[4] The Two-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, two-seats-in-side-by-side configuration, tricycle landing gear and a single 64 hp (48 kW) Rotax 582 two-stroke engine in pusher configuration.
In flight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw.
The occupants are 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 429 lb (195 kg).