AD/CL-600/7 - Horizontal Stabiliser Pitch Trim Actuator - Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08627 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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

 

AD/CL-600/7 Horizontal Stabiliser Pitch Trim Actuator - Modification

Applicability: Pitch trim actuators as listed in requirement document. Document: Canadair Challenger Alert SB No. A600-0084.

Note: Canadian Dept. of Transport AD CF-82-05 refers.

 

Compliance: Before issue of Australian Certificate of Airworthiness.


3/83

 

Background: Pitch trim actuators are suspected of having possible loose motor drive gear pinions.

This could result in damage to internal control wiring.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.