AE3007A1E

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

37.16 kN

Bypass Ratio

4.72

Overall Pressure Ratio

19.06

Fuel Flow Take Off

0.4122 kg/s

NOx Unitaryto CAEP8

84.8 % 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 Type 3
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 4.72	Overall Pressure Ratio 19.06	Afterburner No

Pictures

No pictures yet for this family.

Similar reaction turbines

Name	Aircraft Engine Manufacturer	Maximum Takeoff Thrust (kN)	Bypass Ratio	Overall Pressure Ratio
AE3007A1E	Rolls-Royce	37.16	4.72	19.06	Compare
AE3007A1	Rolls-Royce	34.91	4.77	17.97	Compare
AE3007A1/1	Rolls-Royce	34.74	4.77	17.9	Compare
AE3007A1P	Rolls-Royce	34.74	4.77	17.9	Compare
AE3007A1 series	Rolls-Royce	33.73	4.76	17.81	Compare
AE3007A3	Rolls-Royce	33	4.72	17.2	Compare

All data (58 fields)

Name: AE3007A1E
EASA ID: 6AL020
Aircraft Engine Manufacturer: Rolls-Royce
Aircraft Engine Type: Turbofan
Fuel: Jet A
Geared Fan: No
Combustion Chamber: Type 3
Afterburner: No
Streams: 2
Bypass Ratio: 4.72
Overall Pressure Ratio: 19.06
Maximum Takeoff Thrust (kN): 37.16
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): 3.52
Hydrocarbon Unitary Average (g/kN): 7.1
Hydrocarbon Unitary Characteristic (g/kN): 10.93
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 55.8
Hydrocarbon LTO (g): 264
Carbon Monoxide Take Off (g/kg fuel): 0.77
Carbon Monoxide Climb Out (g/kg fuel): 0.64
Carbon Monoxide Approach (g/kg fuel): 5.63
Carbon Monoxide Idle (g/kg fuel): 37.97
Carbon Monoxide Unitary Average (g/kN): 81.18
Carbon Monoxide Unitary Characteristic (g/kN): 99.64
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 84.4
NOx Take Off (g/kg fuel): 17.17
NOx Climb Out (g/kg fuel): 14.91
NOx Approach (g/kg fuel): 7.42
NOx Idle (g/kg fuel): 4.26
NOx Unitary Average (g/kN): 40.38
NOx Unitary Characteristic (g/kN): 46.81
NOx Unitaryto Standard (% of limit): 59.9
NOx Unitaryto CAEP2 (% of limit): 74.9
NOx Unitaryto CAEP4 (% of limit): 77.6
NOx Unitaryto CAEP6 (% of limit): 78.9
NOx Unitaryto CAEP8 (% of limit): 84.8
NOx LTO (g): 1501
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): 0.4122
Fuel Flow Climbout (kg/s): 0.3425
Fuel Flow Approach (kg/s): 0.12
Fuel Flow Idle (kg/s): 0.0475
Fuel LTO (kg): 165
Fuel Venting Compliant: No
Carbon Monoxide LTO (g): 3018
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 01P06AL032
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)