, BETWEEN RIB 13 AND RIB 27, INCLUDING
650 RUNOUTS, AIR TRANSFER HOLES AND BUTT STRAP AT
660 STRINGER 11, INCLUDING RUNOUT AT FRONT SPAR AT RIB 18
572126-01-1 ************** TASK DELETED ************** N/A
572126-01-2 ************** TASK DELETED ************** N/A
572126-01-3 ************** TASK DELETED ************** N/A
3-57 572129-01-1 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-1 572100-200-015 28900 FC 6300 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 50200 FH 10900 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
3-57 572129-01-2 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-2 572100-200-015 38000 FC 6500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 76000 FH 13000 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
3-57 572129-01-3 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-3 572100-200-015 32400 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 64800 FH 9800 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
3-57 572129-01-4 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-4 572100-200-015 45700 FC 7300 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 91400 FH 14600 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
3-57 572129-01-5 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-5 572100-200-015 14800 FC 6300 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 63600 FH 27000 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
APPENDIX A
AEG/AMP/A320 Page 176 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572129-01-7 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 8-15 AF ALI ALI 572129-01-7 572100-200-015 34900 FC 10700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 69800 FH 21400 FH
SURFACE AT ATTACHMENTS TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 8 AND RIB 15, EXCLUDING AREAS COVERED BY
PYLON REINFORCING, PYLON FAIRING AND FLAP TRACK 3
FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572130-01-2 ************** TASK DELETED ************** N/A
3-57 572130-01-4 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 15-22 AF ALI ALI 572130-01-4 572100-200-016 38000 FC 6500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 76000 FH 13000 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572130-01-7 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 15-22 AF ALI ALI 572130-01-7 572100-200-016 46000 FC 14100 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 92000 FH 28200 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572130-01-8 500 DET OUTER WING BOTTOM SKIN ATTACH RIB 15-22 AF ALI ALI 572130-01-8 572100-200-016 21500 FC 10700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 43000 FH 21400 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 15 AND RIB 22, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572131-01-1 ************** TASK DELETED ************** N/A
572131-01-2 ************** TASK DELETED ************** N/A
572131-01-3 ************** TASK DELETED ************** N/A
572131-01-4 ************** TASK DELETED ************** N/A
572131-01-5 ************** TASK DELETED ************** N/A
3-57 572131-01-6 500 DET OUTER WING BOTTOM SKIN LWR SURFACE AF ALI ALI 572131-01-6 572100-200-017 36100 FC 10700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 72200 FH 21400 FH
SURFACE AT ATTACHMENT TO FRONT SPAR AND REAR SPAR,
BETWEEN RIB 22 AND RIB 27
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572134-01-2 540 DET OUTER WING BOTTOM SKIN TRACK 3 AND 4 AF ALI ALI 572134-01-2 572100-200-018 53500 FC 8800 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 107000 FH 17600 FH
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
3-57 572134-01-3 540 DET OUTER WING BOTTOM SKIN TRACK 3 AND 4 AF ALI ALI 572134-01-3 572100-200-018 46100 FC 10400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 92300 FH 20900 FH
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
APPENDIX A
AEG/AMP/A320 Page 177 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572134-01-5 540 DET OUTER WING BOTTOM SKIN TRACK 3 AND 4 AF ALI ALI 572134-01-5 572100-200-018 28300 FC 10600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 60000 FH 24200 FH
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
3-57 572134-01-6 540 DET OUTER WING BOTTOM SKIN TRACK 3 AND 4 AF ALI ALI 572134-01-6 572100-200-018 16400 FC 8400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 70500 FH 36200 FH
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
3-57 572134-01-8 540 DET OUTER WING BOTTOM SKIN TRACK 3 AND 4 AF ALI ALI 572134-01-8 572100-200-018 31100 FC 6200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 62200 FH 12400 FH
SURFACE IN AREAS OF FLAP TRACK 3 AND 4 FORWARD AND
AFT PICK UP FITTINGS, INCLUDING ATTACHMENT TO REAR
SPAR
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572137-01-2 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572137-01-2 572100-200-019 58200 FC 5500 FC APPL
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 116400 FH 11000 FH
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
3-57 572137-01-3 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572137-01-3 572100-200-019 24000 FC 4900 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 9800 FH
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
3-57 572137-01-7 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572137-01-7 572100-200-019 10500 FC 4200 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 45100 FH 18000 FH
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
3-57 572137-01-8 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572137-01-8 572100-200-019 24000 FC 4700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 42000 FH 7900 FH
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
3-57 572137-01-9 500 DET OUTER WING BOTTOM SKIN RUNOUTS AF ALI ALI 572137-01-9 572100-200-019 24200 FC 7700 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48400 FH 15400 FH
SURFACE AT RUNOUT OF STRINGER 4 (RIB BAY 10-11),
STRINGER 5 (RIB BAY 13-14), STRINGER 13 (RIB BAY
8-9), STRINGER 6 (RIB BAY 16-17), STRINGER 7 (RIB BAY
19-20) AND STRINGER 12 (RIB BAY 17-18)
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 178 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572139-01-1 540 DET OUTER WING BOTTOM SKIN RIB BAY CUTOUTS AF MRB CPCP MRB 572139-01-1 572100-200-004 10 YE 5 YE N/A
640
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER
AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS IN RIB
BAYS 8-9, 9-10, 10-11, 11-12 AND 12-13
3-57 572139-01-2 540 DET OUTER WING BOTTOM SKIN RIB BAY CUTOUTS AF MRB CPCP MRB 572139-01-2 572100-200-004 12 YE 6 YE APPL
640
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, UPPER
AND LOWER SURFACES AROUND ACCESS DOOR CUTOUTS IN RIB
BAYS 8-9, 9-10, 10-11, 11-12 AND 12-13
3-57 572139-02-1 540 SDI OUTER WING BOTTOM SKIN RIB BAY CUTOUTS NDT ALI ALI 572139-02-1 572100-200-020 52800 FC 15000 FC APPL
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 105600 FH 30000 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13.
572139-02-2 ************** TASK DELETED ************** N/A
572139-02-3 ************** TASK DELETED ************** N/A
3-57 572139-02-6 540 SDI OUTER WING BOTTOM SKIN RIB BAY CUTOUTS NDT ALI ALI 572139-02-6 572100-200-020 31500 FC 14600 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 63000 FH 29200 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572139-02-7 540 SDI OUTER WING BOTTOM SKIN RIB BAY CUTOUTS NDT ALI ALI 572139-02-7 572100-200-020 56800 FC 15000 FC N/A
640 OR OR
SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 113700 FH 30000 FH
BOTTOM SKIN, UPPER AND LOWER SURFACES AROUND ACCESS
DOOR CUTOUTS IN RIB BAYS 8-9, 9-10, 10-11, 11-12 AND
12-13.
3-57 572140-01-1 540 DET OUTER WING BOTTOM SKIN CUTOUTS AF MRB CPCP MRB 572140-01-1 572100-200-021 10 YE 7.5 YE N/A
550
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
640 SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS,
650 BETWEEN RIB 13 AND RIB 27
660
3-57 572140-01-2 540 DET OUTER WING BOTTOM SKIN CUTOUTS AF MRB CPCP MRB 572140-01-2 572100-200-021 12 YE 7.5 YE APPL
550
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
640 SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL BAYS,
650 BETWEEN RIB 13 AND RIB 27
660
3-57 572140-02-3 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572140-02-3 572100-210-001 40900 FC 3400 FC N/A
540 OR OR
550 GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 81800 FH 6800 FH
560 LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
600 BAYS, BETWEEN RIB 13 AND RIB 27
640
650
660
3-57 572140-02-4 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572140-02-4 572100-210-001 42900 FC 3300 FC APPL
540 OR OR
550 GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 85800 FH 6600 FH
560 LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
600 BAYS, BETWEEN RIB 13 AND RIB 27
640
650
660
APPENDIX A
AEG/AMP/A320 Page 179 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572140-02-6 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572140-02-6 572100-210-001 9000 FC 2600 FC N/A
540 OR OR
550 GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 38700 FH 11100 FH
560 LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
600 BAYS, BETWEEN RIB 13 AND RIB 27
640
650
660
3-57 572140-02-7 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572140-02-7 572100-210-001 31000 FC 1400 FC N/A
540 OR OR
550 GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 62000 FH 2800 FH
560 LOWER SURFACES, AROUND ACCESS DOOR CUTOUTS IN ALL
600 BAYS, BETWEEN RIB 13 AND RIB 27
640
650 NOTE:
660 PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572142-01-2 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572142-01-2 572100-210-002 48300 FC 5600 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 96600 FH 11200 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
3-57 572142-01-3 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572142-01-3 572100-210-002 24000 FC 4000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42000 FH 6800 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
3-57 572142-01-5 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572142-01-5 572100-210-002 42700 FC 4000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 85400 FH 8000 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
3-57 572142-01-6 500 GVI OUTER WING BOTTOM SKIN CUTOUTS AF ALI ALI 572142-01-6 572100-210-002 12400 FC 4000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 53300 FH 17200 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS,
BETWEEN RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR
SPAR, EXCLUDING AREAS COVERED BY PYLON FAIRING AND
FLAP TRACK 3 FAIRING
3-57 572142-02-1 500 DET OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572142-02-1 572100-220-807 34400 FC 3300 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 68800 FH 6600 FH
SURFACE AT ATTACHMENT TO RIBS AND STRINGERS, BETWEEN
RIB 8 AND RIB 15, FROM FRONT SPAR TO REAR SPAR,
EXCLUDING AREAS COVERED BY PYLON FAIRING AND FLAP
TRACK 3 FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572143-01-2 532 DET OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572143-01-2 572100-200-022 53500 FC 10900 FC APPL
533 OR OR
632 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 107000 FH 21800 FH
633 SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA
COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4
FAIRING.
APPENDIX A
AEG/AMP/A320 Page 180 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572143-01-3 532 DET OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572143-01-3 572100-200-022 39200 FC 9800 FC N/A
533 OR OR
632 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 78400 FH 19600 FH
633 SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA
COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4
FAIRING.
3-57 572143-01-4 532 DET OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572143-01-4 572100-200-022 17800 FC 9400 FC N/A
533 OR OR
632 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 76500 FH 40400 FH
633 SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA
COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4
FAIRING
3-57 572143-01-5 532 DET OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572143-01-5 572100-200-022 31700 FC 9400 FC N/A
533 OR OR
632 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 54000 FH 16000 FH
633 SURFACE AT ATTACHMENT TO RIBS AND STRINGERS IN AREA
COVERED BY FLAP TRACK 3 FAIRING AND FLAP TRACK 4
FAIRING
3-57 572144-01-5 500 GVI OUTER WING BOTTOM SKIN AF ALI ALI 572144-01-5 572100-210-803 50800 FC 6700 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN, 101600 FH 13400 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
BETWEEN RIB 15 AND RIB 27 FROM FRONT SPAR TO REAR
SPAR EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING.
3-57 572144-01-6 500 GVI OUTER WING BOTTOM SKIN AF ALI ALI 572144-01-6 572100-210-803 51800 FC 4100 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN, 103600 FH 8300 FH
LOWER SURFACE AT ATTACHMENT TO RIBS AND STRINGERS
BETWEEN RIB 15 AND RIB 27 FROM FRONT SPAR TO REAR
SPAR EXCLUDING AREA COVERED BY FLAP TRACK 4 FAIRING.
