Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.
AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes
AD/CL-600/62 Angle of Attack Vane 2/2005 AD/CL-600/62 Angle of Attack Vane 2/2005 TX
AD/CL-600/62 Angle of Attack Vane 2/2005 TX
Applicability: Bombardier Inc. “Challenger” aircraft listed below with angle of attack (AOA) vane Part Number (P/N) 600-59154-5 installed:
Aircraft Model Aircraft Model
Aircraft Model
CL-600-1A11 (CL-600) CL-600-2A12 (CL-601)
CL-600-2B16 (CL-601-3A/-3R) CL-600-2B16 (CL-604)
Serial Number Range Serial Number Range
Serial Number Range
1004 to 1085
3001 to 3066
5001 to 5194
5301 and subsequent
Aircraft Model Aircraft Model
Aircraft Model
CL-600-1A11 (CL-600) CL-600-2A12 (CL-601)
CL-600-2B16 (CL-601-3A/-3R) CL-600-2B16 (CL-604)
ASB
A600-0729 dated 14 October 2004
A601-0571 dated 14 October 2004
A601-0571 dated 14 October 2004
A604-27-026 dated 14 October 2004
Aircraft Model Aircraft Model
Aircraft Model
CL-600-1A11 (CL-600) CL-600-2A12 (CL-601)
CL-600-2B16 (CL-601-3A/-3R) CL-600-2B16 (CL-604)
AMM
PSP 602 Chapter 27-39-11
PSP 601-2 Chapter 27-39-11
PSP 601-2 Chapter 27-39-11
AMM Task 27-35-04-720-801