ICAS msg: Rudder Overboost
If both systems running > 135 kts
Normally sys #1 shut off >135 kts
Flap System consist off:
If one flap motor fail
Flaps will extend slower
Pitch Trim components
HSA Excessive load protection
Trim system shuts off a channel if switch actuated for period of time that totalizes 16sec when Horizontal Stabilizer Actuator is stalled
Rudder Hardover Protection
The rudder systems auto shut off if:
Trim switch logic
Rudder Panels
* AFT Rudder ( deflects further )
FECU will stop flap movement if flap difference is ..°?
2° ( by flap velocity sensors )
Trim switch protection
If 1/2 of any pitch trim switch in stuck for 7 seconds continuously, Control Unit will deactivate that faulty switch
What some of the systems attached to HSCU?
What HSCU main channel control?
What trim?
Control column (yoke) trim (Main trim)
How many degrees can you pitch horizontal stab up/dn?
Up - 10°
Down - 4°
Can you lock gust lock in-flight?
NO
How do you trim ailerons?
You move the center position of the aileron
What do you lose when you disconnected ailerons if:
Left:
• Left aileron
• Autopilot servo
• Pusher
Right:
• Right aileron
• Artificial feel unit
What type of Rudders do we have?
Two in-tandem rudders
Rudder on rudder
Do you have a feel unit on the elevators?
No
Aileron Disconnect Pull
What control do you have?
* FO side - right aileron
What type of flaps?
Two double slotted flap panels
How many Jack screws are there to move horizontal stab?
2
* Servo Tab
Pitch control consists of:
Tail
* All moving horizontal stabilizer
Control Column / Cabin Vibration
could be caused by?
How to check?
Elevator horn when elevator is not aligned with horizontal stabilizer
•Pitch slightly up or down