3-57 572148-01-2 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572148-01-2 572100-210-003 48300 FC 6000 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 96600 FH 12000 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
3-57 572148-01-5 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572148-01-5 572100-210-003 24000 FC 4500 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 9000 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
3-57 572148-01-7 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572148-01-7 572100-210-003 24000 FC 3500 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42000 FH 5700 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
3-57 572148-01-8 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572148-01-8 572100-210-003 12100 FC 3800 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 52300 FH 16300 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
APPENDIX A
AEG/AMP/A320 Page 181 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572148-02-1 500 DET OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572148-02-1 572100-220-803 32300 FC 3000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 64600 FH 6000 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 8 AND RIB 18, EXCLUDING
AREAS COVERED BY PYLON FAIRING AND BY FLAP TRACK 3
FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572149-01-2 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572149-01-2 572100-210-004 56500 FC 6000 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 113000 FH 12000 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572149-01-3 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572149-01-3 572100-210-004 25800 FC 5100 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42000 FH 8300 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572149-01-4 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572149-01-4 572100-210-004 27000 FC 5300 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 54000 FH 10600 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572149-01-5 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572149-01-5 572100-210-004 32200 FC 5300 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 64400 FH 10600 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572149-01-7 500 GVI OUTER WING BOTTOM SKIN RIB/STRINGER ATTACHMENT AF ALI ALI 572149-01-7 572100-210-004 12600 FC 3900 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 54400 FH 16800 FH
LOWER SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
3-57 572149-02-1 500 DET OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 572149-02-1 572100-220-804 35900 FC 3000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 71800 FH 6000 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 21, ADJACENT TO
FRONT SPAR AND REAR SPAR, EXCLUDING AREA COVERED BY
FLAP TRACK 4 FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572150-01-2 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF ALI ALI 572150-01-2 572100-200-023 53500 FC 7800 FC APPL
632 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 107000 FH 15600 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
APPENDIX A
AEG/AMP/A320 Page 182 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572150-01-3 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF ALI ALI 572150-01-3 572100-200-023 24000 FC 9400 FC N/A
632 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 42000 FH 16000 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
3-57 572150-01-4 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF ALI ALI 572150-01-4 572100-200-023 24000 FC 9400 FC N/A
632 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 48000 FH 18800 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
3-57 572150-01-6 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF ALI ALI 572150-01-6 572100-200-023 12500 FC 6200 FC N/A
632 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 53700 FH 26800 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
3-57 572150-01-8 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF ALI ALI 572150-01-8 572100-200-023 31100 FC 3600 FC N/A
632 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 62200 FH 7200 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572150-09-2 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF MRB FMP MRB 572150-09-2 24 YE NOTE APPL
632 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572150-09-8 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF MRB FMP MRB 572150-09-8 12 YE NOTE N/A
632 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572150-09-9 532 DET OUTER WING BOTTOM SKIN JOINTS RIB 11-13 AF MRB FMP MRB 572150-09-9 18 YE 6 YE N/A
632 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 11 AND RIB 13 IN AREAS
COVERED BY FLAP TRACK 3 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 183 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572151-01-2 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF ALI ALI 572151-01-2 572100-200-024 56500 FC 10900 FC APPL
633 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 113000 FH 21800 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
572151-01-4 ************** TASK DELETED ************** N/A
572151-01-5 ************** TASK DELETED ************** N/A
572151-01-6 ************** TASK DELETED ************** N/A
3-57 572151-01-8 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF ALI ALI 572151-01-8 572100-200-024 44100 FC 5700 FC N/A
633 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 88200 FH 11400 FH
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572151-09-10 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF MRB FMP MRB 572151-09-10 18 YE 6 YE N/A
633 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572151-09-2 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF MRB FMP MRB 572151-09-2 24 YE NOTE APPL
633 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572151-09-4 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF MRB FMP MRB 572151-09-4 18 YE 6 YE N/A
633 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
APPENDIX A
AEG/AMP/A320 Page 184 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572151-09-8 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF MRB FMP MRB 572151-09-8 18 YE NOTE N/A
633 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572151-09-9 533 DET OUTER WING BOTTOM SKIN JOINTS RIB 18-20 AF MRB FMP MRB 572151-09-9 18 YE 6 YE N/A
633 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, SPANWISE SKIN JOINTS AT STRINGER 8 AND
STRINGER 11, BETWEEN RIB 18 AND RIB 20 IN AREA
COVERED BY FLAP TRACK 4 FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 572153-01-1 500 DET OUTER WING BOTTOM SKIN DRAIN HOLES AF MRB CPCP MRB 572153-01-1 572100-200-025 6 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE, AT DRAIN HOLES FOR SLAT CANS 5,6,7,8,9,10,11
AND 12 (RIB BAYS 9-10, 11-12, 13-14, 16-17, 18-19,
21-22, 23-24 & 25-26) DRY BAY DRAIN HOLES IN RIB BAY
26-27 AND MAGNETIC LEVEL INDICATOR POSITIONS ADJACENT
TO RIB 9 AND RIB 12
572153-01-2 ************** TASK DELETED ************** N/A
572153-01-3 ************** TASK DELETED ************** N/A
572153-01-4 ************** TASK DELETED ************** N/A
3-57 572155-01-1 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-1 572100-200-026 48300 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 96600 FH 30000 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
3-57 572155-01-2 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-2 572100-200-026 22500 FC 11700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 45000 FH 23400 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
3-57 572155-01-3 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-3 572100-200-026 30500 FC 15500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 61000 FH 31000 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
3-57 572155-01-6 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-6 572100-200-026 16000 FC 11800 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 68800 FH 50900 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
3-57 572155-01-7 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-7 572100-200-026 28700 FC 11200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 54600 FH 21300 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
APPENDIX A
AEG/AMP/A320 Page 185 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572155-01-8 540 DET OUTER WING BOTTOM SKIN RIB 8-21 AF ALI ALI 572155-01-8 572100-200-026 31100 FC 12200 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN UPPER 62200 FH 24400 FH
SURFACE BUTT STRAPS AT STRINGER 8 AND STRINGER 11,
BETWEEN RIB 8 AND RIB 21
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572157-01-1 ************** TASK DELETED ************** N/A
572157-01-2 ************** TASK DELETED ************** N/A
572157-01-3 ************** TASK DELETED ************** N/A
572157-01-4 ************** TASK DELETED ************** N/A
572157-01-5 ************** TASK DELETED ************** N/A
3-57 572157-01-6 500 SDI OUTER WING BOTTOM SKIN RUNOUT NDT ALI ALI 572157-01-6 572100-200-027 21800 FC 15000 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (X-RAY) OF OUTER WING, 43600 FH 30000 FH
BOTTOM SKIN, RUNOUT OF BUTTSTRAP AT STRINGER 8,
BETWEEN RIB 20 AND RIB 21, ADJACENT TO FRONT SPAR AND
RUNOUT OF BUTTSTRAP, AT STRINGER 11, ADJACENT TO RIB
21 AT REAR SPAR
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572158-01-10 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-10 572100-200-028 42000 FC 10400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 84000 FH 20800 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
3-57 572158-01-11 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-11 572100-200-028 45300 FC 9500 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 90600 FH 19000 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
3-57 572158-01-12 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-12 572100-200-028 31100 FC 9700 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 62200 FH 19400 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572158-01-2 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-2 572100-200-028 48300 FC 15000 FC APPL
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 96600 FH 30000 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
3-57 572158-01-3 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-3 572100-200-028 24000 FC 11900 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 23800 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
3-57 572158-01-5 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-5 572100-200-028 29900 FC 11400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 60000 FH 23000 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
APPENDIX A
AEG/AMP/A320 Page 186 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572158-01-7 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-7 572100-200-028 15600 FC 10600 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 67000 FH 45500 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
3-57 572158-01-8 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 8-18 AF ALI ALI 572158-01-8 572100-200-028 28600 FC 15400 FC N/A
640 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 57200 FH 30800 FH
STRINGERS (INCLUDING DRAIN HOLES), BETWEEN RIB 8 AND
RIB 18, COMPRISING STRINGERS 4,5,6,7,8,11,12 AND 13
572160-01-2 ************** TASK DELETED ************** N/A
3-57 572160-01-3 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 18-27 AF ALI ALI 572160-01-3 572100-200-029 24000 FC 16100 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 32200 FH
640 STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
650 STRINGERS 7, 8 AND 11
660
3-57 572160-01-4 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 18-27 AF ALI ALI 572160-01-4 572100-200-029 12700 FC 12700 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 54600 FH 54600 FH
640 STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
650 STRINGERS 7, 8 AND 11
660
3-57 572160-01-5 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 18-27 AF ALI ALI 572160-01-5 572100-200-029 34000 FC 15500 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 58700 FH 26800 FH
640 STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
650 STRINGERS 7, 8 AND 11
660
3-57 572160-01-6 540 DET OUTER WING BOTTOM SKIN STRINGER RIB 18-27 AF ALI ALI 572160-01-6 572100-200-029 27800 FC 9700 FC N/A
550 OR OR
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN 55600 FH 19400 FH
640 STRINGERS, BETWEEN RIB 18 AND RIB 27, COMPRISING
650 STRINGERS 7, 8 AND 11
660
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572161-01-1 ************** TASK DELETED ************** N/A
3-57 572161-01-10 540 DET MAIN STRUCTURE AF MRB CPCP MRB 572161-01-10 572100-200-030 10 YE 10 YE N/A
550
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN,
640 ACCESS DOORS BETWEEN RIB 13 AND RIB 27
650
660
3-57 572161-01-11 540 DET MAIN STRUCTURE AF MRB CPCP MRB 572161-01-11 572100-200-030 12 YE 12 YE APPL
550
560 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN,
640 ACCESS DOORS BETWEEN RIB 13 AND RIB 27
650
660
572161-01-2 ************** TASK DELETED ************** N/A
572161-01-5 ************** TASK DELETED ************** N/A
572161-01-6 ************** TASK DELETED ************** N/A
572161-01-7 ************** TASK DELETED ************** N/A
572161-01-8 ************** TASK DELETED ************** N/A
572161-01-9 ************** TASK DELETED ************** N/A
3-57 572164-01-1 500 DET OUTER WING BOTTOM SKIN FUEL DRAIN AF MRB CPCP MRB 572164-01-1 574100-200-005 6 YE 6 YE APPL
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB
15-16 AND RIB 22-23.
APPENDIX A
AEG/AMP/A320 Page 187 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572164-02-6 500 GVI OUTER WING BOTTOM SKIN FUEL DRAIN AF ALI ALI 572164-02-6 572100-210-802 48700 FC 8200 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 97400 FH 16400 FH
LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN
RIB 15-16 AND RIB 22-23
3-57 572164-02-7 500 GVI OUTER WING BOTTOM SKIN FUEL DRAIN AF ALI ALI 572164-02-7 572100-210-802 35900 FC 1400 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 71800 FH 2800 FH
LOWER SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN
RIB 15-16 AND RIB 22-23
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572164-03-1 500 DET OUTER WING AF MRB CPCP MRB 572164-03-1 574100-220-801 6 YE 6 YE N/A
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB
22-23, AND MAGNETIC LEVEL INDICATOR POSITION BETWEEN
RIB 15-16
3-57 572164-04-1 500 DET OUTER WING AF MRB CPCP MRB 572164-04-1 574100-220-802 6 YE 6 YE N/A
600
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
SURFACE AT FUEL TANK WATER DRAIN HOLES BETWEEN RIB
22-23.
3-57 572172-01-1 500 DET OUTER WING AF ALI ALI 572172-01-1 572100-220-805 32000 FC 4400 FC N/A
600 OR OR
DETAILED INSPECTION OF FRONT SPAR JOINT AT RIB 24, 64000 FH 8900 FH
AFT FACE.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
572172-02-1 ************** TASK DELETED ************** N/A
3-57 572174-01-1 500 SDI OUTER WING NDT ALI ALI 572174-01-1 572100-280-807 19500 FC 3800 FC N/A
600 OR OR
SPECIAL DETAILED INSPECTION (HFEC AND US) OF BOTTOM 39000 FH 7600 FH
COVER, STRINGERS 8, 11 AND STEEL STRAPS RIB BAYS NOTE
12-26.
NOTE:
THRESHOLD:
- FOR POST 160080 AIRCRAFT THRESHOLD IS TO BE COUNTED
FROM SB 57-1193 EMBODIMENT.
3-57 572177-01-1 500 DET OUTER WING AF ALI ALI 572177-01-1 572100-200-803 39200 FC 7600 FC N/A
600 OR OR
DETAILED INSPECTION OF FRONT SPAR JOINT AT RIB 24, 78400 FH 15200 FH
FWD FACE
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 572178-01-1 574 DET OUTER WING AF MRB CPCP MRB 572178-01-1 572100-220-811 6 YE 6 YE APPL
575
674 DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
675 SURFACE, OVERHANG FROM RIB 8 TO RIB 11
3-57 572179-01-1 575 DET OUTER WING AF MRB CPCP MRB 572179-01-1 572100-220-812 6 YE 6 YE APPL
675
DETAILED INSPECTION OF OUTER WING, TOP SKIN, LOWER
SURFACE, OVERHANG FROM RIB 11 TO RIB 27
572601-01-1 ************** TASK DELETED ************** N/A
572601-01-2 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 188 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
572601-01-3 ************** TASK DELETED ************** N/A
572601-02-1 ************** TASK DELETED ************** N/A
572601-02-2 ************** TASK DELETED ************** N/A
572601-02-3 ************** TASK DELETED ************** N/A
572604-01-1 ************** TASK DELETED ************** N/A
572604-01-3 ************** TASK DELETED ************** N/A
572604-01-4 ************** TASK DELETED ************** N/A
3-57 572607-01-1 531 DET FLAP TRACK BEAMS FWD SPIGOT ATTACH AF MRB CPCP MRB 572607-01-1 572600-200-006 6 YE 6 YE APPL
532
533 DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
631 2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS.
632
633
3-57 572607-01-2 531 DET FLAP TRACK BEAMS FWD SPIGOT ATTACH AF MRB CPCP MRB 572607-01-2 572600-200-006 6 YE 6 YE N/A
532
533 DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
631 2,3,4 FORWARD SPIGOT PINS, BOLTS AND FITTINGS.
