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AIR COND CTL 1(2) - A(B) FAULT
Applicable to: ,
L2 Informs pilots of which air conditioning system controller (1 or 2) lane (A or B) is faulty.
Crew awareness
STATUS
INOP SYS
COND CTL 1(2)-A(B)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AIR CONDITIONING / PRESSURIZATION / VENTILATION
A318/A319/A320/A321 FLEET PRO-ABN-21 P 78/78
FCOM 19 AUG 10
AIR COND CTL 1(2) - A(B) FAULT
Applicable to:
L2 Informs pilots of which air conditioning system controller (1 or 2) lane (A or B) is faulty.
Crew awareness
STATUS
INOP SYS
COND CTL 1(2)-A(B)
AIR COND CTL 1(2) - A(B) FAULT
Applicable to: ,
MSN,,,,
L2 Informs pilots of which air conditioning system controller (1 or 2) lane (A or B) is faulty.
Crew awareness
STATUS
INOP SYS
COND CTL 1(2)-A(B)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 1/62
FCOM 19 AUG 10
AUTO FLT YAW DAMPER 1(2)
Applicable to:
L2Crew awareness.
Note: The crew can try to reset the affected FAC by using the FAC pb-sw. On ground only, if the
reset is unsuccessful, the taxi and takeoff can be continued with the failed yaw damper
inoperative.
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
AUTO FLT YAW DAMPER 1(2)
Applicable to:
L2Crew awareness.
L2Crew awareness.
Note: The crew can try to reset the affected FAC by using the FAC pb-sw. On ground only, if the
reset is unsuccessful, the taxi and takeoff can be continued with the failed yaw damper
inoperative.
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 2/62
FCOM 19 AUG 10
AUTO FLT YAW DAMPER 1(2)
Applicable to: ,
L2Crew awareness.
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
AUTO FLT YAW DAMPER 1(2)
Applicable to: ,
MSN,,,
L2Crew awareness.
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
AUTO FLT YAW DAMPER 1(2)
Applicable to:
L2Crew awareness.
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 3/62
FCOM 19 AUG 10
AUTO FLT YAW DAMPER 1(2) (Cont'd)
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
AUTO FLT YAW DAMPER 1(2) - FWSPAGE
Applicable to: MSN
STATUS
CAT 3 SINGLE ONLY INOP SYS
CAT 3 DUAL
YAW DAMPER 1(2)
AUTO FLT YAW DAMPER SYS
Applicable to:
L2 Loss of yaw dampers 1 + 2.
L1 FAC 1.......................................................................................................................... OFF THEN ON
FAC 2.......................................................................................................................... OFF THEN ON
If fault remains:
L12
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2 F/CTL normal laws are lost. All protections, except maneuver protections, are lost.
L1MAX SPEED...................................................................................................................... 320 KT
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 4/62
FCOM 19 AUG 10
AUTO FLT YAW DAMPER SYS (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
Speed is limited, due to the loss of high-speed protections.
APPR PROC
FOR LDG...................................................................USE FLAP 3
GPWS LDG FLAP 3................................................................. ON
Will be 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
F/CTL PROT
YAW DAMPER
AP 1 + 2
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(93)
