H85-200

Engine model
Manufacturer GE Aviation Czech
Engine type Turboprop

Technical specifications

Design
Compressor stages
3
Control system Hydromechanical
Gas generator stages
1
Power turbine stages
1
Dimensions
Height
0.65 m
2.13 ft
Length
1.68 m
5.51 ft
Width
0.59 m
1.94 ft
Power limits
Max. continuous power
634 kW
850 hp
Max. takeoff power
634 kW
850 hp
Rotation speeds
N1 RPM
36,660
N2 RPM
30,960
Output shaft RPM
1,950
Weights
Dry weight
202 kg
445 lb