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CFM56-7B26 ✕
Family CFM56-7B
EASA ID 8CM051
Aircraft Engine Manufacturer CFM International
Aircraft Engine Type Turbofan
Comment Boeing 737 Next Generation
Dry Weight (kg) 2366
Diameter (mm) 1549
Max Rotating Diameter (mm) 1549
Length (mm) 2507
Wikipedia Article (URL) en.wikipedia.org/wiki/CFM_International_CFM56
Fuel Jet A
Fan Blades 24
Geared Fan No
Low-Pressure Compressor Stages 3
High-Pressure Compressor Stages 9
High Pressure Compressor Stages 1
Low-Pressure Turbine Stages 4
Afterburner No
Streams 2
Bypass Ratio 5.1
Overall Pressure Ratio 27.61
Maximum Takeoff Thrust (kN) 116.99
Hydrocarbon Take Off (g/kg fuel) 0.1
Hydrocarbon Climb Out (g/kg fuel) 0.1
Hydrocarbon Approach (g/kg fuel) 0.1
Hydrocarbon Idle (g/kg fuel) 1.9
Hydrocarbon Unitary Average (g/kN) 3.06
Hydrocarbon Unitary Characteristic (g/kN) 4.7
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 24
Hydrocarbon LTO (g) 361
Carbon Monoxide Take Off (g/kg fuel) 0.2
Carbon Monoxide Climb Out (g/kg fuel) 0.6
Carbon Monoxide Approach (g/kg fuel) 1.6
Carbon Monoxide Idle (g/kg fuel) 18.8
Carbon Monoxide Unitary Average (g/kN) 30.33
Carbon Monoxide Unitary Characteristic (g/kN) 37.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 31.5
NOx Take Off (g/kg fuel) 28.8
NOx Climb Out (g/kg fuel) 22.5
NOx Approach (g/kg fuel) 10.8
NOx Idle (g/kg fuel) 4.7
NOx Unitary Average (g/kN) 52.64
NOx Unitary Characteristic (g/kN) 61
NOx Unitaryto Standard (% of limit) 64
NOx Unitaryto CAEP2 (% of limit) 80.1
NOx Unitaryto CAEP4 (% of limit) 96.6
NOx Unitaryto CAEP6 (% of limit) 109.7
NOx Unitaryto CAEP8 (% of limit) 130.5
NOx LTO (g) 6149
Smoke Take Off (SN) 14.7
Smoke Climb Out (SN) 11.9
Smoke Approach (SN) 0
Smoke Idle (SN) 0
Smoke Max (SN) 14.7
Smoke Characteristic (SN) 18.9
Smoke Characteristicto Regulatory (% of limit) 83.4
Fuel Flow Take Off (kg/s) 1.221
Fuel Flow Climbout (kg/s) 0.999
Fuel Flow Approach (kg/s) 0.338
Fuel Flow Idle (kg/s) 0.113
Fuel LTO (kg) 441
Carbon Monoxide LTO (g) 3533
Compressor Description 1 fan, 3-stage LP, 9-stage HP
Emissions Data Status C
Engine Status Out of production
Turbine Description 1-stage HP, 4-stage LP