The Jazz was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. 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 its double surface wing covered in Dacron sailcloth. Its 9.831NaN1 span wing is supported by a single tube-type kingpost and uses an "A" frame weight-shift control bar. The standard supplied powerplant is a twin cylinder, liquid-cooled, two-stroke, dual-ignition 640NaN0 Rotax 582 engine. The aircraft has an empty weight of 1860NaN0 and a gross weight of 4500NaN0, giving a useful load of 2640NaN0. With full fuel of the payload is 2350NaN0.
A number of different wings can be fitted to the basic carriage, including the Kompol Stratus 15 and the higher aspect ratio and smaller area Stratus 13. Other manufacturer's wings can also be used.
The Jazz has been widely used in competition flying and has won many microlight events.