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recover the affected ELAC on the ground, if the reset was unsuccessful, switch OFF the
G,Y and B HYD PUMPS sw (PARK BRK handle ON), wait 1 min, then reset the ELAC
pb. After 8 s (end of power up test indicated by the disappearance of the ELAC FAULT
warning), switch the G, Y and B HYD PUMPS to ON/AUTO.
3. 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 41/146
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT
(ONE COMPUTER FAILED)
Applicable to:
CAUTION Do not reset ELAC, if uncommanded maneuvers occurred during the flight.
ELAC (AFFECTED).....................................................................................................OFF THEN ON
Note: 1. In some sidestick transducer failure cases, ELAC 1(2) FAULT is triggered without the
proc, and FAULT It on associated pb does not come on.
2. ELAC FAULT may be triggered during engine start, due to the electrical transient. To
recover the affected ELAC on the ground, if the reset was unsuccessful, switch OFF the
G,Y and B HYD PUMPS sw (PARK BRK handle ON), wait 1 min, then reset the ELAC
pb. After 8 s (end of power up test indicated by the disappearance of the ELAC FAULT
warning), switch the G, Y and B HYD PUMPS to ON/AUTO.
3. 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)
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)
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 42/146
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT (Cont'd)
(ONE COMPUTER FAILED)
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC 1(2)
CAT 3 DUAL
F/CTL ELAC 1(2) FAULT
(ONE COMPUTER FAILED)
Applicable to: ,
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 43/146
FCOM 19 AUG 10
F/CTL ELAC 1(2) FAULT
(ONE COMPUTER FAILED)
Applicable to:
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
　
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