The last two digits of each variant model number represent the nominal power at takeoff, in hundreds of horsepower.
Other variants ; PW119 : , no longer in service. ; PW124 : , no longer in service. ; PW124A : No longer in service. ; PW125 : No longer in service. ; PW125A : No longer in service. ; PW127TS : turboshaft version that powered the first 2 prototypes of the
Mil Mi-38 helicopter and was to be used on the Mi-38-1 variant. ; PW127XT-S : Selected to power the
Deutsche Aircraft D328eco in June 2022. ; PW130 : Unsuccessfully offered for the
Saab 2000 and
IPTN N-250 aircraft. Proposed for the unbuilt
Fokker 50-400 aircraft. ; PW150 Twin Pack : Proposed powerplant for the
Airbus A400M. Two PW150-based engines would be used to drive a single propeller. The powerplant was eliminated from contention by Airbus in early June 1999, since it was short of providing the required to drive the eight-bladed propeller at the time, and its specific fuel consumption (SFC) was excessive. ; PW150B : Proposed powerplant for the
Shaanxi Y-8F-600. Abandoned in December 2008 when the United States government barred a U.S.-based subcontractor from exporting the engine control software for the PW150B. ; PW150C : Proposed powerplant for the
Xian MA700. Includes a third-stage power turbine, larger-diameter propellers, modified
reduction gearbox, and optimized low-pressure compressor. Has higher thrust, higher speed, and extended range compared to the PW150A. Blocked from an export license by the Canadian government in 2020, because of the Chinese government's retaliatory detention of Canadian citizens (the "
two Michaels") starting in 2018. ; ST18M : Marine application for the PW100. ; ST40 : PW150 derivative adapted for the
Bombardier JetTrain, which was proposed for use in high-speed train travel in North America. ; ST40M : Marine application for the PW150A. ==Applications==