[1][2][3][4] The aircraft was designed to comply with US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 254 lb (115 kg).

It features a "top-less" strut-braced hang glider-style high-wing, weight-shift controls, a single-seat, open cockpit, tricycle landing gear and a single engine in pusher configuration.

[1][4] The aircraft is made from bolted-together aluminum tubing, with its single surface wing covered in Dacron sailcloth.

Its 31.5 ft (9.6 m) span wing is supported by streamlined struts, in place of the more commonly used cables and kingpost.

In 2008 the aircraft was improved with a folding wing pylon and increased baggage space.