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CFM56-5C3/P ✕ Shenyang WS-10 ✕
Family CFM56-5C
EASA ID 7CM046
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 6.7
Overall Pressure Ratio 29.2
Maximum Takeoff Thrust (kN) 143.33 135
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) 5.4
Hydrocarbon Unitary Average (g/kN) 6.6
Hydrocarbon Unitary Characteristic (g/kN) 10.2
Hydrocarbon Unitary Characteristicto Regulatory (% of limit) 52
Hydrocarbon LTO (g) 943
Carbon Monoxide Take Off (g/kg fuel) 0.8
Carbon Monoxide Climb Out (g/kg fuel) 0.7
Carbon Monoxide Approach (g/kg fuel) 1.9
Carbon Monoxide Idle (g/kg fuel) 33.4
Carbon Monoxide Unitary Average (g/kN) 42.8
Carbon Monoxide Unitary Characteristic (g/kN) 52.6
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) 44.6
NOx Take Off (g/kg fuel) 31.6
NOx Climb Out (g/kg fuel) 25.1
NOx Approach (g/kg fuel) 9.6
NOx Idle (g/kg fuel) 4
NOx Unitary Average (g/kN) 47.8
NOx Unitary Characteristic (g/kN) 55.4
NOx Unitaryto Standard (% of limit) 56.3
NOx Unitaryto CAEP2 (% of limit) 70.4
NOx Unitaryto CAEP4 (% of limit) 84.3
NOx Unitaryto CAEP6 (% of limit) 95.8
NOx Unitaryto CAEP8 (% of limit) 113.1
NOx LTO (g) 6858
Smoke Take Off (SN) 11.6
Smoke Climb Out (SN) 9
Smoke Approach (SN) 1
Smoke Idle (SN) 1.1
Smoke Max (SN) 11.6
Smoke Characteristic (SN) 14.9
Smoke Characteristicto Regulatory (% of limit) 69.5
Fuel Flow Take Off (kg/s) 1.316
Fuel Flow Climbout (kg/s) 1.085
Fuel Flow Approach (kg/s) 0.355
Fuel Flow Idle (kg/s) 0.112
Fuel LTO (kg) 458
Fuel Venting Compliant No
Carbon Monoxide LTO (g) 6142
Emissions Data Status C
Engine Status Out of production