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V-STOL Super Solution 2000 : ウィキペディア英語版
V-STOL Super Solution 2000

The V-STOL Super Solution 2000 is an American STOL homebuilt aircraft that was designed by Dick Turner and produced by V-STOL Aircraft Corporation of Fort Myers, Florida. When it was available the aircraft was supplied as a kit for amateur construction.〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition'', page 280. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1〕
==Design and development==
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 span wing uses a single surface high-lift airfoil, mounts flaps and has a wing area of . The cockpit width is . The acceptable power range is and the standard engine used is the 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 and a gross weight of , giving a useful load of . With full fuel of the payload for the pilot, passenger and baggage is .〔
The standard day, sea level, no wind, take off with a engine is and the landing roll is . The take-off speed while flying solo is.〔
The manufacturer estimated the construction time from the supplied kit as 100 hours.〔

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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