AD/CL-600/17 - Flight Controls - Elevator Cable Inspection
1AD/CL-600/17 - Flight Controls - Elevator Cable Inspection
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
AD/CL-600/17 Flight Controls - Elevator Cable Inspection 11/88
Applicability: Model CL-600-1A11 (CL-600), Serial Numbers 1004 to 1085. Requirement: Action in accordance with Canadair SB 600-0522.
Compliance: Within 100 hours time in service after 3 November 1988, or prior to issue of a Certificate of Airworthiness.
Background: The possibility exists for fouling between the wiring harness leading to the autopilot pitch servo and the elevator control cables. This inspection includes a remedy if fouling is discovered.