The Stingray features a strut-braced parasol wing, a single-seat enclosed cockpit under a bubble canopy, retractable conventional landing gear and a single engine in pusher configuration.
The aircraft is made from a combination of metal tubing, with its flying surfaces covered in Dacron sailcloth doped aircraft fabric and a reinforced fiberglass hull. Its 30.831NaN1 span wing has a wing area of 150square feet and is supported by a central pylon behind the cockpit, "V" struts and jury struts. The wing also mounts outrigger pontoons that provide stability on the water. The acceptable power range is 40to and the standard engine used is the 400NaN0 Rotax 447 twin cylinder, two stroke powerplant.
The Stingray has a typical empty weight of 475lb and a gross weight of 800lb, giving a useful load of 325lb. With full fuel of the payload for the pilot and baggage is 289lb.
The standard day, sea level, no wind, take off on land with a 400NaN0 engine is 1900NaN0 and the landing roll is 2200NaN0.
The manufacturer estimates the construction time from the supplied kit as 350 hours.
By 1998 the company reported that five aircraft were completed and flying.
In January 2014 four examples were registered in the United States with the Federal Aviation Administration, although a total of nine had been registered at one time.[2]