|National origin||United States|
Design and development
The aircraft was designed as a US FAR 103 Ultralight Vehicles two-seat trainer. It features a parachute-style high-wing, two seats in side-by-side configuration, tricycle landing gear and a single engine in pusher configuration. The standard engines supplied were the 45 hp (34 kW) 2si 460F-45 and the 45 hp (34 kW) Zenoah G-50 engine, although any light two-cylinder, two-stroke engine can be used.
The aircraft is built from bolted-together anodized aluminum tubing to save weight. Inflight steering is accomplished via foot pedals that actuate the canopy brakes, creating roll and yaw. On the ground the aircraft has tiller-controlled nosewheel steering. The main landing gear does not incorporate suspension and the aircraft relies on large tundra tires to provide this.
Data from Cliche
- Crew: one
- Capacity: one passenger
- Empty weight: 230 lb (104 kg)
- Fuel capacity: 13.5 U.S. gallons (51 L; 11.2 imp gal)
- Powerplant: 1 × 2si 460F-45 twin cylinder, two-stroke, air-cooled aircraft engine, 45 hp (34 kW)
- Cruise speed: 25 mph (22 kn; 40 km/h)
- Cliche, Andre: Ultralight Aircraft Shopper's Guide 8th Edition, page D-4. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4