PZL-10W is a turboshaft engine model used in aircraft.
Engine Family: turboshaft
Compressor stages: 7
Dry weight: 141 kilogram
Gas generator stages: 2
Height: 0.6 metre
Length: 1.88 metre
Max. continuous power: 574 kilowatt
Max. takeoff power: 662 kilowatt
Ng RPM: 31486
Np RPM: 22490
Output shaft RPM: 23615
Power turbine stages: 1
Width: 0.74 metre
ICAO: W3
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