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
Pacific Aerospace Corporation Cresco Series Aeroplanes
AD Name AD Number
Nose Landing Gear Cylinder Assembly AD/CRESCO/1
Wing Spar Web AD/CRESCO/2
Elevator Tip Rib AD/CRESCO/3
Rudder Top Hinge AD/CRESCO/4 Amdt 1
Aileron Control Cables AD/CRESCO/5
Fin Forward Attachment Fitting AD/CRESCO/6
Engine Mount Structure AD/CRESCO/7
Horizontal Stabiliser Main Spar Top Cap AD/CRESCO/8
Overview
The Airworthiness Directives 2004, enacted by David Alan Villiers, delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, aimed to address the need for the continuous and accurate regulation of airworthiness standards for specific aircraft models. This legislative instrument revokes and re-makes existing Airworthiness Directives concerning the Pacific Aerospace Corporation Cresco Series Aeroplanes, ensuring the directives are updated and consistent with the latest published editions. The objective of these directives is to enhance the safety and reliability of these aircraft by mandating specific maintenance and inspection requirements for identified components such as the nose landing gear cylinder assembly, wing spar web, and other critical parts. The enactment by the Civil Aviation Safety Authority underscores the commitment to maintaining stringent airworthiness standards to protect public safety in civil aviation.
Scope and Application
The Airworthiness Directives 2004 is a legislative instrument issued by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority (CASA) under the Civil Aviation Safety Regulations 1998. The Act revokes and remakes several airworthiness directives that pertain specifically to the Pacific Aerospace Corporation Cresco Series Aeroplanes, addressing various components such as the nose landing gear cylinder assembly, wing spar web, elevator tip rib, rudder top hinge, aileron control cables, fin forward attachment fitting, engine mount structure, and horizontal stabiliser main spar top cap. These directives are aimed at ensuring the ongoing airworthiness of these aircraft by mandating specific maintenance, repair, and inspection procedures. The scope of this legislation is geographically and jurisdictionally limited to the Commonwealth of Australia, applying directly to the specified aircraft and their owners, operators, and maintenance personnel. The Act does not explicitly detail exclusions, exemptions, or thresholds, but it is understood that these would be addressed within the detailed provisions of each re-made airworthiness directive. Additionally, the Act extends its application through subordinate instruments, which are the specific airworthiness directives attached and re-made as separate instruments in the legislation.
Key Provisions
The Airworthiness Directives 2004, made under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, involve the revocation of certain existing Airworthiness Directives and their re-making as separate instruments (section 1). Specifically, these directives relate to the Pacific Aerospace Corporation Cresco Series Aeroplanes and cover a range of structural and mechanical components, including the nose landing gear cylinder assembly, wing spar web, elevator tip rib, rudder top hinge, aileron control cables, fin forward attachment fitting, engine mount structure, and horizontal stabiliser main spar top cap (Schedule 1).
These provisions mandate that the specified Airworthiness Directives be revoked and subsequently re-made as individual instruments (section 1(a) and (b)). This process ensures that each directive is updated and presented in its latest form, aligning with the most recent published editions. This approach helps maintain clarity and accuracy in the regulatory framework governing aircraft airworthiness, ensuring that all stakeholders are operating under the most current and relevant standards.
The obligations imposed by these directives are primarily directed towards aircraft manufacturers, operators, and maintenance providers. They must adhere to the specific requirements outlined in each re-made Airworthiness Directive, ensuring that the aircraft components and systems comply with the latest safety and maintenance standards. This includes conducting necessary inspections, repairs, or modifications to the specified parts of the Pacific Aerospace Corporation Cresco Series Aeroplanes to maintain their airworthiness (section 1).
Failure to comply with these Airworthiness Directives can result in serious consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance may lead to civil penalties, including fines. The maximum penalties can vary, but they are designed to enforce strict adherence to safety regulations. Additionally, operators found in breach of these directives may face enforcement actions, which can include grounding of the affected aircraft until the required actions are completed, thereby ensuring that safety is not compromised.