| Family |
CFM56-5B |
|
| EASA ID |
3CM025 |
14IA018 |
| Aircraft Engine Manufacturer |
CFM International |
International Aero Engines |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Comment |
Airbus A318, A319, A320, A321 |
|
| Dry Weight (kg) |
2381 |
|
| Diameter (mm) |
1735 |
|
| Max Rotating Diameter (mm) |
1735 |
|
| Length (mm) |
2601 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/CFM_International_CFM56 |
|
| Fuel |
Jet A |
Jet A |
| Fan Blades |
36 |
|
| Geared Fan |
No |
No |
| Low-Pressure Compressor Stages |
4 |
|
| High-Pressure Compressor Stages |
9 |
|
| Combustion Chamber |
|
Floatwall |
| High Pressure Compressor Stages |
1 |
|
| Low-Pressure Turbine Stages |
4 |
|
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
5.6 |
4.52 |
| Overall Pressure Ratio |
32.78 |
32.3 |
| Maximum Takeoff Thrust (kN) |
142.35 |
134.8 |
| Hydrocarbon Take Off (g/kg fuel) |
0.1 |
0.01 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.2 |
0.02 |
| Hydrocarbon Approach (g/kg fuel) |
0.5 |
0.09 |
| Hydrocarbon Idle (g/kg fuel) |
3.5 |
0.07 |
| Hydrocarbon Unitary Average (g/kN) |
5 |
0.2 |
| Hydrocarbon Unitary Characteristic (g/kN) |
7.7 |
0.3 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
39.3 |
1.5 |
| Hydrocarbon LTO (g) |
708 |
28 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.8 |
0.39 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.9 |
0.41 |
| Carbon Monoxide Approach (g/kg fuel) |
1.7 |
1.57 |
| Carbon Monoxide Idle (g/kg fuel) |
19.2 |
10.17 |
| Carbon Monoxide Unitary Average (g/kN) |
26.48 |
18.6 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
32.5 |
21.2 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
27.5 |
18 |
| NOx Take Off (g/kg fuel) |
37.3 |
32.17 |
| NOx Climb Out (g/kg fuel) |
28.5 |
24.28 |
| NOx Approach (g/kg fuel) |
11.2 |
11.14 |
| NOx Idle (g/kg fuel) |
4.7 |
5.58 |
| NOx Unitary Average (g/kN) |
58.81 |
55.8 |
| NOx Unitary Characteristic (g/kN) |
68.2 |
61.4 |
| NOx Unitaryto Standard (% of limit) |
64.6 |
58.7 |
| NOx Unitaryto CAEP2 (% of limit) |
80.8 |
73.4 |
| NOx Unitaryto CAEP4 (% of limit) |
94 |
85.8 |
| NOx Unitaryto CAEP6 (% of limit) |
105.7 |
96.7 |
| NOx Unitaryto CAEP8 (% of limit) |
122.5 |
112.2 |
| NOx LTO (g) |
8360 |
7521 |
| Smoke Take Off (SN) |
4.7 |
2.3 |
| Smoke Climb Out (SN) |
5.1 |
6 |
| Smoke Approach (SN) |
0.2 |
6.3 |
| Smoke Idle (SN) |
0.5 |
1.3 |
| Smoke Max (SN) |
5.4 |
9.4 |
| Smoke Characteristic (SN) |
7 |
11.1 |
| Smoke Characteristicto Regulatory (% of limit) |
32.6 |
50.9 |
| Fuel Flow Take Off (kg/s) |
1.43 |
1.329 |
| Fuel Flow Climbout (kg/s) |
1.141 |
1.079 |
| Fuel Flow Approach (kg/s) |
0.366 |
0.391 |
| Fuel Flow Idle (kg/s) |
0.115 |
0.144 |
| Fuel LTO (kg) |
478 |
517 |
| Fuel Venting Compliant |
No |
Yes |
| Carbon Monoxide LTO (g) |
3777 |
2503 |
| Compressor Description |
1 fan, 4-stage LP, 9-stage HP |
|
| Emissions Data Status |
C |
C |
| Emissions Data Superseded |
|
Yes |
| Emissions Superseded By |
|
01P14IA026 |
| Engine Status |
Out of production |
|
| NOx Compliance Demonstration |
|
2.3.2 d) |
| Turbine Description |
1-stage HP, 4-stage LP |
|