AD/PA-32/38 - Quick Disconnect Seat Retention Mechanism - Inspection
1AD/PA-32/38 - Quick Disconnect Seat Retention Mechanism - 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-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/38 Quick Disconnect Seat Retention Mechanism - Inspection
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Applicability: Model PA32-260 with S/Nos. 32-01 to 32-7500002. Model PA-32-300 with S/Nos.
32-40001 to 32-7540028.
Document: Piper SL No. 763.
Compliance: Within 100 hours time in service after 30 January 1976.