| |
CFM56-3-B1 |
-3B-2 |
-3C-1 |
TAKEOFF CONDITIONS
(sea level) |
| - Max. takeoff (lb) |
20,000 |
22,000 |
23,500 |
| - Airflow (lb/sec) |
638-655 |
683 |
638-710 |
| - Bypass ratio |
6.0 |
5.9 |
6.0 |
IN-FLIGHT PERFORMANCE (installed)
(35,000 ft-Mach=0.80-ISA) |
| - Max. climb thrust (lb) |
4,860 |
5,260 |
5,540 |
| - Overall pressure ratio at max. climb |
27.5 |
28.8 |
30.6 |
| - Max. cruise thrust (lb) |
4,650 |
5,040 |
5,370 |
| - Max. cruise thrust (lb) |
0.671 |
0.657 |
0.648 |
| ENGINE CHARACTERISTICS |
| - Length (in) |
93 |
93 |
93 |
| - Fan diameter (in) |
60 |
60 |
60 |
| - Basic dry weight (lb) |
4,276 |
4,301 |
4,301 |
| APPLICATIONS |
| |
737-300
737-500
|
737-300
737-400
|
737-300
737-400
737-500
|
| |
-3-B1
|
-3B-2
|
-3C-1
|
|
