Federal Register of Legislation
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY SCHEDULE OF AIRWORTHINESS DIRECTIVES
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.
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