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Aviation Industries of Iran AVA-202 : ウィキペディア英語版 | Aviation Industries of Iran AVA-202
The Aviation Industries of Iran AVA-202 is an Iranian two-seat, light aircraft designed as a trainer and sporting aircraft. It was intended for the Iranian domestic market to avoid dependence on imports.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 156. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The AVA-202 was based on the Van's Aircraft RV-6A and was designed to comply with European JAR-22 and JAR-VLA aircraft certification rules. It features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, fixed tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from aluminum sheet. Its span wing employs a NACA 63-215 airfoil at the wing root and a NACA 63-015 airfoil at the wing tip. The wingspan is greater than the RV-6's wingspan of from which it is derived. The AVA-202's wing has an area of and is equipped with flaps. The standard engine fitted is the Lycoming AEIO-320-B2B four-stroke aerobatic powerplant.〔
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「Aviation Industries of Iran AVA-202」の詳細全文を読む
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