Maximum Takeoff Thrust
75.44 kN
Bypass Ratio
5.09
Overall Pressure Ratio
25.1
Fuel Flow Take Off
0.769 kg/s
NOx Unitaryto CAEP8
86.4 % 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 SAC
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 5.09 Overall Pressure Ratio 25.1 Afterburner No

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Name Aircraft Engine Manufacturer Maximum Takeoff Thrust (kN) Bypass Ratio Overall Pressure Ratio
CF34-10E2A1 GE Aircraft Engines 75.44 5.09 25.1 Compare
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CF34-10E6 GE Aircraft Engines 77.4 5.09 25.6 Compare
CF34-10A16/B/C/D General Electric Company 76.9538 5.5806 24.8449 Compare
BR-700-725A1-12 Rolls-Royce Deutschland 75.7 4.35 26.16 Compare
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All data (78 fields)
Name
CF34-10E2A1
EASA ID
01P08GE203
Aircraft Engine Manufacturer
General Electric Company
Aircraft Engine Type
Turbofan
Fuel
Jet A-1
Geared Fan
No
Combustion Chamber
SAC
Afterburner
No
Streams
2
Bypass Ratio
5.09
Overall Pressure Ratio
25.1
Maximum Takeoff Thrust (kN)
75.44
Hydrocarbon Take Off (g/kg fuel)
0.04
Hydrocarbon Climb Out (g/kg fuel)
0.05
Hydrocarbon Approach (g/kg fuel)
0.1
Hydrocarbon Idle (g/kg fuel)
5.44
Hydrocarbon Unitary Average (g/kN)
9.56
Hydrocarbon Unitary Range (g/kN)
9-9.9
Hydrocarbon Unitary Characteristic (g/kN)
14.72
Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
75.1
Hydrocarbon LTO (g)
721
Carbon Monoxide Take Off (g/kg fuel)
0.41
Carbon Monoxide Climb Out (g/kg fuel)
0.38
Carbon Monoxide Approach (g/kg fuel)
4.46
Carbon Monoxide Idle (g/kg fuel)
50.81
Carbon Monoxide Unitary Average (g/kN)
91.61
Carbon Monoxide Unitary Range (g/kN)
88.5-93.4
Carbon Monoxide Unitary Characteristic (g/kN)
112.4
Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
95.3
NOx Take Off (g/kg fuel)
17.98
NOx Climb Out (g/kg fuel)
15.26
NOx Approach (g/kg fuel)
7.64
NOx Idle (g/kg fuel)
3.56
NOx Unitary Average (g/kN)
36.34
NOx Unitary Range (g/kN)
35.8-36.9
NOx Unitary Characteristic (g/kN)
42.1
NOx Unitaryto Standard (% of limit)
46.7
NOx Unitaryto CAEP2 (% of limit)
58.4
NOx Unitaryto CAEP4 (% of limit)
68
NOx Unitaryto CAEP6 (% of limit)
74.6
NOx Unitaryto CAEP8 (% of limit)
86.4
NOx LTO (g)
2742
Smoke Take Off (SN)
3.93
Smoke Climb Out (SN)
1.68
Smoke Approach (SN)
0.39
Smoke Idle (SN)
0.85
Smoke Max (SN)
3.93
Smoke Range (SN)
3.2-5
Smoke Characteristic (SN)
5.06
Smoke Characteristicto Regulatory (% of limit)
19.8
Fuel Flow Take Off (kg/s)
0.769
Fuel Flow Climbout (kg/s)
0.64
Fuel Flow Approach (kg/s)
0.222
Fuel Flow Idle (kg/s)
0.084
Fuel LTO (kg)
301
Fuel Venting Compliant
Yes
Carbon Monoxide LTO (g)
6911
Emissions Data Status
C
Engine Status
Out of production
nvPME Imass Approach (mg/kg)
1.6415
nvPME Imass Climb Out (mg/kg)
31.3234
nvPME Imass Idle (mg/kg)
13.4163
nvPME Imass Max (mg/kg)
52.0096
nvPME Imass Take Off (mg/kg)
52.0096
nvPME Inum Approach (#/kg)
93021370000000
nvPME Inum Climb Out (#/kg)
392697900000000
nvPME Inum Idle (#/kg)
673309900000000
nvPME Inum Max (#/kg)
673309900000000
nvPME Inum Take Off (#/kg)
450447700000000
nvPMLTO Mass (mg)
6141.035
nvPMLTO Mass Per Thrust (mg/kN)
113.1511
nvPMLTO Mass To CAEP11 (% of limit)
15.5109
nvPMLTO Number (#)
140061200000000000
nvPMLTO Number Per Thrust (#/kN)
2580685000000000
nvPMLTO Number To CAEP11 (% of limit)
29.3116
nvPM Mass Concentration Characteristic (mg/m³)
1810.586
nvPM Mass Concentration Max (mg/m³)
1406.644
nvPM Mass Concentration To CAEP10 (% of limit)
23.4856