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‐ RE-ENTER the barometer
altimeter setting value, if
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
29/32
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.
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
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: 1. The fuel quantity indication will be re-established within
one min.
2. The fuel leak detection function will be lost for the
remainder of the flight. The flight crew must monitor the fuel
quantity according toRefer to FCOM/PRO-NOR-SOP-15-A
28 Cruise - Flight Progress
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
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:
　
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