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be introduced.
L1Note: In case of GPWS (EGPWS ) alerts, since protections are lost, respect stall warnings
when applying the GPWS (EGPWS ) procedure.
MAX SPEED...........................................................................................................................320 KT
L2 (320/.77 if dual hydraulic system low pressure). Speed is limited to 320 /.82 or 320/.77 for dual
hydraulic failure, due to the loss of high-speed protection.
L1 SPD BRK (IF L OR R ELEVATOR FAULT) .................................................................DO NOT USE
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 84/146
FCOM 19 AUG 10
F/CTL ALTN LAW (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
(320/.77, if dual hydraulic system low pressure).
SPD BRK (IF L OR R ELEVATOR FAULT)....DO NOT USE
APPR PROC
FOR LDG...................................................................USE FLAP 3
GPWS LDG FLAP 3 ................................................................ ON
APPR SPD .....................................................................VREF+10
LDG DIST PROC ...............................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
• If no AP engaged:
WHEN L/G DN: DIRECT LAW
At landing gear extension, control reverts to direct law in
pitch, as well as in roll. Refer to PRO-ABN-27-J F/CTL
DIRECT LAW
• If AP engaged:
WHEN L/G DN AND AP OFF: DIRECT LAW
If the autopilot is disengaged:
Before landing gear extension, ‐ flight control alternate law is
active.
‐ After landing gear extension, flight control direct law is active.
Refer to PRO-ABN-27-J F/CTL DIRECT LAW
ALTN LAW: PROT LOST
INOP SYS
F/CTL PROT
CONFIG RUD TRIM NOT IN T.O RANGE
Applicable to: ALL
L2Crew awareness
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 85/146
FCOM 19 AUG 10
F/CTL FCDC 1 (2) FAULT
Applicable to:
L2Crew awareness
STATUS
INOP SYS
FCDC 1(2)
F/CTL FCDC 1 (2) FAULT
Applicable to: ,
L2Crew awareness
STATUS
INOP SYS
FCDC 1(2)
F/CTL FCDC 1 (2) FAULT
Applicable to: ,
MSN,,,,
L2Crew awareness
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 86/146
FCOM 19 AUG 10
F/CTL FCDC 1 (2) FAULT (Cont'd)
STATUS
INOP SYS
FCDC 1(2)
F/CTL FCDC 1+2 FAULT
Applicable to:
MONITOR F/CTL OVHD PNL
L2 F/CTL data on ECAM is lost.
Control laws remains normal.
Note: When both FCDCs fails:
F/CTL warning are ‐ not available on the ECAM.
‐ Stall warning may be triggered as in alternate or direct law (it may occur at speeds
greater than Vα max).
‐ Bank and pitch limits are no longer displayed on the PFD.
‐ Vα prot, Vα max are lost on the PFD.
‐ Vsw, displayed on the PFD, corresponds to the stall warning of the alternate or direct
law.
STATUS
F/CTL INDICATIONS LOST INOP SYS
FCDC 1 + 2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 87/146
FCOM 19 AUG 10
F/CTL FCDC 1+2 FAULT
Applicable to: ,
MONITOR F/CTL OVHD PNL
L2 F/CTL data on ECAM is lost.
Control laws remains normal.
Note: When both FCDCs fails:
F/CTL warning are ‐ not available on the ECAM.
‐ Stall warning may be triggered as in alternate or direct law (it may occur at speeds
greater than Vα max).
‐ Bank and pitch limits are no longer displayed on the PFD.
‐ Vα prot, Vα max are lost on the PFD.
‐ Vsw, displayed on the PFD, corresponds to the stall warning of the alternate or direct
law.
STATUS
F/CTL INDICATIONS LOST INOP SYS
FCDC 1 + 2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 88/146
FCOM 19 AUG 10
F/CTL FCDC 1+2 FAULT
Applicable to: ,
MSN,,,,
MONITOR F/CTL OVHD PNL
L2 F/CTL data on ECAM is lost.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(97)