632
633
572607-02-1 ************** TASK DELETED ************** N/A
572607-02-2 ************** TASK DELETED ************** N/A
572610-01-1 ************** TASK DELETED ************** N/A
572610-01-2 ************** TASK DELETED ************** N/A
3-57 572610-02-1 531 DET FLAP TRACK BEAMS AFT SPIGOT AF MRB CPCP MRB 572610-02-1 572600-200-010 6 YE 6 YE APPL
532
533 DETAILED INSPECTION OF OUTER WING, FLAP TRACK BEAMS
631 2,3,4 AFT SPIGOT
632
633
3-57 572650-01-1 571 DET OUTER WING REAR SPAR SIDESTAY FITTING AF MRB CPCP MRB 572650-01-1 572600-200-008 12 YE 12 YE APPL
671
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE
SIDESTAY FITTING
3-57 572651-01-1 571 DET OUTER WING REAR SPAR JACK FITTING AF MRB CPCP MRB 572651-01-1 572600-200-007 6 YE 6 YE APPL
671
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE
RETRACTION JACK FITTING
3-57 572651-01-2 571 DET OUTER WING REAR SPAR JACK FITTING AF MRB CPCP MRB 572651-01-2 572600-200-007 6 YE 6 YE N/A
671
DETAILED INSPECTION OF OUTER WING, REAR SPAR AFT FACE
RETRACTION JACK FITTING
NOTE:
REMOVAL OF ACTUATOR AND BEARING ASSEMBLY NOT REQUIRED
FOR POST 39730 OR POST 150311 AIRCRAFT.
3-57 572652-01-1 571 GVI OUTER WING AF MRB CPCP MRB 572652-01-1 572600-210-802 12 YE 12 YE APPL
671
GENERAL VISUAL INSPECTION OF OUTER WING, REAR SPAR,
AFT FACE, FORWARD PINTLE FITTING
3-57 572653-01-1 531 DET FLAP TRACK 2 AFT ATTACH FITTINGS AF MRB CPCP MRB 572653-01-1 572600-200-001 12 YE 12 YE APPL
532
533 DETAILED INSPECTION OF OUTER WING, FLAP TRACK 2, AFT
631 ATTACHMENT FITTINGS ON WING BOTTOM SKIN AT FALSE REAR
632 SPAR, AND FLAP TRACK 3 & 4, AFT ATTACHMENT FITTINGS
633 AT REAR SPAR
572653-01-2 ************** TASK DELETED ************** N/A
572653-01-5 ************** TASK DELETED ************** N/A
572653-01-6 ************** TASK DELETED ************** N/A
572654-01-1 ************** TASK DELETED ************** N/A
572654-01-2 ************** TASK DELETED ************** N/A
572654-01-3 ************** TASK DELETED ************** N/A
3-57 572656-01-1 500 DET OUTER WING PYLON SPIGOT AF MRB CPCP MRB 572656-01-1 572600-200-002 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF OUTER WING, PYLON SPIGOT
FITTING
APPENDIX A
AEG/AMP/A320 Page 189 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 572657-01-1 500 DET OUTER WING PYLON AFT FITTING LUG AF MRB CPCP MRB 572657-01-1 572600-200-003 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF OUTER WING, AFT PYLON
ATTACHMENT FITTING LUG
3-57 572658-01-1 531 DET OUTER WING BOTTOM SKIN TRACK BEAM FTG AF MRB CPCP MRB 572658-01-1 572600-200-009 12 YE 12 YE 24 YE 12 YE APPL
532
533 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
631 SURFACE, FORWARD ATTACHMENT FITTING FOR FLAP TRACK
632 BEAMS 2,3 & 4
633
3-57 572658-01-2 531 DET OUTER WING BOTTOM SKIN TRACK BEAM FTG AF MRB CPCP MRB 572658-01-2 572600-200-009 12 YE 12 YE 24 YE 12 YE N/A
532
533 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER
631 SURFACE, FORWARD ATTACHMENT FITTING FOR FLAP TRACK
632 BEAMS 2,3 & 4
633
2-57 572900-01-1 500 OPC MISCELLANEOUS (DRAINS) FOR OUTER WING AF MRB 9 MRB 57.29.00/01 572900-210-002 144 MO APPL
600
OPERATIONAL CHECK OF DRAIN HOLES AND HOSES FOR
CLOGGING
3-57 573101-01-1 534 DET WING TIP BOTTOM SKIN LWR SURFACE JOINT AF ALI ALI 573101-01-1 573000-200-001 60000 FC 15000 FC APPL
634 OR OR
DETAILED INSPECTION OF WING TIP, BOTTOM SKIN LOWER 120000 FH 30000 FH
SURFACE JOINT, OUTBOARD OF RIB 27
573101-01-2 ************** TASK DELETED ************** N/A
3-57 573101-01-3 534 DET WING TIP BOTTOM SKIN LWR SURFACE JOINT AF ALI ALI 573101-01-3 573000-200-001 15600 FC 12400 FC N/A
634 OR OR
DETAILED INSPECTION OF WING TIP, BOTTOM SKIN LOWER 67100 FH 53300 FH
SURFACE JOINT, OUTBOARD OF RIB 27
3-57 573101-01-4 534 DET WING TIP BOTTOM SKIN LWR SURFACE JOINT AF ALI ALI 573101-01-4 573000-200-001 27900 FC 12400 FC N/A
634 OR OR
DETAILED INSPECTION OF WING TIP, BOTTOM SKIN LOWER 39000 FH 17300 FH
SURFACE JOINT, OUTBOARD OF RIB 27
3-57 573102-01-1 534 DET WING TIP AF MRB CPCP MRB 573102-01-1 573100-220-801 12 YE 12 YE N/A
634
DETAILED INSPECTION OF WING TIP, RIB 27 LUGS
3-57 573102-02-1 534 DET WING TIP AF MRB CPCP MRB 573102-02-1 573100-220-802 12 YE 12 YE N/A
634
DETAILED INSPECTION OF WING TIP, RIB 27 LUGS
3-57 573106-01-1 534 DET WING TIP AF MRB CPCP MRB 573106-01-1 573100-220-804 12 YE 12 YE N/A
634
DETAILED INSPECTION OF WING TIP, SHARKLET, RIB 27A
LUGS
3-57 573107-01-1 534 SDI WING TIP NDT ALI ALI 573107-01-1 573100-280-801 12 YE 12 YE N/A
634 MRB CPCP MRB 573107-01-1 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF WING TIP, 40600 FC 15000 FC
SHARKLET INTERNAL STRUCTURE FROM RIB 27A TO SPAR OR OR
SPLICE BRACKETS OUTBOARD OF MID RIB 3 81200 FH 30000 FH
NOTE:
PLANNING:
- THROUGH INSPECTION HOLES.
- FOR POST 160500 AIRCRAFT THRESHOLD IS TO BE COUNTED
FROM SB 57-1173 OR SB 57-1186 EMBODIMENT.
- FOR POST 160080 AIRCRAFT THRESHOLD IS TO BE COUNTED
FROM SB 57-1193 EMBODIMENT.
3-57 573107-01-2 534 SDI WING TIP NDT ALI ALI 573107-01-2 573100-280-801 12 YE 12 YE N/A
634 MRB CPCP MRB 573107-01-1 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF WING TIP, 37700 FC 15000 FC
SHARKLET INTERNAL STRUCTURE FROM RIB 27A TO SPAR OR OR
SPLICE BRACKETS OUTBOARD OF MID RIB 3 75400 FH 30000 FH
NOTE:
PLANNING:
- THROUGH INSPECTION HOLES.
- FOR POST 160023 AIRCRAFT THRESHOLD IS TO BE COUNTED
FROM SB 57-1187 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 190 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 573107-01-3 534 SDI WING TIP NDT ALI ALI 573107-01-3 573100-280-801 12 YE 12 YE N/A
634 MRB CPCP MRB 573107-01-1 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF WING TIP, 37800 FC 15000 FC
SHARKLET INTERNAL STRUCTURE FROM RIB 27A TO SPAR OR OR
SPLICE BRACKETS OUTBOARD OF MID RIB 3 75700 FH 30000 FH
NOTE:
PLANNING:
- THROUGH INSPECTION HOLES.
3-57 573107-01-4 534 SDI WING TIP NDT MRB CPCP MRB 573107-01-1 573100-280-801 12 YE 12 YE N/A
634
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF WING TIP,
SHARKLET INTERNAL STRUCTURE FROM RIB 27A TO SPAR
SPLICE BRACKETS OUTBOARD OF MID RIB 3
NOTE:
PLANNING:
- THROUGH INSPECTION HOLES.
3-57 573107-01-5 534 SDI WING TIP NDT ALI ALI 573107-01-5 573100-280-801 12 YE 12 YE N/A
634 MRB CPCP MRB 573107-01-1 OR OR
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF WING TIP, 34200 FC 6500 FC
SHARKLET INTERNAL STRUCTURE FROM RIB 27A TO SPAR OR OR
SPLICE BRACKETS OUTBOARD OF MID RIB 3 68500 FH 13100 FH
NOTE:
PLANNING:
- THROUGH INSPECTION HOLES.
3-57 573109-01-1 534 DET WING TIP AF MRB CPCP MRB 573109-01-1 573100-220-803 12 YE 12 YE N/A
634
DETAILED INSPECTION OF WING TIP, SHARKLET, RIB 27A,
BOTTOM FLANGE FORWARD
3-57 573109-01-2 534 DET WING TIP AF ALI ALI 573109-01-2 573100-220-803 12 YE 12 YE N/A
634 MRB CPCP MRB 573109-01-1 OR OR
DETAILED INSPECTION OF WING TIP, SHARKLET, RIB 27A, 39500 FC 9200 FC
BOTTOM FLANGE FORWARD OR OR
79100 FH 18500 FH
2-57 573900-01-1 530 VCK MISCELLANEOUS (DRAINS) FOR WING TIP AF MRB 9 MRB 57.39.00/01 573900-200-002 144 MO APPL
630
VISUAL CHECK OF DRAIN HOLES FOR CLOGGING
3-57 574101-01-1 521 DET FIXED LE ROLLER PIN HOLES AF ALI ALI 574101-01-1 574100-200-012 12 YE 6 YE N/A
522 MRB CPCP MRB 574101-01-3 OR OR
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING 48000 FC 15000 FC
622 EDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB OR OR
1 TO 12 96000 FH 30000 FH
3-57 574101-01-2 521 DET FIXED LE ROLLER PIN HOLES AF MRB CPCP MRB 574101-01-3 574100-200-012 12 YE 6 YE N/A
522
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING
622 EDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB
1 TO 12
3-57 574101-01-3 521 DET FIXED LE ROLLER PIN HOLES AF ALI ALI 574101-01-3 574100-200-012 12 YE 6 YE APPL
522 MRB CPCP MRB 574101-01-3 OR OR
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING 52200 FC 20600 FC
622 EDGE, ROLLER PIN HOLES AND OTHER CUTOUTS IN TRACK RIB OR OR
1 TO 12 104400 FH 41200 FH
574101-01-5 ************** TASK DELETED ************** N/A
574101-01-6 ************** TASK DELETED ************** N/A
574101-01-7 ************** TASK DELETED ************** N/A
574102-01-1 ************** TASK DELETED ************** N/A
574102-01-3 ************** TASK DELETED ************** N/A
574102-01-4 ************** TASK DELETED ************** N/A
574102-01-5 ************** TASK DELETED ************** N/A
574106-01-1 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 191 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 574106-01-3 521 DET FIXED LE BOTTOM ATTACH JOINT AF MRB CPCP MRB 574106-01-3 574100-200-014 12 YE 6 YE 24 YE 6 YE APPL
522
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING
622 EDGE, BOTTOM ATTACHMENT JOINT ON TRACK RIB 1 TO 12
574106-01-4 ************** TASK DELETED ************** N/A
574106-01-5 ************** TASK DELETED ************** N/A
574106-01-6 ************** TASK DELETED ************** N/A
574106-01-7 ************** TASK DELETED ************** N/A
574106-01-8 ************** TASK DELETED ************** N/A
3-57 574112-01-1 521 DET FIXED LE MAIN BOTTOM WING SKIN AF MRB CPCP MRB 574112-01-1 574100-200-015 12 YE 6 YE 24 YE 6 YE APPL
522
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING
622 EDGE, BOTTOM WING SKIN, UPPER AND LOWER SURFACES,
FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB 27,
INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND RIB
BAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLES
3-57 574112-02-3 521 GVI FIXED LE MAIN BOTTOM WING SKIN AF ALI ALI 574112-02-3 574100-210-801 31200 FC 6600 FC N/A
522 OR OR
621 GENERAL VISUAL INSPECTION OF OUTER WING, FIXED 62400 FH 13200 FH
622 LEADING EDGE, BOTTOM WING SKIN, UPPER AND LOWER
SURFACES, FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB
27, INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND
RIB BAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLES
3-57 574112-02-4 521 GVI FIXED LE MAIN BOTTOM WING SKIN AF ALI ALI 574112-02-4 574100-210-801 24900 FC 6000 FC N/A
522 OR OR
621 GENERAL VISUAL INSPECTION OF OUTER WING, FIXED 49800 FH 12000 FH
622 LEADING EDGE, BOTTOM WING SKIN, UPPER AND LOWER
SURFACES, FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB
27, INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND
RIB BAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLES
3-57 574112-02-5 521 GVI FIXED LE MAIN BOTTOM WING SKIN AF ALI ALI 574112-02-5 574100-210-801 24700 FC 6700 FC N/A
522 OR OR
621 GENERAL VISUAL INSPECTION OF OUTER WING, FIXED 49400 FH 13400 FH
622 LEADING EDGE, BOTTOM WING SKIN, UPPER AND LOWER
SURFACES, FORWARD OF FRONT SPAR, FROM RIB 1 TO RIB
27, INCLUDING SIGHTING ROD HOLES IN RIB BAY 8-9 AND
RIB BAY 26-27, LIFTING BEAM HOLES AND DRAIN HOLES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 574113-01-1 521 DET FIXED LE TOP WING SKIN AF MRB CPCP MRB 574113-01-1 574100-200-016 12 YE 6 YE 24 YE 6 YE APPL
522
621 DETAILED INSPECTION OF OUTER WING, FIXED LEADING EDGE
622 TOP WING SKIN, UPPER AND LOWER SURFACES, FORWARD OF
FRONT SPAR, FROM RIB 1 TO RIB 27
574114-01-1 ************** TASK DELETED ************** N/A
574114-01-2 ************** TASK DELETED ************** N/A
574114-01-4 ************** TASK DELETED ************** N/A
3-57 574114-01-5 521 SDI FIXED LE PINION FITTING NDT ALI ALI 574114-01-5 574100-200-017 36600 FC 14400 FC N/A
522 OR OR
621 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 73200 FH 28800 FH
622 FIXED LEADING EDGE PINION FITTING BOLTING AND
ACTUATOR BOLTING LOWER BOLT HOLES ON RIB
2,3,5,6,7,8,9,10,11 AND 12
3-57 574114-01-6 521 SDI FIXED LE PINION FITTING NDT ALI ALI 574114-01-6 574100-200-017 47500 FC 13400 FC N/A
522 OR OR
621 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 95000 FH 26800 FH
622 FIXED LEADING EDGE PINION FITTING BOLTING AND
ACTUATOR BOLTING LOWER BOLT HOLES ON RIB
2,3,5,6,7,8,9,10,11 AND 12
APPENDIX A
AEG/AMP/A320 Page 192 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 574114-01-7 521 SDI FIXED LE PINION FITTING NDT ALI ALI 574114-01-7 574100-200-017 36900 FC 12300 FC N/A
522 OR OR
621 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 60000 FH 24600 FH
622 FIXED LEADING EDGE PINION FITTING BOLTING AND
ACTUATOR BOLTING LOWER BOLT HOLES ON RIB
2,3,5,6,7,8,9,10,11 AND 12
3-57 574201-01-1 500 DET SLAT 1, TRACKS 1-4 AF MRB CPCP MRB 574201-01-1 574100-200-002 12 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
574201-01-4 ************** TASK DELETED ************** N/A
3-57 574202-01-1 500 DET SLAT 1 TRACKS 1-4 ATTACHMENTS AF MRB CPCP MRB 574202-01-1 574200-200-001 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574202-01-2 500 DET SLAT 1 TRACKS 1-4 ATTACHMENTS AF MRB CPCP MRB 574202-01-2 574200-200-001 12 YE 6 YE N/A
600
DETAILED INSPECTION OF SLAT 1, TRACKS 1 TO 4
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574204-01-1 500 DET SLAT 1 SKIN CONNECTIONS AF MRB CPCP MRB 574204-01-1 574200-200-004 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SLAT 1, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH.
