[1] The T-Lite was designed as both a cross country powered aircraft and self-launching motor glider for soaring.
The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category as well as the US FAR 103 Ultralight Vehicles rules.
It features a cable-braced hang glider-style high-wing, weight-shift controls, a single-seat open cockpit, tricycle landing gear and a single engine in pusher configuration.
The 9.5 m (31.2 ft) span Core wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar.
The powerplant is a purpose-designed, single cylinder, air-cooled, four-stroke, 22 hp (16 kW) Bailey B200 engine, with electric starting and a 3.2:1 reduction drive.