Commonwealth legislation

AD/AUS/16 Amdt 1 - Strengthened Actuator Lever Assemblies on Flap Control Torque Shaft

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of specified Auster/Beagle A.61-series aeroplanes to fit strengthened actuator-lever assemblies to the flap-control torque shaft, by following Auster S.B. Issue 48, Mod. 3663. Compliance is immediate ("Forthwith"); operators must obtain the service bulletin, arrange parts and installation, and bear the costs. The Civil Aviation Safety Authority issued the directive.

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AD/AUS/16 Amdt 1 - Strengthened Actuator Lever Assemblies on Flap Control Torque Shaft

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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 Auster/Beagle A.61 Series Aeroplanes

AD/AUS/16

Amdt 1

Strengthened Actuator Lever Assemblies on Flap Control Torque Shaft

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Applicability: (a) Models: Mk4, Mk5, Mk5C, Mk5D;

(b) Models: J1, J1B, J1N, J1U;

(c) Models: J5, J5B, J5F, J5G, J5H, J5K, J5L, J5P, J5Q, J5R, J5V. Requirement: Action in accordance with Auster S.B. Issue 48, Mod. 3663. Compliance: Forthwith.

Background: Amendment issued to incorporate reference to applicable aircraft models.

Source text

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