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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 5/62
FCOM 19 AUG 10
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
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)
INOP SYS
F/CTL PROT
YAW DAMPER
AP 1 + 2
CAT 2
(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 6/62
FCOM 19 AUG 10
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 7/62
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
00000610 **Not found** DIRECT LAW procedure).
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 8/62
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
　
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