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L2 Fuel consumption increases by approximately 1 %.
L1 AVOID ICING CONDITIONS
CTR TK XFR BY GRVTY
CTR TK UNUSABLE IF < 15 T
MAX BRK PR.......................................................................................................................1 000 PSI
L12
ASSOCIATED PROCEDURES
F/CTL ELEV REDUND LOST
Refer to PRO-ABN-27-J F/CTL ELEV REDUND LOST (Ailerons Are Preset Upwards) for
this procedure’s description.
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 149/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
AVOID ICING CONDITIONS
MAX BRK PR.......................................................1 000 PSI
APPR PROC
�� FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G................................................................................ DOWN
�� IF ICE ACCRETION:
APPR SPD...........................................................VLS +10 KT
�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT IN
CLIMB:
T TANK MODE................................................................ FWD
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
R FUEL GRVTY FEED ONLY
ENG (All) AUTO START ONLY
INCREASED FUEL CONSUMP
CTR TO INR: MAN ONLY
PACK AT FIXED TEMP
FUEL CELL 2 BY GRVTY ONLY
ENG HI IDLE
CTR TK UNUSABLE < 15 T
MCDU BACK UP NAV AVAIL
SLATS/FLAPS SLOW
• IF NEW F/CTL FAILURE:
EXPECT MAN P. TRIM ONLY
INOP SYS
See below
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 150/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
INOP SYS
PRIM 2+3 ANTI SKID WING A. ICE
FM 1+2 BMC 1+4 SEC 2
TURB DAMP LGCIU 2 CAB PR 2
MAN CAB PR N. W. STRG GALLEYS
AUTO BRK FUEL PUMP 2+STBY FUEL PUMP 3+STBY
FUEL PUMP 4+STBY ENG 4 LOOP B BSCU CH 1+2
G ELEC PUMP B ELEC PUMP Y ELEC PUMP
WINDOW HEAT GND COOL CB DISPLAY
REAC W/S DET FCDC 2 RUD TRIM 2
RUD TRV LIM 2 YAW DAMPER 2 FCMC 2
APU LOOP B ENG 1 LOOP B ENG 2 LOOP B
CAT 2 F. STBY PUMP 1 F. CTL PUMPS
F. TK PUMP AP 1+2 TR 1+2
VHF 2+3 MOST SPLRS REVERSERS
WSHLD HEAT FUEL AFT XFR CAPT STAT HEAT
F/O STAT HEAT STBY STAT HEAT ACP 3
ZONE REGUL R OUTR AIL ENG 3 LOOP B
Other INOP SYS
SFCC 2 RMP 2+3 SDCU 2
BLOW DET BRAKE TEMP IND ENG SQUIB B
F/O RAIN REP �� Lower ECAM DU SELCAL
DATA LOADER CARGO SQUIB B CDLS ��
TPIS �� PACK 1+2 REGUL WIPER
L/G SAFETY VALVE LDG LTS PART COCKPIT LTS
Note: The warning may be caused by a failure in a sub BUS. 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 151/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT
Applicable to:
WING X FEED.............................................................................................................................. ON
L2 Only the L FUEL PUMP 2 is supplied.
L1 FM SOURCE.................................................................................................................... BOTH ON 1
SEC 2.................................................................................................................................KEEP ON
FUEL IMBALANCE..............................................................................................................MONITOR
L2 Due to the fact that fuel is fed from one side only, the flight crew must monitor fuel balance. To
maintain fuel balance, L PUMP 2 can be set to OFF. R PUMP 2 will then automatically start, and
the corresponding FAULT light will go off.
L1�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT IN CLIMB:
T TANK MODE...................................................................................................................... FWD
SECONDARY FAILURES
*F/CTL
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
ELECTRICAL
　
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