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CFM56-5C4/P ✕ Shenyang WS-10 ✕
Family CFM56-5C
EASA ID 7CM047
Aircraft Engine Manufacturer CFM International Shenyang
Aircraft Engine Type Turbofan Turbofan
Comment Airbus A340-200/-300
Dry Weight (kg) 3990 1795
Diameter (mm) 1836
Max Rotating Diameter (mm) 1836
Wikipedia Article (URL) en.wikipedia.org/wiki/CFM_International_CFM56 en.wikipedia.org/wiki/Shenyang_WS-10
Fuel Jet A
Geared Fan No No
Combustion Chamber SAC annular
Afterburner No Yes
Streams 2 2
Bypass Ratio 6.6
Overall Pressure Ratio 30.5
Maximum Takeoff Thrust (kN) 149.9 135
Thrust To Weight 8.8
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
Hydrocarbon Unitary Average (g/kN) 6
Hydrocarbon Unitary Characteristic (g/kN) 9.3
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 47.4
Hydrocarbon LTO (g) 897
Carbon Monoxide Take Off (g/kg fuel) 0.8
Carbon Monoxide Climb Out (g/kg fuel) 0.7
Carbon Monoxide Approach (g/kg fuel) 1.6
Carbon Monoxide Idle (g/kg fuel) 31.6
Carbon Monoxide Unitary Average (g/kN) 39.9
Carbon Monoxide Unitary Characteristic (g/kN) 48.9
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 41.4
NOx Take Off (g/kg fuel) 34.1
NOx Climb Out (g/kg fuel) 26.7
NOx Approach (g/kg fuel) 9.9
NOx Idle (g/kg fuel) 4.1
NOx Unitary Average (g/kN) 50.9
NOx Unitary Characteristic (g/kN) 59
NOx Unitaryto Standard (% of limit) 58.4
NOx Unitaryto CAEP2 (% of limit) 73
NOx Unitaryto CAEP4 (% of limit) 86.8
NOx Unitaryto CAEP6 (% of limit) 98.4
NOx Unitaryto CAEP8 (% of limit) 115.4
NOx LTO (g) 7641
Smoke Take Off (SN) 12
Smoke Climb Out (SN) 9.6
Smoke Approach (SN) 1
Smoke Idle (SN) 1.1
Smoke Max (SN) 12
Smoke Characteristic (SN) 15.4
Smoke Characteristicto Regulatory (% of limit) 72.7
Fuel Flow Take Off (kg/s) 1.395
Fuel Flow Climbout (kg/s) 1.143
Fuel Flow Approach (kg/s) 0.37
Fuel Flow Idle (kg/s) 0.115
Fuel LTO (kg) 478
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 5964
Emissions Data Status C
Engine Status Out of production