AD/AMD 10/2 Amdt 1 - Oxygen Pressure Reducing Valve Installation - Modification

Overview

The Civil Aviation Regulations 1998, amended by the instrument F2006B02335, addresses issues related to the airworthiness of Falcon 10 Series Aeroplanes. Enacted by the Commonwealth of Australia, this legislation falls under the purview of the Civil Aviation Safety Authority (CASA) and is intended to ensure that all aircraft meet the required safety standards. The specific problem or gap this piece of legislation aims to fill pertains to the installation of oxygen pressure reducing valves, as outlined in the Airworthiness Directive. This directive mandates that all Falcon 10 Series Aeroplanes must incorporate modifications to their oxygen systems to maintain compliance with safety standards. The policy objective behind this directive is to enhance the safety of air travel by ensuring that the oxygen systems in these aircraft operate within specified parameters.

Scope and Application

The Civil Aviation Regulations 1998, as amended by Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically address the Falcon 10 Series Aeroplanes, covering all models. The directive mandates the installation of an oxygen pressure reducing valve, as detailed in Amendment Service Bulletin BA F10-0135 R2 (F10-35-001). Compliance with this directive is required forthwith, and aircraft that have previously adhered to issues of this directive are considered compliant with this current version. The regulation applies to all entities and individuals operating Falcon 10 Series Aeroplanes within the Commonwealth of Australia, thereby extending its jurisdictional reach across the national airspace. There are no stated exclusions or thresholds specified within the directive, and its application is enforced by the Civil Aviation Safety Authority, potentially extended or restricted through subordinate instruments as necessary.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail the Airworthiness Directives (AD) concerning the AMD Falcon 10 Series Aeroplanes. This particular directive, AD/AMD 10/2 Amendment 1, applies to all models of the Falcon 10 series (Section 105.01). It mandates the installation of an oxygen pressure reducing valve as specified in the document AMD Service Bulletin BA F10-0135 R2 (Section 105.02). Compliance with this directive is required forthwith, and aircraft that previously complied with earlier versions of this directive are considered to be in compliance with this updated version (Section 105.03). Under this legislation, the entities governed must ensure that the specified modification to the oxygen pressure reducing valve is carried out without delay. This requirement is imperative for maintaining the safety and airworthiness of the aircraft. Operators and owners of the affected aircraft must adhere to the detailed instructions provided in the referenced service bulletin to effect the necessary changes. The directive also stipulates that aircraft that previously complied with the previous issue of this directive are deemed to meet the current requirements, thereby providing a seamless transition for ongoing compliance (Section 105.04). Failure to comply with the requirements outlined in the AD/AMD 10/2 Amendment 1 can result in serious legal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations strictly. Non-compliance may lead to the suspension or revocation of the aircraft's certificate of airworthiness, which could prevent the aircraft from operating legally. Additionally, operators found in breach of these directives may face financial penalties and legal action. The seriousness of these consequences underscores the importance of adhering to the stipulated modifications and ensuring ongoing compliance with the airworthiness directives (Section 105.05).