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
Beechcraft 99 Series Aeroplanes
AD Name AD Number
Elevator Spar - Inspection and Modification AD/BEECH 99/1
Stabiliser Actuator - Replacement AD/BEECH 99/2
Wing Attach Fittings, Bolts and Nuts AD/BEECH 99/3
Vertical Stabiliser Main Spar AD/BEECH 99/4
MLG Drag Leg Lock Link Roll Pin AD/BEECH 99/5
Wing Structural Fatigue Limitations AD/BEECH 99/6
Pilot and Co-Pilot Chair Locking Mechanism AD/BEECH 99/7
Overview
The Airworthiness Directives 2004 is a legislative instrument enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, on 20 December 2004. This instrument operates under the authority granted by subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. Its primary function is to revoke certain existing Airworthiness Directives and simultaneously re-make them as separate instruments, ensuring that they remain consistent with the latest published editions. This approach was adopted to maintain the integrity and currency of airworthiness standards for specific aircraft, specifically the Beechcraft 99 Series Aeroplanes, which are subject to detailed inspection and modification requirements outlined in the attached directives.
The enacting body, the Civil Aviation Safety Authority, aimed to address the need for updated and precise regulatory standards to ensure the safety and airworthiness of these aircraft. By revoking and re-making the directives, the authority aimed to rectify any gaps or outdated provisions, thereby enhancing safety and compliance within the aviation sector. This legislative action underscores a commitment to rigorous safety standards and continuous improvement in aviation safety protocols.
Scope and Application
The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, pertains specifically to the airworthiness of Beechcraft 99 series aeroplanes. This legislative instrument, executed by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, focuses on the revocation and re-making of certain Airworthiness Directives, which are detailed in Schedule 1. These directives apply to the specified series of aeroplanes, targeting aspects such as elevator spar inspection and modification, stabiliser actuator replacement, and other structural components and limitations. The geographical reach of this legislation is inherently linked to the Australian jurisdiction, governed by the Commonwealth. The legislative instrument does not specify exclusions or exemptions but instead ensures that each airworthiness directive is re-made in the same form as it appears in the latest published edition. The authority to extend or restrict the application of these directives through subordinate instruments is implicitly granted, as the directives are subject to the overarching Civil Aviation Safety Regulations 1998.
Key Provisions
The primary operative sections of this legislative instrument are found in Section 1, which revokes the existing Airworthiness Directives listed in Schedule 1 and Section 2, which mandates the remaking of these directives as separate instruments, each attached to the legislation. This ensures that the updated directives are legally enforceable and reflect the most current safety standards. The remaking of these directives is intended to maintain consistency with the latest published editions, ensuring that all relevant stakeholders have access to the most up-to-date safety requirements for the specified aircraft.
The obligations imposed by this legislation primarily concern the entities governed by the Civil Aviation Safety Regulations 1998, including aircraft manufacturers, operators, and maintenance service providers. These entities are required to comply with the re-made Airworthiness Directives, which detail specific inspection, modification, and replacement requirements for various components of the Beechcraft 99 series aeroplanes. This includes directives such as AD/BEECH 99/1 for elevator spar inspection and modification, AD/BEECH 99/2 for stabiliser actuator replacement, and others listed in Schedule 1. Compliance with these directives is critical to maintaining the airworthiness of the aircraft and ensuring passenger safety.
Failure to adhere to the provisions of these Airworthiness Directives can result in significant legal and financial consequences. The legislation does not explicitly outline specific offences or penalties within the text itself, but breaches of Airworthiness Directives can typically result in enforcement actions under the Civil Aviation Safety Regulations 1998. These actions may include fines, suspension or revocation of airworthiness certificates, and other regulatory penalties. The maximum penalties for such breaches can vary, but they are generally substantial, reflecting the importance of adhering to airworthiness standards to prevent accidents and ensure the safety of all persons on board.