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.

Description of ultralight aviation site

Country

Aquila A 210

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.

Germany

AT-3 VLA from Aero Ltd.

AT-3 is one of few all metal aeroplanes certified by EASA in the VLA (Very Light Aeroplane) category.

Poland

H.F.Dorna

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 .

Iran

Nordic Aircraft

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.

Sweden

Opus Aircraft

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.

USA

P2002-JR from Tecnam

The P2002-JR (compliant to EASA CS-VLA) matches any possible customer desire. The Tecnam P2002, a simphony of aerodynamic and structure effectiveness.

Italy