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Ekolot JK-05L Junior : ウィキペディア英語版 | Ekolot JK-05L Junior
The Ekolot JK-05L Junior is a Polish ultralight aircraft, designed and produced by Ekolot of Krosno. It was certified in Poland in February 2010. The aircraft is supplied as a kit for amateur construction or as a complete ready-to-fly aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 44. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The JK-05L was designed to comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced high wing, an enclosed cockpit with two seats in side-by-side configuration, fixed tricycle landing gear and a single engine in tractor configuration.〔 The aircraft is made from composites. Its span wing employs an NN-1817 airfoil, has an area of and employs carbon fibre flaperons. The twin fuel tanks are located behind the seats. A ballistic parachute is available. The controls include a single, centrally-mounted centre stick and electric trim. The standard engine is the Rotax 912UL four-stroke powerplant.〔 The JK-05L was later developed into the Ekolot KR-030 Topaz.〔
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