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standby indicator, disregard standby indicator (probe not deiced).
L1 LDG ELEV............................................................................................................................ ADJUST
L2 Landing elevation has to be manually set since both FMGCs are lost.
L1AVOID ICING CONDITIONS
L2Wing anti ice, windshields, windows heat are lost.
Note: Engine anti ice is on regardless ‐ of pushbutton position. Fuel consumption increases by
approximately 1.5 %.
‐ Aircraft is out of trim due to the right aileron up float.
The rudder trim control remains operative despite no indication on control panel
(pedestal).
L1MAX FL.........................................................................................................................................350
MAX SPEED.............................................................................................................................../0.80
L2 Flight level and speed are limited due to the loss of redundancy for flight controls.
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 41/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
L1CTR TK XFR BY GRVTY
CTR TK UNUSABLE IF < 15 T
L2Note: 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
(although it is indicated FAULT when fuel PUMP 1 is ON).
‐ The T TANK MODE FWD light is not powered. Check FUEL SD page for valve position.
L1 FM SOURCE........................................................................................................................... NORM
MCDU B/UP NAV...................................................................................................................SELECT
NAVAID TUNING..............................................................................................................USE RMP 1
L2 Only VOR 1 or ADF 1 (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 position on the FCU must be
in accordance with the VOR/ADF selector on the DDRMI.
L1 LDG ELEV.....................................................................................................................MAN ADJUST
L2 Landing elevation has to be manually set, since both FMGCs are lost.
L1 FOR SLATS EXTENSION:
LAND RECOVERY................................................................................................................... ON
L2 ILS 1, SFCC 1, LGCIU 1, are recovered. The remaining fuel pump is lost.
L1 FOR L/G GRVTY EXTN:
MAX SPEED...................................................................................................................... 200 KT
L/G GRVTY EXTN..............................................................................................................DOWN
WHEN L/G DOWNLOCKED:
L/G LEVER......................................................................................................................... DOWN
MAX BRK PR........................................................................................................................ 1000 PSI
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
ELECTRICAL
A330/A340 FLEET PRO-ABN-24 P 42/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX FL.......................................................................... 350
MAX SPEED.......................................................... 305/0.80
AVOID ICING CONDITIONS
MAX BRK PR.......................................................1 000 PSI
APPR PROC
FOR SLATS EXTENSION:
LAND RECOVERY............................................................. ON
FOR LDG...................................................................USE FLAP 3
This line is replaced by "FOR LDG: USE FLAP 3" when CONF 3
is selected, as a reminder.
FOR L/G GRVTY EXTN:
MAX SPEED................................................................ 200 KT
L/G GRVTY EXTN........................................................DOWN
WHEN L/G DOWNLOCKED:
L/G LEVER................................................................... DOWN
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(157)
