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time is indicated)
‐ Set the related normal cockpit control to ON, or push the corresponding reset pushbutton or circuit
breaker
‐ Wait 3 s for the end of the reset.
WARNING Do not reset more than one computer at the same time, unless instructed to do so.
Note: Due to the many customization possibilities of the C/B panel:
‐ Before taking any action on the C/B panel, the flight crew must crosscheck that the C/B
label corresponds to the affected system.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-SUP-24 P 2/14
FCOM 19 AUG 10
COMPUTER RESET TABLE
Applicable to: ALL
The computers that are most prone to reset are listed in the table of the next pages with the
associated reset procedure, or FCOM reference when applicable.
Specific reset procedures, included in OEB or Temporary revisions, are normally not referenced in
this table and, when issued, superseed this table.
Note: Repetitive resets have to be reported to maintenance.
On ground, almost all computers can be reset, and are not ‐ limited to the ones indicated in the
table.
Following computers are not allowed to be reset in all circumstances:
‐ ECU (Engine Control Unit on CFM engines) or EEC (Electronic Engine Control on IAE engines)
and EIU (Engine Interface Unit) while the engine is running.
‐ BSCU (Brake Steering Control Unit) if the aircraft is not stopped. (Refer to PRO-SUP-32 BSCU
Reset).
‐ In flight, as a general rule, the crew must restrict computer resets to those listed in the table, or to
those in applicable TRs or OEBs. Before taking any action on other computer the flight crew must
consider and fully understand the consequences.
CAUTION Do not pull the following circuit breakers:
‐ SFCC (could lead to SLATS/FLAPS locked)
‐ ECU or EEC, EIU.
Note: In the table’s “reset” column, the “if applicable” note signifies that, depending on the
computer standard, the reset procedure may no longer be necessary. If this is the case, the
reset procedure is removed from the applicable FCOM section.
Applicable to:
,
,
MSN,,,,
ATA System malfunction or
ECAM warning/caution Affected system Reset
21
VENT AVNCS SYS FAULT AEVC On ground only:
‐ Pull C/B Y 17 C/B on 122VU.
‐ Wait 1 s before pushing the C/B.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-SUP-24 P 3/14
FCOM 19 AUG 10
Applicable to:
ATA System malfunction or
ECAM warning/caution Affected system Reset
VENT AVNCS SYS FAULT AEVC On ground only:
Pull ‐ C/B Y 17 C/B on 122VU.
21 ‐ Wait 1 s before pushing the C/B.
AIR PACK 1(2) REGUL FAULT PACK CONTROLLER
1(2)
Refer to PRO-ABN-21-E AIR PACK 1(2) REGUL
FAULT
22
AUTO FLT FCU 1(2) FAULT FCU In flight:
‐ Pull the C/B B05 C/B on 49VU for FCU1, or M21
C/B on 121VU for FCU2.
‐ Push it after 5 s .
‐ CHECK the displayed targets and the barometer
reference, and correct them if necessary.
On ground:
‐ Pull the C/B B05 C/B on 49VU for FCU1, or M21
C/B 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
C/B on 49VU and M21 C/B 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)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-SUP-24 P 4/14
FCOM 19 AUG 10
Continued from previous page
ATA System malfunction or
ECAM warning/caution Affected system Reset
AUTO FLT FCU 1 + 2 FAULT FCU In flight:
‐ Pull the C/B B05 C/B on 49VU for FCU1, and
then pull M21 C/B 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 C/B on 49VU for FCU1, and
then pull M21 C/B on 121VU for FCU2.
‐ Push the C/Bs 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
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