NOTE:
DETAILED INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT
1.
574204-01-5 ************** TASK DELETED ************** N/A
3-57 574204-02-1 500 SDI SLAT 1 SKIN CONNECTIONS NDT MRB CPCP MRB 574204-02-1 574200-200-005 12 YE 12 YE 24 YE 12 YE APPL
600
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 1,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE:
SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 1
(ENDOSCOPE).
574204-03-1 ************** TASK DELETED ************** N/A
3-57 574205-01-1 500 DET SLAT 1 TRAILING EDGE AF MRB CPCP MRB 574205-01-1 574200-200-006 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 1, TRAILING EDGE, LOWER
FACE, LH/RH
3-57 574301-01-1 500 DET SLAT 2 TRACK 5-6 ROLLER CONTACT AREA AF MRB CPCP MRB 574301-01-1 574100-200-008 12 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
3-57 574302-01-1 500 DET SLAT 2 TRACK 5-6 ATTACHMENTS AF MRB CPCP MRB 574302-01-1 574300-200-008 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574302-01-2 500 DET SLAT 2 TRACK 5-6 ATTACHMENTS AF MRB CPCP MRB 574302-01-2 574300-200-008 12 YE 6 YE N/A
600
DETAILED INSPECTION OF SLAT 2, TRACKS 5 AND 6
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574304-01-1 500 DET SLAT 2 SKIN CONNECTIONS AF MRB CPCP MRB 574304-01-1 574300-200-002 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SLAT 2, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH
NOTE:
DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 2.
APPENDIX A
AEG/AMP/A320 Page 193 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 574304-02-2 500 SDI SLAT 2 SKIN CONNECTIONS NDT MRB CPCP MRB 574304-02-2 574300-200-003 12 YE 12 YE 24 YE 12 YE APPL
600
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 2,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE:
SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 2.
574304-03-1 ************** TASK DELETED ************** N/A
3-57 574305-01-1 500 DET SLAT 2 TRAILING EDGE AF MRB CPCP MRB 574305-01-1 574300-200-001 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 2, TRAILING EDGE, LOWER
FACE, LH/RH
3-57 574401-01-1 500 DET SLAT 3 TRACK 7-8 ROLLER CONTACT AREA AF MRB CPCP MRB 574401-01-1 574100-200-009 12 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
3-57 574402-01-1 500 DET SLAT 3 TRACK 7-8 ATTACHMENTS AF MRB CPCP MRB 574402-01-1 574400-200-010 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574402-01-2 500 DET SLAT 3 TRACK 7-8 ATTACHMENTS AF MRB CPCP MRB 574402-01-2 574400-200-010 12 YE 6 YE N/A
600
DETAILED INSPECTION OF SLAT 3, TRACKS 7 AND 8
ATTACHMENTS, INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574404-01-1 500 DET SLAT 3 SKIN CONNECTIONS AF MRB CPCP MRB 574404-01-1 574400-200-007 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SLAT 3, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH
NOTE:
DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 3.
574404-01-5 ************** TASK DELETED ************** N/A
3-57 574404-02-1 500 SDI SLAT 3 SKIN CONNECTIONS NDT MRB CPCP MRB 574404-02-1 574400-200-008 12 YE 12 YE 24 YE 12 YE APPL
600
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 3,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE:
SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 3.
3-57 574405-01-1 500 DET SLAT 3 TRAILING EDGE AF MRB CPCP MRB 574405-01-1 574400-200-009 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 3, TRAILING EDGE, LOWER
FACE, LH/RH
3-57 574501-01-1 500 DET SLAT 4 TRACK 9-10 ROLLER CONTACT AREA AF MRB CPCP MRB 574501-01-1 574100-200-010 12 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
3-57 574502-01-1 500 DET SLAT 4 TRACK 9-10 ATTACHMENTS AF MRB CPCP MRB 574502-01-1 574500-200-008 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574502-01-2 500 DET SLAT 4 TRACK 9-10 ATTACHMENTS AF MRB CPCP MRB 574502-01-2 574500-200-008 12 YE 6 YE N/A
600
DETAILED INSPECTION OF SLAT 4, TRACKS 9 AND 10
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
APPENDIX A
AEG/AMP/A320 Page 194 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 574504-01-1 500 DET SLAT 4 SKIN CONNECTIONS AF MRB CPCP MRB 574504-01-1 574500-200-005 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SLAT 4, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH
NOTE:
DET INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT 4.
574504-01-5 ************** TASK DELETED ************** N/A
3-57 574504-02-1 500 SDI SLAT 4 SKIN CONNECTIONS NDT MRB CPCP MRB 574504-02-1 574500-200-006 12 YE 12 YE 24 YE 12 YE APPL
600
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 4,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE:
SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 4.
3-57 574505-01-1 500 DET SLAT 4 TRAILING EDGE AF MRB CPCP MRB 574505-01-1 574500-200-007 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 4, TRAILING EDGE, LOWER
FACE, LH/RH
3-57 574601-01-1 500 DET SLAT 5 TRACK 11-12 ROLLER CONTACT AREA AF MRB CPCP MRB 574601-01-1 574100-200-011 12 YE 6 YE 24 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12 :
VISIBLE PART OF ROLLER CONTACT AREA WHEN SLAT IS
FULLY EXTENDED, LH/RH
3-57 574602-01-1 500 DET SLAT 5 TRACK 11-12 ATTACHMENTS AF MRB CPCP MRB 574602-01-1 574600-200-008 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574602-01-2 500 DET SLAT 5 TRACK 11-12 ATTACHMENTS AF MRB CPCP MRB 574602-01-2 574600-200-008 12 YE 6 YE N/A
600
DETAILED INSPECTION OF SLAT 5, TRACKS 11 AND 12
ATTACHMENTS INCLUDING TRACK RIB LUGS, TRACK LUGS,
BOLTS, LINKS AND SIDE PLATES, LH/RH
3-57 574604-01-1 500 DET SLAT 5 SKIN CONNECTIONS AF MRB CPCP MRB 574604-01-1 574600-200-005 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SLAT 5, SKIN CONNECTIONS IN
AREA OF LOWER GIRDER AT TRACK RIB STATIONS, LH/RH.
NOTE:
DETAILED INSPECTION IS OF EXTERNAL STRUCTURE OF SLAT
5.
574604-01-4 ************** TASK DELETED ************** N/A
3-57 574604-02-1 500 SDI SLAT 5 SKIN CONNECTIONS NDT MRB CPCP MRB 574604-02-1 574600-200-006 12 YE 12 YE 24 YE 12 YE APPL
600
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF SLAT 5,
SKIN CONNECTIONS IN AREA OF LOWER GIRDER AT TRACK RIB
STATIONS, LH/RH.
NOTE:
SDET INSPECTION IS OF INTERNAL STRUCTURE OF SLAT 5.
