1AD/AC-112/2 - Wing Structural 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 Gulfstream (Rockwell) 112 Series Aeroplanes

 

AD/AC-112/2 Wing Structural Life Limitation 1/76

Applicability: All models with wing main spar caps exceeding 11200 hours’ time in service. Requirement:               Retire the wing main spar from service.

Compliance: 30 January 1976.