Airworthiness Directives 2004 - Revocation and Remaking - Cessna 650 (Citation III) Series Aeroplanes

Overview

The Airworthiness Directives 2004, enacted under the authority of the Civil Aviation Safety Regulations 1998, was introduced to address the need for updated and specific regulations governing the airworthiness of certain aircraft models. The legislation was enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, and aims to ensure that airworthiness directives are clearly communicated and effectively implemented. This instrument revokes previous directives and remakes them to reflect the latest regulatory standards, ensuring that the safety and airworthiness of the specified aircraft models, such as the Cessna 650 (Citation III) Series Aeroplanes, are maintained in accordance with contemporary safety requirements. By re-making these directives, the legislation seeks to maintain high standards of aviation safety and ensure compliance with current regulatory expectations.

Scope and Application

The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority under the Civil Aviation Safety Regulations 1998, pertains to the regulation of airworthiness standards for specific aircraft. The legislation applies to the Cessna 650 (Citation III) Series Aeroplanes and covers various airworthiness directives, including those related to elevator balance, airborne auxiliary power, elevator torque tube inboard attach fittings, thrust reverser throttle load limiter, engine and flight data monitoring, and the main landing gear side brace assembly. These directives are designed to ensure that the specified aircraft maintain their airworthiness by adhering to certain safety standards and procedures. The scope of the Act extends across the Commonwealth of Australia, as it is issued under the authority of the Civil Aviation Safety Regulations 1998, which have a national jurisdictional reach. The directives are specifically tailored to address safety concerns and operational standards for the mentioned aircraft series, and they are re-made to reflect the latest published editions to ensure that they remain current and effective. Any exclusions, exemptions, or thresholds are implicitly addressed within the individual airworthiness directives, which are detailed in the attached schedules.

Key Provisions

The Airworthiness Directives 2004, issued under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, primarily serves to revoke and re-make a series of Airworthiness Directives related to the Cessna 650 (Citation III) Series Aeroplanes (sections 1(a) and (b)). These directives are listed in Schedule 1 and are being re-made to match the latest published editions. Specifically, the directives address various safety concerns, including elevator balance (AD/CESSNA 650/1), inspection of the main fuel manifold for airborne auxiliary power (AD/CESSNA 650/2), elevator torque tube inboard attach fittings (AD/CESSNA 650/3), thrust reverser throttle load limiter (AD/CESSNA 650/4), engine and flight data monitoring (AD/CESSNA 650/5), and the MLG side brace assembly (AD/CESSNA 650/6). The Airworthiness Directives impose specific obligations on the operators of the Cessna 650 (Citation III) Series Aeroplanes. Operators must adhere to the requirements outlined in each directive, such as conducting regular inspections and maintenance of the elevator balance, ensuring the airborne auxiliary power's main fuel manifold is inspected, and confirming that the elevator torque tube inboard attach fittings are secure. Additionally, operators need to ensure that the thrust reverser throttle load limiter is functioning correctly, monitor engine and flight data as specified, and maintain the MLG side brace assembly in accordance with the directive. Compliance with these obligations is essential to ensure the airworthiness and safety of the aircraft. Failure to comply with the Airworthiness Directives can lead to significant consequences. The Civil Aviation Safety Regulations 1998 provide that non-compliance may result in enforcement actions by the Civil Aviation Safety Authority (CASA). Under these regulations, CASA may issue enforcement notices, administrative penalties, or even prosecute individuals or companies for breaches. The penalties for non-compliance can include substantial fines, which may reach up to $100,000 for individuals and $500,000 for corporations, depending on the severity of the breach. Additionally, serious non-compliance could result in imprisonment for individuals, with penalties varying based on the nature and extent of the violation. Thus, it is imperative for operators to strictly adhere to the directives to avoid these serious repercussions.