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FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 GPS 2
Y ELEC PUMP SDAC 2 FWC 2
R WNDW HEAT CAT 2 L+R TK PUMP 2
CTR TK PUMP 2 LGCIU 2 RA 2
F/O PITOT F/O AOA F/O TAT
MAIN GALLEY YAW DAMPER 2 RUD TRIM 2
RUD TRV LIM 2 BRK SYS 2 REVERSER 2
VENT EXTRACT GND COOL �� DMC 2
RECORDER SYS R WSHLD HEAT
Other INOP SYS
Right cabin fan Brake fans 1, 2, 3 and 4 �� ADF 2 ��
DME 2 RADAR 2 �� MCDU 2
ENG 2 ignition B VOR 2 F/O PFD and ND
QAR ATC 2 ECAM lower DU
HF 2 ��
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 49/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT
Applicable to:
EXTRACT.................................................................................................................................OVRD
L2 The avionics ventilation system is in the closed circuit configuration.
Air conditioning is added to the ventilation air.
L1
ASSOCIATED PROCEDURES
L/G LGCIU 2 FAULT
L12
ASSOCIATED PROCEDURES
ENG 2 EPR MODE FAULT
L2 Refer to 99 Duref Cible FCOM
L1
SECONDARY FAILURES
* AVNCS VENT
* FUEL
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 50/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
PACK 2 AT FIXED TEMP
See (1)
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 GPS 2
Y ELEC PUMP SDAC 2 FWC 2
DMC 2 FDIU R WSHLD HEAT
CTR TK PUMP 2 LGCIU 2 RA 2
F/O PITOT F/O AOA F/O TAT
R WNDW HEAT CAT 2 L+R TK PUMP 2
RUD TRV LIM 2 BRAKES SYS 2 REVERSER 2
VENT EXTRACT GND COOL �� PACK 2 REGUL
MAIN GALLEY YAW DAMPER 2 RUD TRIM 2
Other INOP SYS
Right cabin fan Brake fans 1, 2, 3 and 4 �� ADF 2 ��
DME 2 RADAR 2 �� MCDU 2
ENG 2 ignition B VOR 2 F/O PFD and ND
QAR ATC 2 ECAM lower DU
HF 2 ��
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 Pack 2 controller, the pack outlet temperature is controlled by the pack anti-ice
valve and is stabilized to a temperature between 5 °C (41 °F) and 30 °C (86 °F) within a maximum
of 6 min.
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 51/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 GPS 2
Y ELEC PUMP SDAC 2 FWC 2
R WNDW HEAT CAT 2 L+R TK PUMP 2
CTR TK PUMP 2 LGCIU 2 RA 2
F/O PITOT F/O AOA F/O TAT
MAIN GALLEY YAW DAMPER 2 RUD TRIM 2
RUD TRV LIM 2 BRK SYS 2 REVERSER 2
VENT EXTRACT GND COOL �� DMC 2
RECORDER SYS R WSHLD HEAT
Other INOP SYS
Right cabin fan Brake fans 1, 2, 3 and 4 �� ADF 2 ��
DME 2 RADAR 2 �� MCDU 2
ENG 2 ignition B VOR 2 F/O PFD and ND
QAR ATC 2 ECAM lower DU
HF 2 ��
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 52/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT
Applicable to:
EXTRACT.................................................................................................................................OVRD
L2 The avionics ventilation system is in the closed circuit configuration.
Air conditioning is added to the ventilation air.
L1
ASSOCIATED PROCEDURES
L/G LGCIU 2 FAULT
L12
ASSOCIATED PROCEDURES
ENG 2 EPR MODE FAULT
L2 Refer to 99 Duref Cible FCOM
L1
SECONDARY FAILURES
* AVNCS VENT
* FUEL
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 53/252
FCOM 19 AUG 10
ELEC AC BUS 2 FAULT (Cont'd)
L12
STATUS
PACK 2 AT FIXED TEMP
See (1)
INOP SYS
See below
INOP SYS
ADR 2 ILS 2 GPS 2
　
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