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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 ...
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.
[2]: §4.3 It collects and analyses safety data, drafts and advises on safety legislation and co-ordinates with similar organisations in other parts of the world. [2]: §4.3 The idea of a European-level aviation safety authority goes back to 1996, but the agency was legally established only in 2002; it began its work in 2003. [2]: §4.3
The aircraft is undergoing EASA VLA and Serbian certification. [2] [8] Sila 950 Four seat model, with a maximum take-off weight of 950 kg (2,090 lb). Standard engines available are the 115 hp (86 kW) Rotax 914 and the 160 hp (119 kW) Lycoming O-320 four-stroke powerplants. The aircraft is no longer advertised on the company website. [2]
AWM 523-VLA The Federal Aviation Administration , the Aviation Certification Authority in USA, accepted the use of JAR-VLA as an alternative to Part 23 by means of an Advisory Circular AC 21.17-3 on 21 December 1992.
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.
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 ]
The aircraft will fit the into the EASA CS-VLA category and will be of all-composite construction, with a low-wing, tricycle gear and two seats in side-by-side configuration. [1] [2] [3] A stablemate of the Europa XS, the Elite features a crucifrom empennage and elliptical wings and tailplane. Three different sizes of engine will be available ...