Maximum Takeoff Thrust
111.2 kN
Overall Pressure Ratio
26.6
Fuel Flow Take Off
1.051 kg/s
NOx Unitaryto CAEP8
103.5 % 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
6 |
Overall Pressure Ratio
26.6 |
Afterburner
No |
Pictures
No pictures yet for this family.
Similar reaction turbines
All data (62 fields)
- Name
- CFM56-5-A1
- EASA ID
- 1CM008
- Aircraft Engine Manufacturer
- CFM International
- Aircraft Engine Type
- Turbofan
- Fuel
- Jet A
- Geared Fan
- No
- Afterburner
- No
- Streams
- 2
- Bypass Ratio
- 6
- Overall Pressure Ratio
- 26.6
- Maximum Takeoff Thrust (kN)
- 111.2
- Hydrocarbon Take Off (g/kg fuel)
- 0.23
- Hydrocarbon Climb Out (g/kg fuel)
- 0.23
- Hydrocarbon Approach (g/kg fuel)
- 0.4
- Hydrocarbon Idle (g/kg fuel)
- 1.4
- Hydrocarbon Unitary Average (g/kN)
- 2.6
- Hydrocarbon Unitary Sigma (g/kN)
- 0.5
- Hydrocarbon Unitary Range (g/kN)
- 2.3-3.2
- Hydrocarbon Unitary Characteristic (g/kN)
- 4
- Hydrocarbon Unitary Characteristicto Regulatory (% of limit)
- 20.4
- Hydrocarbon LTO (g)
- 285
- Carbon Monoxide Take Off (g/kg fuel)
- 0.9
- Carbon Monoxide Climb Out (g/kg fuel)
- 0.9
- Carbon Monoxide Approach (g/kg fuel)
- 2.5
- Carbon Monoxide Idle (g/kg fuel)
- 17.6
- Carbon Monoxide Unitary Average (g/kN)
- 27.9
- Carbon Monoxide Unitary SD (g/kN)
- 0.7
- Carbon Monoxide Unitary Range (g/kN)
- 27-28.4
- Carbon Monoxide Unitary Characteristic (g/kN)
- 34.2
- Carbon Monoxide Unitary Characteristicto Regulatory (% of limit)
- 29
- NOx Take Off (g/kg fuel)
- 24.6
- NOx Climb Out (g/kg fuel)
- 19.6
- NOx Approach (g/kg fuel)
- 8
- NOx Idle (g/kg fuel)
- 4
- NOx Unitary Average (g/kN)
- 40.5
- NOx Unitary SD (g/kN)
- 0.6
- NOx Unitary Range (g/kN)
- 39.9-40.9
- NOx Unitary Characteristic (g/kN)
- 46.9
- NOx Unitaryto Standard (% of limit)
- 50.4
- NOx Unitaryto CAEP2 (% of limit)
- 63
- NOx Unitaryto CAEP4 (% of limit)
- 76.3
- NOx Unitaryto CAEP6 (% of limit)
- 86.7
- NOx Unitaryto CAEP8 (% of limit)
- 103.5
- NOx LTO (g)
- 4506
- Smoke Take Off (SN)
- 15.8
- Smoke Climb Out (SN)
- 14
- Smoke Approach (SN)
- 4.4
- Smoke Idle (SN)
- 2.3
- Smoke Max (SN)
- 15.8
- Smoke Sigma (SN)
- 2
- Smoke Range (SN)
- 13.5-17.3
- Smoke Characteristic (SN)
- 20.3
- Smoke Characteristicto Regulatory (% of limit)
- 88.5
- Fuel Flow Take Off (kg/s)
- 1.051
- Fuel Flow Climbout (kg/s)
- 0.862
- Fuel Flow Approach (kg/s)
- 0.291
- Fuel Flow Idle (kg/s)
- 0.1011
- Fuel LTO (kg)
- 385
- Fuel Venting Compliant
- No
- Carbon Monoxide LTO (g)
- 3093
- Emissions Data Status
- R
- Engine Status
- Out of production