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Piper PA-23 Main Landing Gear Drag Link Bolt

Lennuamet · 27. veebruar 2017
Viit
3-1/17/818-1
Registreeritud
27. veebruar 2017
Dokumendi liik
Bulletin
Funktsioon
3 Rahvusvahelise koostöö korraldamine
Sari
3-1 Kirjavahetus lennundusküsimustes
Toimik
3-1/2017
Vastutaja
Kaupo Toodu

Failid

  • 📎CE-17-08.pdf29 KB
  • 📎E-kiri.pdf246 KB
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Sisu (failidest)

FAA SPECIAL AIRWORTHINESS Aviation Safety INFORMATION BULLETIN SAIB: CE-17-08 SUBJ: Main Landing Gear – Drag Link Bolt Date: February 21, 2017 This is information only. Recommendations aren’t mandatory. Introduction This Special Airworthiness Information Bulletin (SAIB) alerts you, owners or operators of Piper Aircraft Inc. (Piper) Models PA-23-150, PA-23-160, PA-23-235, and PA-23-250 airplanes about a potential airworthiness concern regarding a failure of the main landing gear drag link bolt, which can cause the main gear to collapse. Fatigue cracking can develop at the midpoint of the bolt shank, which can result in bolt failure and subsequent main gear collapse. At this time, this airworthiness concern is not an unsafe condition that would warrant AD action under Title 14 of the Code of Federal Aviation Regulations (14CFR part 39). Background This SAIB is a result of an incident on a Piper Model PA-23-250 airplane where the right main landing gear collapsed during landing. The investigation revealed that the right main landing gear drag link center attach bolt had sheared in the center of the bolt shank due to fatigue. Recommendations We recommend that you incorporate Piper Service Bulletin No. 1299, dated January 6, 2017, which recommends periodic replacement of main landing gear drag link bolt and the inspection of the mating bushings. For Further Information Contact Hector Hernandez, Aerospace Engineer, FAA, Central Region, Atlanta Aircraft Certification Office, 1701 Columbia Avenue, College Park, GA 30337; phone (404) 474-5587; fax (404) 474-5606; email: [email protected]. For Related Service Information Contact Piper Aircraft Inc., 2926 Piper Drive, Vero Beach, Florida, 32960; website: http://www.piper.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/CE-17-08 . 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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