TL Ultralight TL-22 Duo


The TL Ultralight TL-22 Duo is a Czech ultralight trike that was designed and produced by TL Ultralight of Hradec Králové. Production has been completed, but when it was available the aircraft was supplied as a complete ready-to-fly-aircraft or as a kit for amateur construction.

Design and development

The aircraft was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of. The aircraft has a maximum gross weight of. It features a cable-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit with a cockpit fairing, tricycle landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with a fibreglass cockpit fairing and its double surface wing covered in Dacron sailcloth. Its span wing is supported by a single tube-type kingpost, uses an "A" frame weight-shift control bar and has a wing area of. The standard powerplant used is a twin cylinder, liquid-cooled, two-stroke, dual-ignition Rotax 582 engine. The aircraft has an empty weight of and a gross weight of, giving a useful load of. With full fuel of the payload is.

Operational history

By 1998 the company reported that 50 aircraft were flying.

Specifications (TL-22 Duo)