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┃ aw aw ,, ~L,~ A319             ┃                            ┃          ┃          ┃
┃ Lli,~ A320                     ┃                            ┃          ┃          ┃
┃      A~7-~'M" A321             ┃                            ┃          ┃          ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                            ┃          ┃          ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━━━━━━━┻━━━━━┻━━━━━┛
ROLL CONTROL - SCHEMATIC
        FSPD-BI~
I~GND-SPL~
      FSPD-BI~
I~GND-SPL~
┏━━━━━━━━━━━━━━━━┳━━━━━━━━┳━━━━━━━━━┓
┃I  -~ A318                      ┃FLIGHT CONTROLS ┃1.27.10     P 15  ┃
┃  .*,,.8, ,, ~L,~ A319          ┃                ┃                  ┃
┃ Lli,~ A320                     ┃                ┃                  ┃
┃                                ┃                ┣━━━━┳━━━━┫
┃      A~7-~'M" A321             ┃   DESCRIPTION  ┃SEQ 001 ┃REV 23  ┃
┃   FLIGHT CREW OPERATING MANUAL ┃                ┃        ┃        ┃
┗━━━━━━━━━━━━━━━━┻━━━━━━━━┻━━━━┻━━━━┛
YAW CONTROL
One rudder surface controls yaw
ELECTRICAL RUDDER CONTROL
The yaw damping and turn coordination functions are automatic.
The ELACs compute yaw orders for coordinating turns and damping yaw oscillations, and
transmit them to the FACs.
MECHANICAL RUDDER CONTROL
The pilots can use conventional rudder pedals to control the rudder
RUDDER ACTUATION
Three independent hydraulic servojacks, operating in parallel, actuate the rudder. In
automatic operation (yaw damping, turn coordination) a green servo actuator drives all
three servojacks. A yellow servo actuator remains synchronized and takes over if there is
a failure.
There is no feedback to the rudder pedals from the yaw damping and turn coordination
functions.
CCM ALL
┏━━━━━━━━━━━━━━━━┳━━━━━━━━━━━━━━┳━━━━━━━━━━━┓
┃                                ┃                            ┃1.27.10     P 16      ┃
┃                                ┃                            ┣━━━━━┳━━━━━┫
　
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本文鏈接地址：AIRBUS A320 Flight Crew Operating Manual3(81)