Commonwealth legislation

AD/CL-600/26 - Flap Actuators

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Requires operators of Bombardier (Canadair) CL-600 Challenger aeroplanes (specified serial-number ranges) to perform the inspection/rectification set out in Canadair Alert Service Bulletin A601‑0415 (or Alert Wire TA601‑0415‑036) because a flap actuator failure was linked to an incorrectly installed shoulder bolt. Compliance is mandatory within 10 hours time-in-service after 11 August 1993 or before 11 September 1993. The aircraft operator/owner must arrange and pay for the maintenance (Applicability; Requirement; Compliance).

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Current sections

Direct links to the current provisions in AD/CL-600/26 - Flap Actuators.

AD/CL-600/26 - Flap Actuators

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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 Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

AD/CL-600/26 Flap Actuators 10/93 DM

Applicability: Model CL-600-2A12 with serial numbers 3002 through 3066. Model CL-600-2B16 with serial numbers 5001 through 5131.

Requirement: Action in accordance with Canadair Challenger Alert Service Bulletin A601-0415 or Alert Wire TA601-0415-036.

Note: Transport Canada AD CF-93-18 refers.

Compliance: Unless already accomplished, within 10 hours time in service after 11 August 1993 or prior to 11 September 1993, whichever occurs first.

Background: The recent failure of a flap actuator was found to be caused by the incorrect installation of the shoulder bolt which secures the flap actuator to the wing trailing edge.

Source text

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