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

80.7 % 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 4.81	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 (57 fields)

Name: AE3007A1/3
EASA ID: 6AL013
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: 4.81
Overall Pressure Ratio: 17.22
Maximum Takeoff Thrust (kN): 33.05
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): 3.81
Hydrocarbon Unitary Average (g/kN): 8.15
Hydrocarbon Unitary Characteristic (g/kN): 12.55
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 64
Hydrocarbon LTO (g): 269
Carbon Monoxide Take Off (g/kg fuel): 0.5
Carbon Monoxide Climb Out (g/kg fuel): 0.5
Carbon Monoxide Approach (g/kg fuel): 7.62
Carbon Monoxide Idle (g/kg fuel): 38.47
Carbon Monoxide Unitary Average (g/kN): 88.3
Carbon Monoxide Unitary Characteristic (g/kN): 108.38
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 91.8
NOx Take Off (g/kg fuel): 15.42
NOx Climb Out (g/kg fuel): 13.49
NOx Approach (g/kg fuel): 6.93
NOx Idle (g/kg fuel): 4.27
NOx Unitary Average (g/kN): 37.66
NOx Unitary Characteristic (g/kN): 43.65
NOx Unitaryto Standard (% of limit): 58.6
NOx Unitaryto CAEP2 (% of limit): 73.3
NOx Unitaryto CAEP4 (% of limit): 74.9
NOx Unitaryto CAEP6 (% of limit): 75.7
NOx Unitaryto CAEP8 (% of limit): 80.7
NOx LTO (g): 1245
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): 0.3589
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
Carbon Monoxide LTO (g): 2919
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 01P06AL030
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)