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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 in ‐ the following order: G02 on 49VU, M05
on 121VU.
‐ Wait for 1 min, then:
‐ Push the C/Bs in the following order: M05, 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 or Tape
reproducer PRAM On ground, or in flight:
‐ Pull C/B M14 (or Q14 �� ) of the FAP in the 121VU.
‐ Wait 10 s before pushing the C/B.
IF UNSUCCESSFUL:
‐ Pull the tape reproducer/PRAM C/B F07 on 2 000VU
(cabin)
‐ Wait 10 s before pushing the C/B.
26
SMOKE LAV + CRG DET
FAULT
SDCU On ground only:
‐ Pull C/B C06 on 49VU, and C/B T18 on 122VU.
‐ Wait 10 s before pushing both C/Bs.
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.
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)
32 Braking malfunction BSCU Refer to FCOM/PRO-SUP-32 BSCU Reset
To be continued on next page
ABN-80
30/30
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
Continued from previous page
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.
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.
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
　
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