Search results
Results from the WOW.Com Content Network
The Aero AT-3 R100 is an EASA Very Light Aircraft certified two-seater rated with 582 kg max takeoff weight, a 75 kW engine, 200 km/h cruise speed and 904 km range. EASA CS-VLA is the European Aviation Safety Agency Certification Specification for Very Light Aircraft.
[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]
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.
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 ...
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.
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.
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.