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Other INOP SYS
STBY ALTI
SDCU 1
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 142/166
FCOM 19 AUG 10
ELEC DC ESS BUS SHED (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
FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
WING A. ICE
AP 1
CAPT AOA
FM 1
CAT 3 DUAL
BRAKES SYS 1
L WSHLD HEAT
ATC 1
L WNDOW HEAT
RUD TRIM 1
FCMC 1
jettison
Other INOP SYS
FCMC 2 (part)
STBY ALTIMETER
SFCC FLAPS 1
LANDING LTS CTL
SCDU 1
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 143/166
FCOM 19 AUG 10
ELEC DC ESS BUS SHED
Applicable to:
L2 AC ESS SHED BUS is also lost.
Refer to the corresponding caution for additional procedures and status.
L1 FM SOURCE.................................................................................................................... BOTH ON 2
AVOID ICING CONDITIONS
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 144/166
FCOM 19 AUG 10
ELEC DC ESS BUS SHED (Cont'd)
L12
STATUS
AVOID ICING CONDITIONS
• IF SEVERE ICE ACCRETION:
MIN SPD............................................VLS + 10/G DOT
MANEUVER WITH CARE
APPR PROC
GPWS FLAP MODE................................................................OFF
�� IF SEVERE 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
FLAPS SLOW
CAT 3 SINGLE ONLY
INOP SYS
WING A. ICE
AP 1
CAPT AOA
FM 1
CAT 3 DUAL
BRAKES SYS 1
L WSHLD HEAT
ATC 1
L WNDOW HEAT
RUD TRIM 1
FCMC 1
HF1
Other INOP SYS
FCMC 2 (part)
STBY ALTIMETER
SFCC FLAPS 1
LANDING LTS CTL
SCDU 1
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 145/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT
Applicable to:
X FEED (ALL)............................................................................................................................... ON
L2 Only Fuel PUMP 1 is supplied.
L1 FM SOURCE........................................................................................................................... NORM
NAVAID TUNING..............................................................................................................USE RMP 1
LDG ELEV.....................................................................................................................MAN ADJUST
FUEL IMBALANCE..............................................................................................................MONITOR
L2 To stop the imbalance, consider descent to gravity feed ceiling Refer to PRO-ABN-28 GRVTY
FUEL FEEDING, in order to use gravity feeding on the right side. In this case, close the XFEED
3+4.
L1 SPD BRK.......................................................................................................................DO NOT USE
L2 Since PRIM 2+3 are lost.
L1�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
L2 Fuel consumption increases by approximately 1 %.
　
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