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The Pratt & Whitney Canada PW200 is a family of turbine engines developed specifically for helicopter applications. ==Variants== ;PW206A :Maximum continuous power 550 shp (410 kW) 〔 for use on the MD Explorer ;PW206B :Maximum continuous power ,〔 for use on the Eurocopter EC135 ;PW206B2 :Maximum continuous power .〔 ;PW206C :Maximum continuous power ,〔 for use on the Agusta A109 Power ;PW206E :Maximum continuous power .〔 for use on the MD Explorer ;PW207C :Maximum continuous power .〔 ;PW207D :Maximum continuous power .〔 ;PW207D1 :Variant of the PW207 with increased mechanical power, maximum continuous power .〔 ;PW207D2 :Variant of the PW207D1 with a fuel heater installed, maximum continuous power .〔 ;PW207E :Maximum continuous power .〔 for use on the MD 902 ;PW210:Approx 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「Pratt & Whitney Canada PW200」の詳細全文を読む スポンサード リンク
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