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L1 AT LDG ROLL:
DIFF BRAKING............................................................................................................. AS RQRD
L12
STATUS
RUD WITH CARE ABV 160 KT
AT LDG ROLL:
DIFF BRAKING....................................................... AS RQRD
CAT 3 SINGLE ONLY
INOP SYS
RUD TRV LIM
CAT 3 DUAL
Note: An autoland must
not be performed
with a crosswind
greater than 12 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 20/62
FCOM 19 AUG 10
AUTO FLT RUD TRV LIM SYS
Applicable to: , , MSN
RUD WITH CARE ABV 160 KT
L2 Depending on when the failure occurs, the rudder travel limiter system may not be in the correct
position for the flight speed. Therefore, to prevent damage to the aircraft structure, use the rudder
with care, when the speed is greater than 160 kt.
At slats’ extension, full rudder travel authority can be recovered.
L1 FAC 1.......................................................................................................................... OFF THEN ON
FAC 2.......................................................................................................................... OFF THEN ON
If TLU (rudder or pedals) remains locked at high speed after slat extension:
MAX X WIND FOR LDG 15 KT
AUTO BRK..............................................................................................................DO NOT USE
L2 Do not use the autobrake, so as not to delay the application of differential braking at landing
roll.
L1 AT LDG ROLL:
DIFF BRAKING............................................................................................................. AS RQRD
L12
STATUS
RUD WITH CARE ABV 160 KT
• If TLU (rudder or pedals) remains locked at high speed
after slat extension:
MAX X WIND FOR LDG 15 KT
AUTO BRK..............................................DO NOT USE
Do not use the autobrake, so as not to delay the
application of differential braking at landing roll.
AT LDG ROLL:
DIFF BRAKING....................................................... AS RQRD
CAT 3 SINGLE ONLY
INOP SYS
RUD TRV LIM
CAT 3 DUAL
Note: An autoland must
not be performed
with a crosswind
greater than 12 kt.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 21/62
FCOM 19 AUG 10
AUTO FLT RUD TRV LIM SYS
Applicable to: MSN,,
RUD WITH CARE ABV 160 KT
L2 Depending on when the failure occurs, the rudder travel limiter system may not be in the correct
position for the flight speed. Therefore, to prevent damage to the aircraft structure, use the rudder
with care, when the speed is greater than 160 kt.
At slats’ extension, full rudder travel authority can be recovered.
L1 FAC 1.......................................................................................................................... OFF THEN ON
FAC 2.......................................................................................................................... OFF THEN ON
If TLU (rudder or pedals) remains locked at high speed after slat extension:
MAX X WIND FOR LDG 15 KT
AUTO BRK..............................................................................................................DO NOT USE
L2 Do not use the autobrake, so as not to delay the application of differential braking at landing
roll.
L1 AT LDG ROLL:
DIFF BRAKING............................................................................................................. AS RQRD
AUTO FLT FAC 1(2) FAULT
Applicable to:
FAC (AFFECTED)....................................................................................................... OFF THEN ON
IF UNSUCCESSFUL:
FAC (AFFECTED).................................................................................................................. OFF
L2 All functions are performed by the remaining FAC.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 22/62
FCOM 19 AUG 10
AUTO FLT FAC 1(2) FAULT (Cont'd)
L12
STATUS
BOTH PFD ON SAME FAC
See (1)
CAT 3 SINGLE ONLY
INOP SYS
CAT 3 DUAL
FAC 1(2)
(1) CL2haracteristic speeds, displayed on the two PFDs, are computed by the same FAC.
AUTO FLT FAC 1(2) FAULT
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(98)
