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CAUTION In case of discrepancies between the airspeed indications on the
Captain’s PFD and on standby indicator, disregard the standby indicator
(probe not deiced).
AVOID ICING CONDITIONS
Wing anti-ice, windshields, and windows heat are lost.
Note: ‐ Engine anti-ice pb-sw is on, regardless of the pushbutton’s position. Fuel
consumption increases by approximately 1.5 %.
‐ Aircraft is out of trim, due to the right aileron upfloat. Rudder trim control
remains operative, despite no indication on control panel (pedestal).
MAX FL..........................................................................................................................350
MAX SPEED................................................................................................................../.80
Flight level and speed are limited due to the loss of flight controls redundancy.
CTR TK XFR BY GRVTY
CTR TK UNUSABLE IF < 15 T
Note: ‐ As fuel is fed from one side only, fuel balance must be monitored. To
maintain fuel balance, fuel PUMP 1 can be selected OFF, then STBY PUMP
4 will automatically start (althought it is indicated FAULT when fuel PUMP 1
is on).
‐ The T TANK MODE FWD light is not powered. Check the ECAM fuel page
for valve position.
FM SOURCE............................................................................................................ NORM
MCDU B/UP NAV..................................................................................................SELECT
NAVAID TUNING.............................................................................................USE RMP 1
Only VOR 1 selector or ADF 1 selector (as selected on the DDRMI) is available. No
DME is available. If the ND is displayed (using the PFD/ND pb ), the ADF/VOR selector
selector position on the FCU must be in accordance with the VOR/ADF selector selector
on the DDRMI.
LDG ELEV............................................................................................................. ADJUST
Landing elevation must be manually set, because both FMGC are lost.
�� FOR SLATS EXTENSION:
LAND RECOVERY.................................................................................................. ON
SFCC 1, LGCIU 1, are recovered. The remaining fuel pump is lost.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A330/A340 FLEET PRO-ABN-26 P 86/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
�� FOR L/G GRVTY EXTN:
MAX SPEED..................................................................................................... 200 KT
L/G GRVTY EXTN.............................................................................................DOWN
�� WHEN L/G DOWNLOCKED:
L/G lever............................................................................................................ DOWN
�� 3 MIN/2000 FT BEFORE LDG:
Restore all generators 3 min before landing or at 2 000 ft AAL to recover normal
braking and normal flight control law, while minimizing possible reactivation of a
smoke source. Just before restoring all generators, switch First Officer Side on IR3,
since:
IR3 is not ‐ lost in EMER ELEC CONFIG,
‐ IR2 is recovered but faulty since not aligned, and PFD2 and ND2 are recovered
after that generators are on.
ATT HDG SWTG.......................................................................................... F/O ON 3
ALL GEN..................................................................................................................ON
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
SPD BRK...................................................................................................................DO NOT USE
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A330/A340 FLEET PRO-ABN-26 P 87/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
TO SELECT ELEC EMER CONFIG
EMER ELEC PWR.............................................................................................................MAN ON
�� WHEN EMER GEN AVAIL:
GEN 1............................................................................................................................... OFF
GEN 2............................................................................................................................... OFF
APU GEN............................................................................................................................OFF
ASSOCIATED PROCEDURES
ELEC EMER CONFIG
　
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