| Family |
CFM56-5B |
CFM56-5A |
| EASA ID |
01P08CM110 |
4CM036 |
| Aircraft Engine Manufacturer |
CFM International |
CFM International |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Comment |
Airbus A318, A319, A320, A321 |
Airbus A319, A320 |
| Dry Weight (kg) |
2381 |
2266 |
| Diameter (mm) |
1735 |
1735 |
| Max Rotating Diameter (mm) |
1735 |
1735 |
| Length (mm) |
2601 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/CFM_International_CFM56 |
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 |
Tech Insertion |
|
| High Pressure Compressor Stages |
1 |
|
| Low-Pressure Turbine Stages |
4 |
|
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
5.9 |
6 |
| Overall Pressure Ratio |
24.2 |
25.1 |
| Maximum Takeoff Thrust (kN) |
103.6 |
104.53 |
| Hydrocarbon Take Off (g/kg fuel) |
0.02 |
0.23 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.03 |
0.23 |
| Hydrocarbon Approach (g/kg fuel) |
0.07 |
0.45 |
| Hydrocarbon Idle (g/kg fuel) |
3.01 |
1.53 |
| Hydrocarbon Unitary Average (g/kN) |
4.36 |
2.8 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.49 |
|
| Hydrocarbon Unitary Range (g/kN) |
3.81-4.74 |
|
| Hydrocarbon Unitary Characteristic (g/kN) |
5.09 |
4.3 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
26 |
22 |
| Hydrocarbon LTO (g) |
452 |
297 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.16 |
1.1 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.17 |
1.1 |
| Carbon Monoxide Approach (g/kg fuel) |
4.42 |
2.8 |
| Carbon Monoxide Idle (g/kg fuel) |
38.8 |
18.5 |
| Carbon Monoxide Unitary Average (g/kN) |
58.34 |
30.3 |
| Carbon Monoxide Unitary SD (g/kN) |
2.8 |
|
| Carbon Monoxide Unitary Range (g/kN) |
55.2-60.2 |
|
| Carbon Monoxide Unitary Characteristic (g/kN) |
63.1 |
37.2 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
53.5 |
31.5 |
| NOx Take Off (g/kg fuel) |
17.54 |
24.79 |
| NOx Climb Out (g/kg fuel) |
14.76 |
19.98 |
| NOx Approach (g/kg fuel) |
8.26 |
8.94 |
| NOx Idle (g/kg fuel) |
3.92 |
4.29 |
| NOx Unitary Average (g/kN) |
32.58 |
41.8 |
| NOx Unitary SD (g/kN) |
1.1 |
|
| NOx Unitary Range (g/kN) |
31.6-33.8 |
|
| NOx Unitary Characteristic (g/kN) |
34.5 |
48.5 |
| NOx Unitaryto Standard (% of limit) |
39 |
53.7 |
| NOx Unitaryto CAEP2 (% of limit) |
48.8 |
67.1 |
| NOx Unitaryto CAEP4 (% of limit) |
59.8 |
81.9 |
| NOx Unitaryto CAEP6 (% of limit) |
67.9 |
93.1 |
| NOx Unitaryto CAEP8 (% of limit) |
82.2 |
112.2 |
| NOx LTO (g) |
3377 |
4367 |
| Smoke Take Off (SN) |
11.2 |
14.3 |
| Smoke Climb Out (SN) |
8.4 |
12.6 |
| Smoke Approach (SN) |
2.1 |
4.4 |
| Smoke Idle (SN) |
2.1 |
2.4 |
| Smoke Max (SN) |
11.2 |
14.3 |
| Smoke Sigma (SN) |
2.5 |
|
| Smoke Range (SN) |
8.3-12.9 |
|
| Smoke Characteristic (SN) |
12.3 |
18.4 |
| Smoke Characteristicto Regulatory (% of limit) |
52.5 |
78.7 |
| Fuel Flow Take Off (kg/s) |
0.956 |
0.972 |
| Fuel Flow Climbout (kg/s) |
0.793 |
0.799 |
| Fuel Flow Approach (kg/s) |
0.278 |
0.276 |
| Fuel Flow Idle (kg/s) |
0.095 |
0.098 |
| Fuel LTO (kg) |
359 |
365 |
| Fuel Venting Compliant |
Yes |
No |
| Carbon Monoxide LTO (g) |
6047 |
3175 |
| Compressor Description |
1 fan, 4-stage LP, 9-stage HP |
|
| Emissions Data Status |
C |
C |
| Engine Status |
Out of production |
Out of production |
| NOx Compliance Demonstration |
2.3.2 e) |
|
| nvPME Imass Approach (mg/kg) |
1.06 |
|
| nvPME Imass Climb Out (mg/kg) |
30.3 |
|
| nvPME Imass Idle (mg/kg) |
0.85 |
|
| nvPME Imass Max (mg/kg) |
42.7 |
|
| nvPME Imass Take Off (mg/kg) |
42.7 |
|
| nvPME Inum Approach (#/kg) |
44900000000000 |
|
| nvPME Inum Climb Out (#/kg) |
411000000000000 |
|
| nvPME Inum Idle (#/kg) |
46100000000000 |
|
| nvPME Inum Max (#/kg) |
431000000000000 |
|
| nvPME Inum Take Off (#/kg) |
431000000000000 |
|
| nvPMLTO Mass (mg) |
5080 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
68.1 |
|
| nvPMLTO Mass To CAEP11 (% of limit) |
12.7 |
|
| nvPMLTO Number (#) |
70100000000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
941000000000000 |
|
| nvPMLTO Number To CAEP11 (% of limit) |
14.5 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
1216 |
|
| nvPM Mass Concentration Max (mg/m³) |
945 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
18.7 |
|
| Turbine Description |
1-stage HP, 4-stage LP |
|