CFM56-7B22/B1 is a turbofan engine model used in aircraft.
Engine Family: turbofan
Bypass ratio: 5.3
Control system: Dual channel FADEC
Dry weight: 2386 kilogram
Fan blades: 24
Fan diameter: 1.55 metre
Fan stages: 1
HP compressor stages: 9
HP turbine stages: 1
Height: 1.83 metre
LP compressor stages: 3
LP turbine stages: 4
Length: 2.51 metre
Max. continuous thrust: 99.2 kilonewton
N1 RPM: 5175
N2 RPM: 14460
Overall pressure ratio: 32.7
Max. takeoff thrust: 100.97 kilonewton
Width: 2.12 metre
