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
C.A.C. CA-18 (Mustang) Series Aeroplanes
AD Name AD Number
Wing Front Spar AD/MUSTANG/1 Amdt 2
Main Landing Gear Pivot Shaft - Inspection AD/MUSTANG/2 Amdt 1
Overview
The Airworthiness Directives 2004, enacted on 20 December 2004, were introduced to address the need for updated and consolidated regulations regarding airworthiness directives for certain aircraft. The Civil Aviation Safety Authority (CASA) issued these directives as a delegate under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The policy objective of this legislative instrument was to revoke previously issued directives and remake them in their latest form, ensuring that the most current safety standards and requirements are uniformly applied to the specified aircraft, namely C.A.C CA-18 (Mustang) Series Aeroplanes. This initiative aimed to enhance the safety and regulatory compliance of these aircraft, aligning with the overarching goal of maintaining high standards in aviation safety.
Each directive was remade in the same form as it appeared in the latest published edition, reflecting the commitment to providing clear, up-to-date, and precise instructions to aircraft operators and maintenance personnel. By consolidating and updating these directives, the legislation aimed to address any gaps or inconsistencies that may have existed in previous regulatory frameworks, thereby reinforcing the safety protocols and operational standards for the specified aircraft within Australia’s aviation sector.
Scope and Application
The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, applies to all entities and persons involved in the operation, maintenance, and airworthiness certification of aircraft, specifically targeting the maintenance and inspection requirements of the C.A.C CA-18 (Mustang) Series Aeroplanes. This legislation extends to all Commonwealth jurisdictions within Australia and is administered by the Civil Aviation Safety Authority (CASA). The Act includes the revocation and remaking of specific Airworthiness Directives aimed at ensuring that aircraft meet necessary safety standards. Notably, the directives in question pertain to critical components such as the wing front spar and the main landing gear pivot shaft, and are designed to address potential safety issues through required inspections and maintenance actions. There are no stated exclusions or exemptions in this legislative instrument, implying that all relevant aircraft and operators must comply with the directives as specified. The scope of the Act is further extended through subordinate instruments that may detail specific procedures and compliance requirements for the directives.
Key Provisions
The Airworthiness Directives 2004, made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), primarily consist of two main provisions. Firstly, section 2 of the legislation revokes the existing Airworthiness Directives listed in Schedule 1 (subsection 2(a)). Secondly, the Act re-issues each of these directives as separate instruments, with each directive attached to the legislation (subsection 2(b)). The directives are reproduced in their entirety as they appear in the latest published edition.
These Airworthiness Directives impose specific obligations on the holders and operators of the aircraft types covered by the directives. For example, they require compliance with specified maintenance and inspection procedures to ensure the continued airworthiness of the aircraft. This includes adherence to detailed technical instructions for tasks such as inspecting and repairing the wing front spar and the main landing gear pivot shaft. These obligations are designed to maintain high safety standards in the operation of these aircraft.
Failure to comply with the requirements set out in these Airworthiness Directives can result in significant consequences. Under the Civil Aviation Safety Regulations 1998, breaches of these directives can lead to enforcement actions by CASA. The specific consequences may include fines, suspension or revocation of airworthiness certificates, and in severe cases, criminal charges. The maximum penalties for non-compliance with airworthiness regulations can be substantial, reflecting the critical nature of ensuring aircraft safety. The exact penalties will depend on the nature and severity of the breach, as well as any previous history of non-compliance by the offender.