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if necessary.
On ground:
‐ Pull the C/B B05 on 49VU for
FCU1, or M21 on 121VU for
FCU2.
‐ Push it after 5 s.
‐ If FCU1(2) FAULT
disappears, CHECK the
displayed targets and
barometer reference, and
correct them if necessary
(RESET successful)
‐ If FCU1(2) FAULT remains,
pull both C/B B05 on 49VU
and M21 on 121VU
‐ Push them after 7 min, with
a delay of less than 5 s
between side 1 and 2
‐ Wait at least 30 s for FCU1
and FCU2 safety tests
completion
‐ CHECK the displayed
targets and barometer
reference, and correct
them if necessary (RESET
successful)
To be continued on next page
ABN-80
28/32
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
Continued from previous page
AUTO FLT FCU 1+2 FAULT FCU In flight:
‐ Pull the C/B B05 on 49VU
for FCU1, and then M21 on
121VU for FCU2.
‐ Push them after 5 s.
‐ CHECK the displayed
targets and the barometer
reference, and correct them
if necessary.
On ground:
‐ Pull the C/B B05 on 49VU
for FCU1, and then M21 on
121VU for FCU2.
‐ Push them after 5 s
‐ If FCU 1+2 FAULT
disappears, CHECK the
displayed targets and
barometer reference, and
correct them if necessary
(RESET successful)
‐ If FCU 1+2 FAULT remains,
pull again both C/B B05 on
49VU and M21 on 121VU
‐ Push them after 7 min, with
a delay of less than 5 s
between side 1 and 2
‐ Wait for at least 30 s for
FCU1 and FCU2 safety tests
completion
‐ CHECK the displayed
targets and barometer
reference, and correct
them if necessary (RESET
successful)
FCU targets are synchronized
on current aircraft values, and
displayed as selected targets.
‐ 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,
　
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