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BARO REF.............................................................................................................................CHECK
GPWS..........................................................................................................................................OFF
T TK UNUSBL PROC...............................................................................................................APPLY
L2Note: 1. Trim tank fuel may be trapped and become unusable, depending on the position of the
valves (associated with the forward transfer) at the moment the failure occurs.
In this case, Refer to PRO-ABN-28 TRIM TANK FUEL UNUSABLE.
2. To shut down the engines on ground, the fire pb must be used.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 134/166
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
L12
STATUS
APPR PROC
GPWS FLAP MODE................................................................OFF
SLATS/FLAPS SLOW
INOP SYS
See below
INOP SYS
ESS TR VHF 1 JETTISON
ACP 1+2 CAT 3 DUAL BMC 2
BMC 3 ENG 4 LOOP A PART FCU
LGCIU 1 CAB PR 1 FUEL PUMP 1
F STBY PUMP 4 GPWS ATC 1
FCDC 1 RUD TRIM 1 RUD TRV LIM 1
FCMC 1 APU LOOP A ENG 1 LOOP A
ENG 2 LOOP A ENG 3 LOOP A
Other INOP SYS
FLT INTERPHONE RMP 1 ECP
STBY ALTI MCDU 1 SFCC 1
CAPT RAIN REP SDCU 1 STBY HORIZON
CVR L/G IND. PANEL CREW OXY CTL
PRESS INDICATOR APU
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 135/166
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
L12
STATUS
AVOID ICING CONDITIONS
APPR PROC
GPWS FLAP MODE................................................................OFF
IF ICE ACCRETION:
APPR SPD..........................................................VLS + 10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref
Cible FCOM.
BOTH PFD ON SAME FMGC
SLATS/FLAPS SLOW
INOP SYS
See below
INOP SYS
WING A. ICE AP 1 VHF 1
CAPT AOA ACP 1+2 HF 1
FM 1 BRAKES SYS 1 CAT 2
L WSHLD HEAT L WNDOW HEAT PART FCU
LGCIU 1 FCMC 1 ENG 1+2 LOOP A
CAB PR 1 L FUEL PUMP 2 GPWS
FCDC 1 RUD TRIM 1 APU LOOP A
Other INOP SYS
CAPT ND BMC 1 SFCC 1
RMP 1 STBY ALTIMETER (vibration) FCMC 2 (part)
DME 1 MCDU 1 FLT INTERPHONE
L/G IND. PANEL PRESS INDICATOR CAPT RAIN REP
ECP APU CVR
HF 1 STBY COMPASS PAX OXY AUTO CTL
SDCU 1 LANDING LTS CTL RADAR 1
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 136/166
FCOM 19 AUG 10
ELEC DC ESS BUS FAULT (Cont'd)
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
ELEC DC ESS BUS FAULT
Applicable to:
L2 AC ESS SHED, DC ESS SHED and AC LAND RCVRY buses are also lost.
For AC ESS SHED and DC ESS SHED BUS FAULT, refer to corresponding cautions for additional
procedures.
L1 ECAM SWTG DMC............................................................................................................................3
L2 Allows the STATUS page to be recovered.
L1 PFD BARO REF: STD ONLY
L2 This line is only displayed, if the DC2 BUS is also lost.
In this case, the BARO REF ........ CHECK line is not displayed.
L1 AUDIO SWTG.........................................................................................................................SELECT
VHF 2 OR 3/ATC 2.......................................................................................................................USE
BARO REF.............................................................................................................................CHECK
GPWS SYS................................................................................................................................. OFF
T TK UNUSBL PROC...............................................................................................................APPLY
L2Note: 1. Trim tank fuel may be trapped and become unusable, depending on the position of the
valves (associated with the forward transfer) at the moment the failure occurs.
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(14)
