Commonwealth legislation

AD/BEECH 76/5 - Main Landing Gear Fork Pin

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

Requires inspection/modification of the Model 76 main landing gear fork pin per Beechcraft Service Instruction No. 1073 for aircraft serials ME-1 to ME-228, to be done within 50 hours TIS after 28 August 1979. Owners/operators and maintenance providers must schedule and fund the work to prevent possible wheel/fork separation; the regulator mandates compliance while delegating procedural detail to the manufacturer’s service instruction.

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Current sections

Direct links to the current provisions in AD/BEECH 76/5 - Main Landing Gear Fork Pin.

AD/BEECH 76/5 - Main Landing Gear Fork Pin

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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 Beechcraft 76 (Duchess) Series Aeroplanes

AD/BEECH 76/5 Main Landing Gear Fork Pin 8/79

Applicability: All model 76 with S/Nos. ME-1 to ME-228. Requirement: Action in accordance with Beechcraft SI No. 1073.

Compliance: Within 50 hours’ time in service, unless already accomplished, after 28 August 1979.

Background: Failure of the existing fork pin retaining pin could result in separation of the wheel and fork assembly.

Source text

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