AE3007A

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
33.73 kN
Bypass Ratio
5.23
Overall Pressure Ratio
18.08
Fuel Flow Take Off
0.377 kg/s
NOx Unitaryto CAEP8
92.4 % 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 5.23 Overall Pressure Ratio 18.08 Afterburner No

Pictures

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
ALF 502L-2 Textron Lycoming 33.4 5.1 13.15 Compare
AE3007A1 series Rolls-Royce 33.73 4.76 17.81 Compare
AE3007C2 Rolls-Royce 32.73 4.99 17.44 Compare
AE3007A1/3 Rolls-Royce 33.05 4.81 17.22 Compare
AE3007A3 Rolls-Royce 33 4.72 17.2 Compare
AE3007A1/1 Rolls-Royce 34.74 4.77 17.9 Compare
All data (54 fields)
Name
AE3007A
EASA ID
4AL003
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Fuel
Jet A/JP-8
Geared Fan
No
Afterburner
No
Streams
2
Bypass Ratio
5.23
Overall Pressure Ratio
18.08
Maximum Takeoff Thrust (kN)
33.73
Hydrocarbon Take Off (g/kg fuel)
0.25
Hydrocarbon Climb Out (g/kg fuel)
0.29
Hydrocarbon Approach (g/kg fuel)
0.64
Hydrocarbon Idle (g/kg fuel)
2.51
Hydrocarbon Unitary Average (g/kN)
6.65
Hydrocarbon Unitary Characteristic (g/kN)
8.7
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
44.1
Hydrocarbon LTO (g)
226
Carbon Monoxide Take Off (g/kg fuel)
0.75
Carbon Monoxide Climb Out (g/kg fuel)
0.92
Carbon Monoxide Approach (g/kg fuel)
3.28
Carbon Monoxide Idle (g/kg fuel)
17.35
Carbon Monoxide Unitary Average (g/kN)
43.15
Carbon Monoxide Unitary Characteristic (g/kN)
49.2
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
41.7
NOx Take Off (g/kg fuel)
20.54
NOx Climb Out (g/kg fuel)
17.47
NOx Approach (g/kg fuel)
7.79
NOx Idle (g/kg fuel)
3.83
NOx Unitary Average (g/kN)
46.3
NOx Unitary Characteristic (g/kN)
50.9
NOx Unitaryto Standard (% of limit)
66.8
NOx Unitaryto CAEP2 (% of limit)
83.6
NOx Unitaryto CAEP4 (% of limit)
85.6
NOx Unitaryto CAEP6 (% of limit)
86.6
NOx Unitaryto CAEP8 (% of limit)
92.4
NOx LTO (g)
1563
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)
3.7
Fuel Flow Take Off (kg/s)
0.377
Fuel Flow Climbout (kg/s)
0.315
Fuel Flow Approach (kg/s)
0.117
Fuel Flow Idle (kg/s)
0.049
Fuel LTO (kg)
162
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
1468
Emissions Data Status
C
Engine Status
Out of production