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necessary.
AUTO FLT YAW DAMPER 1(2)
FAULT
FAC 1(2)
WINDSHEAR DET FAULT or
REAC W/S DET FAULT ��
FAC 1+2
Refer to FCOM/PRO-ABN-22-A
AUTO FLT YAW DAMPER
1(2), if applicable
One MCDU locked, or blank MCDU Refer to FCOM/99 Duref Cible
FCOM
Both MCDU locked, or blank FMGC
FMGC malfunction FMGC
23
COM CIDS 1+2 FAULT CIDS On ground, or in flight:
Pull theC/‐ Bs in the following order:
P13 �� and P14 �� on 121VU
M05 and, M06 on 121VU,
G01 and G02 on 49VU.
‐ Wait 10 s, then:
‐ Push the C/B in the following order:
G01, G02, M05, M06.
P13 �� , P14 ��
‐ After CIDS reset, wait approximately 4 min, before
recovering normal operation.
To be continued on next page
ABN-80
30/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
Continued from previous page
Uncommanded EVAC
horn activation
CIDS On ground, or in flight:
Press the EVAC HORN SHUT OFF pb. Set the EVAC
CAPT & PURS CAPT sw to the CAPT only position. Wait
for 3 s. IF UN SUCCESSFUL:
‐ Pull the C/Bs for DIR2 in the following order: G02 on
49VU, M06 on 121VU.
IF UNSUCCESSFUL
‐ Pull the C/Bs for DIR1 in the following order: G01 on
49VU, M05 on 121VU.
‐ Wait for 1 min, then:
‐ Push the C/Bs for DIR2 in the following order: M06, G02.
‐ After CIDS reset, wait approximately 4 min, before
recovering normal operation.
Frozen RMP RMP Refer to FCOM/PRO-SUP-23 FROZEN RMP
FAP freezing FAP On ground, or in flight:
‐ Pull theC/Bs in the following order:
H01 on 49VU, Q14 on 121VU.
‐ Wait 10 s, then:
‐ Push the C/Bs in the following order:
Q14, H01.
24
GPU cannot be connected
to the aircraft
GAPCU On ground only:
The GPU cannot be connected to the electrical network of the
aircraft (AVAIL light is OFF):
•If at least one power source (IDG 1 or 2, APU GEN or batteries)
is connected to the electrical network of the aircraft.
Reset the EXT PWR ‐ pb on 35VU (Press and release)
•If no power source is connected to the electrical network of the
aircraft.
‐ Set the BAT 1 pb-sw and BAT 2 pb-sw to AUTO.
F/CTL ELAC 1(2)
FAULT
F/CTL ALTN LAW
F/CTL ELAC 1(2)
PITCH FAULT
ELAC ‐ Refer to FCOM/PRO-ABN-27-F F/CTL ELAC 1(2) FAULT (One
Computer
Failed), if applicable.
27
ELAC or SEC
malfunction
ELAC or SEC
WARNING
Do not reset more than one computer at a time.
‐ It is possible to reset the flight control computers in flight,
even if not requested by the ECAM, provided only one reset is
performed at a time:
For the ELAC only, in case of uncommanded maneuvers during
the flight, the reset is not recommended.
Note: ‐ When an ELAC reset is performed on ground, the
crew must check the pitch trim position.
‐ If a reset is performed on ground, the flight crew
must then perform a flight control check, as per
SOP.
28
Loss of fuel quantity
indication or Simultaneous
triggering of FUEL L XFR
VALVE CLOSED and
FUEL R XFR VALVE
CLOSED, although FUEL
SD indicates no anomaly.
FQIC On ground, or in flight:
‐ Pull the 3 C/B:
•Channel 1 (A13 on 49VU)
•Channel 2 (M27 on 121VU)
•Channel 1 and 2 (L26 on 121VU)
‐ Wait 5 s, before pushing the 3 C/B.
Note: The fuel quantity indication will be re-established within one min.
To be continued on next page
ABN-80
31/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
Continued from previous page
CAUTION
The FUEL AUTO FEED FAULT ECAM caution will be
lost for the remainder of the flight.
In flight:
‐ If center tank is not empty, while one inner tank
contains less than 5 000 kg (11 000 lb) of fuel:
•FUEL MODE SEL (MAN)
‐ When center tank is empty:
•CTR TK PUMP 1 and 2 (OFF)
•FUEL MODE SEL (MAN)
31
FWS FWC 1(2) FAULT FWC On ground:
Pull, then push, the C/B of the affectedFWC:
‐ FWC 1 (E2 on 49VU)
‐ FWC 2.(Q7 on 121VU)
Wait 50 s after pushing the C/Bs.
In flight:
Pull, then push, the C/B of the affected FWC:
‐ FWC 1 (E2 on 49VU)
‐ FWC 2 (Q7 on 121VU)
Braking malfunction BSCU Refer to FCOM/PRO-SUP-32 BSCU Reset
32
L/G LGCIU 1(2) FAULT LGCIU 1(2) On ground only:
The flight crew must reset the LGCIU after depressurizing the green
hydraulic system.
　
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