PW206B2

Engine model
Manufacturer Pratt & Whitney Canada
Engine type Turboshaft

Technical specifications

Design
Compressor stages
1
Control system Single channel FADEC + Hydromechanical backup control
Gas generator stages
1
Power turbine stages
1
Dimensions
Height
0.73 m
2.4 ft
Length
1.04 m
3.41 ft
Width
0.52 m
1.71 ft
Power limits
Max. continuous power
321 kW
430 hp
Max. takeoff power
333 kW
447 hp
Rotation speeds
N1 RPM
58,000
N2 RPM
39,123
Output shaft RPM
6,134
Torque limits
Max. continuous torque
50 daN/m
368.8 lbf⋅ft
Max. takeoff torque
51.9 daN/m
382.8 lbf⋅ft
Max. transient overtorque
73.2 daN/m
539.9 lbf⋅ft
Weights
Dry weight
117 kg
258 lb

Aircraft models

Manufacturer Name Aircraft family
Airbus Helicopters EC135 P2 (CPDS) Helicopter
Airbus Helicopters EC135 P2+ Helicopter
Airbus Helicopters EC635 P2+ Helicopter
Military