COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 320 Series Aeroplanes
AD/CESSNA 320/13 Fuel Crossover Line - Modification 6/70
Applicability: All models.
Document: Rex Aviation Tech. Memo No. TM-26/A. Compliance: Within 100 hours time in service after 30 June 1970.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA) under the legislative framework of the Civil Aviation Act 1988, were enacted to ensure the safety of civil aviation in Australia. These regulations encompass a broad range of areas, including the maintenance and airworthiness of aircraft, with the overarching objective of protecting the public and ensuring the safe operation of aircraft within Australia. The specific legislative instrument referenced, F2006B08191, pertains to Airworthiness Directives for the Cessna 320 series aeroplanes, addressing a particular safety concern related to the fuel crossover line. This directive was introduced to mandate a modification to the fuel crossover line within 100 hours of time in service after 30 June 1970, thereby mitigating potential safety risks associated with this component. The policy objective is to maintain and enhance the safety standards of civil aviation by ensuring that aircraft meet stringent airworthiness criteria.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, pertain to the maintenance and operational standards of Cessna 320 series aeroplanes. This regulation applies to all models of Cessna 320 aeroplanes, ensuring that they meet specific safety and operational criteria set forth by the Civil Aviation Safety Authority. The directive, AD/CESSNA 320/13, mandates a modification to the fuel crossover line, as detailed in Rex Aviation Technical Memorandum No. TM-26/A, and requires compliance within 100 hours of time in service after 30 June 1970. This regulation extends to all operators of the Cessna 320 series aeroplanes within the Commonwealth of Australia, ensuring that the aircraft maintain a standard of airworthiness as prescribed by the Civil Aviation Safety Authority. The scope of the legislation is comprehensive, covering the geographic and jurisdictional reach of the Commonwealth, thereby applying uniformly across all states and territories of Australia. There are no stated exclusions or exemptions to this directive, and compliance is mandatory for all aircraft falling within its purview. The applicability of this regulation may be further detailed or extended through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, particularly in Part 39 under Schedule of Airworthiness Directives, specifies the requirements for maintaining the airworthiness of aircraft, including modifications to the Cessna 320 series aeroplanes. Specifically, AD/CESSNA 320/13 addresses the modification of the fuel crossover line (Section 6/70). This directive is applicable to all models within the Cessna 320 series. The requirement is to comply with the technical memorandum Rex Aviation Tech. Memo No. TM-26/A within 100 hours of time in service after 30 June 1970.
The obligations imposed by this directive on the operators of Cessna 320 series aeroplanes are quite clear. They must ensure that the fuel crossover line is modified as specified in the technical memorandum within the stipulated timeframe. This involves adhering to the technical specifications and procedures outlined in the document to maintain the safety and airworthiness of the aircraft. Compliance with this directive is critical as it directly impacts the operational safety of the aeroplanes involved.
Breaching the requirements set forth in AD/CESSNA 320/13 can have serious consequences. If an operator fails to implement the necessary modifications to the fuel crossover line within the specified timeframe, it could result in the aeroplane being deemed unairworthy. This could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). In terms of penalties, while the specific maximum penalties are not detailed in the text, non-compliance could result in fines, operational restrictions, or even grounding of the aircraft until the required modifications are completed. The severity of the penalties may depend on the extent of non-compliance and the impact on aviation safety.