AE3007A1P

Turbofan · Rolls-Royce

Reaction Turbines

Maximum Takeoff Thrust

34.74 kN

Bypass Ratio

4.77

Overall Pressure Ratio

17.9

Fuel Flow Take Off

0.3806 kg/s

NOx Unitaryto CAEP8

81.8 % 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 (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 4.77	Overall Pressure Ratio 17.9	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
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 (57 fields)

Name: AE3007A1P
EASA ID: 6AL016
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: 4.77
Overall Pressure Ratio: 17.9
Maximum Takeoff Thrust (kN): 34.74
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): 3.86
Hydrocarbon Unitary Average (g/kN): 8.06
Hydrocarbon Unitary Characteristic (g/kN): 12.41
Hydrocarbon Unitary Characteristicto Regulatory (% of limit): 63.3
Hydrocarbon LTO (g): 280
Carbon Monoxide Take Off (g/kg fuel): 0.74
Carbon Monoxide Climb Out (g/kg fuel): 0.55
Carbon Monoxide Approach (g/kg fuel): 6.79
Carbon Monoxide Idle (g/kg fuel): 39.97
Carbon Monoxide Unitary Average (g/kN): 88.88
Carbon Monoxide Unitary Characteristic (g/kN): 109.1
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit): 92.5
NOx Take Off (g/kg fuel): 16.1
NOx Climb Out (g/kg fuel): 14.01
NOx Approach (g/kg fuel): 7.12
NOx Idle (g/kg fuel): 4.17
NOx Unitary Average (g/kN): 38.41
NOx Unitary Characteristic (g/kN): 44.52
NOx Unitaryto Standard (% of limit): 58.7
NOx Unitaryto CAEP2 (% of limit): 73.4
NOx Unitaryto CAEP4 (% of limit): 75.2
NOx Unitaryto CAEP6 (% of limit): 76.5
NOx Unitaryto CAEP8 (% of limit): 81.8
NOx LTO (g): 1334
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): 0.3806
Fuel Flow Climbout (kg/s): 0.3163
Fuel Flow Approach (kg/s): 0.1126
Fuel Flow Idle (kg/s): 0.046
Fuel LTO (kg): 157
Carbon Monoxide LTO (g): 3087
Emissions Data Status: C
Emissions Data Superseded: Yes
Emissions Superseded By: 01P06AL031
Engine Status: Out of production
NOx Compliance Demonstration: 2.3.2 e)