The Pratt & Whitney Canada PW200 is a family of turboshaft engines developed specifically for helicopter applications. It entered service in the 1990s.
Variants PW205B First run 1987. Flown in twin-engine MBB BO105 for demonstration only."Power The Pratt & Whitney Canada Story" Sullivan and Milberry, CANAV Books 1989, , p.300 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 PW207K Maximum continuous power . for use on the Kazan Ansat PW209T Maximum continuous power . "Twin-pack" First run 1985, cancelled 1987. Intended for Bell TwinRanger PW210 Enhanced version of the PW200. Enhancements include; Lower fuel consumption, Dual Channel Full Authority Digital Engine Control (FADEC), Reduced environmental emissions and an Increase in power output ranging from to .
Applications AgustaWestland AW109 AgustaWestland AW169 Airbus Helicopters H160 (prototype only) Bell 360 Invictus (planned) Bell 429 GlobalRanger Boeing A160 Hummingbird Eurocopter EC135 Kazan Ansat MD Helicopters MD Explorer Sikorsky S-76D
Specifications
References
External links Pratt & Whitney Canada PW200 webpage Pratt & Whitney Canada PW210 webpage