CF34-10E6A1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 5.4
Dry weight: 2079 kilogram
Fan diameter: 1.3 metre
Fan stages: 1
HP compressor stages: 9
HP turbine stages: 1
Height: 2.2 metre
LP compressor stages: 3
LP turbine stages: 4
Length: 4.52 metre
Max. continuous thrust: 75.8 kilonewton
N1 RPM: 5954
N2 RPM: 17160
Overall pressure ratio: 29
Max. takeoff thrust: 83.72 kilonewton
Width: 1.86 metre
ICAO: E190
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