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┃I -~ A318 ┃I FLIGHTDESCRIPTION ┃SEQ 100 1 ┃I REV 24 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃ ┃
┃ A~7-~'M" A321 ┃ ┃ ┃ ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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RUDDER TRAVEL LIMIT
The deflection of the rudder and the pedals is limited as a function of speed.
Each channel of the limiter is controlled and monitored by its associated FAC. If both FACs
fail, maximum deflection is available when the slats are extended.
RUDDER TRIM
RAXRUDDER DEFLECTION
3./.~
140
CAS (KT)
The two electric motors that position the artificial feel unit also trim the rudder. In normal
operation, motor N~ 1, controlled by FAC1, drives the trim, and FAC2 with motor N~ 2
remains synchronized as back-up.
In manual flight, the pilot can apply rudder trim with the rotary RUD TRIM switch on the
pedestal.
- Maximum deflection is _+ 25~.
- Budder trim speed is one degree per second.
- In addition to limitation by TLU, if rudder trim is applied, maximum rudder deflection may
be reduced in the opposite direction.
The pilot can use a button on the BUD TRIM panel to reset the rudder trim to zero.
Note : With the autopilot engaged, the FMGC computes the rudder trim orders. The rudder
trim rotary switch and the rudder trim reset pushbutton are not active.
CCM ALL
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┃I -~ A318 ┃FLIGHT CONTROLS ┃1.27.10 P 17 ┃
┃ .,,,.8, ,, ~L,~ A319 ┃ ┃ ┃
┃ Lli,~ A320 ┃ ┃ ┃
┃ ┃ ┣━━━━┳━━━━┫
┃ A~7-~'M" A321 ┃ DESCRIPTION ┃SEQ 001 ┃REV 23 ┃
┃ FLIGHT CREW OPERATING MANUAL ┃ ┃ ┃ ┃
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YAW CONTROL - SCHEMATIC
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┃I -~ A318 ┃FLIGHT CONTROLS ┃1.27.20 P 1 ┃
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本文链接地址：
AIRBUS A320 Flight Crew Operating Manual3(82)
