[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, open cockpit, tricycle landing gear and a single engine in tractor configuration.
The wing incorporates a quick-folding mechanism that allows it to be folded back along the fuselage for ground transport or for storage.
[1][2] Due to its introduction just before the collapse of the US ultralight industry in 1984, the design was not a commercial success and only a small number were completed and sold.
[1] Data from Cliche and the Virtual Ultralight Museum[1][2]General characteristics Performance