When it was available the aircraft was supplied as a kit and also in the form of plans for amateur construction.
It features a biplane layout, a single-seat open cockpit, fixed conventional landing gear and a single engine in tractor configuration.
[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 standard engine used is the 48 hp (36 kW) Christine Aero powerplant.
With full fuel of 5 U.S. gallons (19 L; 4.2 imp gal) the payload for the pilot and baggage is 191 lb (87 kg).