|
The Tecnam 2010 is a four-seat, high wing, single engine light aircraft of mixed metal and carbon-fiber-reinforced polymer construction. Designed and built in Italy, it was first presented in public in April 2011. ==Design and development== The Tecnam P2010 is a larger, four seat relative of the Tecnam P2008 two seat braced high wing light aircraft. Both types have metal wings and tailplane on a composite fuselage with integrated fin.〔 The wing leading edge is straight except for some pinching at the root and the wing has constant chord on the inner section. Outboard, the trailing edge is tapered; the straight wing tips are slightly upturned. Ailerons span the outboard panels and the inner sections carry flaps. There is a single lift strut on each side, attached to the lower fuselage. The P2010 has a low set all-moving constant chord tailplane with an anti-balance tab. The fin is swept and the rudder moves above the tailplane.〔 The P2010 is powered by a 135 kW (180 hp) Lycoming IO-360-M1A horizontally opposed four cylinder piston engine. The cabin seats the pilot and three passengers in two side-by-side rows, accessed by three doors. Its fixed tricycle undercarriage has spring cantilever main legs and a castoring nosewheel. All wheels have speed fairings.〔〔 The P2010 was first seen in public at AERO Friedrichshafen 2011〔 and first flew on 12 April 2012. The company initially planned to have US FAR Part 23 certification completed by November 2012 and said it would refund deposits if the aircraft was not certified by the end of 2014.〔 European European Aviation Safety Agency certification was completed in September 2014, but American Federal Aviation Administration certification was still ongoing in July 2015.〔(【引用サイトリンク】title=Tecnam P2010 Nearing FAA Certification )〕 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「Tecnam P2010」の詳細全文を読む スポンサード リンク
|