AE3007C2

Turbofan · Rolls-Royce
Reaction Turbines
Maximum Takeoff Thrust
32.73 kN
Bypass Ratio
4.99
Overall Pressure Ratio
17.44
Fuel Flow Take Off
0.3263 kg/s
NOx Unitaryto CAEP8
86.15 % 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 2
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 4.99 Overall Pressure Ratio 17.44 Afterburner No

Pictures

No pictures yet for this family.

Similar reaction turbines

Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
AE3007A1/3 Rolls-Royce 33.05 4.81 17.22 Compare
ALF 502L-2 Textron Lycoming 33.4 5.1 13.15 Compare
AE3007A3 Rolls-Royce 33 4.72 17.2 Compare
AE3007C1 Rolls-Royce 31.5 5.1 16.6 Compare
AE3007A1 series Rolls-Royce 33.73 4.76 17.81 Compare
AE3007A Rolls-Royce 33.73 5.23 18.08 Compare
All data (56 fields)
Name
AE3007C2
EASA ID
13AL027
Aircraft Engine Manufacturer
Rolls-Royce
Aircraft Engine Type
Turbofan
Fuel
Jet A
Geared Fan
No
Combustion Chamber
Type 2
Afterburner
No
Streams
2
Bypass Ratio
4.99
Overall Pressure Ratio
17.44
Maximum Takeoff Thrust (kN)
32.73
Hydrocarbon Take Off (g/kg fuel)
0
Hydrocarbon Climb Out (g/kg fuel)
0.01
Hydrocarbon Approach (g/kg fuel)
0.22
Hydrocarbon Idle (g/kg fuel)
2.57
Hydrocarbon Unitary Average (g/kN)
5.94
Hydrocarbon Unitary Characteristic (g/kN)
9.15
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
46.68
Hydrocarbon LTO (g)
194.8
Carbon Monoxide Take Off (g/kg fuel)
0
Carbon Monoxide Climb Out (g/kg fuel)
0
Carbon Monoxide Approach (g/kg fuel)
1.97
Carbon Monoxide Idle (g/kg fuel)
23.09
Carbon Monoxide Unitary Average (g/kN)
53.4
Carbon Monoxide Unitary Characteristic (g/kN)
65.55
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
55.55
NOx Take Off (g/kg fuel)
21.25
NOx Climb Out (g/kg fuel)
18.11
NOx Approach (g/kg fuel)
6.56
NOx Idle (g/kg fuel)
3.14
NOx Unitary Average (g/kN)
40.54
NOx Unitary Characteristic (g/kN)
46.99
NOx Unitaryto Standard (% of limit)
70.25
NOx Unitaryto CAEP2 (% of limit)
78.44
NOx Unitaryto CAEP4 (% of limit)
80.12
NOx Unitaryto CAEP6 (% of limit)
80.88
NOx Unitaryto CAEP8 (% of limit)
86.15
NOx LTO (g)
1326.3
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)
0.3263
Fuel Flow Climbout (kg/s)
0.2714
Fuel Flow Approach (kg/s)
0.0985
Fuel Flow Idle (kg/s)
0.0472
Fuel LTO (kg)
147
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
1746.7
Emissions Data Status
C
Engine Status
Out of production
NOx Compliance Demonstration
2.3.2 e)