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┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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YAW DAMPING
Yaw damping stabilizes the aircraft in yaw and coordinates its turns.
In automatic flight (AP engaged) during takeoff and go around, it assists rudder application
after an engine failure (short-term yaw compensation).
Note : When the AP is engaged, the FMGS sends orders to the FAC to give
- yaw damping during approach
- yaw control for runway alignment in ROLL OUT mode
CCM ALL
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┃I ~-Z A318 ┃ AUTO FLIGHT ┃1.22.40 P 3 ┃
┃ aw aw ,, ~L,~ A319 ┃ ┃ ┃
┃ ┃ ┣━━━━━┳━━━━━┫
┃ Lii,~ A320 ┃ ┃SEQ 110 [ ┃ REV 26 ┃
┃ A~7-~'M" A321 ┃FLIGHT AUGMENTATION ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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RUDDER TRIM
The rudder trim function :
- Executes trim orders the pilot enters with the manual trim knob
- When AP is engaged
. executes trim orders from the FMGS.
. Assists the system in recovering from engine failure (long-term yaw compensation) in
all flight guidance modes.
. If the pilot pushes the rudder more than 10~ out of trim, it disengages the AP.
Note" When the AP is engaged, the rudder
FMGC sends rudder trim orders to the
RUDDER TRAVEL LIMITATION
trim knob is inoperative ~ the master
FAC,
This function limits rudder deflection as a function of speed in order to avoid high structura
loads. It is governed by the following law ~
MAX
RUDDER
DEFLECTION
30
3.4~
140
380 SPEEb
(KT)
If both FACs lose the rudder travel limitation function, the value of the rudder deflection limit
is locked at the time of the second failure.
When the slats are extended, the FACs automatically set the rudder deflection limit at the
low-speed setting (maximum authorized deflection).
EEM ALL
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┃ ┃ ┃1.22.40 P 4 ┃
┃ ┃ ┣━━━━━┳━━━━━┫
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual2(94)
