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

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Legislation au F2006B08628 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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

 

AD/CL-600/8 Landing Gear Electrical Harnesses - Modification 3/83

Applicability: All model CL600 aeroplanes as per requirement document. Document: Canadair Challenger SB No. 600-0159.

Compliance: Before issue of Australian Certificate of Airworthiness.

 

Background: To prevent landing gear proximity switches from being affected by electromagnetic interference. This may result in loss of aircraft brakes while landing and taxiing with anti-skid system in use.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B08628, address a critical safety concern involving Bombardier (Canadair) CL-600 (Challenger) Series aeroplanes. Specifically, Airworthiness Directive AD/CL-600/8 mandates a modification to the landing gear electrical harnesses to prevent potential failure of landing gear proximity switches due to electromagnetic interference. This interference can lead to the loss of aircraft brakes during landing and taxiing, particularly when the anti-skid system is operational. Enacted by the Australian Parliament, the directive aims to ensure the safety and reliability of CL600 aeroplanes within the Australian aviation sector by requiring compliance before the issuance of an Australian Certificate of Airworthiness. This legislative measure underscores the importance of addressing electromagnetic interference to safeguard against critical operational failures.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the application of Airworthiness Directives to ensure the safety of aircraft operating within Australian airspace. This particular directive, AD/CL-600/8, applies to all Bombardier (Canadair) CL-600 (Challenger) Series aeroplanes as outlined in the requirement document, Canadair Challenger SB No. 600-0159. The directive necessitates compliance before the issuance of an Australian Certificate of Airworthiness, underscoring the importance of this safety measure. Its purpose is to mitigate risks associated with landing gear proximity switches being affected by electromagnetic interference, which could lead to significant safety hazards such as the loss of aircraft brakes during landing and taxiing with the anti-skid system in operation. The directive's scope is confined to the specified model of aeroplanes, and while it is a Commonwealth regulation, it ensures compliance with national and international safety standards.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Schedule of Airworthiness Directives, address the safety requirements for Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes. Section AD/CL-600/8 pertains to the modification of landing gear electrical harnesses (AD/CL-600/8). This directive applies to all model CL600 aeroplanes, as detailed in the requirement document, Canadair Challenger SB No. 600-0159. Compliance with this directive is mandatory before the issue of an Australian Certificate of Airworthiness. The directive aims to prevent landing gear proximity switches from being affected by electromagnetic interference, which could lead to the loss of aircraft brakes during landing and taxiing, particularly when the anti-skid system is in use. The obligations imposed by this regulation require that the specified modifications to the landing gear electrical harnesses must be implemented to ensure the aircraft's safety. Operators of Bombardier (Canadair) CL-600 aeroplanes must adhere to the detailed instructions provided in the Canadair Challenger SB No. 600-0159. This includes the proper installation and testing of the modified electrical harnesses to mitigate any risk of electromagnetic interference affecting the landing gear proximity switches. These modifications are critical to maintaining the airworthiness of the aircraft and ensuring the safety of all passengers and crew on board. Failure to comply with the requirements set forth in this airworthiness directive may result in significant civil and criminal consequences. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions against operators who do not adhere to these safety directives. In the event of non-compliance, CASA can impose penalties, including fines and the suspension or revocation of the aircraft's Certificate of Airworthiness. The maximum penalties for such breaches are determined by the severity of the non-compliance and can lead to substantial financial and operational repercussions for the affected parties. Ensuring strict adherence to these directives is therefore essential to avoid these adverse outcomes.

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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.