CFM56-2A is a turbofan engine model used in aircraft.
Engine Family: turbofan
Max. takeoff thrust: 106.76 kilonewton
Max. continuous thrust: 102.3 kilonewton
Bypass ratio: 5.9
Control system: Hydro mechanical and limited electronic
Dry weight: 2200 kilogram
Fan blades: 44
Fan diameter: 1.73 metre
Fan stages: 1
HP compressor stages: 9
HP turbine stages: 1
Height: 2.14 metre
LP compressor stages: 3
LP turbine stages: 4
Length: 2.43 metre
N1 RPM: 5176
N2 RPM: 14460
Overall pressure ratio: 31.8
Width: 1.83 metre
