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__NOTOC__ The Mustang Aeronautics Mustang II is a two-seat aerobatic sports airplane developed and marketed in the United States for homebuilding.〔Vandermeullen, Richard: ''2012 Kit Aircraft Buyer's Guide'', Kitplanes, Volume 28, Number 12, December 2011, page 62. Belvoir Publications. ISSN 0891-1851〕〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 113. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== Robert Bushby acquired the rights to the Long Midget Mustang in 1959 and four years later began development of a two-seat, side-by-side version. This eventually flew in 1966 and plans were made available soon thereafter. Rights to both the Midget Mustang and the Mustang II were sold to Mustang Aeronautics in 1992. 〔(【引用サイトリンク】 Mustang Aeronautics - About )〕 A single engine in tractor configuration airplane, the Mustang II features cantilever low-wing, two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed conventional landing gear, or, optionally, tricycle landing gear.〔 The aircraft is made from riveted sheet aluminum with a rounded turtle deck and flat sides and bottom skins. Its span wing employs a NACA 64A212 airfoil at the wing root, transitioning to a NACA 64A210 at the wingtip. Standard engines used include the Lycoming O-320, the Lycoming O-360 and the fuel-injected Lycoming IO-360 four-stroke powerplants.〔 Standard fuel capacity is 25 US gallons, but optional wet wings increase the fuel capacity to 61 US gallons.〔(【引用サイトリンク】 Mustang II Specifications )〕 Several other fuel tank options are available.〔(【引用サイトリンク】 M-II FAQs Fuel Options )〕 A folding wing option may be installed.〔(【引用サイトリンク】 Mustang II Folding Wing )〕 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「Mustang Aeronautics Mustang II」の詳細全文を読む スポンサード リンク
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