3-57 574605-01-1 500 DET SLAT 5 TRAILING EDGE AF MRB CPCP MRB 574605-01-1 574600-200-007 12 YE 6 YE APPL
600
DETAILED INSPECTION OF SLAT 5, TRAILING EDGE, LOWER
FACE LH/RH
3-57 575101-01-1 531 DET TRAILING EDGE FLAP ACTUATOR BRACKETS AF MRB CPCP MRB 575101-01-1 575100-220-004 12 YE 12 YE APPL
532
533 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE FLAP
631 ACTUATOR BRACKETS AT FLAP TRACKS 2,3 AND 4
632
633
575101-02-1 ************** TASK DELETED ************** N/A
575101-02-2 ************** TASK DELETED ************** N/A
575101-02-3 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 195 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575104-01-1 500 DET TRAILING EDGE SPOILER 1 HINGE FITTINGS AF MRB CPCP MRB 575104-01-1 575100-220-006 12 YE 12 YE APPL
600
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
SPOILER 1 ACTUATOR AND HINGE FITTINGS
575104-01-5 ************** TASK DELETED ************** N/A
575106-01-1 ************** TASK DELETED ************** N/A
575106-01-3 ************** TASK DELETED ************** N/A
575106-02-1 ************** TASK DELETED ************** N/A
575106-02-3 ************** TASK DELETED ************** N/A
3-57 575106-03-1 574 DET TRAILING EDGE SPOILERS HINGE PINS AF MRB CPCP MRB 575106-03-1 575100-210-002 12 YE 12 YE APPL
575
582 DETAILED INSPECTION OF OUTER WING TRAILING EDGE
583 SPOILERS 1,2,3,4 AND 5 HINGE PINS
584
585
586
674
675
682
683
684
685
686
3-57 575107-01-1 575 DET TRAILING EDGE SPOILER 2-5 FITTINGS AF MRB CPCP MRB 575107-01-1 575100-220-009 12 YE 6 YE APPL
583
584 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
585 SPOILERS 2,3,4 AND 5 ACTUATOR AND HINGE FITTINGS
586
675
683
684
685
686
575107-02-1 ************** TASK DELETED ************** N/A
575107-02-2 ************** TASK DELETED ************** N/A
575107-02-3 ************** TASK DELETED ************** N/A
3-57 575119-01-1 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF MRB CPCP MRB 575119-01-1 575100-220-001 12 YE 12 YE APPL
590
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES
3-57 575119-01-10 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-10 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 13600 FC 6000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES OR OR
58400 FH 25800 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575119-01-11 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-11 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 36500 FC 15000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES OR OR
73100 FH 30000 FH
3-57 575119-01-12 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-12 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 29000 FC 15000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES OR OR
58000 FH 30000 FH
575119-01-2 ************** TASK DELETED ************** N/A
575119-01-5 ************** TASK DELETED ************** N/A
575119-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 196 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575119-01-7 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-7 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 29900 FC 15000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND 'A' FRAMES OR OR
59800 FH 30000 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575119-01-8 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-8 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 24700 FC 15000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES OR OR
49400 FH 30000 FH
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575119-01-9 575 DET TRAILING EDGE AILERON HINGE FITTINGS AF ALI ALI 575119-01-9 575100-220-001 12 YE 12 YE N/A
590 MRB CPCP MRB 575119-01-1 OR OR
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE, 34900 FC 15000 FC
690 AILERON HINGE FITTINGS 1 TO 5 AND "A" FRAMES OR OR
69800 FH 30000 FH
575120-01-1 ************** TASK DELETED ************** N/A
575120-01-3 ************** TASK DELETED ************** N/A
575120-02-1 ************** TASK DELETED ************** N/A
575120-02-2 ************** TASK DELETED ************** N/A
3-57 575120-03-1 575 DET TRAILING EDGE AILERON HINGE PINS AF MRB CPCP MRB 575120-03-1 575100-220-016 12 YE 7.5 YE APPL
590
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
690 AILERON HINGE PINS 1 TO 5
3-57 575121-01-1 575 DET TRAILING EDGE AILERON ACTUATOR FITTING AF MRB CPCP MRB 575121-01-1 575100-220-003 6 YE 6 YE 24 YE 6 YE APPL
590
675 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE,
690 AILERON, INBOARD AND OUTBOARD ACTUATOR FITTINGS
575121-01-2 ************** TASK DELETED ************** N/A
575121-01-5 ************** TASK DELETED ************** N/A
575121-01-6 ************** TASK DELETED ************** N/A
575130-01-2 ************** TASK DELETED ************** N/A
3-57 575140-01-1 147 DET FLAP TRACK 1 AF MRB CPCP MRB 575140-01-1 575100-200-003 12 YE 12 YE 24 YE 12 YE APPL
148
DETAILED INSPECTION OF FLAP TRACK 1, INCLUDING
ATTACHMENT BRACKETS TO FUSELAGE, STRUT, CARRIAGE AND
SWINGING LINK (PENDULUM), LH/RH
575140-01-4 ************** TASK DELETED ************** N/A
3-57 575142-01-1 147 DET INBOARD FLAP ACTUATOR DRIVE ARM AF MRB CPCP MRB 575142-01-1 575100-200-004 12 YE 12 YE 24 YE 12 YE APPL
148
DETAILED INSPECTION OF INBOARD FLAP, INBOARD ACTUATOR
DRIVE ARM, DRIVE STRUT AND OUTER PART OF TRUNNION,
LH/RH
575142-01-4 ************** TASK DELETED ************** N/A
3-57 575150-01-1 571 DET OUTER WING MLG SUPPORT RIBS AF MRB CPCP MRB 575150-01-1 575100-200-005 10 YE 5 YE N/A
671
DETAILED INSPECTION OF OUTER WING, MLG SUPPORT RIB 5,
OUTBOARD AND INBOARD FACES
3-57 575150-01-2 571 DET OUTER WING MLG SUPPORT RIBS AF MRB CPCP MRB 575150-01-2 575100-200-005 12 YE 6 YE APPL
671
DETAILED INSPECTION OF OUTER WING, MLG SUPPORT RIB 5,
OUTBOARD AND INBOARD FACES
3-57 575151-01-10 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-10 575100-200-006 23400 FC 2400 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 46800 FH 4800 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
APPENDIX A
AEG/AMP/A320 Page 197 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575151-01-11 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-11 575100-200-006 11000 FC 700 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 47600 FH 3300 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-01-12 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-12 575100-200-006 35500 FC 3600 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 71100 FH 7200 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-01-13 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-13 575100-200-006 26500 FC 1600 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 53000 FH 3200 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575151-01-14 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-14 575100-200-006 12100 FC 700 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 24200 FH 1500 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575151-01-15 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-15 575100-200-006 23500 FC 1000 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 47000 FH 2000 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
575151-01-2 ************** TASK DELETED ************** N/A
575151-01-3 ************** TASK DELETED ************** N/A
575151-01-4 ************** TASK DELETED ************** N/A
575151-01-5 ************** TASK DELETED ************** N/A
3-57 575151-01-6 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-6 575100-200-006 28900 FC 2000 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 57800 FH 4000 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-01-7 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-7 575100-200-006 26400 FC 3900 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 52800 FH 7800 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-01-8 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-8 575100-200-006 13200 FC 900 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 56700 FH 3800 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-01-9 573 DET INNER REAR SPAR TRAILING EDGE AF ALI ALI 575151-01-9 575100-200-006 25600 FC 1400 FC N/A
574 OR OR
673 DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 51200 FH 2800 FH
674 FALSE REAR SPAR, FORWARD AND AFT FACES
3-57 575151-02-1 573 GVI TRAILING EDGE AF MRB CPCP MRB 575151-02-1 575100-210-804 6 YE 6 YE APPL
574
673 GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING
674 EDGE, FALSE REAR SPAR, FORWARD AND AFT FACES
575151-03-10 ************** TASK DELETED ************** N/A
575151-03-13 ************** TASK DELETED ************** N/A
575151-03-14 ************** TASK DELETED ************** N/A
575151-03-6 ************** TASK DELETED ************** N/A
575151-03-7 ************** TASK DELETED ************** N/A
575151-03-9 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 198 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575154-01-1 570 DET OUTER WING TRAILING EDGE OVERWING PANEL AND FITTINGS AF ALI ALI 575154-01-1 575100-220-803 25600 FC 15000 FC N/A
670 OR OR
DETAILED INSPECTION OF OUTER WING, TRAILING EDGE 51200 FH 30000 FH
OVERWING PANEL FITTINGS
3-57 575155-01-4 500 GVI OUTER WING TRAILING EDGE TOP SKIN AF ALI ALI 575155-01-4 575100-210-802 55800 FC 10200 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 111600 FH 20400 FH
EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR
BETWEEN RIB 1 AND RIB 9
3-57 575155-01-5 500 GVI OUTER WING TRAILING EDGE TOP SKIN AF ALI ALI 575155-01-5 575100-210-802 52400 FC 8000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 104800 FH 16000 FH
EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR
BETWEEN RIB 1 AND RIB 9
3-57 575155-01-6 500 GVI OUTER WING TRAILING EDGE TOP SKIN AF ALI ALI 575155-01-6 575100-210-802 30900 FC 6200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 61800 FH 12400 FH
EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR
BETWEEN RIB 1 AND RIB 9
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575155-01-7 500 GVI OUTER WING TRAILING EDGE TOP SKIN AF ALI ALI 575155-01-7 575100-210-802 29000 FC 4900 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 58000 FH 9800 FH
EDGE, TOP SKIN UPPER SURFACE, AFT OF REAR SPAR
BETWEEN RIB 1 AND RIB 9
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575158-01-1 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-1 575100-210-003 24000 FC 5200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 42000 FH 8800 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
3-57 575158-01-10 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-10 575100-210-003 24000 FC 5200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 10400 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS AND FLAP TAB DRIVE 1A FAIRINGS
3-57 575158-01-5 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-5 575100-210-003 25400 FC 13600 FC APPL
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 50800 FH 27200 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
3-57 575158-01-6 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-6 575100-210-003 24000 FC 13600 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 48000 FH 27200 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
APPENDIX A
AEG/AMP/A320 Page 199 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575158-01-8 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-8 575100-210-003 20300 FC 9000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 40600 FH 18000 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575158-01-9 500 GVI OUTER WING BOTTOM SKIN LOWER SURFACE AF ALI ALI 575158-01-9 575100-210-003 19100 FC 8700 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, BOTTOM SKIN 38200 FH 17400 FH
LOWER SURFACE, AFT OF REAR SPAR BETWEEN RIB 1 AND RIB
9, EXCLUDING AREAS COVERED BY FLAP TRACK 2 FAIRINGS
AND PYLON FAIRINGS
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
575159-01-1 ************** TASK DELETED ************** N/A
3-57 575159-01-2 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 575159-01-2 575100-200-007 21800 FC 7800 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN LOWER 43600 FH 15600 FH
SURFACE, CURVED SKIN EDGE AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
575159-01-4 ************** TASK DELETED ************** N/A
575159-01-5 ************** TASK DELETED ************** N/A
3-57 575159-01-6 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 575159-01-6 575100-200-007 41200 FC 7500 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 60000 FH 12000 FH
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
3-57 575159-01-7 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 575159-01-7 575100-200-007 31400 FC 15000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 62800 FH 30000 FH
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575159-01-8 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF ALI ALI 575159-01-8 575100-200-007 29600 FC 15000 FC N/A
600 OR OR
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 59200 FH 30000 FH
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
APPENDIX A
AEG/AMP/A320 Page 200 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575159-09-1 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF MRB FMP MRB 575159-09-1 24 YE 6 YE APPL
600 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575159-09-7 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF MRB FMP MRB 575159-09-7 12 YE NOTE N/A
600 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575159-09-8 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF MRB FMP MRB 575159-09-8 12 YE NOTE N/A
600 NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575159-09-9 500 DET OUTER WING BOTTOM SKIN/REAR SPAR AF MRB FMP MRB 575159-09-9 18 YE 6 YE N/A
600 NOTE NOTE
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER
SURFACE CURVED SKIN EDGE, AFT OF REAR SPAR JUST
INBOARD OF MLG SUPPORT RIB 5
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575160-01-1 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-1 575100-200-008 24000 FC 11800 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 38400 FH 18900 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
3-57 575160-01-10 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-10 575100-200-008 39500 FC 2900 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 79000 FH 5800 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575160-01-2 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-2 575100-200-008 24000 FC 12300 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 48000 FH 24600 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
APPENDIX A
AEG/AMP/A320 Page 201 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575160-01-3 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-3 575100-200-008 24000 FC 11900 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 48000 FH 23800 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
3-57 575160-01-5 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-5 575100-200-008 60000 FC 11800 FC APPL
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 120000 FH 23600 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
3-57 575160-01-6 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-6 575100-200-008 13400 FC 8600 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 57600 FH 37300 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
3-57 575160-01-7 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-7 575100-200-008 23100 FC 11800 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 46200 FH 23600 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
3-57 575160-01-9 574 SDI TRAILING EDGE BOTTOM SKIN REAR SPAR NDT ALI ALI 575160-01-9 575100-200-008 41900 FC 3000 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (X-RAY AND HFEC) OF OUTER 83800 FH 6000 FH
WING, TRAILING EDGE BOTTOM SKIN AFT OF REAR SPAR,
ABOVE MLG REINFORCING
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575161-01-1 500 GVI TRAILING EDGE BOTTOM SKIN REAR SPAR AF ALI ALI 575161-01-1 575100-210-004 24000 FC 3800 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 42000 FH 6400 FH
EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM
RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT
RIB 9 AND SIGHTING ROD HOLE AT RIB 10
3-57 575161-01-2 500 GVI TRAILING EDGE BOTTOM SKIN REAR SPAR AF ALI ALI 575161-01-2 575100-210-004 24000 FC 4000 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 48000 FH 8000 FH
EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM
RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT
RIB 9 AND SIGHTING ROD HOLE AT RIB 10
3-57 575161-01-8 500 GVI TRAILING EDGE BOTTOM SKIN REAR SPAR AF ALI ALI 575161-01-8 575100-210-004 34700 FC 13100 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TRAILING 69400 FH 26300 FH
EDGE BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR FROM
RIB 9 TO RIB 12, INCLUDING JACKING FITTING HOLE AT
RIB 9 AND SIGHTING ROD HOLE AT RIB 10
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
3-57 575163-01-2 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIR NDT ALI ALI 575163-01-2 575100-220-011 48000 FC 13200 FC APPL
674 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, 96000 FH 26400 FH
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
3-57 575163-01-3 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIR NDT ALI ALI 575163-01-3 575100-220-011 41500 FC 3600 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, 83000 FH 7200 FH
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
575163-01-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 202 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575163-01-5 574 SDI OUTER WING BOTTOM SKIN UNDER PYLON FAIRING NDT ALI ALI 575163-01-5 575100-220-011 45200 FC 12600 FC N/A
674 OR OR
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING, 90400 FH 25200 FH
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING.
575163-01-6 ************** TASK DELETED ************** N/A
3-57 575163-09-2 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIRING NDT MRB FMP MRB 575163-09-2 24 YE NOTE APPL
674 NOTE
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575163-09-3 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIRING NDT MRB FMP MRB 575163-09-3 18 YE NOTE N/A
674 NOTE
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575163-09-5 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIRING NDT MRB FMP MRB 575163-09-5 18 YE NOTE N/A
674 NOTE
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE B. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575163-09-7 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIRING NDT MRB FMP MRB 575163-09-7 18 YE 6 YE N/A
674 NOTE NOTE
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575163-09-8 574 SDI OUTER WING BOTTOM SKIN UND PYLON FAIRING NDT MRB FMP MRB 575163-09-8 18 YE 6 YE N/A
674 NOTE NOTE
SPECIAL DETAILED INSPECTION (LFEC) OF OUTER WING,
BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, UNDER
PYLON FAIRING
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
575164-01-2 ************** TASK DELETED ************** N/A
3-57 575164-01-3 531 SDI OUTER WING BOTTOM SKIN UND FLAP TRACK2 NDT ALI ALI 575164-01-3 575100-220-012 21400 FC 3900 FC N/A
574 OR OR
631 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 42800 FH 7800 FH
674 BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, AROUND
FLAP TRACK 2 FORWARD FITTINGS
APPENDIX A
AEG/AMP/A320 Page 203 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575164-01-4 531 SDI OUTER WING BOTTOM SKIN UND FLAP TRACK2 NDT ALI ALI 575164-01-4 575100-220-012 24000 FC 3900 FC N/A
574 OR OR
631 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING, 48000 FH 7800 FH
674 BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, AROUND
FLAP TRACK 2 FORWARD FITTINGS
3-57 575164-09-2 531 SDI OUTER WING BOTTOM SKIN UND FLAP TRACK2 NDT MRB FMP MRB 575164-09-2 18 YE 6 YE N/A
574 NOTE NOTE
631 SPECIAL DETAILED INSPECTION (HFEC) OF OUTER WING,
674 BOTTOM SKIN LOWER SURFACE, AFT OF REAR SPAR, AROUND
FLAP TRACK 2 FORWARD FITTINGS.
