Airworthiness Directives 2004 - Revocation and Remaking - Extra EA-300 Series Aeroplanes

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07863 In force Legislative Instrument

Legislation content

 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.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Repeal & Amendment
Regulatory Standards

Interactions

Authorises

All Versions

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.