| Family |
CFM56-7B |
|
| EASA ID |
4CM039 |
4BR003 |
| Aircraft Engine Manufacturer |
CFM International |
Rolls-Royce Deutschland |
| 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 |
AVTUR |
| Fan Blades |
24 |
|
| Geared Fan |
No |
No |
| Low-Pressure Compressor Stages |
3 |
|
| High-Pressure Compressor Stages |
9 |
|
| High Pressure Compressor Stages |
1 |
|
| Low-Pressure Turbine Stages |
4 |
|
| Afterburner |
No |
No |
| Streams |
2 |
2 |
| Bypass Ratio |
5.4 |
4.6 |
| Overall Pressure Ratio |
22.77 |
30.47 |
| Maximum Takeoff Thrust (kN) |
91.63 |
89.68 |
| Hydrocarbon Take Off (g/kg fuel) |
0.07 |
0 |
| Hydrocarbon Climb Out (g/kg fuel) |
0.23 |
0.01 |
| Hydrocarbon Approach (g/kg fuel) |
0.36 |
0 |
| Hydrocarbon Idle (g/kg fuel) |
8.11 |
0.17 |
| Hydrocarbon Unitary Average (g/kN) |
14.61 |
0.3 |
| Hydrocarbon Unitary Range (g/kN) |
13.8-15.9 |
0.24-0.37 |
| Hydrocarbon Unitary Characteristic (g/kN) |
17 |
0.5 |
| Hydrocarbon Unitary Characteristicto Regulatory (% of limit) |
86.9 |
2.3 |
| Hydrocarbon LTO (g) |
1340 |
27 |
| Carbon Monoxide Take Off (g/kg fuel) |
4.26 |
0.78 |
| Carbon Monoxide Climb Out (g/kg fuel) |
11.38 |
0.76 |
| Carbon Monoxide Approach (g/kg fuel) |
11.37 |
3.38 |
| Carbon Monoxide Idle (g/kg fuel) |
49.71 |
15.56 |
| Carbon Monoxide Unitary Average (g/kN) |
108.63 |
30.08 |
| Carbon Monoxide Unitary Range (g/kN) |
102.1-114.9 |
29.44-31.21 |
| Carbon Monoxide Unitary Characteristic (g/kN) |
117.5 |
36.9 |
| Carbon Monoxide Unitary Characteristicto Regulatory (% of limit) |
99.6 |
31.3 |
| NOx Take Off (g/kg fuel) |
13.25 |
27.21 |
| NOx Climb Out (g/kg fuel) |
10.81 |
20.34 |
| NOx Approach (g/kg fuel) |
9.39 |
11.38 |
| NOx Idle (g/kg fuel) |
3.75 |
5.54 |
| NOx Unitary Average (g/kN) |
30.58 |
51.1 |
| NOx Unitary Range (g/kN) |
30.4-30.8 |
50.79-51.54 |
| NOx Unitary Characteristic (g/kN) |
32.4 |
59.2 |
| NOx Unitaryto Standard (% of limit) |
37.9 |
58.7 |
| NOx Unitaryto CAEP2 (% of limit) |
47.3 |
73.3 |
| NOx Unitaryto CAEP4 (% of limit) |
58.4 |
87.2 |
| NOx Unitaryto CAEP6 (% of limit) |
66.4 |
98.9 |
| NOx Unitaryto CAEP8 (% of limit) |
81.1 |
115.9 |
| NOx LTO (g) |
2802 |
4583 |
| Smoke Take Off (SN) |
0.7 |
3.55 |
| Smoke Climb Out (SN) |
0.7 |
2.9 |
| Smoke Approach (SN) |
1.5 |
1.03 |
| Smoke Idle (SN) |
0.7 |
0.89 |
| Smoke Max (SN) |
1.52 |
3.55 |
| Smoke Range (SN) |
0-3.4 |
3.24-3.8 |
| Smoke Characteristic (SN) |
1.7 |
4.6 |
| Smoke Characteristicto Regulatory (% of limit) |
6.9 |
18.9 |
| Fuel Flow Take Off (kg/s) |
0.903 |
0.905 |
| Fuel Flow Climbout (kg/s) |
0.754 |
0.743 |
| Fuel Flow Approach (kg/s) |
0.278 |
0.259 |
| Fuel Flow Idle (kg/s) |
0.102 |
0.098 |
| Fuel LTO (kg) |
363 |
351 |
| Fuel Venting Compliant |
No |
No |
| Carbon Monoxide LTO (g) |
9963 |
2693 |
| Compressor Description |
1 fan, 3-stage LP, 9-stage HP |
|
| Emissions Data Status |
C |
C |
| Engine Status |
Out of production |
Out of production |
| Turbine Description |
1-stage HP, 4-stage LP |
|