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BUS supplies SEC 2. However, in this case, the SEC 2 FAULT light, on the overhead
panel, comes on. Do not attempt a reset: Selecting OFF would result in a loss of the SEC
2 backup power supply.
L1 IF CG AFT 32 %, AND WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
L2Note: If the trim tank pump is inoperative, apply the action if the CG is aft of 32 %, and when
the SPD is greater than 270 kt, and not in climb.
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 124/166
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 BRAKES SYS 2 FUEL AFT XFR
F. STBY PMP 1 F. STBY PMP 2 FUEL PUMP 3
FUEL PUMP 4 F T.tK PUMP 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.
(1) (if CH B in control on ENG 1 or 4)
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 125/166
FCOM 19 AUG 10
ELEC DC BUS 2 FAULT (Cont'd)
(2) (if CH B in control on ENG 2)
(3) (if CH B in control on ENG 3)
L12
STATUS
IF CG AFT 32 %, WHEN SPD > 270 KT AND NOT IN
CLIMB:
T TANK MODE................................................................ FWD
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
BOTH PFD ON SAME FMGEC
PACK 2 AT FIXED TEMP
SLATS/FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
PRIM 2 BMC 2 ZONE CTLR 2
FCDC 2 CAB PR 2 GALLEY
FCMC 2 ENG 1+2 LOOP B F T.TK PUMP
R WSHLD HEAT R WNDW HEAT HALF SPLRS
REV 2 F/O TAT FM 2
TR 2 CAT 3 DUAL Y ELEC PUMP
AP 2 (FMGC 2) VHF 2 LGCIU 2
FUEL AFT XFR L+R F/O STAT HEAT R FUEL PUMP 1
L FUEL PUMP 1 BRAKES SYS 2
Other INOP SYS
PACK 2 REGUL SDCU 2 BRAKE TEMP IND (1 to 4)
CARGO SQUIB B F/O WIPER F/O RAIN REP.
ENG 1+2 SQUIB B AUTOBRAKE SFCC 2
RMP 2 PART COCKPIT LTS CDLS
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 126/166
FCOM 19 AUG 10
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 faults, refer to the 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..........................................................................................................................................OFF
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(11)
