Maximum Takeoff Thrust
267.3 kN
Overall Pressure Ratio
31.58
Fuel Flow Take Off
2.581 kg/s
NOx Unitaryto CAEP8
101.7 % 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
5.1 |
Overall Pressure Ratio
31.58 |
Afterburner
No |
Pictures
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All data (61 fields)
- Name
- CF6-80C2A5
- EASA ID
- 1GE020
- Aircraft Engine Manufacturer
- General Electric Company
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 5.1
- Overall Pressure Ratio
- 31.58
- Maximum Takeoff Thrust (kN)
- 267.3
- Hydrocarbon Take Off (g/kg fuel)
- 0.07
- Hydrocarbon Climb Out (g/kg fuel)
- 0.08
- Hydrocarbon Approach (g/kg fuel)
- 0.2
- Hydrocarbon Idle (g/kg fuel)
- 8.99
- Hydrocarbon Unitary Average (g/kN)
- 11.12
- Hydrocarbon Unitary Sigma (g/kN)
- 1.3
- Hydrocarbon Unitary Range (g/kN)
- 10.02-12.49
- Hydrocarbon Unitary Characteristic (g/kN)
- 14.5
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 73.8
- Hydrocarbon LTO (g)
- 2966
- Carbon Monoxide Take Off (g/kg fuel)
- 0.52
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.52
- Carbon Monoxide Approach (g/kg fuel)
- 1.93
- Carbon Monoxide Idle (g/kg fuel)
- 41.65
- Carbon Monoxide Unitary Average (g/kN)
- 52.35
- Carbon Monoxide Unitary SD (g/kN)
- 3.03
- Carbon Monoxide Unitary Range (g/kN)
- 49.73-55.2
- Carbon Monoxide Unitary Characteristic (g/kN)
- 59.6
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 50.5
- NOx Take Off (g/kg fuel)
- 34.38
- NOx Climb Out (g/kg fuel)
- 22.86
- NOx Approach (g/kg fuel)
- 9.11
- NOx Idle (g/kg fuel)
- 3.79
- NOx Unitary Average (g/kN)
- 49.25
- NOx Unitary SD (g/kN)
- 2.23
- NOx Unitary Range (g/kN)
- 46.22-49.73
- NOx Unitary Characteristic (g/kN)
- 54.2
- NOx Unitaryto Standard (% of limit)
- 52.5
- NOx Unitaryto CAEP2 (% of limit)
- 65.6
- NOx Unitaryto CAEP4 (% of limit)
- 77.2
- NOx Unitaryto CAEP6 (% of limit)
- 87.2
- NOx Unitaryto CAEP8 (% of limit)
- 101.7
- NOx LTO (g)
- 12735
- Smoke Take Off (SN)
- 7.8
- Smoke Climb Out (SN)
- 5.4
- Smoke Approach (SN)
- 2.3
- Smoke Idle (SN)
- 3
- Smoke Max (SN)
- 7.8
- Smoke Sigma (SN)
- 1.3
- Smoke Range (SN)
- 6.1-8.4
- Smoke Characteristic (SN)
- 9.1
- Smoke Characteristicto Regulatory (% of limit)
- 50.6
- Fuel Flow Take Off (kg/s)
- 2.581
- Fuel Flow Climbout (kg/s)
- 2.082
- Fuel Flow Approach (kg/s)
- 0.687
- Fuel Flow Idle (kg/s)
- 0.207
- Fuel LTO (kg)
- 871
- Carbon Monoxide LTO (g)
- 13967
- Emissions Data Status
- R
- Engine Status
- Out of production