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Aeroprakt A-28 Victor
The Aeroprakt A-28 Victor is a Ukrainian light aircraft, designed and produced by Aeroprakt of Kiev. The aircraft is supplied as a complete ready-to-fly-aircraft.〔Bayerl, Robby; Martin Berkemeier; et al: ''World Directory of Leisure Aviation 2011-12'', page 154. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X〕
==Design and development==
The design goals for the A-28 included twin engines for safety over hazardous terrain, a payload of with four seats, 10 hours endurance, as well as good short and rough field capabilities. The resulting design features a cantilever low-wing, a four-seat enclosed cabin accessed through a hinged windshield, a T-tail, fixed conventional landing gear and a twin engines in tractor configuration.〔
The aircraft has mixed construction, with the forward fuselage made from fibreglass and the tail cone of aluminum sheet. The wings and tail are all-aluminum, while the control surfaces are aluminum frames covered in doped aircraft fabric. Its span wing employs a TsAGI P-IIIA-15 airfoil, has an area of and mounts flaps. The standard engines fitted are two Rotax 912 or two Rotax 912S powerplants. The conventional landing gear fits wheel pants and features a steerable tailwheel.〔
The A-28 has an empty weight of and a gross weight of , giving a useful load of .〔
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
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