PW210S

Engine model
Manufacturer Pratt & Whitney Canada
Engine type Turboshaft

Technical specifications

Design
Compressor stages
2
Control system Dual channel EECU
Gas generator stages
1
Power turbine stages
2
Dimensions
Length
1.11 m
3.64 ft
Power limits
Max. continuous power
599 kW
803 hp
Max. takeoff power
599 kW
803 hp
Rotation speeds
N1 RPM
51,000
N2 RPM
26,383
Output shaft RPM
6,409
Torque limits
Max. continuous torque
89.2 daN/m
657.9 lbf⋅ft
Max. takeoff torque
89.2 daN/m
657.9 lbf⋅ft
Max. transient overtorque
121.2 daN/m
893.9 lbf⋅ft
Weights
Dry weight
162 kg
357 lb

Aircraft models

Manufacturer Name Aircraft family
Sikorsky S-76D Helicopter