Commonwealth legislation

AD/BEECH 56/8 - Engine Mount Bolt Nuts

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

1/10 complexity

What this does This directive mandates safety action for specific Beechcraft aircraft to fix a problem with engine mount bolt nuts (the fasteners that hold the engine to the airframe).

Who it affects Owners and operators of Beechcraft 56TC (Turbo Baron) Series aeroplanes with serial numbers TG64 and subsequent (i.e., TG64 and all later serial numbers).

What you must do You must follow the manufacturer's instructions in Beechcraft Service Instruction No. 0396-241 regarding the engine mount bolt nuts.

When you must do it Within 25 hours of flight time after 21 August 1970.

Why this matters Loose or faulty engine mount hardware could cause the engine to detach from the aircraft during flight. This directive ensures the aircraft remains airworthy and safe to operate.

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AD/BEECH 56/8 - Engine Mount Bolt Nuts

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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 56TC (Turbo Baron) Series Aeroplanes

AD/BEECH 56/8 Engine Mount Bolt Nuts 8/70

Applicability: All models with S/Nos. TG64 and subsequent. Requirement: Action in accordance with Beechcraft SI No. 0396-241. Compliance: Within 25 hours’ time in service after 21 August 1970.

Source text

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