NOTE:
THRESHOLD/INTERVAL:
- CALENDAR TIME REQUIREMENT WITH A SOURCE "FATIGUE
MONITORING PROGRAM" TYPE A. REFER TO STRUCTURE
SECTION INTRODUCTION FOR ADDITIONAL GUIDANCE.
3-57 575165-01-2 531 DET OUTER WING BOTTOM SKIN UND FLAP 2 FAIR AF ALI ALI 575165-01-2 575100-200-009 35400 FC 12700 FC N/A
574 OR OR
631 DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN, LOWER 70800 FH 25400 FH
674 SURFACE, AFT OF REAR SPAR UNDER FLAP TRACK 2 FAIRING
AND FLAP TAB DRIVE 1A FAIRING
575165-01-3 ************** TASK DELETED ************** N/A
575165-01-5 ************** TASK DELETED ************** N/A
575166-01-2 ************** TASK DELETED ************** N/A
575166-01-3 ************** TASK DELETED ************** N/A
575166-01-4 ************** TASK DELETED ************** N/A
3-57 575167-01-1 574 DET OUTER WING BOTTOM SKIN UPPER SURFACE AF MRB CPCP MRB 575167-01-1 575100-200-011 6 YE 6 YE APPL
674
DETAILED INSPECTION OF OUTER WING, BOTTOM SKIN PANEL
NO. 3, UPPER SURFACE, BETWEEN REAR SPAR AND FALSE
REAR SPAR, AND BETWEEN GEAR SUPPORT RIB 5 AND RIB 8.
3-57 575170-01-1 500 GVI OUTER WING TOP SKIN EXTERNAL SURFACE AF ALI ALI 575170-01-1 575100-210-005 22800 FC 14200 FC N/A
600 OR OR
GENERAL VISUAL INSPECTION OF OUTER WING, TOP SKIN 45600 FH 28400 FH
EXTERNAL SURFACE, AFT OF REAR SPAR, BETWEEN RIB 10 TO
20 AT BUTTSTRAP ATTACHMENT.
NOTE:
PLANNING:
- FOR AIRCRAFT POST 160080 REFER TO INTRODUCTION
SECTION OF THE ALS PART2 (ALI) FOR FIRST TASK
ACCOMPLISHMENT AFTER SB 57-1193 EMBODIMENT.
2-57 575200-01-1 500 DET INBOARD FLAP AF LUR MRB 27.50.00/14 575200-200-010 144 MO N/A
600 MRB 6 OR
DETAILED INSPECTION OF FLAP TRACK NO 1 DRIVE LEVER 12000 FC
ARM FOR SIDE PLAY
3-57 575203-01-1 581 DET INBOARD FLAP TRUNNION ATTACH BRACKET AF MRB CPCP MRB 575203-01-1 575200-200-007 12 YE 12 YE 24 YE 12 YE APPL
681
DETAILED INSPECTION OF INBOARD FLAP, TRUNNION
ATTACHMENT BRACKET INCLUDING INBOARD TRUNNION, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575203-02-1.
575203-01-4 ************** TASK DELETED ************** N/A
3-57 575203-02-1 581 SDI INBOARD FLAP TRUNNION ATTACH BRACKET NDT MRB CPCP MRB 575203-02-1 575200-220-006 12 YE 12 YE 24 YE 12 YE APPL
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, TRUNNION ATTACHMENT BRACKET INCLUDING INBOARD
TRUNNION, LH/RH
NOTE:
- INSPECTION IS THROUGH INSPECTION HOLES
- THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575203-01-1.
575203-02-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 204 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575205-01-1 531 DET INBOARD FLAP DRIVE STRUT AND LEVER AF MRB CPCP MRB 575205-01-1 575200-200-008 12 YE 12 YE APPL
581
631 DETAILED INSPECTION OF INBOARD FLAP, DRIVE STRUT FOR
681 FLAP AND DRIVE LEVER FOR FLAP TRACK FAIRING,
INCLUDING ATTACHMENT BRACKETS TO THE FLAP AND
SURROUNDING SKIN AT TRACK 2, LH/RH
575205-01-4 ************** TASK DELETED ************** N/A
3-57 575206-01-1 581 SDI INBOARD FLAP INTERNAL BRACKETS NDT MRB CPCP MRB 575206-01-1 575200-220-008 12 YE 12 YE 24 YE 12 YE APPL
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, INTERNAL BRACKETS AT TRACK 2, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
575206-01-4 ************** TASK DELETED ************** N/A
3-57 575207-01-1 531 DET INBOARD FLAP CARRIAGE ATTACH BRACKET AF MRB CPCP MRB 575207-01-1 575200-200-009 12 YE 12 YE 24 YE 12 YE APPL
581
631 DETAILED INSPECTION OF INBOARD FLAP, FLAP TO CARRIAGE
681 ATTACHMENT BRACKET AT TRACK 2, INCLUDING SURROUNDING
SKIN, LH/RH
575207-01-4 ************** TASK DELETED ************** N/A
3-57 575209-01-1 477 DET INBOARD FLAP ATTACH BRACKET OF FAIRING AF MRB CPCP MRB 575209-01-1 575200-200-002 12 YE 12 YE 24 YE 12 YE APPL
487
581 DETAILED INSPECTION OF INBOARD FLAP, ATTACHMENT
681 BRACKET OF PYLON AFT FAIRING, INCLUDING SURROUNDING
SKIN, LH/RH
575209-01-4 ************** TASK DELETED ************** N/A
3-57 575210-01-1 581 SDI INBOARD FLAP INTERNAL SUPPORT BRACKET NDT MRB CPCP MRB 575210-01-1 575200-200-003 12 YE 12 YE 24 YE 12 YE APPL
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
FLAP, INTERNAL SUPPORT BRACKET OF PYLON AFT FAIRING
ATTACHMENT, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
575210-01-4 ************** TASK DELETED ************** N/A
3-57 575211-01-1 581 DET INBOARD FLAP END RIB AF MRB CPCP MRB 575211-01-1 575200-200-004 12 YE 12 YE APPL
681
DETAILED INSPECTION OF INBOARD FLAP, END RIB,
INCLUDING ROLLER AND INTERCONNECTION STRUT ATTACHMENT
BRACKET, LH/RH
3-57 575221-01-1 500 GVI INBOARD FLAP END RIB AF ALI ALI 575221-01-1 575200-210-009 5500 FC 5500 FC N/A
600
GENERAL VISUAL INSPECTION OF INBOARD DOUBLE-SLOTTED
FLAP, EXTERNAL SURFACE OF UPPER AND LOWER SKIN, LH/RH
3-57 575223-01-1 581 DET INBOARD DOUBLE SLOTTED FLAP TRUNNION AF MRB CPCP MRB 575223-01-1 575200-210-001 12 YE 12 YE 24 YE 12 YE N/A
681
DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
TRUNNION ATTACHMENT BRACKET, INCLUDING INBOARD
TRUNNION, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575223-02-1.
3-57 575223-02-1 581 SDI INBOARD DOUBLE SLOTTED FLAP TRUNNION NDT MRB CPCP MRB 575223-02-1 575200-220-009 12 YE 12 YE 24 YE 12 YE N/A
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
DOUBLE-SLOTTED FLAP, TRUNNION ATTACHMENT BRACKET,
INCLUDING INBOARD TRUNNION, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES THIS TASK HAS
TO BE PERFORMED THE SAME TIME AS TASK 575223-01-1.
APPENDIX A
AEG/AMP/A320 Page 205 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575225-01-1 531 DET INBOARD DOUBLE SLOTTED FLAP DRIVE AF MRB CPCP MRB 575225-01-1 575200-210-002 12 YE 12 YE N/A
581
631 DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
681 DRIVE STRUT FOR FLAP AND DRIVE LEVER FOR FLAP TRACK
FAIRING, INCLUDING ATTACHMENT BRACKETS TO THE FLAP AT
TRACK 2, LH/RH
3-57 575226-01-1 581 SDI INBD DOUBLE SLOTTED FLAP INTL BRACK NDT MRB CPCP MRB 575226-01-1 575200-220-010 12 YE 12 YE 24 YE 12 YE N/A
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
DOUBLE-SLOTTED FLAP, INTERNAL BRACKETS AT TRACK 2,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575227-01-1 531 DET INBD DOUBLE SLOTTED FLAP FLAP/CARRIAGE AF MRB CPCP MRB 575227-01-1 575200-210-003 12 YE 12 YE 24 YE 12 YE N/A
581
631 DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
681 FLAP TO CARRIAGE ATTACHMENT BRACKET AT TRACK 2, LH/RH
3-57 575229-01-1 477 DET INBD DOUBLE SLOTTED FLAP PYLON FAIR AT AF MRB CPCP MRB 575229-01-1 575200-210-004 12 YE 12 YE 24 YE 12 YE N/A
487
581 DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
681 ATTACHMENT BRACKET OF PYLON AFT FAIRING, INCLUDING
SURROUNDING SKIN, LH/RH
3-57 575230-01-1 581 SDI INBD DOUBLE SLOTTED FLP INT SUPP BRACK NDT MRB CPCP MRB 575230-01-1 575200-220-011 12 YE 12 YE 24 YE 12 YE N/A
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) INBOARD
DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT BRACKETS PYLON
AFT FAIRING ATTACHMENT, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575231-01-1 581 DET INBOARD DOUBLE SLOTTED FLAP END RIB AF MRB CPCP MRB 575231-01-1 575200-210-005 12 YE 12 YE 24 YE 12 YE N/A
681
DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
END RIB, INCLUDING INTERCONNECTION STRUT ATTACHMENT
BRACKET AND LEVER, LH/RH
3-57 575233-01-1 535 DET INBOARD DOUBLE SLOTTED FLAP TAB DRIVE AF MRB CPCP MRB 575233-01-1 575200-210-006 12 YE 12 YE 24 YE 12 YE N/A
572
635 DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
672 TAB DRIVE ASSEMBLY AND ARTICULATION AT RIB 3, LH/RH
3-57 575235-01-1 535 DET INBOARD DOUBLE SLOTTED FLAP TAB ARTIC AF MRB CPCP MRB 575235-01-1 575200-210-007 12 YE 12 YE 24 YE 12 YE N/A
635
DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
TAB ARTICULATION AT RIB 6, LH/RH
3-57 575237-01-1 531 DET INBOARD DOUBLE SLOTTED FLAP TAB DRIVE AF MRB CPCP MRB 575237-01-1 575200-210-008 12 YE 12 YE 24 YE 12 YE N/A
631
DETAILED INSPECTION OF INBOARD DOUBLE-SLOTTED FLAP,
TAB DRIVE STRUT AND ARTICULATION AT RIB 9, LH/RH
3-57 575239-01-1 581 SDI INBOARD DOUBLE SLOTTED FLAP RIB 3 NDT MRB CPCP MRB 575239-01-1 575200-220-012 12 YE 12 YE 24 YE 12 YE N/A
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
DOUBLE-SLOTTED FLAP, RIB 3, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575241-01-1 581 SDI INBOARD DOUBLE SLOTTED FLAP RIB 6 NDT MRB CPCP MRB 575241-01-1 575200-220-013 12 YE 12 YE 24 YE 12 YE N/A
681
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF INBOARD
DOUBLE-SLOTTED FLAP, RIB 6, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575250-01-1 500 DET INBOARD FLAP TRACK 2 CARRIAGE AF MRB CPCP MRB 575250-01-1 575200-200-005 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK
2 CARRIAGE FORGING
575250-02-1 ************** TASK DELETED ************** N/A
575250-02-2 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 206 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
575251-01-1 ************** TASK DELETED ************** N/A
575251-01-2 ************** TASK DELETED ************** N/A
575252-01-1 ************** TASK DELETED ************** N/A
575252-01-2 ************** TASK DELETED ************** N/A
3-57 575254-01-1 531 DET INBOARD FLAP TRACK 2 DRIVE LEVER AF MRB CPCP MRB 575254-01-1 575200-200-006 6 YE 6 YE 24 YE 6 YE APPL
631
DETAILED INSPECTION OF OUTER WING, INBOARD FLAP TRACK
2, DRIVE LEVER
575254-02-1 ************** TASK DELETED ************** N/A
575254-02-2 ************** TASK DELETED ************** N/A
3-57 575303-01-1 587 DET OUTBOARD FLAP TRACK 3 ATTACH AREAS AF MRB CPCP MRB 575303-01-1 575300-200-004 6 YE 6 YE N/A
687
DETAILED INSPECTION OF OUTBOARD FLAP, FRONT SPAR
SPLICES AND ATTACHMENT AREAS AT TRACK 3, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575303-02-1.
