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‐ 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)............................................................................................................................
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
�� If Evacuation not required:
CABIN CREW and PASSENGERS
(PA)..................................................................................... NOTIFY
ABN-80
1/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET , , MSN 4473
CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE
LANDING
WEIGHT.........................................................................................................................
...CHECK
�� if the aircraft weight is above the maximum weight for circling in CONF 3 (given
in the table
below):
The aircraft cannot maintain flight level with CONF 3 and the landing gear down.
FOR
LDG............................................................................................................................US
E FLAP 3
CONF 3 is preferred, to minimize a configuration change in short final.
GPWS LDG FLAP
3............................................................................................................................ ON
Delay gear extension.
Note: If the approach is flown at less than ‐ 750 ft RA, the “L/G NOT DOWN”
warning will be
triggered. The pilot can cancel the aural warning by pressing the EMER CANC pb,
located
on the ECAM control panel.
‐ A ”TOO LOW GEAR” warning is to be expected, if the landing gear is not
　
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