曝光台 注意防骗
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indicated in the table.
The following computers are not allowed to be reset in specific 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
FCOM/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 Temporary Revisions or OEBs. Before taking any action on other
computes, 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.
Also refer to the Refer to FCOM/99 Duref Cible QRH
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.
ABN-80
27/30
AQU3I1CK8 R/AEF3E1RE9N/ACE3 H2A0ND/A B3O2OK1
ABNORMAL AND
EMERGENCY PROCEDURES 30 AUG 10
A318/A319/A320/A321 FLEET
COMPUTER RESET TABLE
ATA System malfunction or
ECAM Warning/Caution Affected System Reset
21
VENT AVNCS SYS FAULT AEVC On ground only:
‐ Pull C/B Y 17 on 122VU
‐ Wait 1 s before pushing the C/B.
22
AUTO FLT FCU 1(2) FAULT FCU In flight:
‐ Pull the C/B B05 on 49VU for
FCU1, or M21 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 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
28/30
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 ‐ the C/Bs in the following order:
G02 on 49VU, M05 on 121VU.
‐ Wait 10 s, then
‐ Push the C/B in the following order:
M05, G02.
‐ After CIDS reset, wait approximately 4 min, before
recovering normal operation.
To be continued on next page
ABN-80
29/30
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
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空客320快速检查单QRH QUICK REFERENCE HAND BOOK5(43)
