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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 ...
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.
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.
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A nnmber of Aircraft Type Certificate were issued by FAA, Transport_Canada, Austro Control GmBH (Aviation Certification Authority in Austria) etc.. to permit production and delivery of aircraft with a standard Certificate of Airworthiness (certificate defined by ICAO in Annex 8 to the Chicago convention, that allow flight over member countries ...
EASA has the power to give CAMO second privileges also but not in all cases. These second privileges allow the CAMO to conduct airworthiness review on aircraft, issue (or recommend for issue) Airworthiness Review Certificates and issue 'permit to fly' for maintenance check flights.
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]
The engines are certified according to CS-22 Subpart H [3] for use in motorgliders, CS-LSA [4] and CS-VLA [5] type of aircraft. Most Limbach engines are based on the Volkswagen flat-4 boxer unit with displacement of up to 2.4 liters, and up to 160 BHP in the turbocharged model.