EASA CS-25
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EASA CS-25 is the European 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. If the manufacturer of the aircraft has sufficiently demonstrated all points, the certification authority issues a type certificate.
Certification Specifications are "soft law", which is not legally binding.[2] Manufacturers may apply for exemptions from CS-25 where necessary.
See also[edit]
- List of large aircraft
- List of current production certified light aircraft
- EASA CS-LSA, the European certification for Light Sport Aeroplanes (maximum 600 for land / 650 kg for seaplanes)
- EASA CS-VLA, the European certification for Very Light Aircraft (maximum 750 kg)
- EASA CS-23, Normal, Utility, Aerobatic and Commuter Aeroplanes
- EASA CS-29, Large Rotorcraft
- Federal Aviation Regulations § Part 25
- Transport category
References[edit]
- ^ "EASA.A.064 - Airbus A318, A319, A320, A321 Single Aisle". 2 March 2017.
- ^ "Regulations Structure" (PDF). EASA. 18 March 2014. Retrieved 13 March 2024.
These AMC/GM are so-called 'soft law' (non-binding rules), and put down in form of EASA Decisions. A comprehensive explanation on AMC in form of questions and answers can be found on the FAQ section of the EASA website.. Furthermore, Certification Specifications are also related to the implementing regulations, respectively their parts. Like AMC/GM they are put down as Decisions and are non-binding.
External links[edit]
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