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Boeing 737 Aeroplanes - Fuselage Skin Panels at the Chem-mill Steps

Lennuamet · 19. jaanuar 2017
Viit
3-1/17/239-1
Registreeritud
19. jaanuar 2017
Dokumendi liik
Bulletin
Funktsioon
3 Rahvusvahelise koostöö korraldamine
Sari
3-1 Kirjavahetus lennundusküsimustes
Toimik
3-1/2017
Vastutaja
Kalle Allikson

Failid

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  • 📎NM-17-06.pdf31 KB

Sisu (failidest)

FAA SPECIAL AIRWORTHINESS Aviation Safety INFORMATION BULLETIN SAIB: NM-17-06 SUBJ: Fuselage: Chem-Mill Skin Panels Date: January 4, 2017 This is information only. Recommendations aren’t mandatory. Introduction This Special Airworthiness Information Bulletin (SAIB) advises owners and operators of certain The Boeing Company Model 737-200, -200C, -300, -400, and -500 series airplanes of a new inspection procedure for cracking in the fuselage skin panels at the chem-mill steps. Background Airworthiness Directive (AD) 2011-24-12 and AD 2012-26-02, require inspections for cracking at the chem-mill steps of the fuselage skin in several locations on the Boeing Model 737 series airplanes listed above. The inspections use the Ultrasonic Phased Array methodology specified in the Boeing Non Destructive Testing (NDT) Manual Part 4, Section 53-30-07, dated July 1, 2016. This NDT methodology provides an adequate level of safety for compliance with those ADs. To provide human factors improvements when inspecting large areas of the fuselage skin panels, Boeing published a new inspection procedure in the Boeing 737 NDT Manual, Part 4, Section 53-30-12, dated November 1, 2016, in conjunction with its corresponding probe. The FAA recently approved Boeing Alternative Method of Compliance (AMOC) Notices: 737-53A1234 AMOC 02, dated September 22, 2016, and 737-53A1301 AMOC 01, dated September 22, 2016, allowing the use of the procedure in the Boeing 737 NDT Manual, Part 4, Section 53-30- 12, dated November 1, 2016, as an acceptable alternative to NDT Manual Part 4, Section 53-30-07, required by AD 2011-24-12 and AD 2012-26-02. Recommendations The FAA recommends that operators of the affected airplanes follow the inspection procedure outlined in Boeing 737 NDT Manual, Part 4, Section 53-30-12, dated November 1, 2016. For Further Information Contact Jennifer Tsakoumakis, Aerospace Engineer, Airframe Branch, ANM-120L, FAA, Los Angeles Aircraft Certification Office, 3960 Paramount Boulevard, Lakewood, CA 90712-4137; phone: 562-627- 5264; fax: 562-627-5210; email: [email protected]. For Related Service Information Contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740; telephone 562-797-1717; Internet https://www.myboeingfleet.com. 1 Please find attached a Foreign State of Design Advisory document, endorsed by EASA. This advisory document is also online at http://ad.easa.europa.eu/ad/NM-17-06 . Should you have any questions, please contact the Agency by e-mail at [email protected] or by fax, No.: +49 221 89990 9515. Safety Information Section Email: [email protected] EASA Website (Attachment is in Acrobat PDF format) Postal: Postfach 10 12 53, 50452 Cologne, Germany An agency of the European Union This message is intended for the use of the addressee only and may contain information that is privileged and confidential. If you are not the intended recipient, you are notified that any dissemination of this communication is strictly prohibited. If you have received this communication in error, please notify us immediately by returning this e-mail. Sender accepts no liability for damage of any kind resulting from the risks inherent in the electronic transmission of messages. This communication does not constitute any formal commitment on behalf of the European Aviation Safety Agency.
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