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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:
‐ 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.
‐ ENG MASTER switch 1 OFF
‐ PTU OFF
When there is no green hydraulic pressure:
‐ To reset LGCIU 1:
▪Pull C/B Q34 on 121VU, then C09 on 49VU
▪Wait for 15 s , then push the C/Bs
‐ To reset LGCIU 2:
▪Pull C/B Q35 on 121VU
▪Wait for 15 s , then push the C/B
34
NAV TCAS FAULT TCAS On ground only:
‐ Pull C/B K10 on 121VU.
‐ Wait 5 s, then push the C/B.
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
ISIS malfunction ISIS On ground only:
With aircraft not moving:
‐ Pull C/B F12 on 49VU,
‐ Wait 5 s ,then push the C/B,
‐ Normal operation is expected after approximately 2 min.
Note: In the case of small aircraft motion during the C/B reset (refueling,
cargo loading conditions, etc.), the ATT red flag may appear on the ISIS. In
this case, press the RST P/B for 2 s wait 2 min additional to recover normal
operation.
38
Failure messages on the CIDS
FAP in the cabin
Vacuum System
Controller On ground, or in flight:
‐ Pull C/B 35 MG on 2001VU, aft cabin,
‐ Wait 30 s , then push the C/B 35 MG.
46
ATSU Malfunction ATSU An ATSU reset should be attempted, if: key selection has
no
effect on any of the MCDU ATSU DATALINK submenus.
On ground, or in flight:
‐ Pull the C/Bs in the following order:
L16, L15 on 121VU
‐ Wait 5 s , then:.
‐ Push the C/Bs in the following order:
L15, L16.
ENG IGN A+B FAULT FADEC and EIU Refer to FCOM/PRO-ABN-70-K ENG 1(2)
IGN
70 ENG 1(2) FADEC FAULT (IGN A + B Fault) if applicable.
A(B) FAULT
FADEC Refer to FCOM/PRO-ABN-70 ENG 1(2) FADEC
A(B) FAULT if applicable.
EMERGENCY EVACUATION
AIRCRAFT/PARKING
BRK..............................................................................................................STOP/ON
ATC (VHF
1).....................................................................................................................................
NOTIFY
CABIN CREW
(PA)............................................................................................................................
ALERT
ΔP (only if MAN CAB PR has been
used)...............................................................................CHECK ZERO
If not zero, MODE selector on MAN, V/S CTL FULL UP.
ENG MASTERS
(ALL)............................................................................................................................O
FF
FIRE Pushbuttons (ALL : ENG and
APU)............................................................................................. PUSH
AGENTS (ENG and
APU)...............................................................................................................AS RQRD
�� If Evacuation required:
EVACUATION................................................................................................................
............ INITIATE
　
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