EASA CS-VLA
From Wikipedia, the free encyclopedia
EASA CS-VLA is the European Aviation Safety Agency Certification Specification for Very Light Aircraft.
The Very Light Aircraft or VLA aircraft certification category introduced in 2003 by the EASA (European Aviation Safety Agency) is intended to make it easier and less costly to get full European certification of a general aviation aircraft. The somewhat relaxed certification procedure is available for aircraft satisfying the following criteria:
- A single engine with spark or compression ignition (i.e. no jets).
- One or two seats.
- Maximum take-off weight (MTOW) of not more than 750 kg.
- Stall speed in the landing configuration (VS0) of no more 83 km/h (45 knots).
A CS-VLA aircraft is not certified for aerobatics and may be flown under daylight visual flight rules only.
Examples
- Aero AT-3
- Tecnam P2002 JF
See also
External links
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.