AE3007C1

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

31.5 kN

Bypass Ratio

5.1

Overall Pressure Ratio

16.6

Fuel Flow Take Off

0.322 kg/s

NOx Unitaryto CAEP8

76.4 % 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 5.1	Overall Pressure Ratio 16.6	Afterburner No

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Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
AE3007C1	Rolls-Royce	31.46	5.1	16.58	Compare
LF507-1F, -1H	Textron Lycoming	31	5.1	13	Compare
AE3007C2	Rolls-Royce	32.73	4.99	17.44	Compare
ALF 502L-2	Textron Lycoming	33.4	5.1	13.15	Compare
ALF 502R-5	Textron Lycoming	31	5.6	12	Compare
AE3007C	Rolls-Royce	29.62	5.2	15.8	Compare

All data (56 fields)

Name: AE3007C1
EASA ID: 6AL004
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Fuel: Jet A/JP-8
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 5.1
Overall Pressure Ratio: 16.6
Maximum Takeoff Thrust (kN): 31.5
Hydrocarbon Take Off (g/kg fuel): 0.24
Hydrocarbon Climb Out (g/kg fuel): 0.28
Hydrocarbon Approach (g/kg fuel): 0.66
Hydrocarbon Idle (g/kg fuel): 4.84
Hydrocarbon Unitary Average (g/kN): 10.95
Hydrocarbon Unitary Characteristic (g/kN): 14.25
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 55.9
Hydrocarbon LTO (g): 346
Carbon Monoxide Take Off (g/kg fuel): 0.87
Carbon Monoxide Climb Out (g/kg fuel): 1.07
Carbon Monoxide Approach (g/kg fuel): 3.96
Carbon Monoxide Idle (g/kg fuel): 26.04
Carbon Monoxide Unitary Average (g/kN): 58.61
Carbon Monoxide Unitary Characteristic (g/kN): 66.78
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 56.6
NOx Take Off (g/kg fuel): 17.9
NOx Climb Out (g/kg fuel): 15.35
NOx Approach (g/kg fuel): 7.05
NOx Idle (g/kg fuel): 3.37
NOx Unitary Average (g/kN): 37.36
NOx Unitary Characteristic (g/kN): 41.08
NOx Unitaryto Standard (% of limit): 56.1
NOx Unitaryto CAEP2 (% of limit): 70.2
NOx Unitaryto CAEP4 (% of limit): 71.3
NOx Unitaryto CAEP6 (% of limit): 71.9
NOx Unitaryto CAEP8 (% of limit): 76.4
NOx LTO (g): 1175
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): 1.17
Smoke Characteristicto Regulatory (% of limit): 3.6
Fuel Flow Take Off (kg/s): 0.322
Fuel Flow Climbout (kg/s): 0.269
Fuel Flow Approach (kg/s): 0.099
Fuel Flow Idle (kg/s): 0.042
Fuel LTO (kg): 138
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 1850
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 6AL023
Engine Status: Out of production