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
Extra EA-300 Series Aeroplanes
AD Name AD Number
Rudder Cable AD/EXTRA/1 Amdt 1
Wing Root Rib and Auxiliary Spar Attachment AD/EXTRA/2
Elevator Mass Balance AD/EXTRA/3
Air Inlet Screen AD/EXTRA/4
Upper Longeron Cutout Bridge AD/EXTRA/5 Amdt 1
Rudder Pedal Safety Control Stop AD/EXTRA/6
Upper Longeron at Horizontal Stabiliser AD/EXTRA/7
Fuel selector valve leakage AD/EXTRA/8
Bottom Fuselage Cover/Firewall Sealing AD/EXTRA/9
Overview
The Airworthiness Directives 2004, enacted under the authority of David Alan Villiers, the delegate of the Civil Aviation Safety Authority, aims to streamline and update the regulatory framework governing aircraft airworthiness in Australia. This legislative instrument was introduced to address the need for consistent and up-to-date airworthiness directives to ensure the safety and reliability of aircraft operating in Australia. By revoking and remaking certain directives, the legislation seeks to align the regulatory requirements with the latest industry standards and technological advancements, thereby enhancing the overall safety of air travel. The policy objective is to maintain and improve the airworthiness of aircraft through the enforcement of necessary and effective safety measures.
Scope and Application
The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, apply to specific aircraft types, namely the Extra EA-300 Series Aeroplanes, and encompass various aspects of their airworthiness, such as rudder cables, wing root rib attachments, and fuel selector valve leakage. The legislation is administered by the Civil Aviation Safety Authority (CASA) and applies to all aircraft registered in Australia or operated by Australian operators, irrespective of the aircraft's location. This regulatory framework is designed to ensure the safety and airworthiness of the specified aircraft models by mandating compliance with the detailed directives outlined in the Schedule. The legislative instrument includes the revocation of previously issued airworthiness directives and their re-enactment to ensure they reflect the most current safety standards. Each directive is reproduced verbatim from the latest published edition, ensuring that the regulations remain up-to-date and precise. The scope of the legislation is comprehensive, aiming to enhance safety through strict adherence to the specified airworthiness criteria for the Extra EA-300 Series Aeroplanes.
Key Provisions
The Airworthiness Directives 2004 legislative instrument primarily focuses on the revocation and remaking of certain Airworthiness Directives (AD) for Extra EA-300 series aeroplanes. Section (a) of the instrument revokes the specified ADs mentioned in Schedule 1, while section (b) mandates the remaking of each of these ADs as separate instruments, ensuring they appear in the latest published edition of the Directives. This legal instrument is an exercise of delegation under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998 by David Villiers, who acts as the delegate of the Civil Aviation Safety Authority.
The Airworthiness Directives 2004 impose specific obligations on the parties or entities governed by these ADs. Primarily, it requires compliance with the detailed provisions of each re-made AD, which include specific maintenance, repair, and inspection requirements to ensure the airworthiness of Extra EA-300 series aeroplanes. These obligations are critical in maintaining safety standards within the aviation sector, as they address various aspects of aircraft maintenance, such as rudder cables, wing root rib attachments, elevator mass balance, and fuel selector valve leakage, among others.
The Airworthiness Directives 2004 also outlines the consequences for non-compliance with the ADs. Failure to adhere to the specified requirements can result in civil or criminal penalties, depending on the severity of the breach. The maximum penalties are not explicitly stated in this legislative instrument, but they would generally align with the penalties outlined in the Civil Aviation Safety Regulations 1998. Non-compliance could potentially lead to enforcement actions by the Civil Aviation Safety Authority, which may include fines, legal proceedings, or other regulatory sanctions. Ensuring compliance is thus crucial for all parties involved, as it directly impacts the safety and regulatory compliance of the Extra EA-300 series aeroplanes.