Maximum Takeoff Thrust
28.6 kN
Overall Pressure Ratio
16.2
Fuel Flow Take Off
0.28 kg/s
NOx Unitaryto CAEP8
70.4 % 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
—
|
| 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
5.3 |
Overall Pressure Ratio
16.2 |
Afterburner
No |
Pictures
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All data (56 fields)
- Name
- AE3007C
- EASA ID
- 3AL001
- Aircraft Engine Manufacturer
- Rolls-Royce
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A/JP-8
- Geared Fan
- No
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 5.3
- Overall Pressure Ratio
- 16.2
- Maximum Takeoff Thrust (kN)
- 28.6
- Hydrocarbon Take Off (g/kg fuel)
- 0.29
- Hydrocarbon Climb Out (g/kg fuel)
- 0.33
- Hydrocarbon Approach (g/kg fuel)
- 0.83
- Hydrocarbon Idle (g/kg fuel)
- 5.84
- Hydrocarbon Unitary Average (g/kN)
- 13.46
- Hydrocarbon Unitary Characteristic (g/kN)
- 17.5
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 89.3
- Hydrocarbon LTO (g)
- 387
- Carbon Monoxide Take Off (g/kg fuel)
- 0.97
- Carbon Monoxide Climb Out (g/kg fuel)
- 1.19
- Carbon Monoxide Approach (g/kg fuel)
- 4.5
- Carbon Monoxide Idle (g/kg fuel)
- 29.88
- Carbon Monoxide Unitary Average (g/kN)
- 68
- Carbon Monoxide Unitary Characteristic (g/kN)
- 77.5
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 65.7
- NOx Take Off (g/kg fuel)
- 16.92
- NOx Climb Out (g/kg fuel)
- 14.56
- NOx Approach (g/kg fuel)
- 6.63
- NOx Idle (g/kg fuel)
- 3.24
- NOx Unitary Average (g/kN)
- 34.73
- NOx Unitary Characteristic (g/kN)
- 38.2
- NOx Unitaryto Standard (% of limit)
- 52.8
- NOx Unitaryto CAEP2 (% of limit)
- 66
- NOx Unitaryto CAEP4 (% of limit)
- 66.4
- NOx Unitaryto CAEP6 (% of limit)
- 66.6
- NOx Unitaryto CAEP8 (% of limit)
- 70.4
- NOx LTO (g)
- 991
- Smoke Take Off (SN)
- 1
- Smoke Climb Out (SN)
- 0
- Smoke Approach (SN)
- 0
- Smoke Idle (SN)
- 0
- Smoke Max (SN)
- 1
- Smoke Characteristic (SN)
- 1.2
- Smoke Characteristicto Regulatory (% of limit)
- 3.6
- Fuel Flow Take Off (kg/s)
- 0.28
- Fuel Flow Climbout (kg/s)
- 0.234
- Fuel Flow Approach (kg/s)
- 0.091
- Fuel Flow Idle (kg/s)
- 0.039
- Fuel LTO (kg)
- 125
- Fuel Venting Compliant
- No
- Carbon Monoxide LTO (g)
- 1964
- Emissions Data Status
- C
- Emissions Data Superseded
- Yes
- Emissions Superseded By
- 6AL021
- Engine Status
- Out of production