AE3007A1/3

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

33.05 kN

Bypass Ratio

4.81

Overall Pressure Ratio

17.22

Fuel Flow Take Off

0.3589 kg/s

NOx Unitaryto CAEP8

81.2 % 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 4.81	Overall Pressure Ratio 17.22	Afterburner No

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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
AE3007A3	Rolls-Royce	33	4.72	17.2	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
AE3007A1/1	Rolls-Royce	34.74	4.77	17.9	Compare

All data (55 fields)

Name: AE3007A1/3
EASA ID: 6AL011
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: 4.81
Overall Pressure Ratio: 17.22
Maximum Takeoff Thrust (kN): 33.05
Hydrocarbon Take Off (g/kg fuel): 0.233
Hydrocarbon Climb Out (g/kg fuel): 0.269
Hydrocarbon Approach (g/kg fuel): 0.689
Hydrocarbon Idle (g/kg fuel): 4.64
Hydrocarbon Unitary Average (g/kN): 10.8
Hydrocarbon Unitary Characteristic (g/kN): 14.05
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 71.7
Hydrocarbon LTO (g): 357
Carbon Monoxide Take Off (g/kg fuel): 0.83
Carbon Monoxide Climb Out (g/kg fuel): 1.03
Carbon Monoxide Approach (g/kg fuel): 4.21
Carbon Monoxide Idle (g/kg fuel): 25.58
Carbon Monoxide Unitary Average (g/kN): 59.1
Carbon Monoxide Unitary Characteristic (g/kN): 67.34
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 57.1
NOx Take Off (g/kg fuel): 18.55
NOx Climb Out (g/kg fuel): 15.81
NOx Approach (g/kg fuel): 6.83
NOx Idle (g/kg fuel): 3.39
NOx Unitary Average (g/kN): 39.93
NOx Unitary Characteristic (g/kN): 43.91
NOx Unitaryto Standard (% of limit): 59
NOx Unitaryto CAEP2 (% of limit): 73.7
NOx Unitaryto CAEP4 (% of limit): 75.4
NOx Unitaryto CAEP6 (% of limit): 76.2
NOx Unitaryto CAEP8 (% of limit): 81.2
NOx LTO (g): 1319
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): 0.3589
Fuel Flow Climbout (kg/s): 0.2999
Fuel Flow Approach (kg/s): 0.1077
Fuel Flow Idle (kg/s): 0.0449
Fuel LTO (kg): 151
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 1954
Emissions Data Status: C
Engine Status: Out of production