Developed from the V-STOL Solution, the Super Solution 2000 was developed for flight training, recreational flying and crop dusting. It features a cable-braced parasol wing, a two-seats-in-tandem open cockpit without a windshield, fixed conventional landing gear with wheel pants and a single engine in pusher configuration.
The aircraft is made from bolted-together aluminum tubing, with its flying surfaces covered in Dacron sailcloth. Its 321NaN1 span wing uses a single surface high-lift airfoil, mounts flaps and has a wing area of 165square feet. The cockpit width is 34inches. The acceptable power range is 40to and the standard engine used is the 450NaN0 2si 460 two-stroke powerplant. Original factory options included a full cockpit enclosure and dual controls.
The Super Solution 2000 has a typical empty weight of 380lb and a gross weight of 890lb, giving a useful load of 510lb. With full fuel of the payload for the pilot, passenger and baggage is 450lb.
The standard day, sea level, no wind, take off with a 450NaN0 engine is 1000NaN0 and the landing roll is 1500NaN0. The take-off speed while flying solo is180NaN0.
The manufacturer estimated the construction time from the supplied kit as 100 hours.
By 1998 the company reported that six kits had been sold and two aircraft were completed and flying.
In March 2014 no examples were registered in the United States with the Federal Aviation Administration, although one had been registered at one time.[2]