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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. 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.
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.
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_(28915135713).jpg%2F250px-IndiGo_Airbus_A320neo_F-WWDG_(to_VT-ITI)_(28915135713).jpg&w=3840&q=100)
_(28915135713).jpg%2F250px-IndiGo_Airbus_A320neo_F-WWDG_(to_VT-ITI)_(28915135713).jpg&w=3840&q=75 "EASA CS-25")
_(28915135713).jpg%2F2000px-IndiGo_Airbus_A320neo_F-WWDG_(to_VT-ITI)_(28915135713).jpg&w=3840&q=75 "EASA CS-25")
