1AD/PA-32/11 - Wing Rear Spar Attach Bolts - 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-32/11 Wing Rear Spar Attach Bolts - Inspection 1/68

Applicability: As detailed in Piper SB No. 261. Document:  SB No. 261.

Compliance: Within 100 hours time in service after 25 January 1968.