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ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 87/252
FCOM 19 AUG 10
ELEC DC BUS 1 FAULT
Applicable to: , MSN,
BLOWER.................................................................................................................................. OVRD
EXTRACT.................................................................................................................................OVRD
L2 Avionic ventilation air is supplied to the air conditioning, and exhausted overboard.
L1
SECONDARY FAILURES
*AVNCS VENT
*FUEL
L12
STATUS
CAB ZONE AT FIXED TEMP
See (1)
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
ACP 3 CAPT STAT heat STBY STAT heat
L. WSHLD HEAT REVERSER 1 AVNCS VENT
GALLEY FAN GND COOL �� BRAKES SYS 1
LAV DET PACK 1 REGUL L. WNDW HEAT
CAT 3 DUAL
Other INOP SYS
Left cab fan Zone controller primary channel Sel cal
CFDIU VHF 3 �� RMP 3 ��
L CTR TK XFR valve Hot air Capt wiper
Eng 1 oil press and qty ind. TPIS �� Brake temps ind.
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 88/252
FCOM 19 AUG 10
ELEC DC BUS 1 FAULT
Applicable to: MSN
BLOWER.................................................................................................................................. OVRD
EXTRACT.................................................................................................................................OVRD
L2 Avionic ventilation air is supplied to the air conditioning, and exhausted overboard.
L1
SECONDARY FAILURES
*AVNCS VENT
*FUEL
ELEC DC BUS 2 FAULT
Applicable to:
AIR DATA SWTG...........................................................................................................................F/O
BARO REF.............................................................................................................................CHECK
L2 Since one FCU channel is lost, crosscheck the barometer reference settings on the FCU and PFD.
L1
SECONDARY FAILURES
* CAB PRESS
* FUEL
* WHEEL
* 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 89/252
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH or Refer to 99 Duref Cible FCOM.
ENG 2 APPR IDLE ONLY
BOTH PFD ON SAME FAC
PACK 2 AT FIXED TEMP
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
SPLR 1+2+5 ELAC 2 SEC 2+3
VHF 2 F/O STAT R WSLHD HEAT
R WNDW HEAT AP 2 FCU 2
CAT 3 DUAL FAC 2 L TK PUMP 2
R TK PUMP 2 CTR TK PUMP 2 �� LGCIU 2
REVERSER 2 CAB PR 2 MAIN GALLEY
Y ELEC PUMP (if selected ON) BRAKE SYS 2 GPS 2 ��
ENG 1 LOOP B ENG 2 LOOP A PACK 2 REGUL
FCDC 2
Other INOP SYS
SFCC 2 R cabin fan F/O wiper
F/O rain rplnt Eng 1 and 2 fire ext btl 2 Autobrake (due to loss of 2 SECs)
BMC 2 Bleed X feed auto control RMP 2
FQI channel 2 zone controller sec SDCU 2
Brake fan �� Eng 2 oil low press and qty ind R loudspeaker
rudder trim ind FMGC 2 CDLS ��
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1) LL2ost after 30 s, but recovered at landing gear extension.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 90/252
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT
Applicable to:
AIR DATA SWTG.........................................................................................................................F/O3
BARO REF.............................................................................................................................CHECK
L2 Since one FCU channel is lost, crosscheck the barometer reference settings on the FCU and PFD.
L1
SECONDARY FAILURES
* CAB PRESS
* FUEL
* WHEEL
* F/CTL
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
　
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