[1][2] The aircraft 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 cantilever high-wing, inverted V-tail, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.
Its elliptical planform 32.2 ft (9.8 m) span wing it mounted using several cabane struts and produces a 15:1 glide ratio.
The 25 hp (19 kW) KFM 107 powerplant is mounted behind the pilot's seat, with the propeller in between the upper and lower tailboom tubes.
The design was proof-tested to +9/-9 g. The aircraft exhibits good stability in all axes in flight and can be quickly dismantled for storage or ground transport.