[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 strut-braced high wing, a single-seat, conventional landing gear and a single engine in tractor configuration.
[1][2] The aircraft is made from bolted-together aluminum tubing, covered in Dacron sailcloth.
A single aluminum tube acts as the fuselage keel and supports the tail at the aft end, the wings in the middle and the engine at the front.
The controls are conventional three-axis and include a center stick, adjustable rudder pedals and full-span ailerons.