The aircraft is supplied as a complete ready-to-fly-aircraft, as a kit and in the form of plans for amateur construction.
[1] The manufacturer's website is non-functional and has been so since about 2008, so it is not clear if the company is still in business.
[2] The Ultra Cruiser was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 450 kg (992 lb) and the US FAR 103 Ultralight Vehicles rules, including the category's maximum empty weight of 115 kg (254 lb).
[1] The Ultra Cruiser I features a cantilever high-wing, a single-seat enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in pusher configuration.
The standard engines used are the 28 hp (21 kW) Hirth F-33 two-stroke or the Bilsam TNA 650 55 hp (41 kW) Suzuki automotive conversion powerplant.