AD/BEECH 36/24 - Beryl Aviation Filtrator Assembly

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, address the critical need for stringent safety standards in the aviation sector, specifically concerning the maintenance and airworthiness of aircraft. The regulations are enforced by the Civil Aviation Safety Authority (CASA) and aim to ensure that all aircraft operating within Australian airspace adhere to rigorous safety protocols. One such regulation, AD/BEECH 36/24, pertains to the Beechcraft 36 (Bonanza) series aeroplanes and mandates the replacement of the Beryl Aviation filtrator assembly to enhance the safety and reliability of the aircraft. This directive was introduced to mitigate risks associated with the original filtrator assembly, ensuring that all modifications are compliant with international safety standards as set out by the Federal Aviation Administration (FAA). The overarching policy objective is to maintain the highest standards of air safety, protecting both the passengers and crew aboard these aircraft.

Scope and Application

The Civil Aviation Regulations 1998, as outlined in Part 39 - 105 of the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies specifically to Beechcraft 36 (Bonanza) Series Aeroplanes that have undergone modifications consistent with FAA Supplemental Type Certificate No. SA2653WE. This particular Airworthiness Directive (AD) concerns the Beryl Aviation filtrator assembly and is relevant for all models 36 and A36 that have the specified engine modification. The requirement is to replace the existing Beryl Aviation filtrator assembly P/N B-1116-1 with either P/N B-1116-M or P/N B-1116-RM. Compliance with this directive must be achieved within 100 hours of the aeroplane's time in service following 28 November 1975. The directive is issued under the authority of the Commonwealth of Australia and extends to all applicable aircraft operating within Australia, ensuring adherence to safety standards set forth by the Civil Aviation Safety Authority. The scope of the directive encompasses the modification of the Beryl Aviation filtrator assembly to enhance safety and operational standards of the specified aircraft models. The application of the directive is limited to those aircraft that meet the outlined modification criteria. The directive does not specify any exclusions or exemptions, and compliance is mandatory for the affected aircraft. Additionally, the regulations can be extended or refined through subordinate instruments, ensuring that safety standards remain current and effective. This legislative measure is integral to maintaining the airworthiness and safety of the Beechcraft 36 (Bonanza) Series Aeroplanes within the national airspace.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority, includes detailed Airworthiness Directives (AD) for various aircraft models, including the Beechcraft 36 (Bonanza) series aeroplanes. One such AD is AD/BEECH 36/24 concerning the Beryl Aviation filtrator assembly, applicable to all models 36 and A36 that have undergone modifications according to FAA Supplemental Type Certificate No. SA2653WE (section 1). This directive requires the removal of the existing Beryl Aviation filtrator assembly (Part Number B-1116-1) and the installation of either a P/N B-1116-M or P/N B-1116-RM assembly. The requirement is clearly stated, noting the reference to FAA AD 75-05-02 (section 1), and compliance must be achieved within 100 hours of time in service following the directive's issuance date of 28 November 1975. The AD imposes specific obligations on the operators and owners of Beechcraft 36 (Bonanza) series aeroplanes that meet the criteria outlined. Operators must ensure that the specified modification is carried out by a certified technician within the stipulated timeframe. This involves the removal of the Beryl Aviation filtrator assembly P/N B-1116-1 and the installation of the appropriate replacement part. The directive is aimed at enhancing the safety and airworthiness of the aircraft by addressing potential issues associated with the original filtrator assembly. Operators must maintain records of compliance with this directive to demonstrate adherence to the regulatory requirements set forth by the Civil Aviation Safety Authority. Failure to comply with the requirements of AD/BEECH 36/24 may result in serious consequences. The Civil Aviation Regulations 1998 outline penalties for non-compliance with airworthiness directives. Operators who fail to adhere to the specified timeframe or who do not complete the required modifications may face enforcement actions, including fines and potential grounding of the aircraft. The specific penalties are detailed in the broader regulatory framework of the Civil Aviation Act 1988 and associated regulations, but they may include significant financial penalties and operational restrictions. Ensuring compliance is crucial to avoid these adverse outcomes and to maintain the airworthiness and safety standards of the aircraft.