The aircraft was designed to comply with Canadian basic ultralight rules. It features a parachute-style high wing made from rip-stop nylon, two seats in tandem accommodation, tricycle landing gear and a single 640NaN0 Rotax 582 engine in pusher configuration.
The aircraft is built from bolted-together aluminium tubing. Inflight 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 main landing gear incorporates shock absorber-type suspension. The standard canopy supplied was the Quantum Advantage High Performance of 500square feet area. This canopy provides a cruise speed of 30to and a payload of 510lb. A larger canopy of 550square feet that provides a slower cruise speed of 25to, a slower stall speed, a higher rate of climb and a payload of 610lb was also available.
Factory optional equipment included a windshield, snow skis for winter operations, electric starting, a canopy-monitoring mirror and an agricultural aircraft kit.