575303-01-4 ************** TASK DELETED ************** N/A
3-57 575303-02-1 587 SDI OUTBOARD FLAP TRACK 3 ATTACH AREAS NDT MRB CPCP MRB 575303-02-1 575300-220-003 6 YE 6 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 3, INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES THIS TASK HAS
TO BE PERFORMED THE SAME TIME AS TASK 575303-01-1.
3-57 575303-02-4 587 SDI OUTBOARD FLAP TRACK 3 ATTACH AREAS NDT MRB CPCP MRB 575303-02-4 575300-220-003 6 YE 6 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 3, INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
575303-02-6 ************** TASK DELETED ************** N/A
575303-02-7 ************** TASK DELETED ************** N/A
3-57 575305-01-1 587 DET OUTBOARD FLAP TRACK 4 ATTACH AREAS AF MRB CPCP MRB 575305-01-1 575300-200-006 6 YE 6 YE N/A
687
DETAILED INSPECTION OF OUTBOARD FLAP, FRONT SPAR
SPLICES AND ATTACHMENT AREAS AT TRACK 4, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575305-02-1.
575305-01-4 ************** TASK DELETED ************** N/A
3-57 575305-02-1 587 SDI OUTBOARD FLAP TRACK 4 ATTACH AREAS NDT MRB CPCP MRB 575305-02-1 575300-220-009 6 YE 6 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, FRONT SPAR SPLICES AND ATTACHMENT AREAS AT
TRACK 4, INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575305-01-1.
575305-02-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 207 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575307-01-1 587 DET OUTBOARD FLAP INBOARD RIB AF MRB CPCP MRB 575307-01-1 575300-200-003 12 YE 12 YE APPL
687
DETAILED INSPECTION OF OUTBOARD FLAP, INBOARD RIB,
FORWARD SECTION INCLUDING ROLLER, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575307-02-1.
3-57 575307-02-1 587 SDI OUTBOARD FLAP INBOARD RIB NDT MRB CPCP MRB 575307-02-1 575300-220-002 12 YE 12 YE APPL
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INBOARD RIB, FORWARD SECTION INCLUDING ROLLER,
INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575307-01-1.
3-57 575309-01-1 532 DET OUTBOARD FLAP SUPPORT TRACK 3 AF MRB CPCP MRB 575309-01-1 575300-200-005 12 YE 12 YE 24 YE 12 YE N/A
587
632 DETAILED INSPECTION OF OUTBOARD FLAP SUPPORT AT TRACK
687 3, INCLUDING RIB 5, FITTING ASSEMBLY AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-02-1.
3-57 575309-01-4 532 DET OUTBOARD FLAP SUPPORT TRACK 3 AF MRB CPCP MRB 575309-01-4 575300-200-005 12 YE 12 YE 24 YE 12 YE APPL
587
632 DETAILED INSPECTION OF OUTBOARD FLAP SUPPORT AT TRACK
687 3, INCLUDING RIB 5, FITTING ASSEMBLY AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-02-4.
575309-01-5 ************** TASK DELETED ************** N/A
3-57 575309-02-1 532 SDI OUTBOARD FLAP SUPPORT TRACK 3 NDT MRB CPCP MRB 575309-02-1 575300-220-004 12 YE 12 YE 24 YE 12 YE N/A
587
632 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 FLAP SUPPORT AT TRACK 3, INCLUDING RIB 5, FITTING
ASSEMBLY AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-01-1.
3-57 575309-02-4 532 SDI OUTBOARD FLAP SUPPORT TRACK 3 NDT MRB CPCP MRB 575309-02-4 575300-220-004 12 YE 12 YE 24 YE 12 YE APPL
587
632 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 FLAP SUPPORT AT TRACK 3, INCLUDING RIB 5, FITTING
ASSEMBLY AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575309-01-4.
575309-02-5 ************** TASK DELETED ************** N/A
3-57 575311-01-1 532 DET OUTBOARD FLAP TRACK 3 DRIVE LINKAGE AF MRB CPCP MRB 575311-01-1 575300-200-007 12 YE 12 YE 24 YE 12 YE APPL
587
632 DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
687 AND DRIVE FITTING AT TRACK 3, LH/RH
575311-01-4 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 208 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575312-01-1 587 DET OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT AF MRB CPCP MRB 575312-01-1 575300-200-008 12 YE 12 YE N/A
687
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 3 INCLUDING RIB 6, FITTING AT FRONT
SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575312-02-1.
575312-01-4 ************** TASK DELETED ************** N/A
3-57 575312-02-1 587 SDI OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT NDT MRB CPCP MRB 575312-02-1 575300-220-005 12 YE 12 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 3, INCLUDING RIB 6,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575312-01-1.
3-57 575312-02-4 587 SDI OUTBOARD FLAP TRACK 3 INTERNAL SUPPORT NDT MRB CPCP MRB 575312-02-4 575300-220-005 12 YE 12 YE APPL
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 3, INCLUDING RIB 6,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
575312-02-5 ************** TASK DELETED ************** N/A
3-57 575313-01-1 533 DET OUTBOARD FLAP SUPPORT TRACK 4 AF MRB CPCP MRB 575313-01-1 575300-200-011 12 YE 12 YE N/A
587
633 DETAILED INSPECTION OF OUTBOARD FLAP, SUPPORT AT
687 TRACK 4, INCLUDING RIB 14, FITTING ASSEMBLY, PENDULUM
SUPPORT AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-02-1.
3-57 575313-01-4 533 DET OUTBOARD FLAP SUPPORT TRACK 4 AF MRB CPCP MRB 575313-01-4 575300-200-011 12 YE 12 YE APPL
587
633 DETAILED INSPECTION OF OUTBOARD FLAP, SUPPORT AT
687 TRACK 4, INCLUDING RIB 14, FITTING ASSEMBLY, PENDULUM
SUPPORT AND ATTACHMENT STRUCTURE, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-02-4.
575313-01-6 ************** TASK DELETED ************** N/A
575313-01-7 ************** TASK DELETED ************** N/A
3-57 575313-02-1 533 SDI OUTBOARD FLAP SUPPORT TRACK 4 NDT MRB CPCP MRB 575313-02-1 575300-220-010 12 YE 12 YE N/A
587
633 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 FLAP, SUPPORT AT TRACK 4, INCLUDING RIB 14, FITTING
ASSEMBLY, PENDULUM SUPPORT AND ATTACHMENT STRUCTURE,
INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-01-1.
APPENDIX A
AEG/AMP/A320 Page 209 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575313-02-4 533 SDI OUTBOARD FLAP SUPPORT TRACK 4 NDT MRB CPCP MRB 575313-02-4 575300-220-010 12 YE 12 YE APPL
587
633 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 FLAP, SUPPORT AT TRACK 4, INCLUDING RIB 14, FITTING
ASSEMBLY, PENDULUM SUPPORT AND ATTACHMENT STRUCTURE,
INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575313-01-4.
575313-02-6 ************** TASK DELETED ************** N/A
575313-02-7 ************** TASK DELETED ************** N/A
3-57 575315-01-1 533 DET OUTBOARD FLAP TRACK 4 DRIVE LINKAGE AF MRB CPCP MRB 575315-01-1 575300-200-012 12 YE 12 YE 24 YE 12 YE N/A
587
633 DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
687 AND DRIVE FITTING AT TRACK 4, LH/RH
3-57 575315-01-4 533 DET OUTBOARD FLAP TRACK 4 DRIVE LINKAGE AF MRB CPCP MRB 575315-01-4 575300-200-012 12 YE 12 YE 24 YE 12 YE APPL
587
633 DETAILED INSPECTION OF OUTBOARD FLAP, DRIVE LINKAGE
687 AND DRIVE FITTING AT TRACK 4, LH/RH
575315-01-6 ************** TASK DELETED ************** N/A
575315-01-7 ************** TASK DELETED ************** N/A
3-57 575316-01-1 587 DET OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT AF MRB CPCP MRB 575316-01-1 575300-200-013 12 YE 12 YE 24 YE 12 YE N/A
687
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 4 INCLUDING RIB 15, FITTING AT FRONT
SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-02-1.
3-57 575316-01-4 587 DET OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT AF MRB CPCP MRB 575316-01-4 575300-200-013 12 YE 12 YE 24 YE 12 YE APPL
687
DETAILED INSPECTION OF OUTBOARD FLAP, INTERNAL
SUPPORT AT TRACK 4, INCLUDING RIB 15, FITTING AT
FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-02-4.
575316-01-6 ************** TASK DELETED ************** N/A
575316-01-7 ************** TASK DELETED ************** N/A
3-57 575316-02-1 587 SDI OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT NDT MRB CPCP MRB 575316-02-1 575300-220-012 12 YE 12 YE 24 YE 12 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 4, INCLUDING RIB 15,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-01-1.
3-57 575316-02-4 587 SDI OUTBOARD FLAP TRACK 4 INTERNAL SUPPORT NDT MRB CPCP MRB 575316-02-4 575300-220-012 12 YE 12 YE 24 YE 12 YE APPL
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
FLAP, INTERNAL SUPPORT AT TRACK 4, INCLUDING RIB 15,
FITTING AT FRONT SPAR AND INTERNAL DOUBLER, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575316-01-4.
575316-02-6 ************** TASK DELETED ************** N/A
575316-02-7 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 210 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575321-01-2 500 GVI OUTBOARD DOUBLE SLOTTED FLAP TAB AF ALI ALI 575321-01-2 575300-210-009 8500 FC 8500 FC N/A
600
GENERAL VISUAL INSPECTION OF OUTBOARD DOUBLE-SLOTTED
FLAP, INCLUDING TAB, EXTERNAL SURFACE OF UPPER AND
LOWER SKIN, LH/RH
575321-01-3 ************** TASK DELETED ************** N/A
3-57 575323-01-1 587 SDI OUTBOARD DOUBLE SLOTTED FLAP TAB NDT MRB CPCP MRB 575323-01-1 575300-220-021 12 YE 12 YE 24 YE 12 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
DOUBLE SLOTTED FLAP TAB FRONT SPAR, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575327-01-1 587 DET OUTBD DOUBLE SLOTTED FLAP INBOARD RIB AF MRB CPCP MRB 575327-01-1 575300-210-001 12 YE 12 YE N/A
687
DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
INBOARD RIB, INCLUDING INTERCONNECTION STRUT
ATTACHMENT BRACKET, LEVER AND ROLLER, INTERNAL AND
EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575327-02-1.
3-57 575327-02-1 587 SDI OUTBD DOUBLE SLOTTED FLAP INBOARD RIB NDT MRB CPCP MRB 575327-02-1 575300-220-014 12 YE 12 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
DOUBLE-SLOTTED FLAP, INBOARD RIB, INCLUDING
INTERCONNECTION STRUT ATTACHMENT BRACKET, LEVER AND
ROLLER, INTERNAL AND EXTERNAL, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575327-01-1.
3-57 575329-01-1 532 DET OUTBD DOUBLE SLOTTED FLAP INTL SUPP AF MRB CPCP MRB 575329-01-1 575300-210-002 12 YE 12 YE 24 YE 12 YE N/A
587
632 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
687 INTERNAL SUPPORT FITTING AT TRACK 3, INCLUDING
ATTACHMENT BRACKET, DRIVE BRACKET AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575329-02-1.
3-57 575329-02-1 532 SDI OUTBD DOUBLE SLOTTED FLAP INTL SUPP NDT MRB CPCP MRB 575329-02-1 575300-220-015 12 YE 12 YE 24 YE 12 YE N/A
587
632 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING AT
TRACK 3 INCLUDING ATTACHMENT BRACKET, DRIVE BRACKET
AND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575329-01-1.
3-57 575329-03-1 532 DET OUTBOARD DOUBLE-SLOTTED FLAP AF MRB CPCP MRB 575329-03-1 575300-210-002 12 YE 12 YE 24 YE 12 YE N/A
587
632 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
687 INTERNAL SUPPORT FITTING AT TRACK 3 INCLUDING
ATTACHMENT BRACKET, DRIVE BRACKET AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575329-04-1
APPENDIX A
AEG/AMP/A320 Page 211 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575329-04-1 532 SDI OUTBOARD DOUBLE-SLOTTED FLAP NDT MRB CPCP MRB 575329-04-1 575300-220-015 12 YE 12 YE 24 YE 12 YE N/A
587
632 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING AT
TRACK 3 INCLUDING ATTACHMENT BRACKET, DRIVE BRACKET
AND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575329-03-1.
3-57 575331-01-1 532 DET OUTBD DOUBLE SLOTTED FLAP DRIVE LINK AF MRB CPCP MRB 575331-01-1 575300-210-003 12 YE 12 YE 24 YE 12 YE N/A
632
DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
DRIVE LINKAGE AND DRIVE FITTING AT TRACK 3, LH/RH
3-57 575333-01-1 533 DET OUTBD DOUBLE SLOTTED FLAP INTL SUPP AF MRB CPCP MRB 575333-01-1 575300-210-004 12 YE 12 YE N/A
587
633 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
687 INTERNAL SUPPORT FITTING AT TRACK 4, INCLUDING
PENDULUM SUPPORT, DRIVE BRACKET AND ATTACHMENT
STRUCTURE, INTERNAL AND EXTERNAL, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575333-02-1.
