| AE3007A1P ✕ | |
|---|---|
| EASA ID | 01P06AL031 |
| 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 | 4.77 |
| Overall Pressure Ratio | 17.9 |
| Maximum Takeoff Thrust (kN) | 34.74 |
| Hydrocarbon Take Off (g/kg fuel) | 0.03 |
| Hydrocarbon Climb Out (g/kg fuel) | 0.03 |
| Hydrocarbon Approach (g/kg fuel) | 0.03 |
| Hydrocarbon Idle (g/kg fuel) | 3.86 |
| Hydrocarbon Unitary Average (g/kN) | 8.06 |
| Hydrocarbon Unitary Characteristic (g/kN) | 12.41 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 63.3 |
| Hydrocarbon LTO (g) | 280 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.74 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.55 |
| Carbon Monoxide Approach (g/kg fuel) | 6.79 |
| Carbon Monoxide Idle (g/kg fuel) | 39.97 |
| Carbon Monoxide Unitary Average (g/kN) | 88.88 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 109.1 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 92.5 |
| NOx Take Off (g/kg fuel) | 16.1 |
| NOx Climb Out (g/kg fuel) | 14.01 |
| NOx Approach (g/kg fuel) | 7.12 |
| NOx Idle (g/kg fuel) | 4.17 |
| NOx Unitary Average (g/kN) | 38.41 |
| NOx Unitary Characteristic (g/kN) | 44.52 |
| NOx Unitaryto Standard (% of limit) | 58.7 |
| NOx Unitaryto CAEP2 (% of limit) | 73.4 |
| NOx Unitaryto CAEP4 (% of limit) | 75.2 |
| NOx Unitaryto CAEP6 (% of limit) | 76.5 |
| NOx Unitaryto CAEP8 (% of limit) | 81.8 |
| NOx LTO (g) | 1334 |
| 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 |
| Fuel Flow Take Off (kg/s) | 0.3806 |
| Fuel Flow Climbout (kg/s) | 0.3163 |
| Fuel Flow Approach (kg/s) | 0.1126 |
| Fuel Flow Idle (kg/s) | 0.046 |
| Fuel LTO (kg) | 157 |
| Carbon Monoxide LTO (g) | 3087 |
| Emissions Data Status | C |
| Engine Status | Out of production |
| NOx Compliance Demonstration | 2.3.2 e) |
| nvPME Imass Approach (mg/kg) | 9.8482 |
| nvPME Imass Climb Out (mg/kg) | 34.8851 |
| nvPME Imass Idle (mg/kg) | 18.4055 |
| nvPME Imass Max (mg/kg) | 43.1427 |
| nvPME Imass Take Off (mg/kg) | 43.1427 |
| nvPME Inum Approach (#/kg) | 325901100000000 |
| nvPME Inum Climb Out (#/kg) | 309219000000000 |
| nvPME Inum Idle (#/kg) | 638163000000000 |
| nvPME Inum Max (#/kg) | 638163000000000 |
| nvPME Inum Take Off (#/kg) | 282685700000000 |
| nvPMLTO Mass (mg) | 3907.795 |
| nvPMLTO Mass Per Thrust (mg/kN) | 155.2 |
| nvPMLTO Mass To CAEP11 (% of limit) | 15.4 |
| nvPMLTO Number (#) | 76863340000000000 |
| nvPMLTO Number Per Thrust (#/kN) | 3050000000000000 |
| nvPMLTO Number To CAEP11 (% of limit) | 25.3 |
| nvPM Mass Concentration Characteristic (mg/m³) | 260 |
| nvPM Mass Concentration Max (mg/m³) | 202.0917 |
| nvPM Mass Concentration To CAEP10 (% of limit) | 2.1 |