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In the United States, Federal Aviation Regulations Parts 25 and 29 are applied to the design and certification of transport category airplanes and helicopters respectively. In Europe the European Aviation Safety Agency has similar certification requirements, also titled Parts 25 and 29, for application to transport category airplanes and ...
The airworthiness requirements for transport category (large civil aircraft, both airplanes and helicopters) are contained in Title 14, Code of Federal Regulations (14 CFR) part 25 (commonly referred to as part 25 of the Federal Aviation Regulations (FAR)).
This part contains airworthiness standards for airplanes in the transport category. The Boeing 737 and later types, and Airbus A300 series, are well-known airplane types that were certified according to standards set out in FAR Part 25. Transport category airplanes are either:
ARP4754 was defined in the context of aircraft certification, in particular Part 25 Sections 1301 and 1309 of harmonized civil aviation regulations for transport category airplanes. These are found in the U.S. FAA Federal Aviation Regulations (FAR) at 14 CFR 25.1309 and the corresponding European JAA Joint Aviation Requirements (JAR), which ...
The Hawker 4000 was certified to FAA FAR Part 25 standards, which places a five-year time limit on certification of a new transport category aircraft. The 4000 completed Function and Reliability Tests on May 25, 2006. [6] During September 2005, a prototype underwent testing at the McKinley Climatic Laboratory at Eglin Air Force Base, Florida. [7]
The Lear 45 was certified under FAR Part 25 (transport category rules), rather than FAR Part 23 (often used in earlier business jets). The stricter Part 25 certification requires greater system redundancy, and requires that the airplane reliably meets the performance numbers published in the aircraft's FAA-approved Pilot's Operating Handbook (POH).
AW609 Certification Basis is established by the FAA under the provisions of Part 21.17(b) for "Special Class Aircraft" along with a portion of Part 25 (fixed-wing aircraft) and 29 (helicopter) and new specific tiltrotor parts [48] [46] in a new category called "powered lift". [43]
EASA CS-25 is the European Union Aviation Safety Agency Certification Specification for Large Aeroplanes. This certification procedure applies to large, turbine-powered aircraft, with max take-off weight more than 5,700kg (CS 25.1). It describes the minimum requirements that must be met for the certification of an aircraft in this class.