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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 146/166
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 147/166
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 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
BSCU CH 1+2 G ELEC PUMP B ELEC PUMP
Y ELEC PUMP 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 F. STBY PUMP 1
F. CTL PUMPS F. TK PUMP GPS !+2
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
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 148/166
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
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(17)
