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CFM56-5C2/P ✕ IAE V2500 ✕
Family CFM56-5C
EASA ID 7CM045
Aircraft Engine Manufacturer CFM International IAE
Aircraft Engine Type Turbofan Turbofan
Comment Airbus A340-200/-300
Dry Weight (kg) 3990 2595
Diameter (mm) 1836 1682
Max Rotating Diameter (mm) 1836
Length (mm) 3201
Wikipedia Article (URL) en.wikipedia.org/wiki/CFM_International_CFM56 en.wikipedia.org/wiki/IAE_V2500
Fuel Jet A
Geared Fan No No
Combustion Chamber SAC Annular
Afterburner No No
Streams 2 2
Bypass Ratio 6.8
Overall Pressure Ratio 28.2
Maximum Takeoff Thrust (kN) 137.61 140.56
Thrust To Weight 4.18
Hydrocarbon Take Off (g/kg fuel) 0
Hydrocarbon Climb Out (g/kg fuel) 0
Hydrocarbon Approach (g/kg fuel) 0
Hydrocarbon Idle (g/kg fuel) 5.8
Hydrocarbon Unitary Average (g/kN) 7.2
Hydrocarbon Unitary Characteristic (g/kN) 11.1
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 56.6
Hydrocarbon LTO (g) 986
Carbon Monoxide Take Off (g/kg fuel) 0.8
Carbon Monoxide Climb Out (g/kg fuel) 0.7
Carbon Monoxide Approach (g/kg fuel) 2.1
Carbon Monoxide Idle (g/kg fuel) 35.1
Carbon Monoxide Unitary Average (g/kN) 45.7
Carbon Monoxide Unitary Characteristic (g/kN) 56.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 47.6
NOx Take Off (g/kg fuel) 29.7
NOx Climb Out (g/kg fuel) 23.8
NOx Approach (g/kg fuel) 9.3
NOx Idle (g/kg fuel) 3.9
NOx Unitary Average (g/kN) 45.4
NOx Unitary Characteristic (g/kN) 52.6
NOx Unitaryto Standard (% of limit) 54.6
NOx Unitaryto CAEP2 (% of limit) 68.2
NOx Unitaryto CAEP4 (% of limit) 82.1
NOx Unitaryto CAEP6 (% of limit) 93.2
NOx Unitaryto CAEP8 (% of limit) 110.5
NOx LTO (g) 6240
Smoke Take Off (SN) 10.7
Smoke Climb Out (SN) 8.4
Smoke Approach (SN) 1
Smoke Idle (SN) 1.1
Smoke Max (SN) 10.7
Smoke Characteristic (SN) 13.8
Smoke Characteristicto Regulatory (% of limit) 63.6
Fuel Flow Take Off (kg/s) 1.252
Fuel Flow Climbout (kg/s) 1.035
Fuel Flow Approach (kg/s) 0.342
Fuel Flow Idle (kg/s) 0.109
Fuel LTO (kg) 441
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 6278
Compressor Description 1 fan, 4 low-pressure, 10 high-pressure
Emissions Data Status C
Engine Status Out of production
Turbine Description 2 high-pressure, 5 low-pressure