AD/CL-600/60 - Flap Vane Brackets

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Legislation au F2006B08624 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF 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 39.1 (1) of CAR 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-600/60 Flap Vane Brackets 13/2002 DM

 

Applicability: Model CL-600-2B16 aircraft, serial numbers 5301 through 5499.

 

Requirement: Action in accordance with the requirements of Transport Canada AD CF-2002-37.

 

Note: Bombardier Alert Service Bulletin ASB A604-27-007 Revision 1 refers.

 

Compliance: As specified in the Requirement document, with a revised effective date of 30 October 2002.

 

This Airworthiness Directive becomes effective on 30 October 2002.

 

Background: The aircraft assembly procedures used when installing the flap actuator beam vane brackets, referred to as the flap vane brackets, may have resulted in gaps between flap vane brackets and the adjacent lower skin and between the flap vane brackets and the vane actuator beam. This condition could result in the premature development of cracks in the flap vane brackets, and if not corrected, lead to in- flight loss of the flap vane and subsequent reduced controllability of the aircraft.


 

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 24 October 2002

 

 

 

 

 

 

 

 

 

 

 

 

The above AD is notified in the Commonwealth of Australia Gazette on 30 October 2002.

 


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Overview

The Civil Aviation Regulations 1998 (CAR 1998), under the jurisdiction of the Civil Aviation Safety Authority (CASA), were enacted to ensure the safety of civil aviation in Australia. One of the key provisions of these regulations is the issuance of Airworthiness Directives (ADs), which address specific safety concerns identified in aircraft operations. The AD/CL-600/60 issued on 24 October 2002, for example, targets Bombardier (Canadair) CL-600 (Challenger) Series aeroplanes with serial numbers 5301 through 5499. This directive aims to rectify a manufacturing defect in the flap vane brackets that could lead to structural failure and compromised flight control. The AD mandates corrective actions as outlined by Transport Canada's AD CF-2002-37, reflecting an international collaborative approach to aviation safety, and was made effective from 30 October 2002.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 Airworthiness Directives, addresses safety concerns and mandates corrective actions to ensure the continued safe operation of aircraft within Australia. This Airworthiness Directive applies to Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes, specifically those with serial numbers ranging from 5301 to 5499. The directive mandates that specific maintenance actions be undertaken to rectify potential unsafe conditions related to the flap vane brackets of the affected aircraft. These actions must be in accordance with the requirements outlined by Transport Canada AD CF-2002-37 and should be completed by 30 October 2002, as specified in the compliance section of the directive. The AD extends to all operators of the specified aircraft within the Commonwealth of Australia, ensuring that the safety standards are uniformly applied across the jurisdiction. This directive does not explicitly exclude any entities or circumstances, meaning that it applies broadly to all relevant aircraft operators unless otherwise specified through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998 (CAR 1998) under the authority of the Civil Aviation Safety Authority (CASA) have issued an Airworthiness Directive (AD) concerning Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes, specifically model CL-600-2B16, with serial numbers 5301 through 5499. This AD mandates certain actions to rectify unsafe conditions identified with the flap vane brackets of the affected aircraft (section 1). The directive is grounded on the findings that assembly procedures used during the installation of the flap actuator beam vane brackets may have caused gaps between these brackets and the adjacent lower skin, as well as between the brackets and the vane actuator beam. Such conditions could lead to premature cracking of the flap vane brackets, potentially resulting in in-flight loss of the flap vane and decreased aircraft controllability. The AD requires operators of the specified aircraft to perform corrective actions as detailed in Transport Canada AD CF-2002-37, referencing Bombardier Alert Service Bulletin ASB A604-27-007 Revision 1. These actions are to be carried out under the conditions and instructions outlined in the AD, ensuring the safety and airworthiness of the aircraft. Compliance with these directives must be achieved by the specified revised effective date, which is 30 October 2002, as stated in the compliance section of the AD. The AD imposes clear obligations on the aircraft operators and manufacturers to ensure the airworthiness of the affected aircraft. Operators must follow the prescribed corrective actions detailed in Transport Canada's AD and Bombardier's Alert Service Bulletin. Failure to adhere to these requirements may result in the aircraft not meeting the necessary safety standards, leading to potential operational bans or other regulatory actions by CASA. The AD serves as a regulatory mandate that prioritises the safety and operational integrity of the aircraft in question. Violating the provisions of this AD could have serious legal and operational consequences. While the specific penalties for non-compliance are not detailed in the AD, under CAR 1998, non-compliance with ADs can lead to enforcement actions by CASA. These actions may include fines, suspension or revocation of airworthiness certificates, and potentially criminal charges for operators or manufacturers who fail to comply with safety directives. The severity of the penalties reflects the importance of adhering to the AD to prevent unsafe conditions that could endanger flight safety.

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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.