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Quad City Challenger : ウィキペディア英語版
Quad City Challenger


The Quad City Challenger is a family of one and two seats-in-tandem, pusher configuration, tricycle landing gear ultralight aircraft that is designed and produced by Quad City Aircraft Corporation of Moline, Illinois. The Challenger was first introduced in 1983.〔Vandermeullen, Richard: ''2011 Kit Aircraft Buyer's Guide'', Kitplanes, Volume 28, Number 12, December 2011, page 66 Belvoir Publications. ISSN 0891-1851〕〔(Challenger Advanced Ultralight & Light Sport Aircraft - National Ultralight Canada & Quad City U.S )〕〔Kitplanes Staff: ''2008 Kit Aircraft Directory'', page 67, Kitplanes Magazine December 2007 Volume 24, Number 12, Belvior Publications, Aviation Publishing Group LLC.〕
==Design and development==
The Challenger ultralight is a high wing, tricycle gear kit aircraft with a frame structure built from 6061-T6 aluminum alloy tubing fastened with aircraft grade AN bolts and rivets and covered with either presewn Dacron envelopes or standard aircraft fabric. The engine is mounted in pusher configuration and turns the propeller through a reduction drive that uses a cogged tooth rubber belt.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, pages B-11 & B-71. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕
The kit can be purchased in 4 major sub-kits: the Tail Assembly, Fuselage, Wings, and Engine. The factory kit is supplied with the most difficult mechanical work already completed. This includes the primary fuselage framework along with the controls and the basic wing structures assembled at the factory. The kit builder is required to finish the smaller structural components, cover the aluminum frames with fabric, seal and paint the fabric and do the final assembly.〔
The aircraft has the ability to soar with its motor switched off.
The Challenger design has been criticized by reviewers for its landing gear, which is a rigid cable-braced type and is subject to being bent during hard landings. A number of after-market suppliers have designed steel gear legs as replacements for the stock landing gear in an attempt to rectify this problem. The improved factory-designed Light Sport Special (LSS) model incorporates revised landing gear to address this deficiency.〔Cliche, Andre: ''Ultralight Aircraft Shopper's Guide'' 8th Edition, pages B-75. Cybair Limited Publishing, 2001. ISBN 0-9680628-1-4〕〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 116. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕

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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