| |
CFM56-5C2 |
-5C3 |
-5C4 |
TAKEOFF CONDITIONS
(sea level) |
| - Max. takeoff (lb) |
31,200 |
32,500 |
34,000 |
| - Airflow (lb/sec) |
1,027 |
1,045 |
1,065 |
| - Bypass ratio |
6.6 |
6.5 |
6.4 |
IN-FLIGHT PERFORMANCE (installed)
(35,000 ft-Mach=0.80-ISA) |
| - Max. climb thrust (lb) |
7,370 |
7,370 |
7,580 |
| - Overall pressure ratio at max. climb |
37.4 |
37.4 |
38.3 |
| - Max. cruise thrust (lb) |
6,910 |
6,910 |
7,100 |
| ENGINE CHARACTERISTICS |
| - Length (in) |
103 |
103 |
103 |
| - Fan diameter (in) |
72.3 |
72.3 |
72.3 |
| - Basic dry weight (lb) |
8,796 |
8,796 |
8,796 |
| APPLICATIONS |
A340-200
A340-300
|
A340-200
A340-300
|
A340-200
A340-300
|
|
