AE3007A3

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
33 kN
Bypass Ratio
4.72
Overall Pressure Ratio
17.2
Fuel Flow Take Off
0.3583 kg/s
NOx Unitaryto CAEP8
81.1 % 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 1
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 4.72 Overall Pressure Ratio 17.2 Afterburner No

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Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007A3 Rolls-Royce 33 4.72 17.2 Compare
AE3007A1/3 Rolls-Royce 33.05 4.81 17.22 Compare
AE3007A1 series Rolls-Royce 33.73 4.76 17.81 Compare
AE3007C2 Rolls-Royce 32.73 4.99 17.44 Compare
ALF 502L-2 Textron Lycoming 33.4 5.1 13.15 Compare
HTF7350 (AS907-2-1A) Honeywell 33 4.2 22.88 Compare
All data (55 fields)
Name
AE3007A3
EASA ID
6AL017
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
Type 1
Afterburner
No
Streams
2
Bypass Ratio
4.72
Overall Pressure Ratio
17.2
Maximum Takeoff Thrust (kN)
33
Hydrocarbon Take Off (g/kg fuel)
0.233
Hydrocarbon Climb Out (g/kg fuel)
0.27
Hydrocarbon Approach (g/kg fuel)
0.69
Hydrocarbon Idle (g/kg fuel)
4.705
Hydrocarbon Unitary Average (g/kN)
10.93
Hydrocarbon Unitary Characteristic (g/kN)
14.22
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
72.6
Hydrocarbon LTO (g)
361
Carbon Monoxide Take Off (g/kg fuel)
0.83
Carbon Monoxide Climb Out (g/kg fuel)
1.03
Carbon Monoxide Approach (g/kg fuel)
4.22
Carbon Monoxide Idle (g/kg fuel)
25.73
Carbon Monoxide Unitary Average (g/kN)
59.41
Carbon Monoxide Unitary Characteristic (g/kN)
67.69
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
57.4
NOx Take Off (g/kg fuel)
18.52
NOx Climb Out (g/kg fuel)
15.79
NOx Approach (g/kg fuel)
6.83
NOx Idle (g/kg fuel)
3.38
NOx Unitary Average (g/kN)
39.87
NOx Unitary Characteristic (g/kN)
43.84
NOx Unitaryto Standard (% of limit)
58.9
NOx Unitaryto CAEP2 (% of limit)
73.7
NOx Unitaryto CAEP4 (% of limit)
75.3
NOx Unitaryto CAEP6 (% of limit)
76.1
NOx Unitaryto CAEP8 (% of limit)
81.1
NOx LTO (g)
1316
Smoke Take Off (SN)
1
Smoke Climb Out (SN)
0.01
Smoke Approach (SN)
0.01
Smoke Idle (SN)
0.01
Smoke Max (SN)
1
Smoke Characteristic (SN)
1.17
Smoke Characteristicto Regulatory (% of limit)
3.6
Fuel Flow Take Off (kg/s)
0.3583
Fuel Flow Climbout (kg/s)
0.2995
Fuel Flow Approach (kg/s)
0.1076
Fuel Flow Idle (kg/s)
0.0448
Fuel LTO (kg)
150
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
1960
Emissions Data Status
C
Engine Status
Out of production