AD/PA-32/72 - Nose Landing Gear Downlock - Modification
1AD/PA-32/72 - Nose Landing Gear Downlock - Modification
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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-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/72 Nose Landing Gear Downlock - Modification 1/82
Applicability: PA-32R-300 Lance S/Nos. 32R-768001 to 32R-7880068. PA-32RT-300 Lance II S/N 32R-7885001 to 32R-7985105. PA-32RT-300T Turbo Lance II S/N 32R-7787001,
32R-7887002 to 32R-7987126. PA-32R-301 Saratoga SP S/Nos. 32R-8013001 to
32R-8113112. PA-32R-301T Turbo Saratoga SP S/Nos. 32R-8029001 to 32R-
Document: Piper Service Letter No. 927 and Piper Kit P/N 764135V.
Note: FAA AD 81-24-07 Amdt. 39-4255 refers.
Compliance: Within 100 hours time in service after 31 January 1982.
Background: There have been reports of failures of the nose landing gear down locks on certain Piper PA-32R models.