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‐ 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
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
28
Loss of fuel quantity indication FQIC On ground, or in flight:
‐ Pull the C/B of the affected channel:
•Channel 1 (A13 on 49VU)
•Channel 2 (M27 on 121VU)
‐ Wait 5 s, before pushing the 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 to Refer to FCOM/PRO-NOR-SOP-15-A
Cruise - Flight Progress
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
NAV TCAS FAULT TCAS On ground only:
‐ Pull C/B K10 on 121VU.
‐ Wait 5 s, then push the C/B.
34
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.
To be continued on next page
ABN-80
32/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , ,
Continued from previous page
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)............................................................................................................................
　
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