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CFM56-5B8/P ✕
Family CFM56-5B
EASA ID 7CM048
Aircraft Engine Manufacturer CFM International
Aircraft Engine Type Turbofan
Comment Airbus A318, A319, A320, A321
Dry Weight (kg) 2381
Diameter (mm) 1735
Max Rotating Diameter (mm) 1735
Length (mm) 2601
Wikipedia Article (URL) en.wikipedia.org/wiki/CFM_International_CFM56
Fuel Jet A
Fan Blades 36
Geared Fan No
Low-Pressure Compressor Stages 4
High-Pressure Compressor Stages 9
Combustion Chamber SAC
High Pressure Compressor Stages 1
Low-Pressure Turbine Stages 4
Afterburner No
Streams 2
Bypass Ratio 5.9
Overall Pressure Ratio 22.6
Maximum Takeoff Thrust (kN) 94.7
Hydrocarbon Take Off (g/kg fuel) 0.1
Hydrocarbon Climb Out (g/kg fuel) 0.1
Hydrocarbon Approach (g/kg fuel) 0.9
Hydrocarbon Idle (g/kg fuel) 6.5
Hydrocarbon Unitary Average (g/kN) 10.8
Hydrocarbon Unitary Characteristic (g/kN) 16.6
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 84.7
Hydrocarbon LTO (g) 1023
Carbon Monoxide Take Off (g/kg fuel) 0.8
Carbon Monoxide Climb Out (g/kg fuel) 0.8
Carbon Monoxide Approach (g/kg fuel) 3.9
Carbon Monoxide Idle (g/kg fuel) 32.9
Carbon Monoxide Unitary Average (g/kN) 54.4
Carbon Monoxide Unitary Characteristic (g/kN) 66.8
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 56.6
NOx Take Off (g/kg fuel) 19.7
NOx Climb Out (g/kg fuel) 16.7
NOx Approach (g/kg fuel) 8.4
NOx Idle (g/kg fuel) 3.4
NOx Unitary Average (g/kN) 35.4
NOx Unitary Characteristic (g/kN) 41
NOx Unitaryto Standard (% of limit) 48.1
NOx Unitaryto CAEP2 (% of limit) 60.2
NOx Unitaryto CAEP4 (% of limit) 74.4
NOx Unitaryto CAEP6 (% of limit) 84.5
NOx Unitaryto CAEP8 (% of limit) 103.3
NOx LTO (g) 3358
Smoke Take Off (SN) 5.4
Smoke Climb Out (SN) 1.5
Smoke Approach (SN) 0.3
Smoke Idle (SN) 0.6
Smoke Max (SN) 5.4
Smoke Characteristic (SN) 6.9
Smoke Characteristicto Regulatory (% of limit) 28.7
Fuel Flow Take Off (kg/s) 0.875
Fuel Flow Climbout (kg/s) 0.729
Fuel Flow Approach (kg/s) 0.262
Fuel Flow Idle (kg/s) 0.094
Fuel LTO (kg) 342
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 5176
Compressor Description 1 fan, 4-stage LP, 9-stage HP
Emissions Data Status C
Engine Status Out of production
Turbine Description 1-stage HP, 4-stage LP