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Weller UW-9 Sprint : ウィキペディア英語版 | Weller UW-9 Sprint
The Weller UW-9 Sprint is a German ultralight aircraft designed and produced by Weller Flugzeugbau of Bibersfeld. 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 84. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕 ==Design and development== The UW-9 is intended as a nostalgic 1930s style design that would comply with the Fédération Aéronautique Internationale microlight rules. It features a strut-braced parasol wing, a two-seats-in-tandem open cockpit, fixed conventional landing gear and a single engine in tractor configuration.〔 The aircraft fuselage is made from welded steel tubing, with bolted-together aluminum tubing spar ladder-construction wings, all covered in doped aircraft fabric. Its span wing has an area of and a cut-out in the centre trailing edge for rear cockpit access. The wing is supported by "V"-struts and jury struts. The tailplane is also supported by "V"-struts. Standard engines available are the Sauer UL 2100, the Limbach L2000EA, the Rotax 912ULS four-stroke powerplants, or the Rotec R2800 radial engine. The Sprint is approved for aero-towing gliders and banner towing in Germany.〔〔
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