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ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 108/252
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
BOTH PFD ON SAME FAC
SLATS/FLAPS SLOW
CAT 2 ONLY (1)
INOP SYS
See below
INOP SYS
B HYD SPLR 3 VHF 1
ACP 1+2 WING A. ICE AP 1
A/THR FCU 1 FAC 1
REV 2 ENG 2 START CAB PR 1
VENT EXTRACT B ELEC PUMP GPWS
ENG 1 LOOP A ENG 2 LOOP B FCDC 1
CAT 3
Other INOP SYS
BRK PRESS indicator Flight interphone EIU 2
Capt rain repellent �� Avionics air cond valve Standby compass light
HP fuel shutoff valves SFCC 1 RMP 1
Hyd fire valves Eng 1 and 2 Ram air inlet ECAM Control Panel
Left loudspeaker DC SHED ESS BUS
Note: 1. Before arming the approach mode, the ECAM STATUS displays “CAT 3 SINGLE”.
However, the real landing capability is CAT 2, and is correctly displayed on the
FMA when the approach mode is armed.
2. The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1) AL2utothrust, eng start and reverser inop.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A318/A319/A320/A321 FLEET PRO-ABN-24 P 109/252
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT
Applicable to:
VHF 2 OR 3................................................................................................................................USE
AUDIO SWTG.........................................................................................................................SELECT
L2 ACP 1 and 2 are lost. Therefore, set the AUDIO SWTG rotary selector to CAPT 3 or F/O 3 to
recover communications.
L1 BARO REF.............................................................................................................................CHECK
L2Crosscheck the barometer reference settings on the FCU and the PFD.
L1GPWS..........................................................................................................................................OFF
ASSOCIATED PROCEDURES
NAV GPWS FAULT
GPWS..........................................................................................................................................OFF
L12
Note: To shut down the engines on ground, use the ENG FIRE pb-sw.
SECONDARY FAILURES
* CAB PRESS
* HYD
* 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 110/252
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
L12
STATUS
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM
ENG 1 APPR IDLE ONLY
ENG 2 APPR IDLE ONLY
BOTH PFD ON SAME FAC
SLATS/FLAPS SLOW
CAT 2 ONLY (1)
INOP SYS
See below
INOP SYS
B HYD SPLR 3 VHF 1
ACP 1+2 WING A. ICE AP 1
A/THR FCU 1 FAC 1
REV 2 ENG 2 START CAB PR 1
VENT EXTRACT B ELEC PUMP GPWS
ENG 1 LOOP A ENG 2 LOOP B FCDC 1
CAT 3
Other INOP SYS
BRK PRESS indicator Flight interphone EIU 2
Capt rain repellent �� Avionics air cond valve Standby Horizon
Standby compass light HP fuel shutoff valves SFCC 1
RMP 1 Hyd fire valves Eng 1 and 2 Ram air inlet
ECAM Control Panel Left loudspeaker DC SHED ESS BUS
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 111/252
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
Note: 1. Before arming the approach mode, the ECAM STATUS displays “CAT 3 SINGLE”.
When the approach mode is armed, the ECAM displays “CAT 2 ONLY”, and the
FMA displays CAT 2. However, when the attitude indicator (Standby Horizon)
is inoperative, the real landing category is CAT I (Refer to QRH/OPS Required
Equipment for CAT2 and CAT3), that indicates the “Required Equipment for CAT II
and CAT III Landings”.
2. The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
(1) AL2utothrust, eng start and reverser inop.
ELEC DC ESS BUS FAULT
Applicable to:
VHF 2 OR 3................................................................................................................................USE
　
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