Document ID: chunk:federal_register_of_legislation:F2006B08627:body:0
Version: federal_register_of_legislation:F2006B08627
Segment Type: other
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Character Range: 0–746

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.

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 Background: Pitch trim actuators are suspected of having possible loose motor drive gear pinions.
            This could result in damage to internal control wiring.