[2] The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb).
It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-side-by-side configuration open cockpit with a unique fibreglass cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
[1][2] The aircraft is made from bolted-together aluminum tubing, with its single surface wing covered in Dacron sailcloth.
Its 10 m (32.8 ft) span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar.
The powerplant is a twin cylinder, air-cooled, two-stroke, dual-ignition 64 hp (48 kW) Rotax 582 engine, with the four cylinder, air and liquid-cooled, four-stroke, dual-ignition 80 hp (60 kW) Rotax 912 engine optional.