| 18 |
What conditions must exist for the Standby System to automatically
activate ?
activate ?
Loss of System A or B, and
Flaps extended, and
airborne or wheel speed greater than 60 knots.
FLT CONTROL switch A or B, located on the Flight Control Panel,
must be in the normal guarded ON position.
Flaps extended, and
airborne or wheel speed greater than 60 knots.
FLT CONTROL switch A or B, located on the Flight Control Panel,
must be in the normal guarded ON position.
| Hydraulic Panel and System |