Airworthiness Directives 2004 - Revocation and Remaking - Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes

 AD Name AD Number

 Windshield and Side Windows Reinforcing T Plates - CANCELLED AD/CL-600/1

 Elevator Inboard Hinge Fitting - Inspection and Replacement AD/CL-600/2

 Passenger Door Interior and Exterior Handles and Latch Mechanism -  AD/CL-600/3

 Auxiliary Power Unit Load Control Valve - Special Check and Adjustment AD/CL-600/4

 Main Landing Gear Brake Assemblies - Inspection and Re-Identification AD/CL-600/5

 Branson Fuel Tank - Electrical Harness - Inspection and Modification AD/CL-600/6

 Horizontal Stabiliser Pitch Trim Actuator - Modification AD/CL-600/7

 Landing Gear Electrical Harnesses - Modification AD/CL-600/8

 Junction Box No.2 - Vertical Navigation and Glide Slope Relay - Modification AD/CL-600/9

 Autopilot Duplex Servo - Installation of Protective Cover AD/CL-600/10

 Stick Pusher - Inspection and Modification AD/CL-600/11

 Throttle Quadrant Wear Strips - Special Check and Modification - CANCELLED AD/CL-600/12

 Brake Control Push-Pull Cable AD/CL-600/13 Amdt 1

 Engine Pylon Fuel Feed Tube Assembly - Modification AD/CL-600/14

 Aileron and Elevator Flutter Dampers AD/CL-600/15 Amdt 1

 Wing Outboard Flap Vane and Structure - CANCELLED AD/CL-600/16 Amdt 1

 Flight Controls - Elevator Cable Inspection AD/CL-600/17

 Introduction of Earthing Point AD/CL-600/18

 Fire Extinguishing Bottle Squib Wiring AD/CL-600/19

 ADG Output Harness Chafing AD/CL-600/20

 Tail Cone Fuel Tank AD/CL-600/21 Amdt 2

 Engine Fire Detection, Indication and Extinguishing Systems AD/CL-600/22

 Brakes AD/CL-600/23 Amdt 1

 Generator and APU Feeder Wires AD/CL-600/24

 Throttle Quadrant AD/CL-600/25 Amdt 1

 Flap Actuators AD/CL-600/26

 Rudder Control Quadrant AD/CL-600/27 Amdt 1

 Sunstrand Air Driven Generator AD/CL-600/28

 Horizontal Stabiliser Trim Actuator AD/CL-600/29


 Time Limits and Maintenance Checks AD/CL-600/30

 Fuel Tank Arcing Prevention AD/CL-600/31

 Underfloor Pressure Bulkhead at FS409.00 AD/CL-600/32 Amdt 2

 Overwing Emergency Exit Hatches AD/CL-600/33

 Flap Operation AD/CL-600/34 Amdt 2

 Main Landing Gear Main Fitting AD/CL-600/35 Amdt 1

 Elevator Flutter Damper Shear Pins AD/CL-600/36

 Flight Spoiler Centre Hinge Fitting AD/CL-600/37 Amdt 1

 IDG Cables and Firewall Separator AD/CL-600/38 Amdt 1

 Fuel Level Sensing Wiring Chafing AD/CL-600/39

 Electrical Power - Chafing of IDG Cables AD/CL-600/40

 Fire Warning Control Unit AD/CL-600/41

 Lower Wing Plank AD/CL-600/42

 Cargo Compartment Smoke Detector AD/CL-600/43

 Power Transfer Contactors AD/CL-600/44

 Engine Support Beam AD/CL-600/45

 Main Windshield Fasteners AD/CL-600/46

 Center Tank Fuel Transfer Shutoff Valve AD/CL-600/47

 CVR/FDR Paint Stripping AD/CL-600/48

 Angle of Attack Transducer AD/CL-600/49

 Main Fuel Tank Vent System Modification AD/CL-600/50

 Chafed IDG Cables AD/CL-600/51

 Refuel Floodlight AD/CL-600/52

 Fuel Migration and Centre of Gravity Limit AD/CL-600/53

 CL-600-2B19 RJ Overwing Exit Placards AD/CL-600/54

 Flap Vane System AD/CL-600/55

 APU Cooling Air Exhaust AD/CL-600/56

 Horizontal Stabilizer Trim Actuator AD/CL-600/57

 Aileron Stiffness AD/CL-600/58

 IDG Cables AD/CL-600/59

 Flap Vane Brackets AD/CL-600/60

 Main Landing Gear Side-Brace  Fitting Shaft AD/CL-600/61

 

Overview

The Airworthiness Directives 2004 is a legislative instrument issued by the Civil Aviation Safety Authority (CASA) under the authority of the Civil Aviation Safety Regulations 1998. This instrument was enacted to address the need for continuous updating and management of airworthiness directives pertaining to specific aircraft types, in this case, the Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes. The directives aim to ensure that aircraft maintain the highest safety standards by specifying necessary inspections, modifications, and replacements. The policy objective of these directives is to mitigate risks associated with aircraft operation by enforcing specific maintenance and operational protocols. The enactment was authorised by David Alan Villiers, the delegate of CASA, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The instrument revokes certain existing airworthiness directives and re-makes them to reflect the latest safety requirements. This process ensures that the directives remain relevant and effective in addressing emerging safety issues and technological advancements in aircraft maintenance.

Scope and Application

The Airworthiness Directives 2004 legislative instrument pertains to airworthiness directives issued under the authority of the Civil Aviation Safety Regulations 1998. It applies to Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes, specifically targeting various components and systems such as windshields, side windows, elevator inboard hinge fittings, passenger door handles, auxiliary power unit load control valves, and more. These directives are instrumental in ensuring that the aircraft maintain the necessary safety and airworthiness standards. The directives apply nationally within Australia, extending to all relevant aircraft and operators within the Commonwealth jurisdiction. The instrument revokes some previous directives and re-issues others to maintain updated safety protocols. Notably, certain directives are cancelled, indicating that they are no longer applicable or have been superseded by newer regulations or technological advancements. The instrument also allows for amendments to existing directives, reflecting ongoing safety assessments and improvements. This legislation is critical for maintaining the safety and airworthiness of the specified aircraft models in Australian airspace.

Key Provisions

The Airworthiness Directives 2004 document, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA), primarily involves the revocation and remaking of specific Airworthiness Directives pertaining to Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes (section 1(a) and (b)). This legislative instrument revokes certain existing Airworthiness Directives and re-issues them as separate instruments, maintaining the exact form as the latest published editions (section 1(b)). The specific Airworthiness Directives affected are listed in Schedule 1, detailing each directive's name, number, and the nature of the changes or cancellations. The obligations imposed by this legislative instrument on the parties governed, including aircraft operators, maintenance organisations, and other relevant entities, include compliance with the re-issued Airworthiness Directives. These directives mandate specific actions such as inspections, modifications, replacements, and checks on various aircraft components to ensure airworthiness and safety. Compliance with these directives is critical, as they are designed to address identified safety issues or improvements in aircraft systems and structures (Schedule 1). Failure to comply with the requirements set out in these Airworthiness Directives may result in significant legal consequences. While the specific penalties are not detailed within the text of the Airworthiness Directives 2004, violations of airworthiness regulations generally can attract substantial penalties under the Civil Aviation Safety Regulations 1998. For example, non-compliance with safety directives can lead to civil penalties, including fines up to $275,000 for corporations and $55,000 for individuals, as well as potential criminal charges. These penalties underscore the importance of adhering to the directives to maintain the safety and airworthiness of the aircraft in question.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.