EASA CS-25
Certification procedure
From Wikipedia, the free encyclopedia
EASA CS-25 is the European Union Aviation Safety Agency Certification Specification for turbine powered Large Aeroplanes.
_(28915135713).jpg)
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
- 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-27, Small Rotorcraft
- EASA CS-29, Large Rotorcraft
- Federal Aviation Regulations § Part 25
- Transport category
