The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. The aircraft has a standard empty weight of 2480NaN0. It features a biplane wing arrangement, a single-seat, open cockpit, conventional landing gear and a single engine in tractor configuration.
The aircraft is made from aluminum tubing and covered in Dacron sailcloth. Its 321NaN1 span, unstaggered wings employ both interplane struts and cable bracing. The lower wing has less span than the upper wing. The fuselage consists of a single aluminum rectangular 2x3 inch (5 X 8 cm) tube. The standard recommended engine is a Kawasaki 440 snowmobile engine that produces 380NaN0 and yields a 400NaN0 cruise speed along with a rate of climb of 600 feet per minute (3.0 m/s).
