AE3007A2

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
42.23 kN
Bypass Ratio
4.79
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

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Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007A2 Rolls-Royce 42.23 4.79 20.2 Compare
Snecma Atar ATAR 42 Compare
AE3007A1E Rolls-Royce 37.16 4.72 19.06 Compare
Tumansky R-25 Tumansky 40.3 Compare
Tumansky R-13 Guizhou 39.9 Compare
CF34-3A GE Aircraft Engines 41.01 6.25 19.7 Compare
All data (58 fields)
Name
AE3007A2
EASA ID
10AL026
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
Fuel Venting Compliant
No
Carbon Monoxide LTO (g)
3095
Emissions Data Status
C
Emissions Data Superseded
Yes
Emissions Superseded By
01P10AL033
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)