Commonwealth legislation

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

In ForceCTH

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Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive mandates retirement of the wing main spar on Gulfstream (Rockwell) 112-series aeroplanes once that component exceeds 11,200 hours’ time in service, with CASA setting a fixed compliance date (30 January 1976). It directly affects owners/operators, who bear replacement, downtime and resale-value costs, forces changes to maintenance and scheduling, and raises demand for replacement spars or wing assemblies while removing discretionary inspection relief.

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AD/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

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.