[1][2] With a strut-braced parasol-wing, conventional landing gear, single engine in tractor configuration and its single-seat, open cockpit configuration, the Clipper resembles a small conventional light aircraft and was designed to appeal to private pilots looking for an ultralight aircraft.
[1] 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).
The conventional landing gear features balloon tires and a steerable tailwheel.
The standard powerplant supplied by the factory was the 40 hp (30 kW) Rotax 447, single ignition, two cylinder, two-stroke aircraft engine.
[1] The company was noted for its marketing of the aircraft at trade shows, such as EAA AirVenture.