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 1550NaN0. It features a cable-braced high-wing, a single-seat, open cockpit, conventional landing gear and a single engine in pusher configuration.
The aircraft is made from wood. The fuselage is built around a wooden torsion box that is foam-filled for stiffness. The tailboom is a 30NaN0 diameter 6061-T6 aluminum tube. Its 321NaN1 span wing is constructed from Douglas fir spars and wing ribs, covered with doped aircraft fabric. The wing features half-span ailerons and cable-bracing from a single kingpost. The pilot is accommodated in the open cockpit on a fixed seat. There is no windshield. The landing gear is bungee suspended and the tail wheel is steerable.
Being a plans-built aircraft a variety of engines have been installed, including the McCulloch MAC-101 powerplant of 12.50NaN0 and the Yamaha KT-100 go-cart engine of 150NaN0.