Federal Register of Legislation - Australian Government

Primary content

AD/CL-600/71 Airworthiness Directives/Pt 105 — Aircraft as made
State of Design Airworthiness Directives
Administered by: Infrastructure and Transport
Exempt from sunsetting by the Legislative Instruments Act 2003 s 54(2) item 9
Registered 18 Jun 2007
Tabling HistoryDate
Tabled HR19-Jun-2007
Tabled Senate19-Jun-2007
Date of repeal 09 Jun 2010
Repealed by AD/CL-600/71 Amdt 1 - State of Design Airworthiness Directives

 

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 39.001(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-600/71

State of Design Airworthiness Directives

8/2007 DM

 

Applicability:

Bombardier (formerly Canadair) CL-600-2B19, CL-600-2C10, CL-600-2D15 and CL-600-2D24 ‘Regional Jet’ series aeroplanes, as identified in the individual Transport Canada Aviation (TCA) Airworthiness Directives (AD) identified in
Table 1.

Requirement:

1.    Determine the applicability of the TCA ADs listed in Table 1.

 

2.    If it is determined that an AD listed in Table 1 is applicable and has not been previously accomplished, perform the actions required by that AD.

 

Table 1

 

TCA AD

Effective Date

Title

CF-93-02R1

6 May 1994

Passenger Door De-Icing Agent & Lubrication

CF-93-27R1

12 December 1995

Stall Protection System

CF-93-29

4 December 1993

Integrated Drive Generator

CF-94-14

19 October 1994

ADG Manual Deployment System

CF-94-21R1

30 November 1995

Elevator Damper Shear Pins

CF-95-08R2

3 September 1996

Horizontal Stab Trim Control/AFM Restriction

CF-95-10

8 August 1995

NLG Spring Bungee Assembly

CF-95-14R1

30 December 1996

Aileron Flutter Damper Shear Pin

CF-96-12R1

14 March 1997

MLG Shock Strut Pins Plating

CF-96-16R1

31 July 1998

Copilot’s Air Data System

CF-96-18

12 November 1996

DC Power Fuse Holder

 

 

CF-1998-14R4

25 June 2004

Flap System Failure

CF-98-35

30 October 1998

Electrical Conduits in Fuel Tanks

CF-98-40

23 December 1998

Main and APU Battery Connector

CF-99-09R1

11 June 1999

IDG Cable Harness

CF-2000-28

29 September 2000

Aileron Controls

CF-2002-06

4 March 2002

Rudder Travel Limiter Actuators

CF-2002-19

11 March 2002

Center Tank Fuel Line Failures

CF-2002-22

8 April 2002

Center Tank Fuel Line Failures

CF-2002-35R2

30 January 2005

Aileron Stiffness

CF-2002-41

25 October 2002

Main Landing Gear Side-Brace Fitting Shaft

CF-2003-01R1

25 January 2006

Centre Fuel Tank - Fuel Tube Failure

CF-2003-03

14 March 2003

Landing Gear Control Handle Assembly

CF-2003-07

25 March 2003

Wing Anti-Ice Ducts

CF-2003-14R1

26 February 2005

Wing Root Area Wire Damage

CF-2003-23R2

19 August 2005

Main Landing Gear Door Separation During Flight

CF-2003-26

8 December 2003

Pitch Feel Simulator

CF-2004-04R3

8 April 2004

Fuel Ejector Leak Check

CF-2004-14

24 August 2004

Aft Pressure Bulkhead Structure and Hydraulic Lines

CF-2004-20

1 November 2004

Hydraulic Line Shields

CF-2004-23R1

18 August 2005

Camloc Fasteners on Center Pedestal

CF-2005-01

2 February 2005

Cold Weather Operations

CF-2005-02

2 February 2005

Cold Weather Operations

 

 

CF-2005-13R1

7 November 2005

Cracking of Aft Pressure Bulkhead Web

CF-2005-18

11 July 2005

Missing Restrictor on Refuel / Defuel Shut-Off Valves

CF-2005-31

19 September 2005

Camloc Fasteners on Centre Pedestal - Interference with Rudder Pedals

CF-2005-35

3 October 2005

Junction Boxes - Leach TDH-Series Relays Malfunction

CF-2006-07

25 April 2006

AC Contactor Failure

CF-2006-04

28 April 2006

Aileron Control System - Reduction in Task Interval for Backlash Check

CF-2006-11

19 June 2006

Improper Installation of Chemical Oxygen Generator Release Pin

CF-2006-20R1

16 October 2006

Horizontal Stabilizer Trim - Uncommanded Motion

 

Note:   TCA ADs may be accessed via the internet at the following URL:

            http://www.tc.gc.ca/aviation/applications/cawis-swimn/awd-lv-cs1401.asp?lang=E&rand=

Compliance:

For Requirements 1 and 2 - Within 30 days after the effective date of this Directive or prior to the issue of a Certificate of Airworthiness, whichever occurs later.

 

This Airworthiness Directive becomes effective on 29 June 2007.

Background:

The TCA ADs listed in Table 1 of this Directive require one time actions for which the compliance date and/or period has passed.  CASA has determined that these ADs may be applicable to recently registered or imported Australian aircraft.  This Directive is issued to ensure all State of Design ADs are complied with.

 

CASA appreciates that, due to date of aircraft manufacture or aircraft configuration and modification status, not all the ADs listed in Table 1 will be applicable to all Regional Jet series aeroplanes.


David Punshon
Delegate of the Civil Aviation Safety Authority

14 June 2007