Document ID: chunk:federal_register_of_legislation:F2006B08585:body:0
Version: federal_register_of_legislation:F2006B08585
Segment Type: other
Provision Reference: 
Character Range: 0–1177

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-600/25
 Amdt 1

 Throttle Quadrant 7/94

            Applicability: Model CL-600 aircraft with serial numbers, and with throttle quadrant part numbers listed in the Requirement Document.

            Requirement: Action in accordance with the technical requirements of Transport Canada AD CF-92-23R1.

            Note: Canadair Challenger ASB A600-0615, ASB A601-0374 Revision 1, SB 600-0629, and SB 601-0410 refer.

            Compliance: As specified in the Requirement Document with a revised effective date of 23 June 1994.

            Background: A report had been received of unintentional engine shut-down in flight. This shut- down resulted from the throttle lever overriding the idle stop, during throttle retardation, and moving into the shut-off position. Amendment 1 is issued in response to a revision of the Requirement Document which requires an additional fault detection check and another modification to the aircraft throttle quadrant.