Maximum Takeoff Thrust
42.23 kN
Overall Pressure Ratio
20.2
Fuel Flow Take Off
0.466 kg/s
NOx Unitaryto CAEP8
90.8 % of limit
Architecture
| Fan |
Fan Stages
—
|
Fan Blades
—
|
Fan Technology
—
|
Fan Pressure Ratio
—
|
| Gearbox |
Geared Fan
No |
Gear
—
|
Reduction Ratio
—
|
| LP compressor |
Low-Pressure Compressor Stages
—
|
Low-Pressure Compressor Technology
—
|
BP Compressor Pressure Ratio
—
|
| IP compressor |
Intermediary-Pressure Compressor Stages
—
|
Intermediary-Pressure Compressor Technology
—
|
IP Compressor Pressure Ratio
—
|
| HP compressor |
High-Pressure Compressor Stages
—
|
High-Pressure Compressor Technology
—
|
HP Compressor Pressure Ratio
—
|
| Combustor |
Combustion Chamber
Type 3 (reduced emissions) |
| HP turbine |
High Pressure Compressor Stages
—
|
High-Pressure Turbine Technology
—
|
| IP turbine |
Intermediary-Pressure Turbine Stages
—
|
Intermediary-Pressure Turbine Technology
—
|
| LP turbine |
Low-Pressure Turbine Stages
—
|
Low-Pressure Turbine Technology
—
|
| Whole engine |
Streams
2 |
Bypass Ratio
4.79 |
Overall Pressure Ratio
20.2 |
Afterburner
No |
Pictures
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All data (74 fields)
- Name
- 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