Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-42 (Cheyenne III) Series Aeroplanes

Overview

The Airworthiness Directives 2004 was enacted to address the need for updated regulations governing the airworthiness of specific aircraft models. This legislative instrument was introduced by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority, pursuant to subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The purpose of this instrument was to revoke existing airworthiness directives related to Piper PA-42 (Cheyenne III) series aeroplanes and to re-make them as separate instruments in their latest published form. The objective is to ensure that all airworthiness directives are current and accurately reflect the most recent safety standards, thereby enhancing the overall safety and reliability of the specified aircraft models within Australia's aviation sector.

Scope and Application

The Airworthiness Directives 2004, as re-made by David Alan Villiers, delegate of the Civil Aviation Safety Authority, pertain specifically to Piper PA-42 (Cheyenne III) Series Aeroplanes. These directives apply to aircraft operators, maintenance personnel, and any entity involved in the maintenance or operation of these aeroplanes. The legislation is Commonwealth in nature, operating under the Civil Aviation Safety Regulations 1998. Each Airworthiness Directive, detailed in the Schedule 1, has been re-made to ensure compliance with current safety standards, covering aspects such as powerplant firewall inspections, nacelle fuel tank check valve installation, and various structural and operational checks. The directives do not explicitly state exclusions or exemptions, but they do set specific compliance requirements for certain aircraft components and operational procedures. The scope of the Act extends through subordinate instruments, allowing for amendments and additional directives as necessary to maintain airworthiness standards.

Key Provisions

The legislative instrument (F2006B07963) revokes the existing Airworthiness Directives for Piper PA-42 (Cheyenne III) Series Aeroplanes and remakes them as separate instruments. The revocation and remaking are detailed in Schedule 1, which lists the various ADs by their names and numbers. The main operative sections (subsection 39.001(1) of the Civil Aviation Safety Regulations 1998) require the delegate of the Civil Aviation Safety Authority to carry out these actions. The new directives are re-made in exactly the same form as they appear in the latest published edition, ensuring consistency and clarity for the governed parties. The obligations imposed by these directives primarily pertain to the maintenance, inspection, and modifications of various components of the Piper PA-42 (Cheyenne III) Series Aeroplanes. For example, AD/PA-42/1 mandates the inspection of the powerplant firewall, while AD/PA-42/2 requires the installation of a nacelle fuel tank check valve. Each directive specifies the component in question, the required action, and the rationale behind the directive to ensure airworthiness and safety. Compliance with these directives is crucial for aircraft operators, maintenance personnel, and other stakeholders involved in the upkeep and operation of these aircraft. Failure to comply with the provisions of these Airworthiness Directives can lead to serious consequences. Breaches of the directives can result in civil penalties, such as fines, as well as criminal penalties, including imprisonment. The exact penalties depend on the severity of the breach and the jurisdiction's legal framework. For instance, non-compliance with safety directives can lead to fines under section 13 of the Civil Aviation Act 1988, and more severe breaches may result in criminal charges under section 23 of the same Act, with penalties including imprisonment for up to two years. Additionally, continued operation of an aircraft that does not meet airworthiness standards can lead to revocation of the aircraft's certificate of airworthiness, effectively grounding the aircraft until compliance is achieved.