CFM56-5A4 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Fan diameter: 1.73 metre
HP turbine stages: 1
LP turbine stages: 4
HP compressor stages: 9
LP compressor stages: 3
Fan stages: 1
Fan blades: 36
Dry weight: 2270 kilogram
Overall pressure ratio: 31.3
Bypass ratio: 6.2
N2 RPM: 14460
N1 RPM: 5000
Length: 2.42 metre
Width: 1.91 metre
Height: 2.1 metre
Control system: Dual channel FADEC
Max. continuous thrust: 91.95 kilonewton
Max. takeoff thrust: 97.86 kilonewton
ICAO: A319
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