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Applicable to: ,
FAC (AFFECTED)....................................................................................................... OFF THEN ON
�� IF UNSUCCESSFUL:
FAC (AFFECTED).................................................................................................................. OFF
L2 All functions are performed by the remaining FAC.
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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 23/62
FCOM 19 AUG 10
AUTO FLT FAC 1(2) FAULT
Applicable to: ,
MSN,,,,
FAC (AFFECTED)....................................................................................................... OFF THEN ON
�� IF UNSUCCESSFUL:
FAC (AFFECTED).................................................................................................................. OFF
L2 All functions are performed by the remaining FAC.
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.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 24/62
FCOM 19 AUG 10
AUTO FLT FAC 1 + 2 FAULT
Applicable to:
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 above 160 kt.
At slats’ extension, full rudder travel authority is recovered.
L1 FAC 1 ......................................................................................................................... OFF THEN ON
FAC 2.......................................................................................................................... OFF THEN ON
�� IF UNSUCCESSFUL:
FAC 1 + 2..............................................................................................................................OFF
L2With FAC 1 + 2 inoperative, the rudder travel limit system, rudder trim control, yaw damper and
PFD characteristic speeds are lost.
L12
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
F/CTL normal laws are lost. All protections, except maneuver protections, are lost.
L1MAX SPEED .....................................................................................................................320 KT
L2 Speed is limited, due to the loss of high-speed protections.
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 25/62
FCOM 19 AUG 10
AUTO FLT FAC 1 + 2 FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
RUD WITH CARE ABV 160 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
GPWS LDG FLAP 3................................................................. ON
Displayed, when flaps in CONF 3.
APPR SPD............................................................. VREF + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW : PROT LOST
WHEN L/G DN : DIRECT LAW
See (1)
CAT 1 ONLY
INOP SYS
REAC W/S DET
F/CTL PROT
FAC 1 + 2
AP 1 + 2
A/THR
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
00000610 **Not found** DIRECT LAW procedure).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 26/62
FCOM 19 AUG 10
AUTO FLT FAC 1 + 2 FAULT
Applicable to:
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 above 160 kt.
At slats’ extension, full rudder travel authority is recovered.
L1 FAC 1 ......................................................................................................................... OFF THEN ON
　
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