| Family |
|
CFM56-5A |
| EASA ID |
|
1CM009 |
| Aircraft Engine Manufacturer |
Ivchenko-Progress ZMKB |
CFM International |
| Aircraft Engine Type |
Open-rotor |
Turbofan |
| Comment |
|
Airbus A319, A320 |
| Dry Weight (kg) |
1650 |
2266 |
| Diameter (mm) |
970 |
1735 |
| Max Rotating Diameter (mm) |
|
1735 |
| Length (mm) |
4205 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Progress_D-27 |
en.wikipedia.org/wiki/CFM_International_CFM56 |
| Fuel |
|
Jet A |
| Geared Fan |
Yes |
No |
| Combustion Chamber |
Annular combustion chamber |
|
| Afterburner |
No |
No |
| Streams |
1 |
2 |
| Bypass Ratio |
|
6 |
| Overall Pressure Ratio |
|
27.9 |
| Maximum Takeoff Thrust (kN) |
119 |
117.88 |
| Hydrocarbon Take Off (g/kg fuel) |
|
0.2 |
| Hydrocarbon Climb Out (g/kg fuel) |
|
0.2 |
| Hydrocarbon Approach (g/kg fuel) |
|
0.3 |
| Hydrocarbon Idle (g/kg fuel) |
|
1.3 |
| Hydrocarbon Unitary Average (g/kN) |
|
2.3 |
| Hydrocarbon Unitary Sigma (g/kN) |
|
0.5 |
| Hydrocarbon Unitary Range (g/kN) |
|
1.8-2.8 |
| Hydrocarbon Unitary Characteristic (g/kN) |
|
3.5 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
|
18.1 |
| Hydrocarbon LTO (g) |
|
268 |
| Carbon Monoxide Take Off (g/kg fuel) |
|
0.9 |
| Carbon Monoxide Climb Out (g/kg fuel) |
|
0.9 |
| Carbon Monoxide Approach (g/kg fuel) |
|
2.4 |
| Carbon Monoxide Idle (g/kg fuel) |
|
16.2 |
| Carbon Monoxide Unitary Average (g/kN) |
|
25.1 |
| Carbon Monoxide Unitary SD (g/kN) |
|
0.6 |
| Carbon Monoxide Unitary Range (g/kN) |
|
24.2-25.5 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
|
30.8 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
|
26.1 |
| NOx Take Off (g/kg fuel) |
|
26.4 |
| NOx Climb Out (g/kg fuel) |
|
21.1 |
| NOx Approach (g/kg fuel) |
|
8.3 |
| NOx Idle (g/kg fuel) |
|
4.1 |
| NOx Unitary Average (g/kN) |
|
43.4 |
| NOx Unitary SD (g/kN) |
|
0.7 |
| NOx Unitary Range (g/kN) |
|
42.7-44.2 |
| NOx Unitary Characteristic (g/kN) |
|
50.3 |
| NOx Unitaryto Standard (% of limit) |
|
52.5 |
| NOx Unitaryto CAEP2 (% of limit) |
|
65.6 |
| NOx Unitaryto CAEP4 (% of limit) |
|
79 |
| NOx Unitaryto CAEP6 (% of limit) |
|
89.8 |
| NOx Unitaryto CAEP8 (% of limit) |
|
106.7 |
| NOx LTO (g) |
|
5110 |
| Smoke Take Off (SN) |
|
16.8 |
| Smoke Climb Out (SN) |
|
14.6 |
| Smoke Approach (SN) |
|
4.8 |
| Smoke Idle (SN) |
|
2.7 |
| Smoke Max (SN) |
|
16.8 |
| Smoke Sigma (SN) |
|
2 |
| Smoke Range (SN) |
|
14.6-18.8 |
| Smoke Characteristic (SN) |
|
21.6 |
| Smoke Characteristicto Regulatory (% of limit) |
|
95.6 |
| Fuel Flow Take Off (kg/s) |
|
1.131 |
| Fuel Flow Climbout (kg/s) |
|
0.925 |
| Fuel Flow Approach (kg/s) |
|
0.307 |
| Fuel Flow Idle (kg/s) |
|
0.1044 |
| Fuel LTO (kg) |
|
406 |
| Fuel Venting Compliant |
|
No |
| Carbon Monoxide LTO (g) |
|
2968 |
| Compressor Description |
5-stage axial flow low-pressure compressor (LPC); high-pressure compressor (HPC) with 2 axial stages and 1 centrifugal stage |
|
| Emissions Data Status |
|
C |
| Engine Status |
|
Out of production |
| Turbine Description |
1-stage high-pressure turbine (HPT), 1-stage low-pressure turbine (LPT), 4-stage free power turbine |
|