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
Dornier DO-27 Series Aeroplanes
AD Name AD Number
Steel Band Tensioners - Replacement AD/DO-27/1
Tailplane Front Spar - Modification AD/DO-27/2
Elevator Hinge Bracket - Inspection AD/DO-27/3
Flap Control Lever - Modification AD/DO-27/4
Fuel, Oil and Manifold Pressure Flexible Hoses - Replacement AD/DO-27/5
Fuel and Oil Hose Assemblies - Inspection AD/DO-27/6
Outboard Elevator Hinge Fitting - Inspection AD/DO-27/7
Wing Fuselage Attachment - Inspection AD/DO-27/8
Front Seat Restraint Installation - Modification AD/DO-27/9
Stall Warning System - Installation AD/DO-27/10
Wing Flap Position Selector AD/DO-27/11
Horizontal Tail Bearing Fitting Rivets AD/DO-27/12
Overview
The Airworthiness Directives 2004, enacted on 20 December 2004, are a legislative instrument issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under the authority of subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary purpose of this legislative instrument was to revoke and re-make specific Airworthiness Directives for the Dornier DO-27 Series Aeroplanes, ensuring that these directives are updated to reflect the latest published editions. Each directive, detailed in Schedule 1, has been re-made in exactly the same form as it appears in the most recent publication. This legislative action aimed to maintain the safety and airworthiness of aircraft by addressing specific maintenance and modification requirements as outlined in the individual directives.
The Civil Aviation Safety Authority, through its delegate, sought to address potential gaps in the airworthiness standards for the Dornier DO-27 Series Aeroplanes by ensuring the directives are current and enforceable. This legislative instrument was enacted to provide a clear and updated framework for the maintenance and operation of these aircraft, thereby contributing to the overall safety of civil aviation in Australia.
Scope and Application
The Airworthiness Directives 2004, issued by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, pertains to specific aircraft models, particularly the Dornier DO-27 Series Aeroplanes, and establishes or modifies directives that address various safety and airworthiness concerns. This legislative instrument revokes existing directives and remakes them in the same form as they appear in the latest published edition. The directives apply to all individuals, entities, and industries involved in the operation, maintenance, and management of the affected aircraft models. The scope of these directives extends across the Commonwealth of Australia, ensuring uniform safety standards and regulatory compliance throughout the nation. Notably, the legislation does not specify any exclusions or exemptions, indicating that the directives apply universally to the relevant aircraft types. The Civil Aviation Safety Authority retains the ability to extend or restrict the application of these directives through subordinate instruments, ensuring flexibility in addressing evolving safety issues.
Key Provisions
The main operative sections of this legislation involve the revocation and remaking of various Airworthiness Directives for the Dornier DO-27 Series Aeroplanes, as listed in Schedule 1 (sections 1(a) and 1(b)). The Civil Aviation Safety Authority delegate, David Alan Villiers, has the authority to revoke existing directives and replace them with new ones that mirror the latest published versions. The specific directives mentioned include modifications, inspections, and installations related to the aircraft's components such as steel band tensioners, tailplane front spars, elevator hinge brackets, and other critical parts (Schedule 1). These directives aim to ensure the safety and airworthiness of the aircraft by mandating specific actions to be taken.
The obligations and requirements imposed by this Act on the parties or entities it governs are primarily centred on compliance with the newly remade Airworthiness Directives. Operators and owners of Dornier DO-27 Series Aeroplanes must adhere to the specified modifications, inspections, and installations detailed in the directives. This includes ensuring that components such as fuel, oil, and manifold pressure hoses are replaced or inspected as required, that critical fittings and restraints are installed or modified correctly, and that systems like the stall warning system are implemented. Failure to comply with these directives can result in the aircraft being deemed unairworthy, which could lead to grounding and potential legal consequences.
There are potential consequences and penalties for breaches of these Airworthiness Directives. Although the specific penalties are not detailed within the text of the legislative instrument itself, violations of airworthiness directives generally can result in significant civil or criminal penalties under the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988. These may include substantial fines, enforcement actions by the Civil Aviation Safety Authority, and in severe cases, criminal charges leading to imprisonment. The severity of the penalty often depends on the nature and extent of the breach, the potential risk to safety posed by the non-compliance, and whether it was deliberate or due to negligence.