| Family |
CFM56-7B |
|
| EASA ID |
01P11CM115 |
7PW084 |
| Aircraft Engine Manufacturer |
CFM International |
Pratt & Whitney |
| Aircraft Engine Type |
Turbofan |
Turbofan |
| Comment |
Boeing 737 Next Generation |
|
| Dry Weight (kg) |
2366 |
|
| Diameter (mm) |
1549 |
|
| Max Rotating Diameter (mm) |
1549 |
|
| Length (mm) |
2507 |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/CFM_International_CFM56 |
|
| Fuel |
Jet A |
Jet A |
| Fan Blades |
24 |
|
| Geared Fan |
No |
No |
| Low-Pressure Compressor Stages |
3 |
|
| High-Pressure Compressor Stages |
9 |
|
| Combustion Chamber |
Tech Insertion |
Talon II |
| High Pressure Compressor Stages |
1 |
|
| Low-Pressure Turbine Stages |
4 |
|
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
5.3 |
4.8 |
| Overall Pressure Ratio |
25.6 |
28 |
| Maximum Takeoff Thrust (kN) |
107.6 |
105.87 |
| Hydrocarbon Take Off (g/kg fuel) |
0.02 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.03 |
0.002 |
| Hydrocarbon Approach (g/kg fuel) |
0.06 |
0.001 |
| Hydrocarbon Idle (g/kg fuel) |
2.3 |
0.002 |
| Hydrocarbon Unitary Average (g/kN) |
3.51 |
0 |
| Hydrocarbon Unitary Sigma (g/kN) |
0.45 |
|
| Hydrocarbon Unitary Range (g/kN) |
3.01-3.88 |
|
| Hydrocarbon Unitary Characteristic (g/kN) |
4.09 |
0 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
20.9 |
0.1 |
| Hydrocarbon LTO (g) |
377 |
1 |
| Carbon Monoxide Take Off (g/kg fuel) |
0.18 |
0.68 |
| Carbon Monoxide Climb Out (g/kg fuel) |
0.15 |
0.81 |
| Carbon Monoxide Approach (g/kg fuel) |
3.68 |
3.69 |
| Carbon Monoxide Idle (g/kg fuel) |
34.71 |
25.19 |
| Carbon Monoxide Unitary Average (g/kN) |
54.38 |
46.2 |
| Carbon Monoxide Unitary SD (g/kN) |
2.8 |
|
| Carbon Monoxide Unitary Range (g/kN) |
51.2-56.4 |
|
| Carbon Monoxide Unitary Characteristic (g/kN) |
58.8 |
56.7 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
49.8 |
48.2 |
| NOx Take Off (g/kg fuel) |
18.93 |
21.03 |
| NOx Climb Out (g/kg fuel) |
15.6 |
15.85 |
| NOx Approach (g/kg fuel) |
8.6 |
6.88 |
| NOx Idle (g/kg fuel) |
4.09 |
3.58 |
| NOx Unitary Average (g/kN) |
37.11 |
39.4 |
| NOx Unitary SD (g/kN) |
1.2 |
|
| NOx Unitary Range (g/kN) |
36.1-38.5 |
|
| NOx Unitary Characteristic (g/kN) |
39.3 |
45.7 |
| NOx Unitaryto Standard (% of limit) |
43.1 |
47.6 |
| NOx Unitaryto CAEP2 (% of limit) |
53.9 |
59.5 |
| NOx Unitaryto CAEP4 (% of limit) |
65.5 |
71.6 |
| NOx Unitaryto CAEP6 (% of limit) |
74.5 |
81.4 |
| NOx Unitaryto CAEP8 (% of limit) |
89.5 |
96.6 |
| NOx LTO (g) |
3996 |
4170 |
| Smoke Take Off (SN) |
12.1 |
5.16 |
| Smoke Climb Out (SN) |
8.7 |
4.71 |
| Smoke Approach (SN) |
2.1 |
1.32 |
| Smoke Idle (SN) |
2.1 |
1.51 |
| Smoke Max (SN) |
12.07 |
5.16 |
| Smoke Sigma (SN) |
3.4 |
|
| Smoke Range (SN) |
8.3-14.7 |
|
| Smoke Characteristic (SN) |
13.28 |
6.7 |
| Smoke Characteristicto Regulatory (% of limit) |
57.2 |
28.5 |
| Fuel Flow Take Off (kg/s) |
1.086 |
1.169 |
| Fuel Flow Climbout (kg/s) |
0.895 |
0.939 |
| Fuel Flow Approach (kg/s) |
0.308 |
0.325 |
| Fuel Flow Idle (kg/s) |
0.103 |
0.114 |
| Fuel LTO (kg) |
398 |
429 |
| Fuel Venting Compliant |
Yes |
No |
| Carbon Monoxide LTO (g) |
5854 |
4901 |
| Compressor Description |
1 fan, 3-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) |
2.3.2 e) |
| nvPME Imass Approach (mg/kg) |
1.29 |
|
| nvPME Imass Climb Out (mg/kg) |
33.6 |
|
| nvPME Imass Idle (mg/kg) |
0.8 |
|
| nvPME Imass Max (mg/kg) |
48.6 |
|
| nvPME Imass Take Off (mg/kg) |
48.6 |
|
| nvPME Inum Approach (#/kg) |
54600000000000 |
|
| nvPME Inum Climb Out (#/kg) |
424000000000000 |
|
| nvPME Inum Idle (#/kg) |
36900000000000 |
|
| nvPME Inum Max (#/kg) |
431000000000000 |
|
| nvPME Inum Take Off (#/kg) |
428000000000000 |
|
| nvPMLTO Mass (mg) |
6408 |
|
| nvPMLTO Mass Per Thrust (mg/kN) |
82.8 |
|
| nvPMLTO Mass To CAEP11 (% of limit) |
16.3 |
|
| nvPMLTO Number (#) |
79500000000000000 |
|
| nvPMLTO Number Per Thrust (#/kN) |
1030000000000000 |
|
| nvPMLTO Number To CAEP11 (% of limit) |
16.6 |
|
| nvPM Mass Concentration Characteristic (mg/m³) |
1434 |
|
| nvPM Mass Concentration Max (mg/m³) |
1114 |
|
| nvPM Mass Concentration To CAEP10 (% of limit) |
22.5 |
|
| Turbine Description |
1-stage HP, 4-stage LP |
|