1AD/PA-28/58 - Wing Structural Fatigue Life Limitation

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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-28 Series Aeroplanes

 

AD/PA-28/58 Wing Structural Fatigue Life Limitation 12/76

Applicability: All model PA-28-235. Requirement: Retire the wing from service.

Compliance: At or before 12,500 hours time in service.