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.
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 | ||
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