3-57 575333-02-1 533 SDI OUTBD DOUBLE SLOTTED FLAP INTL SUPP NDT MRB CPCP MRB 575333-02-1 575300-220-016 12 YE 12 YE N/A
587
633 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 DOUBLE-SLOTTED FLAP, INTERNAL SUPPORT FITTING AT
TRACK 4, INCLUDING PENDULUM SUPPORT, DRIVE BRACKET
AND ATTACHMENT STRUCTURE, INTERNAL AND EXTERNAL,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575333-01-1.
3-57 575335-01-1 533 DET OUTBD DOUBLE SLOTTED FLAP DRIVE LINK AF MRB CPCP MRB 575335-01-1 575300-210-005 12 YE 12 YE 24 YE 12 YE N/A
633
DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
DRIVE LINKAGE AND DRIVE FITTING AT TRACK 4, LH/RH
3-57 575337-01-1 537 DET OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC AF MRB CPCP MRB 575337-01-1 575300-210-006 12 YE 12 YE 24 YE 12 YE N/A
538
539 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
587 TAB ARTICULATION AT STATIONS 3 A, 3 B, 3 C, LH/RH
637
638 NOTE:
639 THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
687 575337-02-1.
3-57 575337-02-1 537 SDI OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC NDT MRB CPCP MRB 575337-02-1 575300-220-017 12 YE 12 YE 24 YE 12 YE N/A
538
539 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
587 DOUBLE-SLOTTED FLAP, TAB ARTICULATION AT STATIONS 3
637 A, 3 B, 3 C, LH/RH
638
639 NOTE:
687 INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575337-01-1.
3-57 575339-01-1 532 DET OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC AF MRB CPCP MRB 575339-01-1 575300-210-007 12 YE 12 YE 24 YE 12 YE N/A
587
632 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
687 TAB ARTICULATION AT TRACK 3, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575339-02-1.
APPENDIX A
AEG/AMP/A320 Page 212 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 575339-02-1 532 SDI OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC NDT MRB CPCP MRB 575339-02-1 575300-220-018 12 YE 12 YE 24 YE 12 YE N/A
587
632 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 DOUBLE-SLOTTED FLAP, TAB ARTICULATION AT TRACK 3,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575339-01-1.
3-57 575341-01-1 533 DET OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC AF MRB CPCP MRB 575341-01-1 575300-210-008 12 YE 12 YE 24 YE 12 YE N/A
587
633 DETAILED INSPECTION OF OUTBOARD DOUBLE-SLOTTED FLAP,
687 TAB ARTICULATION AT TRACK 4, LH/RH
NOTE:
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575341-02-1.
3-57 575341-02-1 533 SDI OUTBOARD DOUBLE SLOTTED FLAP TAB ARTIC NDT MRB CPCP MRB 575341-02-1 575300-220-019 12 YE 12 YE 24 YE 12 YE N/A
587
633 SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
687 DOUBLE-SLOTTED FLAP, TAB ARTICULATION AT TRACK 4,
LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES.
THIS TASK HAS TO BE PERFORMED THE SAME TIME AS TASK
575341-01-1.
3-57 575343-01-1 587 SDI OUTBD DOUBLE SLOTTED FLAP RIB 2, 9, 12 NDT MRB CPCP MRB 575343-01-1 575300-220-020 12 YE 12 YE 24 YE 12 YE N/A
687
SPECIAL DETAILED INSPECTION (ENDOSCOPE) OF OUTBOARD
DOUBLE-SLOTTED FLAP, RIB 2, 9 AND 12, LH/RH
NOTE:
INSPECTION IS THROUGH INSPECTION HOLES
3-57 575350-01-1 532 DET OUTBOARD FLAP TRACK 3-4 CARRIAGE AF MRB CPCP MRB 575350-01-1 575300-200-009 12 YE 12 YE 24 YE 12 YE APPL
533
632 DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK
633 3 AND 4 CARRIAGE FORGINGS
575350-02-1 ************** TASK DELETED ************** N/A
575350-02-2 ************** TASK DELETED ************** N/A
575351-01-1 ************** TASK DELETED ************** N/A
575351-01-2 ************** TASK DELETED ************** N/A
575352-01-1 ************** TASK DELETED ************** N/A
575352-01-2 ************** TASK DELETED ************** N/A
3-57 575354-01-1 532 DET OUTBOARD FLAP TRACK 3-4 DRIVE LEVERS AF MRB CPCP MRB 575354-01-1 575300-200-010 6 YE 6 YE 24 YE 6 YE APPL
533
632 DETAILED INSPECTION OF OUTER WING OUTBOARD FLAP TRACK
633 3 AND 4 DRIVE LEVERS
575354-02-1 ************** TASK DELETED ************** N/A
575354-02-2 ************** TASK DELETED ************** N/A
2-57 575900-01-1 500 VCK MISCELLANEOUS (DRAINS) FOR LEADING/TRAILING EDGE AND AF MRB 9 MRB 57.59.00/01 575900-200-002 144 MO APPL
600 LEADING/TRAILING EDGE DEVICES
VISUAL CHECK OF DRAIN HOLES FOR CLOGGING
3-57 576103-01-1 575 DET AILERON HINGE AND ACTUATOR FITTINGS AF ALI ALI 576103-01-1 576000-200-002 12 YE 12 YE APPL
675 MRB CPCP MRB 576103-01-1 OR OR
DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND 38700 FC 18400 FC
ACTUATOR ATTACHMENT FITTINGS
3-57 576103-01-4 575 DET AILERON HINGE AND ACTUATOR FITTINGS AF MRB CPCP MRB 576103-01-1 576000-200-002 12 YE 12 YE N/A
675
DETAILED INSPECTION OF AILERON, HINGE FITTINGS AND
ACTUATOR ATTACHMENT FITTINGS
576103-01-5 ************** TASK DELETED ************** N/A
576103-01-6 ************** TASK DELETED ************** N/A
APPENDIX A
AEG/AMP/A320 Page 213 Rev. 2, 01.06.2020
AIRCRAFT MAINTENANCE PROGRAM A320
TASK TASK SOURCE TASK SAMPLE SAMPLE 100% 100%
SECTION ZONE DESCRIPTION SKILL CODE SOURCE REFERENCE CMP INTERVAL MSN 2157
NUMBER CODE REFERENCE THRESHOLD INTERVAL THRESHOLD INTERVAL
3-57 576104-01-1 500 DET AILERON SKIN ATTACH TO TRAILING EDGE AF MRB MRB 576104-01-1 576000-200-003 12 YE 12 YE APPL
600
DETAILED INSPECTION OF AILERON, UPPER AND LOWER
EXTERNAL SKINS AT ATTACHMENT TO TRAILING EDGE,
INBOARD AND OUTBOARD EDGES, SPARS AND RIBS
3-57 576106-01-1 500 DET AILERON UPPER AND LOWER SKINS AF MRB MRB 576106-01-1 576000-210-001 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF AILERON, UPPER AND LOWER
SKINS, EXTERNAL SURFACE
3-57 576107-01-1 500 DET AILERON UPPER AND LOWER EXTERNAL SKINS AF MRB CPCP MRB 576107-01-1 576000-200-005 6 YE 6 YE N/A
600
DETAILED INSPECTION OF AILERON UPPER AND LOWER
EXTERNAL SKINS AT ATTACHMENT TO TRAILING EDGE AND
OUTBOARD CLOSING RIB
577001-01-1 ************** TASK DELETED ************** N/A
577001-01-4 ************** TASK DELETED ************** N/A
3-57 577001-01-6 500 DET SPOILER 1 FITTING AF MRB CPCP MRB 577001-01-6 577100-200-001 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SPOILER 1, CENTER HINGE
FITTING AND ACTUATOR BRACKET
577001-02-1 ************** TASK DELETED ************** N/A
577001-02-3 ************** TASK DELETED ************** N/A
3-57 577002-01-1 500 DET SPOILER 1 SKINS OF CENTER FITTING AF MRB MRB 577002-01-1 577100-200-002 12 YE 12 YE 24 YE 12 YE APPL
600
DETAILED INSPECTION OF SPOILER 1, UPPER AND LOWER
SKINS, IN REGION OF CENTER HINGE FITTING
3-57 577003-01-1 500 DET SPOILER 1 SKINS AT TRAILING EDGE AF MRB MRB 577003-01-1 577100-200-003 12 YE 12 YE 24 YE
Saatja: Ermo Uuspuu </o=Majandus-Teede-Sideministeerium/ou=Exchange Administrative Group (FYDIBOHF23SPDLT)/cn=Recipients/cn=ef6c45ba2d6d40e68176f8058>
Saaja: 'Oliver Loorits', Ivo Tolga, Lennuamet
Teema: RE: Hooldusprogramm AEG/AMP/A320 Rev 1
Meie: 02.06.2020 nr 4.5-7/20/2301-4
Teie: 01.06.2020 nr 4.5-7/20/2301-1
Lugupeetud hr Oliver Loorits,
Lennuamet kiidab heaks, ES-LAA hooldusprogrammi muudatuse nr 2, puuduseid ega märkusi ei ole. Allkirjastatud hooldusprogrammi leiate manusest.
Lugupidamisega,
Ermo Uuspuu
Lennundustehnika osakonna vaneminspektor
SAFA Riiklik koordinaator
+372 610 3570
www.ecaa.ee <http://www.ecaa.ee/> | Lõõtsa 5, 11415 Tallinn
Lennuamet
From: Ermo Uuspuu
Sent: Monday, June 1, 2020 1:15 PM
To: 'Oliver Loorits' <
[email protected]>
Cc: Ivo Tolga <
[email protected]>; Lennuamet <
[email protected]>
Subject: RE: Hooldusprogramm AEG/AMP/A320 Rev 1
Meie: 01.06.2020 nr 4.5-7/20/2301-3
Teie: 01.06.2020 nr 4.5-7/20/2301-1
Lugupeetud hr Oliver Loorits,
Kinnitame, et oleme kätte saanud õhusõiduki registratsiooniga ES-LAA hooldusprogrammi muudatuse nr 2. Anname Teile peatselt teada märkustest/puudustustest/kommentaaridest kui neid peaks esinema. Juhul kui neid ei esine saame Teie poolt esitatud hooldusprogrammi koheselt ka heaks kiita.
Lugupidamisega
Ermo Uuspuu
Lennundustehnika osakonna vaneminspektor
SAFA Riiklik koordinaator
+372 610 3570
www.ecaa.ee <http://www.ecaa.ee/> | Lõõtsa 5, 11415 Tallinn
Lennuamet
From: Oliver Loorits <
[email protected] <mailto:
[email protected]> >
Sent: Monday, June 1, 2020 10:59 AM
To: Ermo Uuspuu <
[email protected] <mailto:
[email protected]> >
Cc: Ivo Tolga <
[email protected] <mailto:
[email protected]> >; Lennuamet <
[email protected] <mailto:
[email protected]> >
Subject: Re: Hooldusprogramm AEG/AMP/A320 Rev 1
Meie 01.06.2020
Lp hr Ermo Uuspuu
Käesolevaga esitan teile heakskiitmisele lennuki A320 tunnusega ES-LAA hooldusprogrammi muudatuse nr 2.
Juhin tähelepanu, et muudatus seisneb peamiselt Appendix C (Daily Weekly Checklisti) kohandamisel ja väiksemate parandustel.
Lugupidamisega
Oliver Loorits
Airworthiness Manager
Airest Inc
Lõõtsa 8A - C tower, Tallinn 11415 Estonia
www.airest.aero <http://www.airest.aero>
On Jan 7, 2020, at 4:54 PM, Ermo Uuspuu <
[email protected] <mailto:
[email protected]> > wrote:
Meie: 4.5-7/19/5400-2
Teie: 4.5-7/19/5400-1
Lp Härra Oliver Loorits,
Teie poolt esitatud hooldusprogrammi Airest lennuki A320 tunnusega ES-LAA hooldusprogrammi AEG/AMP/A320 rev 1 on läbi vaadatud ja heaks kiidetud. Allkirjastatud hooldusprogramm on manuses.
Lugupidamisega,
Ermo Uuspuu
vaneminspektor
+372 610 3570
www.ecaa.ee <http://www.ecaa.ee/> | Lõõtsa 5, Tallinn 11415
Lennuamet
From: Oliver Loorits <
[email protected] <mailto:
[email protected]> >
Sent: Friday, December 13, 2019 10:17 AM
To: Ermo Uuspuu <
[email protected] <mailto:
[email protected]> >; Lennuamet <
[email protected] <mailto:
[email protected]> >; Kalle Allikson <
[email protected] <mailto:
[email protected]> >
Subject: Hooldusprogramm AEG/AMP/A320 Rev 1
Meie: 13.12.2019
Lp hr Ermo Uuspuu
Käesolevaga esitan teile heakskiitmisele lennuki A320 tunnusega ES-LAA hooldusprogrammi muudatuse nr 1.
Juhin tähelepanu, et muudatus seisneb peamiselt Airbus MPD rev 46 uuendusest ning lisatud on Appendix G ja H.
Lugupidamisega
Oliver Loorits
Airworthiness Manager
Airest Inc
Lõõtsa 8A - C tower, Tallinn 11415 Estonia
www.airest.aero <http://www.airest.aero/>
<AMP AEG MP A320 rev.1 10.12.2019.asice>