| LEAP-1B25 ✕ | LEAP-1A26CJ ✕ | |
|---|---|---|
| Family | LEAP-1B | LEAP-1A |
| EASA ID | 20CM096 | 08P28CM154 |
| Aircraft Engine Manufacturer | CFM International | CFM International |
| Aircraft Engine Type | Turbofan | Turbofan |
| Comment | Boeing 737 MAX | Airbus A320neo family |
| Dry Weight (kg) | 2780 | |
| Full Weight (kg) | 3153 | |
| Diameter (mm) | 1763 | 1981 |
| Max Rotating Diameter (mm) | 1763 | 1981 |
| Length (mm) | 3147 | 3328 |
| Height (mm) | 2256 | 2362 |
| Width (mm) | 2421 | 2543 |
| Wikipedia Article (URL) | en.wikipedia.org/wiki/CFM_International_LEAP | en.wikipedia.org/wiki/CFM_International_LEAP |
| Fuel | Jet A | Jet A |
| Fan Blades | 18 | 18 |
| Geared Fan | No | No |
| Low-Pressure Compressor Stages | 3 | 3 |
| High-Pressure Compressor Stages | 10 | 10 |
| Combustion Chamber | TAPS II | TAPS II |
| High Pressure Compressor Stages | 2 | 2 |
| Low-Pressure Turbine Stages | 5 | 7 |
| Afterburner | No | No |
| Streams | 2 | 2 |
| Bypass Ratio | 8.4 | 10.706 |
| Overall Pressure Ratio | 40.135 | 33.1765 |
| Maximum Takeoff Thrust (kN) | 119.2 | 120.6357 |
| Hydrocarbon Take Off (g/kg fuel) | 0.04 | 0.0274 |
| Hydrocarbon Climb Out (g/kg fuel) | 0.04 | 0.0188 |
| Hydrocarbon Approach (g/kg fuel) | 0.05 | 0.0555 |
| Hydrocarbon Idle (g/kg fuel) | 0.59 | 0.7837 |
| Hydrocarbon Unitary Average (g/kN) | 0.78 | 0.9392 |
| Hydrocarbon Unitary Sigma (g/kN) | 0.09 | 0.246 |
| Hydrocarbon Unitary Range (g/kN) | 0.66-0.84 | 0.57-1.24 |
| Hydrocarbon Unitary Characteristic (g/kN) | 1.2 | 1.0717 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 6.1 | 5.4677 |
| Hydrocarbon LTO (g) | 93 | 113.3032 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.17 | 0.0143 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.14 | 0.1084 |
| Carbon Monoxide Approach (g/kg fuel) | 1.25 | 2.8107 |
| Carbon Monoxide Idle (g/kg fuel) | 15.27 | 23.8311 |
| Carbon Monoxide Unitary Average (g/kN) | 18.94 | 28.5014 |
| Carbon Monoxide Unitary SD (g/kN) | 0.77 | 1.597 |
| Carbon Monoxide Unitary Range (g/kN) | 16.97-18.38 | 27-31.09 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 23.25 | 30.4926 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 19.7 | 25.8412 |
| NOx Take Off (g/kg fuel) | 48.9 | 34.2818 |
| NOx Climb Out (g/kg fuel) | 20.35 | 19.2339 |
| NOx Approach (g/kg fuel) | 11.1 | 8.5622 |
| NOx Idle (g/kg fuel) | 4.57 | 4.3128 |
| NOx Unitary Average (g/kN) | 45.46 | 34.4206 |
| NOx Unitary SD (g/kN) | 1.38 | 2.3144 |
| NOx Unitary Range (g/kN) | 56.39-59.15 | 31.3-37.75 |
| NOx Unitary Characteristic (g/kN) | 52.7 | 36.1713 |
| NOx Unitaryto Standard (% of limit) | 43.8 | 34.0106 |
| NOx Unitaryto CAEP2 (% of limit) | 54.8 | 42.5132 |
| NOx Unitaryto CAEP4 (% of limit) | 60.4 | 49.3112 |
| NOx Unitaryto CAEP6 (% of limit) | 66.5 | 55.3814 |
| NOx Unitaryto CAEP8 (% of limit) | 74.9 | 64.0505 |
| NOx LTO (g) | 5417 | 4152.355 |
| Smoke Take Off (SN) | 0.94 | 0.7037 |
| Smoke Climb Out (SN) | 0.85 | 0.6738 |
| Smoke Approach (SN) | 1.07 | 0.5964 |
| Smoke Idle (SN) | 0.8 | 0.5767 |
| Smoke Max (SN) | 1.16 | 1.203 |
| Smoke Sigma (SN) | 0.29 | 0.3443 |
| Smoke Range (SN) | 0.34-0.9 | 0.81-1.41 |
| Smoke Characteristic (SN) | 1.49 | 1.5485 |
| Smoke Characteristicto Regulatory (% of limit) | 6.6 | 6.8871 |
| Fuel Flow Take Off (kg/s) | 0.96 | 0.8648 |
| Fuel Flow Climbout (kg/s) | 0.784 | 0.7139 |
| Fuel Flow Approach (kg/s) | 0.26 | 0.2455 |
| Fuel Flow Idle (kg/s) | 0.091 | 0.0877 |
| Fuel LTO (kg) | 348 | 326.3452 |
| Fuel Venting Compliant | Yes | Yes |
| Carbon Monoxide LTO (g) | 2257 | 3438.289 |
| Compressor Description | 1 fan, 3-stage LP, 10-stage HP | 1 fan, 3-stage LP, 10-stage HP |
| Emissions Data Status | C | C |
| Emissions Data Superseded | Yes | |
| Emissions Superseded By | 01P20CM135 | |
| NOx Compliance Demonstration | 2.3.2 e) | 2.3.2 e) |
| nvPME Imass Approach (mg/kg) | 1.5252 | |
| nvPME Imass Climb Out (mg/kg) | 0.6526 | |
| nvPME Imass Idle (mg/kg) | 1.5053 | |
| nvPME Imass Max (mg/kg) | 12.3631 | |
| nvPME Imass Take Off (mg/kg) | 0.6288 | |
| nvPME Inum Approach (#/kg) | 52017000000000 | |
| nvPME Inum Climb Out (#/kg) | 12299690000 | |
| nvPME Inum Idle (#/kg) | 26768590000000 | |
| nvPME Inum Max (#/kg) | 444949800000000 | |
| nvPME Inum Take Off (#/kg) | 13497780000 | |
| nvPMLTO Mass (mg) | 380.224 | |
| nvPMLTO Mass Per Thrust (mg/kN) | 3.4978 | |
| nvPMLTO Mass To CAEP11 (% of limit) | 0.8387 | |
| nvPMLTO Number (#) | 6730226000000000 | |
| nvPMLTO Number Per Thrust (#/kN) | 61912850000000 | |
| nvPMLTO Number To CAEP11 (% of limit) | 1.2016 | |
| nvPM Mass Concentration Characteristic (mg/m³) | 165.986 | |
| nvPM Mass Concentration Max (mg/m³) | 152.9229 | |
| nvPM Mass Concentration To CAEP10 (% of limit) | 2.7549 | |
| Turbine Description | 2-stage HP, 5-stage LP | 2-stage HP, 7-stage LP |