CF34-10E2A1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
N1 RPM: 5954
N2 RPM: 17160
Max. takeoff thrust: 75.44 kilonewton
Max. continuous thrust: 67.21 kilonewton
Height: 2.2 metre
Width: 1.86 metre
Length: 4.52 metre
Dry weight: 2079 kilogram
Bypass ratio: 5.4
Overall pressure ratio: 29
Fan diameter: 1.3 metre
Fan stages: 1
LP compressor stages: 3
HP compressor stages: 9
LP turbine stages: 4
HP turbine stages: 1
