| LEAP-1B25 ✕ | CFM56-5-A1 ✕ | |
|---|---|---|
| Family | LEAP-1B | |
| EASA ID | 20CM096 | 1CM008 |
| Aircraft Engine Manufacturer | CFM International | CFM International |
| Aircraft Engine Type | Turbofan | Turbofan |
| Comment | Boeing 737 MAX | |
| Dry Weight (kg) | 2780 | |
| Diameter (mm) | 1763 | |
| Max Rotating Diameter (mm) | 1763 | |
| Length (mm) | 3147 | |
| Height (mm) | 2256 | |
| Width (mm) | 2421 | |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/CFM_International_LEAP | |
| Fuel | Jet A | Jet A |
| Fan Blades | 18 | |
| Geared Fan | No | No |
| Low-Pressure Compressor Stages | 3 | |
| High-Pressure Compressor Stages | 10 | |
| Combustion Chamber | TAPS II | |
| High Pressure Compressor Stages | 2 | |
| Low-Pressure Turbine Stages | 5 | |
| Afterburner | No | No |
| Streams | 2 | 2 |
| Bypass Ratio | 8.4 | 6 |
| Overall Pressure Ratio | 40.135 | 26.6 |
| Maximum Takeoff Thrust (kN) | 119.2 | 111.2 |
| Hydrocarbon Take Off (g/kg fuel) | 0.04 | 0.23 |
| Hydrocarbon Climb Out (g/kg fuel) | 0.04 | 0.23 |
| Hydrocarbon Approach (g/kg fuel) | 0.05 | 0.4 |
| Hydrocarbon Idle (g/kg fuel) | 0.59 | 1.4 |
| Hydrocarbon Unitary Average (g/kN) | 0.78 | 2.6 |
| Hydrocarbon Unitary Sigma (g/kN) | 0.09 | 0.5 |
| Hydrocarbon Unitary Range (g/kN) | 0.66-0.84 | 2.3-3.2 |
| Hydrocarbon Unitary Characteristic (g/kN) | 1.2 | 4 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 6.1 | 20.4 |
| Hydrocarbon LTO (g) | 93 | 285 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.17 | 0.9 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.14 | 0.9 |
| Carbon Monoxide Approach (g/kg fuel) | 1.25 | 2.5 |
| Carbon Monoxide Idle (g/kg fuel) | 15.27 | 17.6 |
| Carbon Monoxide Unitary Average (g/kN) | 18.94 | 27.9 |
| Carbon Monoxide Unitary SD (g/kN) | 0.77 | 0.7 |
| Carbon Monoxide Unitary Range (g/kN) | 16.97-18.38 | 27-28.4 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 23.25 | 34.2 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 19.7 | 29 |
| NOx Take Off (g/kg fuel) | 48.9 | 24.6 |
| NOx Climb Out (g/kg fuel) | 20.35 | 19.6 |
| NOx Approach (g/kg fuel) | 11.1 | 8 |
| NOx Idle (g/kg fuel) | 4.57 | 4 |
| NOx Unitary Average (g/kN) | 45.46 | 40.5 |
| NOx Unitary SD (g/kN) | 1.38 | 0.6 |
| NOx Unitary Range (g/kN) | 56.39-59.15 | 39.9-40.9 |
| NOx Unitary Characteristic (g/kN) | 52.7 | 46.9 |
| NOx Unitaryto Standard (% of limit) | 43.8 | 50.4 |
| NOx Unitaryto CAEP2 (% of limit) | 54.8 | 63 |
| NOx Unitaryto CAEP4 (% of limit) | 60.4 | 76.3 |
| NOx Unitaryto CAEP6 (% of limit) | 66.5 | 86.7 |
| NOx Unitaryto CAEP8 (% of limit) | 74.9 | 103.5 |
| NOx LTO (g) | 5417 | 4506 |
| Smoke Take Off (SN) | 0.94 | 15.8 |
| Smoke Climb Out (SN) | 0.85 | 14 |
| Smoke Approach (SN) | 1.07 | 4.4 |
| Smoke Idle (SN) | 0.8 | 2.3 |
| Smoke Max (SN) | 1.16 | 15.8 |
| Smoke Sigma (SN) | 0.29 | 2 |
| Smoke Range (SN) | 0.34-0.9 | 13.5-17.3 |
| Smoke Characteristic (SN) | 1.49 | 20.3 |
| Smoke Characteristicto Regulatory (% of limit) | 6.6 | 88.5 |
| Fuel Flow Take Off (kg/s) | 0.96 | 1.051 |
| Fuel Flow Climbout (kg/s) | 0.784 | 0.862 |
| Fuel Flow Approach (kg/s) | 0.26 | 0.291 |
| Fuel Flow Idle (kg/s) | 0.091 | 0.1011 |
| Fuel LTO (kg) | 348 | 385 |
| Fuel Venting Compliant | Yes | No |
| Carbon Monoxide LTO (g) | 2257 | 3093 |
| Compressor Description | 1 fan, 3-stage LP, 10-stage HP | |
| Emissions Data Status | C | R |
| Emissions Data Superseded | Yes | |
| Emissions Superseded By | 01P20CM135 | |
| Engine Status | Out of production | |
| NOx Compliance Demonstration | 2.3.2 e) | |
| Turbine Description | 2-stage HP, 5-stage LP |