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AD/PA-36/21 - Rudder Cable and Seat Belt Attachment Shackles - Inspection
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AD/PA-36/21 - Rudder Cable and Seat Belt Attachment Shackles - Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Piper PA-36 (Pawnee Brave) Series Aeroplanes
AD/PA-36/21 Rudder Cable and Seat Belt Attachment Shackles - Inspection
12/81
Applicability: All models PA-36-285/300 and PA-36-375 with S/Nos. referenced in Piper SB No.
729 or with S/Nos. referenced in subsequent issues or revisions of that service bulletin.
Document: Piper SB No. 729.
Compliance: Within 25 hours time in service after 10 November 1981.
Background: Some shackles P/N 486-566 (MS 20115-5) installed for rudder cable/horn attachment and the upper seat belt/cable attachment may have cracks.