Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 60 (Duke) Series Aeroplanes

Overview

The Airworthiness Directives 2004 is a legislative instrument enacted to address the need for updating and revoking existing airworthiness directives for specific aircraft models. Enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, this instrument aims to ensure that the airworthiness directives are current and accurately reflect the latest safety requirements for the specified aircraft. The policy objective behind this legislative instrument is to maintain the highest standards of air safety by ensuring that all relevant airworthiness directives are up-to-date and effectively address any identified safety concerns. This approach helps to safeguard the integrity and safety of the aviation industry by providing clear and precise directives for maintaining the airworthiness of aircraft.

Scope and Application

The Airworthiness Directives 2004, enacted by David Alan Villiers, delegate of the Civil Aviation Safety Authority, primarily concern the aviation industry, specifically targeting the maintenance and safety standards of Beechcraft 60 (Duke) Series aeroplanes. The Act applies to all persons and entities involved in the operation, maintenance, and certification of these aircraft, ensuring compliance with specified safety standards and requirements. These directives cover a range of technical aspects, including but not limited to, cabin door latches, aileron control rods, engine mount bolts, and electrical wiring systems, thereby establishing stringent safety protocols for these components. The directives also extend their application nationally, under the auspices of the Civil Aviation Safety Regulations 1998, thereby ensuring uniformity and compliance across Australia. Each directive is meticulously re-made to reflect the latest published editions, with specific amendments and cancellations noted where applicable. While the Act comprehensively governs the airworthiness of these aircraft, it does not extend to areas not explicitly covered within its stipulations.

Key Provisions

This legislative instrument, the Airworthiness Directives 2004, made by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA) under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, revokes certain Airworthiness Directives (ADs) and re-makes them in the form they appear in the latest published edition (sections 1 and 2). These directives pertain to various parts and systems of the Beechcraft 60 (Duke) series aeroplanes. The Schedule details the specific ADs that are revoked and re-made, including those related to cabin door latches, aileron and aileron tab control rods, elevator and tab controls, heated stall warning switches, and more. The instrument aims to ensure that the ADs are up-to-date and accurately reflect the latest safety requirements and standards. The obligations imposed by this legislation primarily concern aircraft manufacturers, operators, and maintenance providers. They are required to comply with the re-made ADs, which may include conducting inspections, repairs, or modifications to the specified parts of the aircraft. Operators must ensure that their aircraft meet the airworthiness standards set forth in the ADs, while maintenance providers must perform any required actions to bring aircraft into compliance. This includes adhering to the detailed instructions and timelines outlined in each AD. The directives serve to maintain and enhance the safety and airworthiness of the aircraft by addressing specific issues or hazards identified through regulatory oversight. Violations of the ADs, or failure to comply with the directives, can lead to serious consequences. Under the Civil Aviation Act 1988, non-compliance can result in civil penalties, including fines and potential imprisonment. The specific penalties vary depending on the nature and severity of the breach but can include fines of up to $165,200 for individuals and $826,000 for bodies corporate, as well as imprisonment for up to two years. Additionally, non-compliance can lead to criminal charges, with potential penalties including fines of up to $500,000 for individuals and $2.5 million for bodies corporate, and imprisonment for up to five years. Furthermore, CASA has the authority to suspend or revoke an aircraft’s certificate of airworthiness, which can effectively ground the aircraft until the necessary compliance actions are taken.