AD/AMD 20/9 - Fuel Feeder Tank Levels and Wing Tank Pressurisation Drain

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia's Parliament, form the foundational regulatory framework for civil aviation within Australia. The regulations address various aspects of aviation safety, including airworthiness directives, pilot licensing, aircraft maintenance, and operational standards. A specific instance of these regulations is found in Part 39 - 105, which pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives, ensuring that aircraft meet specific safety standards and undergo necessary modifications. This particular legislative instrument, F2006B02376, targets the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes, specifically addressing fuel feeder tank levels and wing tank pressurisation drain as per AMD SBs No. 554 and No. 555. The requirement aims to rectify identified safety issues, with compliance mandated within 100 hours of the aircraft being in service post the directive's issue date of 30 July 1976. The policy objective underpinning these directives is to maintain and enhance the safety of civil aviation operations by ensuring that all aircraft adhere to stringent airworthiness standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, encompasses the Civil Aviation Safety Authority’s schedule of airworthiness directives which mandate safety standards and compliance for civil aviation operations. This regulation applies to all models of the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes, ensuring that these aircraft meet specific safety criteria pertinent to their operation. The directive AD/AMD 20/9 focuses on fuel feeder tank levels and wing tank pressurisation drains, with a requirement that actions are taken in accordance with Airworthiness Service Bulletins No. 554 and No. 555, which correspond to sections 28-46 and 28-47 of the relevant safety documentation. Compliance with these directives is mandatory within 100 hours of time in service following 30 July 1976, underscoring the critical nature of these safety measures. The scope of these regulations extends across the Commonwealth of Australia, governing all entities and persons involved in the operation of the specified aircraft models within its jurisdiction.

Key Provisions

The primary sections of the Civil Aviation Regulations 1998 that are relevant to the AMD Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes are contained within Part 39, specifically in the Schedule of Airworthiness Directives, AD/AMD 20/9. This directive mandates action concerning the fuel feeder tank levels and the wing tank pressurisation drain, with reference to the Bureau Veritas AD 76-50-10 (B). The requirements stipulated in sections 28-46 and 28-47 of the Airworthiness Directives must be implemented to ensure compliance. The obligations imposed by these regulations are clear and specific. Operators and owners of the affected Falcon 20 and Mystere-Falcon 200 series aeroplanes must adhere to the requirements outlined in Airworthiness Service Bulletins No. 554 and No. 555. These obligations include ensuring that the necessary actions are taken to maintain the airworthiness of the aircraft, specifically related to the fuel feeder tank levels and the wing tank pressurisation drain. This compliance must be achieved within 100 hours of time in service after the effective date of 30 July 1976. Failure to comply with the requirements set forth in the Civil Aviation Regulations 1998 and the Airworthiness Directives can result in significant consequences. The Act outlines that non-compliance with airworthiness directives is a serious matter. Such breaches can lead to enforcement actions by the Civil Aviation Safety Authority (CASA), which may include administrative penalties, legal action, or even the grounding of the aircraft in question. The potential penalties underscore the importance of adhering to these regulations to maintain the safety and airworthiness of the aircraft.