The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. The aircraft has a maximum gross weight of 3610NaN0. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with a fibreglass cockpit fairing and its double surface wing covered in Dacron sailcloth. Its 10.61NaN1 span wing is supported by a single tube-type kingpost, uses an "A" frame weight-shift control bar and has a wing area of 13.8m2. The standard powerplant used is a twin cylinder, liquid-cooled, two-stroke, dual-ignition 640NaN0 Rotax 582 engine. The aircraft has an empty weight of 1600NaN0 and a gross weight of 3610NaN0, giving a useful load of 2010NaN0. With full fuel of the payload is 1710NaN0.
By 1998 the company reported that 50 aircraft were flying.