| CFM56-5B8/P ✕ | CFM56-2B-1 ✕ | |
|---|---|---|
| Family | CFM56-5B | CFM56-2 |
| EASA ID | 7CM048 | 1CM002 |
| Aircraft Engine Manufacturer | CFM International | CFM International |
| Aircraft Engine Type | Turbofan | Turbofan |
| Comment | Airbus A318, A319, A320, A321 | DC-8-70, KC-135R, E-3, E-6 |
| Dry Weight (kg) | 2381 | 2186 |
| Diameter (mm) | 1735 | 1735 |
| Max Rotating Diameter (mm) | 1735 | 1735 |
| Length (mm) | 2601 | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/CFM_International_CFM56 | 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 | SAC | |
| High Pressure Compressor Stages | 1 | |
| Low-Pressure Turbine Stages | 4 | |
| Afterburner | No | No |
| Streams | 2 | 2 |
| Bypass Ratio | 5.9 | 6 |
| Overall Pressure Ratio | 22.6 | 23.5 |
| Maximum Takeoff Thrust (kN) | 94.7 | 97.86 |
| Hydrocarbon Take Off (g/kg fuel) | 0.1 | 0.04 |
| Hydrocarbon Climb Out (g/kg fuel) | 0.1 | 0.05 |
| Hydrocarbon Approach (g/kg fuel) | 0.9 | 0.08 |
| Hydrocarbon Idle (g/kg fuel) | 6.5 | 1.83 |
| Hydrocarbon Unitary Average (g/kN) | 10.8 | 3.87 |
| Hydrocarbon Unitary Sigma (g/kN) | 0.41 | |
| Hydrocarbon Unitary Range (g/kN) | 3.4-4.15 | |
| Hydrocarbon Unitary Characteristic (g/kN) | 16.6 | 6 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 84.7 | 30.4 |
| Hydrocarbon LTO (g) | 1023 | 378 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.8 | 0.9 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.8 | 0.9 |
| Carbon Monoxide Approach (g/kg fuel) | 3.9 | 4.2 |
| Carbon Monoxide Idle (g/kg fuel) | 32.9 | 30.7 |
| Carbon Monoxide Unitary Average (g/kN) | 54.4 | 67.2 |
| Carbon Monoxide Unitary SD (g/kN) | 4.1 | |
| Carbon Monoxide Unitary Range (g/kN) | 63.5-71.7 | |
| Carbon Monoxide Unitary Characteristic (g/kN) | 66.8 | 82.5 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 56.6 | 69.9 |
| NOx Take Off (g/kg fuel) | 19.7 | 18.5 |
| NOx Climb Out (g/kg fuel) | 16.7 | 16 |
| NOx Approach (g/kg fuel) | 8.4 | 8.2 |
| NOx Idle (g/kg fuel) | 3.4 | 4 |
| NOx Unitary Average (g/kN) | 35.4 | 39.9 |
| NOx Unitary SD (g/kN) | 0.6 | |
| NOx Unitary Range (g/kN) | 39.4-40.5 | |
| NOx Unitary Characteristic (g/kN) | 41 | 46.3 |
| NOx Unitaryto Standard (% of limit) | 48.1 | 53.2 |
| NOx Unitaryto CAEP2 (% of limit) | 60.2 | 66.5 |
| NOx Unitaryto CAEP4 (% of limit) | 74.4 | 81.7 |
| NOx Unitaryto CAEP6 (% of limit) | 84.5 | 92.9 |
| NOx Unitaryto CAEP8 (% of limit) | 103.3 | 113 |
| NOx LTO (g) | 3358 | 3906 |
| Smoke Take Off (SN) | 5.4 | 6 |
| Smoke Climb Out (SN) | 1.5 | 3 |
| Smoke Approach (SN) | 0.3 | 2.6 |
| Smoke Idle (SN) | 0.6 | 2.2 |
| Smoke Max (SN) | 5.4 | 6 |
| Smoke Sigma (SN) | 0.8 | |
| Smoke Range (SN) | 5.4-6.9 | |
| Smoke Characteristic (SN) | 6.9 | 7.7 |
| Smoke Characteristicto Regulatory (% of limit) | 28.7 | 32.4 |
| Fuel Flow Take Off (kg/s) | 0.875 | 0.985 |
| Fuel Flow Climbout (kg/s) | 0.729 | 0.819 |
| Fuel Flow Approach (kg/s) | 0.262 | 0.311 |
| Fuel Flow Idle (kg/s) | 0.094 | 0.128 |
| Fuel LTO (kg) | 342 | 424 |
| Fuel Venting Compliant | No | No |
| Carbon Monoxide LTO (g) | 5176 | 6578 |
| Compressor Description | 1 fan, 4-stage LP, 9-stage HP | |
| Emissions Data Status | C | C |
| Engine Status | Out of production | Out of production |
| Turbine Description | 1-stage HP, 4-stage LP |