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Airlines and other commercial operators of large, or turbine-powered, aircraft follow a continuous inspection program approved by the Federal Aviation Administration (FAA) in the United States, [1] or by other airworthiness authorities such as the Transport Canada Civil Aviation Directorate (TCCA), or the European Aviation Safety Agency (EASA).
The Certification of Aircraft Electrical and Electronic Systems for Operation in the High Radiated Fields (HIRF) Environment: AC 25.1309-1: System Design and Analysis: ARP4754, ARP4761: AC 20-174 Development of Civil Aircraft and Systems: ARP4754A AC 43.13-1B: Acceptable Methods, Techniques, and Practices - Aircraft Inspection and Repair: AC 70-1
Aircraft maintenance is the performance of tasks required to ensure the continuing airworthiness of an aircraft or aircraft part, including overhaul, inspection, replacement, defect rectification, and the embodiment of modifications, compliance with airworthiness directives and repair. [1] [2]
[2] General requirements to be met by a CAMO are facilities (offices and documentation storage), a Continuing Airworthiness Management Exposition (CAME) which must be approved by the competent authority of the country or EASA and company procedures (to comply with Part M requirements). A CAMO can also be the operator of the aircraft.
Standards And Recommended Practices (SARPs) are technical specifications adopted by the Council of ICAO in accordance with Article 37 of the Convention on International Civil Aviation in order to achieve "the highest practicable degree of uniformity in regulations, standards, procedures and organization in relation to aircraft, personnel, airways and auxiliary services in all matters in which ...
[1] Since their joint release in 2002, compliance with the guidelines and methods described within ARP4754() and its companion ARP4761() [2] have become mandatory for effectively all civil aviation world-wide. [3] Revision A was released in December 2010. It was recognized by the FAA through Advisory Circular AC 20-174 published November 2011.
In 1955, the Civil Aeronautics Board separated the parts authority out of the airworthiness standards, and placed it in a more general location so that one standard would apply to replacement and modification parts for all different forms of aircraft. [11] In 1965 CAR 1.55 became Federal Aviation Regulation section 21.303. [12]
Unlike flight tests, which analyze the aerodynamic design and safety of the aircraft itself, flight inspection comprises reviewing flight procedures (such as routes, approaches and departures) to ensure navigational support is sufficient, there are no obstacles and the procedure is reliable. [1]
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