[5] The One-Seater was designed to comply with the Canadian Basic Ultra-Light Aeroplane rules, but also fit the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb).
It features a 500 sq ft (46 m2) Apco 500 parachute-style wing, single seat accommodation, tricycle landing gear and a single 50 hp (37 kW) Rotax 503 two-stroke engine in pusher configuration.
In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw.
The pilot is protected by a series of circular aluminium tubes in the event of a roll-over.
With full fuel of 10 U.S. gallons (38 L; 8.3 imp gal) the payload for crew and baggage is 317 lb (144 kg).