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Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1)DL2ue to the loss of the galley fan, the Pack 1 controller, and the primary zone controller channel.
(See associated procedures).
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 22/252
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
SLATS SLOW
CAT 2 ONLY
INOP SYS
See below
INOP SYS
BLUE HYD SPLR 3 ADR 3
RA 1 CAPT TAT L WSHLD HEAT
L WNDW HEAT REVERSER 1 L+R TK PUMP 1
CTR TK PUMP 1 VENT BLOWER GALLEY FAN
CRG VENT �� GND COOL �� N.W. STEER
MAIN GALLEY B ELEC PUMP BRAKES SYS 1
DMC 3 GPWS LAV DET
CAT 3
Other INOP SYS
Left cabin fan Radar 1 Stby Pitot/AOA
ATSU Brake fans 5, 6, 7 and 8 �� HUD ��
MCDU 3 �� Engine 1 ignition B EVMU eng 1 and eng 2
Printer COND controller lane A Hydraulic quantity indication
Partial galley PVI TCAS
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 23/252
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT
Applicable to:
L2 AC BUS 1 normally supplies the AC ESS BUS, and, via the TR1, the DC ESS BUS. In the case of
an AC BUS 1 FAULT, the AC ESS BUS and the DC ESS BUS will automatically recover, due to the
fact that the AC BUS 2 will automatically supply the AC ESS BUS.
If AC BUS 2 does not automatically supply the AC ESS BUS, the flight crew can recover the AC
ESS BUS and the DC ESS BUS by setting the AC ESS FEED pb-sw to ALTN, as requested by the
AC ESS BUS FAULT ECAM procedure.
L1 BLOWER.................................................................................................................................. OVRD
L2 The avionics ventilation system is in the closed circuit configuration.
Air conditioning is added to the ventilation air.
L1
ASSOCIATED PROCEDURES
WHEEL N.W. STEER FAULT
ASSOCIATED PROCEDURES
VENT EXTRACT FAULT
EXTRACT.................................................................................................................................OVRD
L12
ASSOCIATED PROCEDURES
ENG 1 EPR MODE FAULT
Refer to PRO-ABN-32 WHEEL N.W. STEER FAULT
SECONDARY FAILURES
* AVNCS VENT
* HYD
* FUEL
* F/CTL
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 24/252
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
CAB ZONE AT FIXED TEMP
See (1)
SLATS SLOW
CAT 2 ONLY
INOP SYS
See below
INOP SYS
BLUE HYD SPLR 3 ADR 3
RA 1 CAPT TAT L WSHLD HEAT
L WNDW HEAT CAT 3 L+R TK PUMP 1
CTR TK PUMP 1 VENT BLOWER GALLEY FAN
CRG VENT �� GND COOL �� N.W. STEER
REVERSER MAIN GALLEY B ELEC PUMP
BRAKES SYS 1 DMC 3 GPWS
LAV DET PACK 1 REGUL
Other INOP SYS
Left cabin fan Radar 1 Stby Pitot/AOA
ACARS �� Brake fans 5, 6, 7 and 8 �� HUD ��
Engine 1 ignition B EVMU eng 1 and eng 2 Printer
MCDU 3 �� Zone controller prim channel Hydraulic quantity indication
Partial galley PVI �� TCAS ��
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1)DL2ue to the loss of the galley fan, the Pack 1 controller, and the primary zone controller channel.
(See associated procedures).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 25/252
FCOM 19 AUG 10
ELEC AC BUS 1 FAULT
Applicable to:
L2 AC BUS 1 normally supplies the AC ESS BUS and, through TR1, the DC ESS BUS. In case of
an AC BUS 1 FAULT both the AC and DC ESS BUS will be lost and therefore the AC ESS BUS
FAULT and the DC ESS BUS FAULT will be displayed on the ECAM. However, both AC and DC
ESS BUS can be recovered by switching the AC ESS FEED pb-sw to ALTN as displayed in the AC
　
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