The Stingray was intended as a budget aircraft model and was introduced in 2007. It was designed to comply with the Fédération Aéronautique Internationale microlight category, including the category's maximum gross weight of 4500NaN0. The aircraft has a maximum gross weight of 4500NaN0. It features a strut-braced hang glider-style high-wing, weight-shift controls, a two-seats-in-tandem open cockpit, tricycle landing gear and a single engine in pusher configuration. A fibreglass cockpit fairing and wheel pants are optional.
The aircraft is made from square welded stainless steel tubing, with its double surface wing covered in Dacron sailcloth. Its 10.11NaN1 span Bautek Pico wing is supported by struts and uses an "A" frame weight-shift control bar. The powerplant is a four stroke air and liquid-cooled, dual-ignition, 800NaN0 Rotax 912UL aircraft engine or optionally a twin cylinder, liquid-cooled, two-stroke, dual-ignition 640NaN0 Rotax 582 powerplant.
With the Rotax 912 engine the Stingray has an empty weight of 1690NaN0 and a gross weight of 4500NaN0, giving a useful load of 2810NaN0. With full fuel of the payload is 2340NaN0.
