Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 300 Series Aeroplanes

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as a delegate of the Civil Aviation Safety Authority under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, serve to revoke existing airworthiness directives pertaining to Beechcraft 300 series aeroplanes and re-make them as separate instruments. This legislative instrument addresses the need to update and reissue specific airworthiness directives to ensure that they reflect the latest safety standards and requirements. Each directive is reproduced in the same form as it appears in the most recent published edition, ensuring consistency and accuracy in the regulatory framework governing the airworthiness of these aircraft. The primary objective of this instrument is to maintain and enhance the safety of civil aviation by ensuring that all relevant airworthiness directives are current and effectively communicate necessary safety measures to aircraft operators. This approach facilitates better compliance with safety regulations and helps to mitigate potential risks associated with the operation of Beechcraft 300 series aeroplanes.

Scope and Application

The Airworthiness Directives 2004, as delegated by David Alan Villiers on behalf of the Civil Aviation Safety Authority, pertains to the specific aviation industry and focuses on the airworthiness of aircraft, particularly the Beechcraft 300 Series Aeroplanes. The legislation applies to the entities and persons involved in the operation, maintenance, and certification of these aircraft within the Commonwealth of Australia. It mandates compliance with the detailed airworthiness directives listed in the Schedule, which cover a range of safety issues and maintenance requirements for the specified aircraft model. The geographic reach of this legislation is national, as it operates under the authority of the Civil Aviation Safety Regulations 1998. Notably, the directives re-made in this legislative instrument are identical to those published in the latest edition, ensuring consistency and up-to-date safety standards. Any exclusions or exemptions are not explicitly stated in this particular legislative instrument, but the overarching regulations may provide further clarification on this aspect.

Key Provisions

The Airworthiness Directives 2004 (F2006B07741) involve the revocation and remaking of certain airworthiness directives (ADs) for the Beechcraft 300 Series aeroplanes. David Alan Villiers, as the delegate of the Civil Aviation Safety Authority, has revoked the specified ADs listed in Schedule 1 and remade them as separate instruments (section 1). The ADs that have been revoked and remade include directives related to the cockpit D side window, wing fatigue life limitation, engine mount assembly attachment bolts, cabin door, aft cowling access door, cabin seat frame, fuselage stringers, wing attach fittings, bolts and nuts, outflow/safety valve, pressurisation control system pneumatic tubing inspection, main landing gear clevis assembly, elevator trim tab system, inspection for flight control interference with wiring, landing gear emergency hand pump, aircraft flight manual, elevator balance weight attachment, external door operating instructions, and engine controls cross shaft. The Act imposes obligations on the parties or entities it governs, including adherence to the newly remade ADs for the specified Beechcraft 300 Series aeroplanes. These ADs outline specific requirements for the maintenance, repair, and operation of the aircraft to ensure airworthiness and safety. Operators of these aircraft must comply with the ADs by implementing the prescribed measures and actions, such as inspections, repairs, and modifications, to maintain the airworthiness of their aircraft. Failure to comply with the ADs may result in civil or criminal consequences, including penalties. The specific offences, penalties, or consequences for breach are not detailed in the legislative instrument itself but would be governed by the broader Civil Aviation Safety Regulations 1998 and other relevant legislation. Penalties for non-compliance with airworthiness directives can include fines, imprisonment, or both, depending on the severity of the breach and the specific provisions of the applicable regulations. The maximum penalties would be determined by the relevant authorities and would be in line with the regulatory framework governing civil aviation safety in Australia.