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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.
That year, the FAA provided a Notice of Proposed Rulemaking (NPRM) relevant to 14 CFR Part 25. Accompanying this notice was the "Draft ARSENAL Revised" of AC 1309–1. [21] Existing definitions and rules in § 25.1309 and related standards had posed certain problems to the certification of transport category airplanes.
EASA CS-VLA is the European Aviation Safety Agency Certification Specification for Very Light Aircraft. The Very Light Aircraft (VLA) aircraft certification category introduced in 2003 by the European Aviation Safety Agency (EASA) is intended to make it easier and less costly to get full European certification, operation and maintenance of a ...
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.
The corresponding EASA Acceptable Means of Compliance AMC 25.1309 (included as a section of CS-25) does recognize ARP4754/ED–79. The FAA and EASA have both subsequently recognized ARP4754/ED–79 as valid for certification of other aircraft categories, and for specific systems such as avionic databuses.
The first flight, originally scheduled for early 2008, was postponed due to delays and financial pressures. EADS announced in January 2008 that engine issues had been responsible for the delay. The rescheduled first flight, set for July 2008, was again postponed. Civil certification under EASA CS-25 was followed by certification for military uses.
Apart from this annex, there are also several certification specifications, including CS-25, for large aircraft, and CS-23, for medium and small aircraft. In application, airworthiness standards include a probability of loss of aircraft (PLOA) that is designed to be controllable (PLOAdc) as an overall attribute. [5]
EASA CS-25 Appendix 1; Lessons Learned From Transport Airplane Accidents Library This page was last edited on 31 December 2024, at 18:35 (UTC). Text is available ...