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-600/13
Amdt 1
Brake Control Push-Pull Cable 11/88
Applicability: Model CL-600-1A11 serial numbers 1004 through 1066, 1068 through 1071, and
1073 through 1083.
Requirement: Action in accordance with Canadair Challenger SB No A600-0254 Revision 1.
Compliance: Inspection to be accomplished prior to the issue of a Certificate of Airworthiness and thereafter at intervals not exceeding 150 landings, until modified in accordance with the Requirement Document.
Background: This Amendment is raised to reflect a revision of the manufacturer’s document which introduces a modification to cancel the inspection requirement.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, are a crucial set of rules designed to maintain and enhance aviation safety across Australia. The specific legislative instrument F2006B08573 addresses a gap in ensuring the safety of Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes by introducing Airworthiness Directives. This particular directive, AD/CL-600/13 Amendment 1, pertains to the brake control push-pull cable of certain Challenger models, specifically those with serial numbers ranging from 1004 through 1066, 1068 through 1071, and 1073 through 1083. The directive aims to ensure that these aircraft meet the required safety standards by mandating compliance with the Canadair Challenger Service Bulletin No A600-0254 Revision 1, which now includes the cancellation of a previous inspection requirement. The policy objective is to maintain airworthiness and safety in line with the latest manufacturer guidance, ensuring that any necessary actions are taken prior to the issuance of a Certificate of Airworthiness and at intervals not exceeding 150 landings.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, governs the application of AD/CL-600/13 Amendment 1, which pertains to the Bombardier (Canadair) CL-600 (Challenger) series aeroplanes. This legislation applies to aircraft model CL-600-1A11 with serial numbers ranging from 1004 through 1066, 1068 through 1071, and 1073 through 1083. The Act mandates actions in accordance with Canadair Challenger Service Bulletin No A600-0254 Revision 1, requiring inspections to be conducted before issuing a Certificate of Airworthiness and subsequently at intervals not exceeding 150 landings until modifications are made as per the Requirement Document. This regulation extends across the Commonwealth of Australia, ensuring that the safety standards are uniformly enforced nationwide. There are no stated exclusions or exemptions in the text, and the scope of the directive is limited to the specified serial numbers of the aircraft model mentioned. The regulations may be further extended or restricted through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The main sections of the Civil Aviation Regulations 1998, Part 39 - 105, specifically addressing the Airworthiness Directive (AD) for the Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes, are AD/CL-600/13 Amendment 1. This amendment pertains to the brake control push-pull cable and was issued on 11 August 1988. According to section 39 - 105, the AD applies to specific model CL-600-1A11 serial numbers ranging from 1004 to 1066, 1068 to 1071, and 1073 to 1083. The directive requires actions to be taken in accordance with Canadair Challenger Service Bulletin (SB) No A600-0254 Revision 1, which includes specific instructions for maintaining or modifying the brake control push-pull cable. The requirement necessitates that an inspection of the brake control push-pull cable be conducted before issuing a Certificate of Airworthiness and subsequently at intervals not exceeding 150 landings, until the modification is implemented as per the requirement document.
This legislative instrument imposes several obligations and requirements on the entities it governs. Primarily, it mandates that the specified aircraft models undergo an inspection of the brake control push-pull cable before receiving a Certificate of Airworthiness. Furthermore, the regulation requires that these inspections be performed at intervals not exceeding 150 landings until the aircraft are modified in accordance with the specified requirements. This ensures that the safety and airworthiness standards are consistently met. The regulation also mandates compliance with the modifications outlined in the Canadair Challenger SB No A600-0254 Revision 1, which includes detailed procedures for inspecting and potentially replacing the brake control push-pull cable to mitigate any safety risks.
The breach of these requirements can lead to serious consequences, both civil and criminal. While the Civil Aviation Regulations 1998 do not explicitly detail penalties for non-compliance with Airworthiness Directives, failure to adhere to these directives can result in significant civil penalties, including fines and potential grounding of the aircraft. Moreover, the safety implications of non-compliance can result in criminal charges under the Civil Aviation Act 1988, potentially leading to imprisonment. The severity of the penalties underscores the importance of strictly adhering to the requirements set forth in the AD/CL-600/13 Amendment 1 to ensure the continued airworthiness and safety of the Bombardier (Canadair) CL-600 (Challenger) Series Aeroplanes.