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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 55/146
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)
INOP SYS
F/CTL PROT
L+R AIL
ELAC 1+2
AP 1+2
CAT 2
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
00011770 **Not found**).
F/CTL ELAC 1 (2) PITCH FAULT
Applicable to:
L2 Pitch function is achieved by the other ELAC.
Crew 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 56/146
FCOM 19 AUG 10
F/CTL ELAC 1 (2) PITCH FAULT (Cont'd)
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC PITCH (1)
CAT 3 DUAL
(1) (If ELAC 1 and 2 PITCH FAULT)
F/CTL ELAC 1 (2) PITCH FAULT
Applicable to: ,
L2 Pitch function is achieved by the other ELAC.
Crew awareness
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC PITCH (1)
CAT 3 DUAL
(1) (If ELAC 1 and 2 PITCH FAULT)
F/CTL ELAC 1 (2) PITCH FAULT
Applicable to: ,
MSN,,,,
L2 Pitch function is achieved by the other ELAC.
Crew 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 57/146
FCOM 19 AUG 10
F/CTL ELAC 1 (2) PITCH FAULT (Cont'd)
STATUS
CAT 3 SINGLE ONLY INOP SYS
ELAC PITCH (1)
CAT 3 DUAL
(1) (If ELAC 1 and 2 PITCH FAULT)
Config SPD BRK NOT RETRACTED
Applicable to: ALL
L2Crew awareness.
F/CTL SEC 1 (2) (3) FAULT
Applicable to:
SEC (AFFECTED).......................................................................................................OFF THEN ON
IF UNSUCCESSFUL:
SEC (AFFECTED).................................................................................................................. OFF
L2 Associated spoilers are lost. If SEC 1 or 2 fails, LAF is degraded (A320 with LAF only).
If all spoilers are inoperative (3 SECs failed), roll direct law and pitch alternate law become
active.
L1 SPD BRK (IF SEC 1 AFFECTED)..........................................................................DO NOT USE
L2 VLS would not be corrected, if speed brakes 2 extend (no speed brake position sent to FACs).
L1 If SEC 1 + 2 + 3 fail.
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
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 58/146
FCOM 19 AUG 10
F/CTL SEC 1 (2) (3) FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
(If SEC 1 is affected.)
FOR LDG...................................................................USE FLAP 3
(If SEC 1 + 2 + 3 fail).
APPR SPD......................................................................VREF+10
(If SEC 1 + 2 + 3 fail).
LDG DIST PROC................................................................APPLY
(Not displayed, if only SEC 2 is affected).
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
• (If SEC 1 + 2 + 3 fail).
ALTN LAW: PROT LOST
• If no AP engaged
or
If SEC 1 + 2 + 3 fail.
WHEN L/G DN : DIRECT LAW
If SEC 1 + 2 + 3 fail. In such a case, the LGCIU
information can no longer be sent to the ELAC. For the
activation of DIRECT law, the ELAC uses the condition
“slats and flaps in CONF 2”, instead of “landing gear
down”.
• If AP engaged
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(89)
