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
80 % 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 4.72 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 (57 fields)
Name
AE3007A3
EASA ID
6AL019
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
17.2
Maximum Takeoff Thrust (kN)
33
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)
4.1
Hydrocarbon Unitary Average (g/kN)
8.75
Hydrocarbon Unitary Characteristic (g/kN)
13.48
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
68.8
Hydrocarbon LTO (g)
289
Carbon Monoxide Take Off (g/kg fuel)
0.5
Carbon Monoxide Climb Out (g/kg fuel)
0.5
Carbon Monoxide Approach (g/kg fuel)
7.65
Carbon Monoxide Idle (g/kg fuel)
41.29
Carbon Monoxide Unitary Average (g/kN)
94.25
Carbon Monoxide Unitary Characteristic (g/kN)
115.69
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
98
NOx Take Off (g/kg fuel)
15.4
NOx Climb Out (g/kg fuel)
13.48
NOx Approach (g/kg fuel)
6.93
NOx Idle (g/kg fuel)
4.12
NOx Unitary Average (g/kN)
37.32
NOx Unitary Characteristic (g/kN)
43.26
NOx Unitaryto Standard (% of limit)
58.1
NOx Unitaryto CAEP2 (% of limit)
72.7
NOx Unitaryto CAEP4 (% of limit)
74.3
NOx Unitaryto CAEP6 (% of limit)
75.1
NOx Unitaryto CAEP8 (% of limit)
80
NOx LTO (g)
1232
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)
0.3583
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
Carbon Monoxide LTO (g)
3111
Emissions Data Status
C
Emissions Data Superseded
Yes
Emissions Superseded By
01P06AL034
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)