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
Avions Mudry Cap Series Aeroplanes
AD Name AD Number
Engine Mount Welds AD/CAP 10/1
Fuel System AD/CAP 10/2
Main Wing Spar - CANCELLED AD/CAP 10/3 Amdt 2
Flight Limitations AD/CAP 10/4 Amdt 3
Front Tank Support Strap AD/CAP 10/5
Lower Torque Link Attachment Weld AD/CAP 10/6
Rudder Lower Support AD/CAP 10/7
Aileron Bellcrank Bolts AD/CAP 10/8
Overview
The Airworthiness Directives 2004 is a legislative instrument made under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998 by David Alan Villiers, a delegate of the Civil Aviation Safety Authority. This legislative instrument revokes and re-makes various airworthiness directives that pertain to specific aircraft models, including the Avions Mudry Cap Series Aeroplanes. The primary purpose of this legislation is to ensure that the airworthiness directives, which are critical for maintaining the safety and airworthiness of aircraft, are current and accurately reflect the latest safety requirements and regulatory standards. By re-making these directives, the Civil Aviation Safety Authority aims to provide clear, updated, and enforceable safety standards to address any identified safety issues or risks related to the specified aircraft models. The re-made directives are intended to be identical to those in the latest published edition, ensuring consistency and reliability in safety compliance.
Scope and Application
The Airworthiness Directives 2004, issued by the delegate of the Civil Aviation Safety Authority, David Alan Villiers, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, pertains to the revocation and remaking of specific Airworthiness Directives for certain aircraft models, namely the Avions Mudry Cap Series Aeroplanes. These directives cover various aspects of aircraft maintenance and operation, including engine mount welds, fuel system, flight limitations, and structural components such as wing spars, tank support straps, torque link attachments, rudder lower supports, and aileron bellcrank bolts. The legislative instrument applies to aircraft operators, maintenance providers, and other entities involved in the aviation industry, ensuring compliance with the specified safety standards. The scope of these directives is national, encompassing all aircraft of the mentioned series registered in Australia. Notably, this legislative instrument does not introduce new directives but rather re-makes existing ones in their latest form, ensuring consistency and clarity for industry participants. The directives apply across the Commonwealth, providing a unified regulatory framework for the maintenance and operation of these aircraft within Australia.
Key Provisions
The primary operative sections of the Airworthiness Directives 2004 (F2006B07730) involve the revocation and remaking of specific Airworthiness Directives, which are detailed in Schedule 1 of the legislative instrument. Section 1 revokes the listed Airworthiness Directives, while section 2 remakes these directives as separate instruments, ensuring they are re-made in the same form as the latest published editions. The Schedule 1 lists specific directives pertaining to Mudry Cap Series Aeroplanes, detailing directives such as Engine Mount Welds (AD/CAP 10/1), Fuel System (AD/CAP 10/2), and others, including their respective amendment numbers and the specifics of what each directive covers.
The Act imposes several obligations and requirements on the parties and entities it governs. Firstly, it mandates the remaking of the revoked directives to maintain compliance with the latest safety standards and regulatory requirements. This ensures that the aviation industry adheres to current safety protocols and that all aircraft within the scope of these directives are maintained to the specified standards. Additionally, the Act requires that any party involved in the manufacturing, maintenance, or operation of the affected aircraft must comply with the re-made directives, ensuring that all necessary safety measures are implemented and adhered to.
Failure to comply with the provisions of the Airworthiness Directives 2004 can result in significant consequences. The Act stipulates that any breach of these directives may lead to enforcement actions, including the imposition of penalties. For instance, Section 39.001 (1) of the Civil Aviation Safety Regulations 1998, under which this legislative instrument is made, provides for the imposition of fines and other penalties for non-compliance. The exact penalties can vary depending on the nature and severity of the breach, but they can include substantial financial penalties and potential criminal charges for more serious violations. This ensures that the regulatory framework is robust and that there are clear deterrents against non-compliance.