| AE3007A2 ✕ | |
|---|---|
| EASA ID | 01P10AL033 |
| Aircraft Engine Manufacturer | Rolls-Royce |
| Aircraft Engine Type | Turbofan |
| Fuel | Jet A |
| Geared Fan | No |
| Combustion Chamber | Type 3 (reduced emissions) |
| Afterburner | No |
| Streams | 2 |
| Bypass Ratio | 4.79 |
| Overall Pressure Ratio | 20.2 |
| Maximum Takeoff Thrust (kN) | 42.23 |
| 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) | 1.71 |
| Hydrocarbon Unitary Average (g/kN) | 3.45 |
| Hydrocarbon Unitary Characteristic (g/kN) | 5.32 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 27.12 |
| Hydrocarbon LTO (g) | 146 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.71 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.74 |
| Carbon Monoxide Approach (g/kg fuel) | 4.08 |
| Carbon Monoxide Idle (g/kg fuel) | 34.17 |
| Carbon Monoxide Unitary Average (g/kN) | 73.29 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 89.96 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 76.24 |
| NOx Take Off (g/kg fuel) | 18.61 |
| NOx Climb Out (g/kg fuel) | 15.99 |
| NOx Approach (g/kg fuel) | 7.9 |
| NOx Idle (g/kg fuel) | 4.39 |
| NOx Unitary Average (g/kN) | 43.03 |
| NOx Unitary Characteristic (g/kN) | 49.88 |
| NOx Unitaryto Standard (% of limit) | 62.04 |
| NOx Unitaryto CAEP2 (% of limit) | 77.55 |
| NOx Unitaryto CAEP4 (% of limit) | 81.66 |
| NOx Unitaryto CAEP6 (% of limit) | 83.78 |
| NOx Unitaryto CAEP8 (% of limit) | 90.8 |
| NOx LTO (g) | 1817 |
| Smoke Take Off (SN) | 0.01 |
| Smoke Climb Out (SN) | 0.01 |
| Smoke Approach (SN) | 0.01 |
| Smoke Idle (SN) | 0.01 |
| Smoke Max (SN) | 0.01 |
| Smoke Characteristic (SN) | 0.01 |
| Smoke Characteristicto Regulatory (% of limit) | 0.04 |
| Fuel Flow Take Off (kg/s) | 0.466 |
| Fuel Flow Climbout (kg/s) | 0.388 |
| Fuel Flow Approach (kg/s) | 0.138 |
| Fuel Flow Idle (kg/s) | 0.055 |
| Fuel LTO (kg) | 189 |
| Carbon Monoxide LTO (g) | 3095 |
| Emissions Data Status | C |
| Engine Status | Out of production |
| NOx Compliance Demonstration | 2.3.2 e) |
| nvPME Imass Approach (mg/kg) | 9.9789 |
| nvPME Imass Climb Out (mg/kg) | 43.8218 |
| nvPME Imass Idle (mg/kg) | 16.6735 |
| nvPME Imass Max (mg/kg) | 48.7993 |
| nvPME Imass Take Off (mg/kg) | 48.7993 |
| nvPME Inum Approach (#/kg) | 298832400000000 |
| nvPME Inum Climb Out (#/kg) | 267616600000000 |
| nvPME Inum Idle (#/kg) | 550514100000000 |
| nvPME Inum Max (#/kg) | 550514100000000 |
| nvPME Inum Take Off (#/kg) | 197332200000000 |
| nvPMLTO Mass (mg) | 4951.397 |
| nvPMLTO Mass Per Thrust (mg/kN) | 163 |
| nvPMLTO Mass To CAEP11 (% of limit) | 17 |
| nvPMLTO Number (#) | 74390130000000000 |
| nvPMLTO Number Per Thrust (#/kN) | 2450000000000000 |
| nvPMLTO Number To CAEP11 (% of limit) | 21.3 |
| nvPM Mass Concentration Characteristic (mg/m³) | 343 |
| nvPM Mass Concentration Max (mg/m³) | 266.6775 |
| nvPM Mass Concentration To CAEP10 (% of limit) | 3.1 |