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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 80/146
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
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 81/146
FCOM 19 AUG 10
F/CTL ALTN LAW
Applicable to: ,
L2 Refer to PRO-SUP-27-10 General for flight characteristics.
With autopilot engaged the FMGC (AP mode) controls the aircraft.
L1 (PROT LOST)
L2 All protections, except maneuver protections, are lost. Depending on the failure, static stability may
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 82/146
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
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 83/146
FCOM 19 AUG 10
F/CTL ALTN LAW
Applicable to: ,
MSN,,,,
L2 Refer to PRO-SUP-27-10 General for flight characteristics.
With autopilot engaged the FMGC (AP mode) controls the aircraft.
L1 (PROT LOST)
L2 All protections, except maneuver protections, are lost. Depending on the failure, static stability may
　
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