With a standard empty weight of 254 lb (115 kg), it was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).
It features a strut-braced high-wing, a single-seat open cockpit with windshield, fixed tricycle landing gear and a single engine in pusher configuration.
[1] The aircraft is made from aluminum tubing, with its flying surfaces covered in Dacron sailcloth.
Its recommended engine power range is 28 to 50 hp (21 to 37 kW); standard engines used include the 50 hp (37 kW) two-stroke Hirth F-23.
[1] By December 2011, the manufacturer reported that ten of the aircraft had been completed and flown.