Commonwealth legislation

AD/BEA 121/18 - Rudder Control Lever

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Operators of Beagle B121 (Pup) aeroplanes fitted with Rudder Control Lever P/N BE 45.10193 must carry out the corrective work specified in Scottish Aviation Service Bulletin No. B121/72 within 100 hours TIS after 31 October 1977. This mandatory, time‑limited airworthiness directive affects only those aircraft with the specified part, places compliance and cost on the owner/operator, and leaves technical procedures to the referenced service bulletin and certificated maintenance personnel.

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Current sections

Direct links to the current provisions in AD/BEA 121/18 - Rudder Control Lever.

AD/BEA 121/18 - Rudder Control Lever

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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 Beagle B121 (Pup) Series Aeroplanes

AD/BEA 121/18 Rudder Control Lever 10/77

Applicability: All models B121 with Rudder Control Lever P/N BE 45.10193. Requirement: Action in accordance with Scottish Aviation SB No. B121/72. Compliance: Within 100 hours time in service after 31 October 1977.

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

Beagle B121 (Pup) Series Aeroplanes

AD/BEA 121/18 Rudder Control Lever 10/77