Construction began in November 1982, with the first flight being in November 1982. Single-seat single-engined high-wing mono-plane with conventional three-axis control. Conventional tail. Control inputs through stick for pitch/roll and pedals for yaw. Wing braced from below by struts; wing profile; double-surface. Undercarriage has three wheels in tail-dragger formation. Push-right go-right tailwheel steering connected to yaw control. Aluminium-tube framework, totally enclosed. Engine mounted below wing driving tractor propeller.
The cockpit is fully enclosed and there is only one seat. Equipped with doors, 4 position flaps, elevator trim, bungee suspension landing gear, steerable tailwheel, brakes, radio and headset. Rotax 503 with electric start gives a 70 mph cruise.