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CFM56-5B4/3 ✕ V2528-D5 ✕
Family CFM56-5B
EASA ID 01P08CM105 1IA004
Aircraft Engine Manufacturer CFM International International Aero Engines
Aircraft Engine Type Turbofan 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 Jet A
Fan Blades 36
Geared Fan No No
Low-Pressure Compressor Stages 4
High-Pressure Compressor Stages 9
Combustion Chamber Tech Insertion
High Pressure Compressor Stages 1
Low-Pressure Turbine Stages 4
Afterburner No No
Streams 2 2
Bypass Ratio 5.7 4.66
Overall Pressure Ratio 27.3 30
Maximum Takeoff Thrust (kN) 120.1 124.5
Hydrocarbon Take Off (g/kg fuel) 0.02 0.043
Hydrocarbon Climb Out (g/kg fuel) 0.02 0.041
Hydrocarbon Approach (g/kg fuel) 0.05 0.058
Hydrocarbon Idle (g/kg fuel) 1.92 0.102
Hydrocarbon Unitary Average (g/kN) 2.61 0.27
Hydrocarbon Unitary Sigma (g/kN) 0.36
Hydrocarbon Unitary Range (g/kN) 2.21-2.93
Hydrocarbon Unitary Characteristic (g/kN) 3.05 0.4
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 15.6 2.1
Hydrocarbon LTO (g) 314 34
Carbon Monoxide Take Off (g/kg fuel) 0.25 0.47
Carbon Monoxide Climb Out (g/kg fuel) 0.16 0.56
Carbon Monoxide Approach (g/kg fuel) 3.24 2.03
Carbon Monoxide Idle (g/kg fuel) 32.07 11.53
Carbon Monoxide Unitary Average (g/kN) 44.84 21.5
Carbon Monoxide Unitary SD (g/kN) 2.4
Carbon Monoxide Unitary Range (g/kN) 42-46.6
Carbon Monoxide Unitary Characteristic (g/kN) 48.5 26.4
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 41.1 22.4
NOx Take Off (g/kg fuel) 21.57 30.5
NOx Climb Out (g/kg fuel) 17.23 25.1
NOx Approach (g/kg fuel) 8.85 9.6
NOx Idle (g/kg fuel) 4.22 4.9
NOx Unitary Average (g/kN) 37.56 53.7
NOx Unitary SD (g/kN) 1.1
NOx Unitary Range (g/kN) 36.6-38.8
NOx Unitary Characteristic (g/kN) 39.8 62.2
NOx Unitaryto Standard (% of limit) 42.1 62.2
NOx Unitaryto CAEP2 (% of limit) 52.6 77.8
NOx Unitaryto CAEP4 (% of limit) 63.5 92.9
NOx Unitaryto CAEP6 (% of limit) 72.2 105.6
NOx Unitaryto CAEP8 (% of limit) 85.9 124.1
NOx LTO (g) 4511 6686
Smoke Take Off (SN) 13.4 5
Smoke Climb Out (SN) 9.9 6.6
Smoke Approach (SN) 2.1 4.5
Smoke Idle (SN) 2.1 2.4
Smoke Max (SN) 13.4 9
Smoke Sigma (SN) 4.5
Smoke Range (SN) 8.4-16.9
Smoke Characteristic (SN) 14.7 11.6
Smoke Characteristicto Regulatory (% of limit) 65.3 52
Fuel Flow Take Off (kg/s) 1.142 1.209
Fuel Flow Climbout (kg/s) 0.939 0.996
Fuel Flow Approach (kg/s) 0.316 0.353
Fuel Flow Idle (kg/s) 0.102 0.134
Fuel LTO (kg) 407 476
Fuel Venting Compliant Yes No
Carbon Monoxide LTO (g) 5386 2680
Compressor Description 1 fan, 4-stage LP, 9-stage HP
Emissions Data Status C C
Engine Status Out of production Out of production
NOx Compliance Demonstration 2.3.2 e)
nvPME Imass Approach (mg/kg) 1.47
nvPME Imass Climb Out (mg/kg) 41.4
nvPME Imass Idle (mg/kg) 0.77
nvPME Imass Max (mg/kg) 61.3
nvPME Imass Take Off (mg/kg) 61.3
nvPME Inum Approach (#/kg) 61800000000000
nvPME Inum Climb Out (#/kg) 433000000000000
nvPME Inum Idle (#/kg) 31800000000000
nvPME Inum Max (#/kg) 433000000000000
nvPME Inum Take Off (#/kg) 416000000000000
nvPMLTO Mass (mg) 8304
nvPMLTO Mass Per Thrust (mg/kN) 96.1
nvPMLTO Mass To CAEP11 (% of limit) 22.8
nvPMLTO Number (#) 83400000000000000
nvPMLTO Number Per Thrust (#/kN) 965000000000000
nvPMLTO Number To CAEP11 (% of limit) 18.6
nvPM Mass Concentration Characteristic (mg/m³) 1918
nvPM Mass Concentration Max (mg/m³) 1490
nvPM Mass Concentration To CAEP10 (% of limit) 31.8
Turbine Description 1-stage HP, 4-stage LP