AE3007A1/1

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

34.74 kN

Bypass Ratio

4.77

Overall Pressure Ratio

17.9

Fuel Flow Take Off

0.3805 kg/s

NOx Unitaryto CAEP8

97.6 % 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 4.77	Overall Pressure Ratio 17.9	Afterburner No

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Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
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
AE3007A1 series	Rolls-Royce	33.73	4.76	17.81	Compare
AE3007A1/3	Rolls-Royce	33.05	4.81	17.22	Compare
AE3007A3	Rolls-Royce	33	4.72	17.2	Compare

All data (54 fields)

Name: AE3007A1/1
EASA ID: 6AL009
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: 4.77
Overall Pressure Ratio: 17.9
Maximum Takeoff Thrust (kN): 34.74
Hydrocarbon Take Off (g/kg fuel): 0
Hydrocarbon Climb Out (g/kg fuel): 0
Hydrocarbon Approach (g/kg fuel): 0.18
Hydrocarbon Idle (g/kg fuel): 5.1
Hydrocarbon Unitary Average (g/kN): 10.67
Hydrocarbon Unitary Characteristic (g/kN): 16.43
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 83.8
Hydrocarbon LTO (g): 370
Carbon Monoxide Take Off (g/kg fuel): 0
Carbon Monoxide Climb Out (g/kg fuel): 0
Carbon Monoxide Approach (g/kg fuel): 1.4
Carbon Monoxide Idle (g/kg fuel): 32.84
Carbon Monoxide Unitary Average (g/kN): 68.8
Carbon Monoxide Unitary Characteristic (g/kN): 84.45
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 71.6
NOx Take Off (g/kg fuel): 22.31
NOx Climb Out (g/kg fuel): 19.49
NOx Approach (g/kg fuel): 7.16
NOx Idle (g/kg fuel): 3.19
NOx Unitary Average (g/kN): 45.84
NOx Unitary Characteristic (g/kN): 53.14
NOx Unitaryto Standard (% of limit): 70.1
NOx Unitaryto CAEP2 (% of limit): 87.6
NOx Unitaryto CAEP4 (% of limit): 90.1
NOx Unitaryto CAEP6 (% of limit): 91.3
NOx Unitaryto CAEP8 (% of limit): 97.6
NOx LTO (g): 1592
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): 0.3805
Fuel Flow Climbout (kg/s): 0.3163
Fuel Flow Approach (kg/s): 0.1125
Fuel Flow Idle (kg/s): 0.0459
Fuel LTO (kg): 156
Carbon Monoxide LTO (g): 2389
Emissions Data Status: C
Engine Status: Out of production