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INOP SYS
See below
INOP SYS
VHF 3 ZONE CTLR 1 FUEL AFT XFR
L+R CAPT STAT HEAT L+R STBY STAT HEAT R FUEL STBY
REV 1 B ELEC PUMP PART GALLEY
L FUEL STBY R FUEL PUMP 2 CAT 3 DUAL
G ELEC PUMP GND COOL PACKBAY VENT
C/B DISPLAY ACP 3 TR 1
GE engine only
Other INOP SYS
SELCAL TPIS �� BLOW DET
PACK 1 REGUL CAPT WIPER DATA LOADER
PART COCKPIT LTS HUD �� Brake Temp ind. (5 to 8)
RMP 3 R LDG LTS
Note: The warning may be caused by a sub BUS failure. Consequently, only a part of the
above-listed systems may be lost.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 117/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT
Applicable to:
AIR DATA SWTG (IF ADR 3 AVAILABLE)..........................................................................F/O ON 3
FM SOURCE.................................................................................................................... BOTH ON 1
PRIM 2............................................................................................................................... KEEP ON
L2Note: PRIM 2 is normally supplied by DC BUS 2. In case of DC BUS 2 failure, DC BUS 1
supplies the PRIM 2.
However, in this case, the PRIM 2 FAULT light, on the overhead panel, comes on. Do not
attempt a reset: The OFF selection would result in a loss of the PRIM 2 backup power
supply.
L1
SECONDARY FAILURES
*F/CTL
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 118/166
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.
INCREASED FUEL CONSUMPTION
BOTH PFD ON SAME FMGC
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
AP 2 (FMGC 2) VHF 2 HALF SPLRS
REV 1 + 4 (1) REV 2 (2) REV 3 (3)
F/O TAT L+R F/O STAT FM 2
CAT 3 DUAL R OUTR AIL R CTR PUMP
TR 2 Y ELEC PUMP R WSHLD HEAT
SEC 2 LGCIU 2 CAB PR 2
GALLEY BRAKE SYS 2 FUEL AFT XFR
F. STBY PMP 1 F. STBY PMP 2 FUEL PUMP 3
FUEL PUMP 4 F T.tK PUMP �� GPS 2 ��
R WNDW HEAT ZONE CTLR 2 FCDC 2
RUD TRIM 2 RUD TRV LIM 2 YAW DAMPER 2
TURB DAMPER FCMC 2 BMC 1+4
ENG 1+2+3+4 LOOP B
Other INOP SYS
CARGO SQUIB B SFCC 2 SDCU 2
CDLS F/O WIPER F/O RAIN REP. ��
ENG 1+2+3+4 SQUIB B PACK 2 REGUL RMP 2
PART COCKPIT LTS
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 119/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT (Cont'd)
(1) (if CH B in control on ENG 1 or 4)
(2) (if CH B in control on ENG 2)
(3) (if CH B in control on ENG 3)
ELEC DC BUS 2 FAULT
Applicable to:
AIR DATA SWTG (IF ADR 3 AVAILABLE)..........................................................................F/O ON 3
FM SOURCE.................................................................................................................... BOTH ON 1
PRIM 2............................................................................................................................... KEEP ON
L2Note: PRIM 2 is normally supplied by DC BUS 2. In case of DC BUS 2 failure, DC BUS 1
supplies the PRIM 2.
However, in this case, the PRIM 2 FAULT light, on the overhead panel, comes on. Do not
attempt a reset: The OFF selection would result in a loss of the PRIM 2 backup power
supply.
L1
SECONDARY FAILURES
*F/CTL
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 120/166
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.
INCREASED FUEL CONSUMPTION
BOTH PFD ON SAME FMGC
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
AP 2 (FMGC 2) VHF 2 HALF SPLRS
REV 1 + 4 (1) REV 2 (2) REV 3 (3)
F/O TAT L+R F/O STAT FM 2
CAT 3 DUAL R OUTR AIL R CTR PUMP
TR 2 Y ELEC PUMP R WSHLD HEAT
SEC 2 LGCIU 2 CAB PR 2
　
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