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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.
The European Aviation Safety Agency (EASA) was created in 2003 and reached full functionality in 2008, and has since taken over most of the JAA functions. JAA Certification Specifications, formerly known as JARs, are recognised by EASA as an acceptable basis for showing compliance with their national airworthiness codes.
For example, EASA cooperates with most of the EU's Eastern Partnership member states through EASA's Pan-European Partners (PANEP) initiative in which countries such as Armenia, [20] Azerbaijan, [21] Georgia, [22] Moldova [23] and Ukraine [24] co-operate on the implementation of EU aviation safety rules and comprehensive aviation agreements.
This revision also harmonizes with international airworthiness regulations such as European Union Aviation Safety Agency (EASA) CS–25.1309. ARP4754 Revision B is an interim release meant to expedite consistency with ARP4761 Revision A, "Safety Assessment Process", which was also released in December 2023.
Where regulations (FAR) and standards (ARP) may use such terms as failure condition, and extremely improbable, AC 25.1309–1 defines their specific meanings, both quantitatively and qualitatively. [7] In this respect, AC 25.1309–1 is comparable to ISO 26262–1 Vocabulary, at least in regard to the relative dependent standards. Key ...
In conjunction with ARP4754, ARP4761 is used to demonstrate compliance with 14 CFR 25.1309 in the U.S. Federal Aviation Administration (FAA) airworthiness regulations for transport category aircraft, and also harmonized international airworthiness regulations such as European Aviation Safety Agency (EASA) CS–25.1309.
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.
In the case of the FAA, the regulation of airworthiness is found in Title 14 in the collected Code of Federal Regulations. The EASA specifications are found in several regulations: as nº 216/2008 (Basic Regulations), nº 748/2012 (Initial Airworthiness), nº 2015/640 (Additional specifications about airworthiness) and nº 1321/2014 (Continuing ...