CFM56-5C4 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Fan diameter: 1.84 metre
HP turbine stages: 1
LP turbine stages: 5
HP compressor stages: 9
LP compressor stages: 4
Fan stages: 1
Fan blades: 36
Dry weight: 2644 kilogram
Overall pressure ratio: 38.3
Bypass ratio: 6.4
N2 RPM: 14460
N1 RPM: 4784
Length: 2.62 metre
Width: 1.95 metre
Height: 2.25 metre
Control system: Dual channel FADEC
Max. continuous thrust: 133.71 kilonewton
Max. takeoff thrust: 151.24 kilonewton
ICAO: A342
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