Maximum Takeoff Thrust
267.2 kN
Overall Pressure Ratio
31.66
Fuel Flow Take Off
2.58 kg/s
NOx Unitaryto CAEP8
97.3 % 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
1862M39 |
| 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
31.66 |
Afterburner
No |
Pictures
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All data (63 fields)
- Name
- CF6-80C2B6
- EASA ID
- 2GE044
- Aircraft Engine Manufacturer
- General Electric Company
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Combustion Chamber
- 1862M39
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 5.1
- Overall Pressure Ratio
- 31.66
- Maximum Takeoff Thrust (kN)
- 267.2
- Hydrocarbon Take Off (g/kg fuel)
- 0.04
- Hydrocarbon Climb Out (g/kg fuel)
- 0.05
- Hydrocarbon Approach (g/kg fuel)
- 0.11
- Hydrocarbon Idle (g/kg fuel)
- 1.48
- Hydrocarbon Unitary Average (g/kN)
- 1.9
- Hydrocarbon Unitary Sigma (g/kN)
- 0.209
- Hydrocarbon Unitary Range (g/kN)
- 1.76-2.24
- Hydrocarbon Unitary Characteristic (g/kN)
- 2.5
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 12.6
- Hydrocarbon LTO (g)
- 509
- Carbon Monoxide Take Off (g/kg fuel)
- 0.06
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.04
- Carbon Monoxide Approach (g/kg fuel)
- 1.91
- Carbon Monoxide Idle (g/kg fuel)
- 18.89
- Carbon Monoxide Unitary Average (g/kN)
- 23.8
- Carbon Monoxide Unitary SD (g/kN)
- 1.196
- Carbon Monoxide Unitary Range (g/kN)
- 22.6-25.5
- Carbon Monoxide Unitary Characteristic (g/kN)
- 27.1
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 23
- NOx Take Off (g/kg fuel)
- 28.57
- NOx Climb Out (g/kg fuel)
- 21.69
- NOx Approach (g/kg fuel)
- 12.53
- NOx Idle (g/kg fuel)
- 4.76
- NOx Unitary Average (g/kN)
- 47.3
- NOx Unitary SD (g/kN)
- 0.5
- NOx Unitary Range (g/kN)
- 46.7-47.9
- NOx Unitary Characteristic (g/kN)
- 52
- NOx Unitaryto Standard (% of limit)
- 50.3
- NOx Unitaryto CAEP2 (% of limit)
- 62.9
- NOx Unitaryto CAEP4 (% of limit)
- 74
- NOx Unitaryto CAEP6 (% of limit)
- 83.5
- NOx Unitaryto CAEP8 (% of limit)
- 97.3
- NOx LTO (g)
- 12640
- Smoke Take Off (SN)
- 6.9
- Smoke Climb Out (SN)
- 5.4
- Smoke Approach (SN)
- 0
- Smoke Idle (SN)
- 0
- Smoke Max (SN)
- 6.9
- Smoke Sigma (SN)
- 0.914
- Smoke Range (SN)
- 5.9-8.2
- Smoke Characteristic (SN)
- 8.1
- Smoke Characteristicto Regulatory (% of limit)
- 44.8
- Fuel Flow Take Off (kg/s)
- 2.58
- Fuel Flow Climbout (kg/s)
- 2.096
- Fuel Flow Approach (kg/s)
- 0.672
- Fuel Flow Idle (kg/s)
- 0.205
- Fuel LTO (kg)
- 866
- Carbon Monoxide LTO (g)
- 6367
- Emissions Data Status
- C
- Engine Status
- Out of production
- NOx Compliance Demonstration
- 2.3.2 e)