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FCU 2 MAIN GALLEY Y ELEC PUMP (if selected ON)
BRAKES SYS 2 F/O STAT R WSLHD HEAT
R WNDW HEAT CAB PR 2
Other INOP SYS
SFCC 2 R cabin fan F/O wiper
F/O rain rplnt Eng 1 and 2 fire ext btl 2 FMGC 2
CDLS BMC 2 Bleed X feed auto control
RMP 2 FQI channel 2 Autobrake (due to loss of 2 SECs)
Brake fan �� Eng 2 oil low press and qty ind R loudspeaker
rudder trim ind CIDS 2 SMOKE DETECT
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 100/252
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
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 101/252
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
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
SPLR 1+2+5 ELAC 2 (1) SEC 2+3
VHF 2 LGCIU 2 REVERSER 2
FCDC 2 CAT 3 DUAL FAC 2
L TK PUMP 2 R TK PUMP 2 ENG 1 LOOP B
ENG 2 LOOP A AP 2 FCU 2
MAIN GALLEY Y ELEC PUMP (if selected ON) BRAKES SYS 2
F/O STAT R WSLHD HEAT R WNDW HEAT
CAB PR 2
Other INOP SYS
SFCC 2 R cabin fan F/O wiper
F/O rain rplnt Eng 1 and 2 fire ext btl 2 FMGC 2
CDLS BMC 2 Bleed X feed auto control
RMP 2 FQI channel 2 Autobrake (due to loss of 2 SECs)
CTR TK XFR valve R Brake fan �� Eng 2 oil low press and qty ind
R loudspeaker rudder trim ind CIDS 2 SMOKE DETECT
(1) (Lost after 30, 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 102/252
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT
Applicable to: , MSN,
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
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 103/252
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
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
SPLR 1+2+5 ELAC 2 (1) SEC 2+3
VHF 2 LGCIU 2 REVERSER 2
FCDC 2 CAT 3 DUAL FAC 2
L TK PUMP 2 R TK PUMP 2 ENG 1 LOOP B
ENG 2 LOOP A AP 2 FCU 2
MAIN GALLEY Y ELEC PUMP (if selected ON) BRAKES SYS 2
F/O STAT R WSLHD HEAT R WNDW HEAT
CAB PR 2
Other INOP SYS
SFCC 2 R cabin fan F/O wiper
F/O rain rplnt Eng 1 and 2 fire ext btl 2 FMGC 2
CDLS BMC 2 Bleed X feed auto control
RMP 2 FQI channel 2 Autobrake (due to loss of 2 SECs)
CTR TK XFR valve R Brake fan �� Eng 2 oil low press and qty ind
R loudspeaker rudder trim ind CIDS 2 SMOKE DETECT
(1) (Lost after 30, 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 104/252
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT
Applicable to: MSN
　
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