| 20 |
What primary flight controls will be available if both System A and
System B fail while airborne with the flaps up ?
System B fail while airborne with the flaps up ?
The ailerons and elevator operated by control cables (Manual
Reversion).
The rudder will not be available unless either FLT CONTROL switch
is positioned to SBY RUD. Standby System pressure will the power
the standby rudder PCU (Power Control Unit) and standby Yaw
Damper.
Reversion).
The rudder will not be available unless either FLT CONTROL switch
is positioned to SBY RUD. Standby System pressure will the power
the standby rudder PCU (Power Control Unit) and standby Yaw
Damper.
| Hydraulic Panel and System |