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
CAP Aviation (Akrotech and Mudry) CAP 232 Series Aeroplanes
AD Name AD Number
Starter Relay AD/CAP 232/1
Control Stick Cover AD/CAP 232/2
Trim Control Tab Axis AD/CAP 232/3 Amdt 3
Engine Mount AD/CAP 232/4
Stick Adjustable Root Stops AD/CAP 232/5
Brake Master Cylinder Attachment Pin AD/CAP 232/6
Aluminium Control Rods AD/CAP 232/7
Flight Envelope AD/CAP 232/8
Elevator Lever Control Rod AD/CAP 232/9
Aileron Hinge Rod End Bearings AD/CAP 232/10
Rudder Lower Support AD/CAP 232/11
Overview
The Airworthiness Directives 2004 is a legislative instrument enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), under the authority of the Civil Aviation Safety Regulations 1998. This instrument was introduced to address the need for updated and consolidated airworthiness directives, ensuring that they remain current and consistent with the latest published editions. The primary objective of this legislative instrument is to revoke existing airworthiness directives and remake them as separate instruments to maintain regulatory compliance and safety standards in civil aviation. Each airworthiness directive in the Schedule is being remade in exactly the same form as it appears in the latest published edition, thereby ensuring that the directives remain effective and relevant.
The Civil Aviation Safety Authority, through this legislative instrument, aims to uphold the highest standards of aviation safety by providing clear, updated, and enforceable directives. This approach ensures that all stakeholders, including aircraft operators and maintenance personnel, have access to the most current regulatory requirements, thereby reducing the risk of non-compliance and enhancing overall aviation safety. The instrument is a practical step in the ongoing effort to maintain the safety and airworthiness of aircraft operating within Australia’s jurisdiction.
Scope and Application
The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, apply to specific types of aircraft and their operators within Australia. This legislative instrument concerns the revocation and remaking of various Airworthiness Directives, as listed in Schedule 1, which detail technical specifications and safety requirements for certain aircraft models, including those manufactured by Akrotech and Mudry. The application of these directives is national in scope, affecting all entities and persons involved in the operation and maintenance of the specified aircraft within Australia. The regulations are designed to ensure that the airworthiness of these aircraft is maintained to the highest safety standards by requiring adherence to the stipulated directives. The revocation and remaking process ensure that the latest safety standards are applied consistently across the industry. Any exclusions or exemptions from these directives are not specified in the text, but they are subject to the broader regulatory framework of the Civil Aviation Safety Regulations 1998. The application of these directives may be extended or restricted through subordinate instruments, ensuring that they are kept up-to-date with evolving safety standards and technological advancements.
Key Provisions
The primary operative sections of the Airworthiness Directives 2004 focus on the revocation and remaking of various airworthiness directives related to CAP Aviation (Akrotech and Mudry) CAP 232 series aeroplanes, as outlined in Schedule 1. Specifically, sections (a) and (b) of the legislation revoke the previously issued airworthiness directives and subsequently re-make each one as a separate instrument. The directives cover a range of safety-critical components and modifications, including the starter relay (AD/CAP 232/1), control stick cover (AD/CAP 232/2), trim control tab axis (AD/CAP 232/3), engine mount (AD/CAP 232/4), stick adjustable root stops (AD/CAP 232/5), brake master cylinder attachment pin (AD/CAP 232/6), aluminium control rods (AD/CAP 232/7), flight envelope (AD/CAP 232/8), elevator lever control rod (AD/CAP 232/9), aileron hinge rod end bearings (AD/CAP 232/10), and rudder lower support (AD/CAP 232/11).
The Act imposes specific obligations on the parties and entities it governs, particularly those involved in the operation, maintenance, and certification of CAP 232 series aeroplanes. These obligations include compliance with the detailed requirements and modifications outlined in each re-made airworthiness directive. Operators and maintenance personnel must adhere to the specified procedures and standards for the installation, inspection, and repair of the affected components to ensure the continued airworthiness and safety of the aircraft. This involves conducting regular checks, following prescribed maintenance schedules, and implementing necessary modifications as directed by the Civil Aviation Safety Authority (CASA).
Failure to comply with the provisions of these airworthiness directives can result in significant legal and safety consequences. The legislation does not explicitly state specific offences or penalties within the text provided, but non-compliance with airworthiness directives can generally lead to enforcement actions by CASA. Such actions may include the issuance of compliance orders, fines, suspension or revocation of airworthiness certificates, and in severe cases, criminal charges for individuals or entities responsible for non-compliance. The severity of the penalties often depends on the nature and extent of the non-compliance, as well as any resulting safety incidents or accidents.