Airworthiness Directives 2004 - Revocation and Remaking - Percival Proctor Series Aeroplanes

Overview

The Airworthiness Directives 2004, enacted on 20 December 2004, were introduced to address the need for updated and consolidated airworthiness directives for specific aircraft types. This legislative instrument was made by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under the authority delegated by the Civil Aviation Safety Regulations 1998. The primary policy objective of these directives is to ensure that certain types of aircraft, in this case, the Percival Proctor Series Aeroplanes, meet the necessary safety standards by specifying required inspections and modifications. Each airworthiness directive is re-made in the same form as appears in the latest published edition to ensure consistency and compliance with current safety regulations. The directives listed in the schedule aim to cover various aspects of aircraft maintenance and safety, including wing rib inspections, fuselage modifications, spar modifications, and control cable adjustments, among others. By revoking and remaking these directives, the Civil Aviation Safety Authority seeks to maintain a high standard of airworthiness for these aircraft, ensuring they are safe for operation. The detailed specifications and requirements are outlined in the attached airworthiness directives, which are reproduced exactly as they appear in the latest published edition.

Scope and Application

The Airworthiness Directives 2004, as promulgated by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, applies specifically to the maintenance and operation of Percival Proctor Series Aeroplanes. This legislation is part of a broader regulatory framework aimed at ensuring the safety and airworthiness of aircraft within Australia. It affects all individuals and entities involved in the maintenance, operation, and certification of these aircraft, including aircraft manufacturers, maintenance providers, and operators. The geographic reach of this Act is nationwide, encompassing all states and territories within Australia. The directives, as outlined in Schedule 1, cover a range of specific maintenance actions and inspections that must be conducted on Percival Proctor Series Aeroplanes to comply with airworthiness standards. This includes detailed requirements for the inspection and modification of various aircraft components such as the wing rib to aileron spar joint, rear fuselage drain holes, control cable pulleys, and fuel tank vents, among others. Each Airworthiness Directive is meticulously remade to align with the latest published editions, ensuring that all requirements remain current and comprehensive. The application of this Act extends through subordinate instruments, which may further detail specific procedures, compliance timelines, and penalties for non-compliance. Notably, this legislation does not specify any exclusions or exemptions, indicating that all Percival Proctor Series Aeroplanes operating within Australia must adhere to the outlined directives without exception.

Key Provisions

The primary operative sections of this legislative instrument (F2006B07941) involve the revocation and remaking of specific Airworthiness Directives (ADs) for the Percival Proctor Series Aeroplanes, as detailed in Schedule 1. Section 1(a) revokes the existing ADs, while section 1(b) re-makes these ADs as separate instruments, maintaining their exact form as per the latest published edition. The ADs being addressed include various modifications and inspections related to different parts of the aircraft, such as the wing rib to aileron spar joint, rear fuselage drain holes, control cable pulley, fuel tank vent, and more. Each directive specifies detailed requirements and procedures that must be followed to ensure the airworthiness of the aircraft. The obligations and requirements imposed by this Act primarily focus on compliance with the re-made ADs. These directives mandate specific actions to be taken regarding aircraft maintenance, modifications, and inspections. For instance, AD/PROCTOR/1 requires an inspection of the wing rib to aileron spar joint, while AD/PROCTOR/2 mandates a modification to the rear fuselage drain holes. Operators and owners of Percival Proctor Series Aeroplanes must adhere to these directives to maintain the airworthiness of their aircraft. Compliance ensures that all aircraft meet safety standards and regulatory requirements, which is crucial for the safety of passengers and crew. Failure to comply with the provisions of the re-made ADs may result in various consequences. Although specific penalties are not detailed in the text, non-compliance generally leads to enforcement actions under the Civil Aviation Safety Regulations 1998. This may include fines, enforcement notices, or more severe measures if the non-compliance poses a significant risk to safety. The Civil Aviation Safety Authority (CASA) has the authority to take action against non-compliant parties, ensuring that all aircraft meet the necessary safety standards. It is imperative for aircraft operators and owners to understand and adhere to the directives to avoid any legal repercussions or safety hazards.