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position (0 °).
�� IF UNSUCCESSFUL:
ELAC (AFFECTED)................................................................................................................ OFF
L2 Functions are performed by the other ELAC. LAF is degraded (A320 with LAF only)
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC 1(2)
CAT 3 DUAL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 44/146
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT
(ONE COMPUTER FAILED)
Applicable to: ,
MSN,,,,
CAUTION Do not reset ELAC, if uncommanded maneuvers occurred during the flight.
ELAC (AFFECTED).....................................................................................................OFF THEN ON
L12
Note: 1. In some sidestick transducer failure cases, ELAC 1(2) FAULT is triggered without the
procedure, and FAULT It on associated pb does not come on.
2. If the ELAC 1 computer is reset on ground the pitch trim returns to the ground setting
position (0 °).
�� IF UNSUCCESSFUL:
ELAC (AFFECTED)................................................................................................................ OFF
L2 Functions are performed by the other ELAC. LAF is degraded (A320 with LAF only)
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC 1(2)
CAT 3 DUAL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 45/146
FCOM 19 AUG 10
F/CTL ELAC 1 (2) FAULT
(BOTH COMPUTERS FAILED)
Applicable to:
ELAC 1........................................................................................................................ OFF THEN ON
L2Note: If the ELAC 1 computer is reset on ground, the pitch trim returns to the ground setting
position (0 °).
L1 ELAC 2........................................................................................................................ OFF THEN ON
�� If both ELAC FAULT remain:
ELAC 1..................................................................................................................................OFF
ELAC 2..................................................................................................................................OFF
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
L2 Pitch and roll normal laws are lost: Refer to PRO-ABN-27-K F/CTL ALTN LAW. THS motor 1
and both ailerons are lost. LAF is degraded and uses spoilers only (A320 only).
L1MAX SPEED...................................................................................................................... 320 KT
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 46/146
FCOM 19 AUG 10
F/CTL ELAC 1 (2) FAULT (Cont'd)
(BOTH COMPUTERS FAILED)
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
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 to the Refer to 99 Duref Cible
FCOM
ALTN LAW: PROT LOST
WHEN L/G DOWN: DIRECT LAW
See (1)
CAT 1 ONLY
INOP SYS
F/CTL PROT
L+R AIL
ELAC 1+2
AP 1+2
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
00011770 **Not found**).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 47/146
FCOM 19 AUG 10
F/CTL ELAC 1 (2) FAULT
(BOTH COMPUTERS FAILED)
Applicable to: ,
ELAC 1........................................................................................................................ OFF THEN ON
L2Note: If the ELAC 1 computer is reset on ground, the pitch trim returns to the ground setting
position (0 °).
L1 ELAC 2........................................................................................................................ OFF THEN ON
�� If both ELAC FAULT remain:
ELAC 1..................................................................................................................................OFF
　
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