The aircraft was designed to comply with the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 2540NaN0. It features a parachute-style high-wing, single-place accommodation, tricycle landing gear and a single 520NaN0 Rotax 503 engine in pusher configuration. The 640NaN0 Rotax 582 engine was a factory option.
The aircraft is built from a combination of aluminium and 4130 steel tubing. In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has lever-controlled nosewheel steering. The aircraft was factory supplied in the form of an assembly kit that requires 40 hours to complete.