Pratt & Whitney Canada PW200

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.


 * PW206A
 * Maximum continuous power 550 shp (410 kW) for use on the MD Explorer


 * PW206B
 * Maximum continuous power 431 shp, for use on the Eurocopter EC135


 * PW206B2
 * Maximum continuous power 431 shp.


 * PW206C
 * Maximum continuous power 561 shp, for use on the Agusta A109 Power


 * PW206E
 * Maximum continuous power 572 shp. for use on the MD Explorer


 * PW207C
 * Maximum continuous power 572 shp.


 * PW207D
 * Maximum continuous power 572 shp.


 * PW207D1
 * Variant of the PW207 with increased mechanical power, maximum continuous power 610 shp.


 * PW207D2
 * Variant of the PW207D1 with a fuel heater installed, maximum continuous power 610 shp.


 * PW207E
 * Maximum continuous power 572 shp. for use on the MD 902


 * PW209T
 * Maximum continuous power 800 shp. "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 800 shp to 1000 shp

Applications

 * AgustaWestland AW109
 * AgustaWestland AW169
 * Airbus Helicopters H160 (prototype only)
 * Bell 360 Invictus (planned)
 * Bell 429 GlobalRanger
 * Boeing A160 Hummingbird
 * Eurocopter EC135
 * MD Helicopters MD Explorer
 * Sikorsky S-76D