CF34-8C1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 4.9
Dry weight: 1227 kilogram
Fan diameter: 1.17 metre
Fan stages: 1
HP compressor stages: 10
HP turbine stages: 2
Height: 1.54 metre
LP turbine stages: 4
Length: 3.87 metre
Max. continuous thrust: 59.05 kilonewton
N1 RPM: 7400
N2 RPM: 17820
Overall pressure ratio: 27
Max. takeoff thrust: 61.34 kilonewton
Width: 1.54 metre
ICAO: CRJ7
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