| AE3007A1E ✕ | |
|---|---|
| EASA ID | 01P06AL032 |
| 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 | 4.72 |
| Overall Pressure Ratio | 19.06 |
| Maximum Takeoff Thrust (kN) | 37.16 |
| 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) | 3.52 |
| Hydrocarbon Unitary Average (g/kN) | 7.1 |
| Hydrocarbon Unitary Characteristic (g/kN) | 10.93 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) | 55.8 |
| Hydrocarbon LTO (g) | 264 |
| Carbon Monoxide Take Off (g/kg fuel) | 0.77 |
| Carbon Monoxide Climb Out (g/kg fuel) | 0.64 |
| Carbon Monoxide Approach (g/kg fuel) | 5.63 |
| Carbon Monoxide Idle (g/kg fuel) | 37.97 |
| Carbon Monoxide Unitary Average (g/kN) | 81.18 |
| Carbon Monoxide Unitary Characteristic (g/kN) | 99.64 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) | 84.4 |
| NOx Take Off (g/kg fuel) | 17.17 |
| NOx Climb Out (g/kg fuel) | 14.91 |
| NOx Approach (g/kg fuel) | 7.42 |
| NOx Idle (g/kg fuel) | 4.26 |
| NOx Unitary Average (g/kN) | 40.38 |
| NOx Unitary Characteristic (g/kN) | 46.81 |
| NOx Unitaryto Standard (% of limit) | 59.9 |
| NOx Unitaryto CAEP2 (% of limit) | 74.9 |
| NOx Unitaryto CAEP4 (% of limit) | 77.6 |
| NOx Unitaryto CAEP6 (% of limit) | 78.9 |
| NOx Unitaryto CAEP8 (% of limit) | 84.8 |
| NOx LTO (g) | 1501 |
| 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) | 0.4122 |
| Fuel Flow Climbout (kg/s) | 0.3425 |
| Fuel Flow Approach (kg/s) | 0.12 |
| Fuel Flow Idle (kg/s) | 0.0475 |
| Fuel LTO (kg) | 165 |
| Carbon Monoxide LTO (g) | 3018 |
| Emissions Data Status | C |
| Engine Status | Out of production |
| NOx Compliance Demonstration | 2.3.2 e) |
| nvPME Imass Approach (mg/kg) | 9.7219 |
| nvPME Imass Climb Out (mg/kg) | 38.0395 |
| nvPME Imass Idle (mg/kg) | 17.9045 |
| nvPME Imass Max (mg/kg) | 45.7 |
| nvPME Imass Take Off (mg/kg) | 45.7 |
| nvPME Inum Approach (#/kg) | 316690200000000 |
| nvPME Inum Climb Out (#/kg) | 300852500000000 |
| nvPME Inum Idle (#/kg) | 611922000000000 |
| nvPME Inum Max (#/kg) | 611922000000000 |
| nvPME Inum Take Off (#/kg) | 260027600000000 |
| nvPMLTO Mass (mg) | 4266.93 |
| nvPMLTO Mass Per Thrust (mg/kN) | 158.5 |
| nvPMLTO Mass To CAEP11 (% of limit) | 16 |
| nvPMLTO Number (#) | 76914950000000000 |
| nvPMLTO Number Per Thrust (#/kN) | 2860000000000000 |
| nvPMLTO Number To CAEP11 (% of limit) | 24.1 |
| nvPM Mass Concentration Characteristic (mg/m³) | 289 |
| nvPM Mass Concentration Max (mg/m³) | 224.3 |
| nvPM Mass Concentration To CAEP10 (% of limit) | 2.4 |