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US Light Aircraft Hornet : ウィキペディア英語版
US Light Aircraft Hornet

The US Light Aircraft Hornet is an American two-seats-in-tandem, pusher configuration, tricycle gear, strut-braced high wing ultralight aircraft, that was produced US Light Aircraft Corporation of Ramona, California between 1994 and circa 2008 in kit form for amateur construction. It was also available as a factory-completed light-sport aircraft.〔〔〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, page B-84. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕〔Downey, Julia: ''1999 Kit Aircraft Directory'', Kitplanes, Volume 15, Number 12, December 1998, page 74. Primedia Publications. ISSN 0891-1851〕〔Downey, Julia: ''2001 Kit Aircraft Directory'', Kitplanes, Volume 17, Number 12, December 2000, page 79. Kitplanes Acquisition Company. ISSN 0891-1851〕〔Purdy, Don: ''AeroCrafter - Homebuilt Aircraft Sourcebook'', page 278. BAI Communications. ISBN 0-9636409-4-1〕〔Bertrand, Noel; Rene Coulon; et al: ''World Directory of Leisure Aviation 2003-04'', pages 22-23. Pagefast Ltd, Lancaster OK, 2003. ISSN 1368-485X〕
After US Light Aircraft ceased production the design was taken up by Higher Class Aviation and then later Oklahoma Light Aircraft of Blackwell, Oklahoma, which reportedly had the Hornet in production in 2011.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 66. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 By July 2012 Oklahoma Light Aircraft's website had been removed and the company appeared to be out of business.
==Design and development==
The Hornet was first introduced at Sun 'n Fun in 1994. Externally the aircraft greatly resembles the Quad City Challenger II, but internally the structure is very different. When it was available the Hornet was priced considerably higher than the Challenger II.〔
The Hornet structure is built up from aluminium tubing, riveted together with gussets. The aircraft is then covered with doped aircraft fabric. The Hornet's wing incorporates dual bridge-section spars, with a single strut and V-jury struts. The wing was sandbag-tested to 7g without failure. The aircraft includes electric flaps and trim, dual controls and two wing-mounted fuel tanks. The landing gear incorporates pneumatic suspension on all three wheels, including the steerable nosewheel, and hydraulic brakes on the mainwheels. The Hornet can also be equipped with floats or skis. Early production aircraft experienced elevator flutter at speeds in excess of but this was addressed by mass-balancing the elevator.〔〔
Reported construction times from the kit are 250–300 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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