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CS-VLA (Very Light Aircraft)CS-VLA (Certification Specification for Very Light Aircraft) are certified aircrafts with 1 or 2 seats, MTOW of 750 kg and a stallspeed of max. 83 kmt. and VFR only. |
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AQUILA Technische Entwicklungen GmbH prondly presents you the Aquila A 210, a new and innovative 2-seat-single-engine aircraft in full composite construction, designed for basic and advanced training and affordable cruising, fully certified under EASA CS-VLA rules within Europe. | |||||||
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AT-3 is one of few all metal aeroplanes certified by EASA in the VLA (Very Light Aeroplane) category. | |||||||
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H.F. Dorna is an Iranian private joint stock company specializing in design and manufacture of light aircraft , covering JAR-VLA and JAR-23 categories . | |||||||
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Nordic Aircraft is developing a top quality and high performance composite light sport aircraft designed to the CS-VLA code. With a maximum take off weight of 560 kg and a stall speed below 65 km/h at 450 kg, it will comply to many aircraft classes including ML, VLA and LSA. | |||||||
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The OPUS Super2 is an all aluminium, shoulder wing aircraft with exceptional all round visibility. - The Super2 gained full production and type certification under British Civil Airworthiness Requirements (BCAR's) inthe United Kingdom and Joint Airworthiness Requirements for Very Light Aircraft (JAR/VLA) certification in Europe. The aircraft has also been accepted as an Advanced Ultralight in Canada and soon Special Light Sport Aircraft certification in the USA. | |||||||
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The P2002-JR (compliant to EASA CS-VLA) matches any possible customer desire. The Tecnam P2002, a simphony of aerodynamic and structure effectiveness. | |||||||
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