The aircraft family was designed to comply with the
Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of . All models feature a
cable-braced hang glider-style
high-wing, weight-shift controls, a two-seats-in-
tandem open cockpit,
tricycle landing gear with
wheel pants and a single engine in
pusher configuration. The aircraft is made from bolted-together
aluminum tubing, with its double surface wing covered in
Dacron sailcloth. Typical wings used have a span wing, are supported by a single tube-type
kingpost and use an "A" frame weight-shift control bar. The standard powerplant is the twin cylinder, air-cooled,
two-stroke,
dual-ignition Rotax 582 engine. Options do not include the
Rotax 912 engine. ==Variants==