Commonwealth legislation

AD/BEECH 23/17 - Electric Flap System Mechanism

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

This is a legally-binding aviation safety order affecting specific light aircraft. Who it affects: Owners and operators of Beechcraft models B19, C23, A24, and A24R that have the optional electric flap system installed (this includes the Musketeer and Sierra series). What it requires: You must immediately inspect or repair the electric flap mechanism following the manufacturer's specific instructions (Beechcraft Service Instruction No. 0415-161). Why it matters: The flap system controls lift during landing and takeoff. This directive addresses a known safety defect that could affect flight safety, and you must comply immediately ('forthwith') before the aircraft can fly.

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Current sections

Direct links to the current provisions in AD/BEECH 23/17 - Electric Flap System Mechanism.

AD/BEECH 23/17 - Electric Flap System Mechanism

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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 19, 23 and 24 Series Aeroplanes

AD/BEECH 23/17 Electric Flap System Mechanism 3/71 Applicability: Models B19, C23, A24 and A24R equipped with the optional electric flap installation. Requirement: Action in accordance with Beechcraft SI No. 0415-161.

Compliance: Forthwith.

Source text

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

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

Beechcraft 19, 23 and 24 Series Aeroplanes

Compliance: Forthwith.