AD/PA-32/20 - Seat Frame - Modification
1AD/PA-32/20 - Seat Frame - 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-32/20 Seat Frame - Modification 5/71
Applicability: All the following models having vertically adjustable pilot and/or co-pilot seat installations:
All PA-32-260 with S/Nos. 32-1251 to 32-1320 and 32-7100001 to 32-7100015.
All PA-32-300 with S/Nos. 32-40851 to 32041018 and 32-7140001 to 32-7140040.
Document: Piper SB No. 337.
Compliance: Within 100 hours time in service after 31 May 1971.