III.6.3 Input for runway length calculation:
| C601 | ||
| Roll friction coefficient | 0.03 | |
| max. break delay | (g) | 0.35 |
| Reaction time | (sec) | 2.5 |
| Weight factor | 1.15 | |
| CA^ with flaps | 2.5 | |
| max flap angle | (°) | 25 |
| CD0 with flaps & gears | 0.016 | |
| Density | (kg/in ) | 1.225 |
| Engine number | 4 | |
| Thrust /weight | 0.263 | |
| Wing load | (kg/m2) | 700 |
| Wing aspect ratio | 8.32 | |
Runway Length according to FAR25 C601
| Take-off Weight | Range with 100% pax | Required Runway |
| kg | km | m |
| 531000 | 13300 | 3300 |
| 511000 | 12100 | 2900 |
| 491000 | 10900 | 2600 |
| 471000 | 9650 | 2400 |
| 451000 | 8300 | 2100 |
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