Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, provide the regulatory framework for ensuring the safety of civil aviation in Australia. One of the specific pieces of legislation under these regulations is the Airworthiness Directive AD/BEECH 36/4 Amendment 2, which applies to all models of the Beechcraft 36 (Bonanza) Series Aeroplanes. This directive was introduced to address specific safety concerns regarding the control wheel adaptor, ensuring that all operators comply with the requirements outlined in Beechcraft Service Information No. 0254-156, Revision IV. The directive mandates that any action required by this amendment must be completed within 100 hours of the aircraft's time in service following 31 August 1972, thereby ensuring continued adherence to safety standards set forth by the Civil Aviation Safety Authority.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, which governs the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, pertains to Beechcraft 36 (Bonanza) Series Aeroplanes. This legislation applies to all models of these aircraft and mandates compliance with the Control Wheel Adaptor requirements outlined in Beechcraft Service Instruction No. 0254-156, Revision IV. Compliance with this directive is required within 100 hours of the aircraft's time in service following 31 August 1972. It is noteworthy that compliance with a previous issue of this directive is considered equivalent to compliance with this updated issue. The regulations extend across the Commonwealth of Australia, ensuring that all operators within the national jurisdiction adhere to these safety standards. The scope of this directive is explicitly limited to the specified aircraft models and does not extend to other types of aircraft or aviation entities unless they fall under the Beechcraft 36 (Bonanza) Series. There are no stated exclusions or exemptions in the directive, but it is noted that compliance with prior versions of the directive satisfies the current requirements.

Key Provisions

The primary operative sections of the Civil Aviation Regulations 1998, particularly in the context of the Beechcraft 36 (Bonanza) Series Aeroplanes, are found in AD/BEECH 36/4 Amendment 2 (section 39-105). This amendment pertains specifically to the control wheel adaptor and requires compliance with Beechcraft Service Information No. 0254-156, Revision IV (section 39-105). The directive mandates that compliance must be achieved within 100 hours of time in service after 31 August 1972. It is noteworthy that compliance with a previous issue of this directive also satisfies the requirements of this amendment, ensuring continuity and consistency in maintenance standards. The obligations imposed by this legislation on the parties or entities it governs, primarily aircraft operators and maintenance personnel, include ensuring that the control wheel adaptor on Beechcraft 36 (Bonanza) Series Aeroplanes is modified as specified in Beechcraft SI No. 0254-156, Revision IV. This involves adhering to the detailed instructions provided in the service information bulletin to ensure that the adaptor meets the necessary safety standards. Operators and maintenance personnel must conduct the required actions within the specified timeframe to maintain the airworthiness of the aircraft. Failure to comply with the provisions of AD/BEECH 36/4 Amendment 2 can result in significant consequences. Although specific offences and penalties are not detailed in the excerpt, non-compliance with airworthiness directives generally can lead to severe civil or criminal penalties under the Civil Aviation Act 1988. The Civil Aviation Safety Authority (CASA) has the authority to impose fines, suspend or revoke aircraft certificates of airworthiness, and take legal action against non-compliant entities. The potential penalties underscore the importance of adhering to the mandated directives to ensure the safety and compliance of aircraft operations.