Commonwealth legislation

AD/BEECH 76/3 - Elevator Trailing Edge Bond

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This mandatory Civil Aviation Safety Authority Airworthiness Directive affects owners/operators of Beechcraft Model 76 Duchess aircraft (serials ME-1–ME-6, ME-8–ME-62). It requires inspecting and repairing the adhesive bond of the elevator trailing edge per Beechcraft Service Instruction No. 1041 because bond failure could detach the trailing edge, damage the tail, or impair control. Compliance was required within 100 flight hours after 30 June 1979.

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Current sections

Direct links to the current provisions in AD/BEECH 76/3 - Elevator Trailing Edge Bond.

AD/BEECH 76/3 - Elevator Trailing Edge Bond

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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 76/3 Elevator Trailing Edge Bond 6/79

Applicability: All model 76 with S/Nos. ME-1 to ME-6 and ME-8 to ME-62. Requirement: Action in accordance with Beechcraft SI No. 1041.

Compliance: Unless already accomplished, within 100 hours’ time in service after 30 June 1979. Background: There is a possibility of in-service separation of the elevator trailing edge bond.

Federal Register of Legislative Instruments F2006B04178

Source text

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