AE3007A1 series

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

33.73 kN

Bypass Ratio

4.76

Overall Pressure Ratio

17.81

Fuel Flow Take Off

0.38 kg/s

NOx Unitaryto CAEP8

89.8 % 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 —
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 4.76	Overall Pressure Ratio 17.81	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
AE3007A1/1	Rolls-Royce	34.74	4.77	17.9	Compare
AE3007A1P	Rolls-Royce	34.74	4.77	17.9	Compare
AE3007A1	Rolls-Royce	34.91	4.77	17.97	Compare
ALF 502L-2	Textron Lycoming	33.4	5.1	13.15	Compare

All data (56 fields)

Name: AE3007A1 series
EASA ID: 4AL002
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Fuel: Jet A/JP-8
Geared Fan: No
Afterburner: No
Streams: 2
Bypass Ratio: 4.76
Overall Pressure Ratio: 17.81
Maximum Takeoff Thrust (kN): 33.73
Hydrocarbon Take Off (g/kg fuel): 0.26
Hydrocarbon Climb Out (g/kg fuel): 0.3
Hydrocarbon Approach (g/kg fuel): 0.72
Hydrocarbon Idle (g/kg fuel): 3.1
Hydrocarbon Unitary Average (g/kN): 8.33
Hydrocarbon Unitary Characteristic (g/kN): 10.8
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 55.3
Hydrocarbon LTO (g): 279
Carbon Monoxide Take Off (g/kg fuel): 0.79
Carbon Monoxide Climb Out (g/kg fuel): 0.97
Carbon Monoxide Approach (g/kg fuel): 3.8
Carbon Monoxide Idle (g/kg fuel): 22.43
Carbon Monoxide Unitary Average (g/kN): 57.03
Carbon Monoxide Unitary Characteristic (g/kN): 65
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 55.1
NOx Take Off (g/kg fuel): 19.78
NOx Climb Out (g/kg fuel): 16.84
NOx Approach (g/kg fuel): 7.22
NOx Idle (g/kg fuel): 3.52
NOx Unitary Average (g/kN): 44.61
NOx Unitary Characteristic (g/kN): 49.1
NOx Unitaryto Standard (% of limit): 64.9
NOx Unitaryto CAEP2 (% of limit): 81.1
NOx Unitaryto CAEP4 (% of limit): 83.1
NOx Unitaryto CAEP6 (% of limit): 84
NOx Unitaryto CAEP8 (% of limit): 89.8
NOx LTO (g): 1502
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): 1.2
Smoke Characteristicto Regulatory (% of limit): 3.7
Fuel Flow Take Off (kg/s): 0.38
Fuel Flow Climbout (kg/s): 0.319
Fuel Flow Approach (kg/s): 0.117
Fuel Flow Idle (kg/s): 0.05
Fuel LTO (kg): 164
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 1910
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 6AL005
Engine Status: Out of production