[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 cable-braced high-wing, canard elevator, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.
[1][2] The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in Dacron sailcloth.
Its compact single-surface 26 ft (7.9 m) span wing is supported by cables attached to a simple tube kingpost.
The standard engine supplied with the kit was the Cuyuna UL II-02 twin cylinder, two-stroke powerplant of 35 hp (26 kW).