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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
A330/A340 FLEET PRO-ABN-24 P 156/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
L12
STATUS
SPD BRK.......................................................DO NOT USE
APPR PROC
�� FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G................................................................................ DOWN
�� IF CG AFT 32 % AND WHEN SPD > 270 KT AND NOT IN
CLIMB:
TTK MODE...................................................................... FWD
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
CTR TANK XFR BY GRVTY
CTR TANK UNUSABLE IF < 15 T
R FUEL GRVTY FEED ONLY
ENG 1 AUTO START ONLY
ENG 2 AUTO START ONLY
PACKS AT FIXED TEMP
ENG HI IDLE
BOTH PFD ON SAME FMGC
SLATS/FLAPS LOW
CAT 3 SINGLE ONLY
INOP SYS
See below
INOP SYS
F/CTL PROT PRIM 2+3 VHF 2+3
GND COOL �� R WNDW HEAT REAC W/S DET
ACP 3 CAT 3 DUAL BRAKES SYS 2
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 157/166
FCOM 19 AUG 10
ELEC DC BUS 1+2 FAULT (Cont'd)
L FUEL PUMP 1 Y ELEC PUMP BMC 2
MAN CAB PR GALLEY AP 2
HALF SPLRS FUEL AFT XFR C/B DISPLAY
L+R STBY STAT HEAT FCMC 2 ZONE REGUL
R FUEL PUMPS B ELEC PUMP F TTK PUMP
LGCIU 2 N/W STRG TR 1+2
REVERSERS L+R CAPT STAT HEAT L+R F/O STAT HEAT
FCDC 2 FM 2 ENG 1+2 LOOP B
G ELEC PUMP L FUEL STBY F CTR PUMPS
R WSHLD HEAT CAB PR 2
Other INOP SYS
RMP 2+3 PACK 1+2 REGUL SELCAL
DATA LOADER R LDG LTS F/O RAIN REP
TPIS �� WIPERS BRAKE TEMP IND
L/G SAFETY VALVE PART COCKPIT LTS AUTOBRAKE
SDCU 2 BLOW DET CARGO SQUIB B
ENG SQUIB B SFCC 2 CDLS ��
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 158/166
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 159/166
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
　
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