曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

CAUTION In case of discrepancies between air speed indications on captain PFD and on
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 53/166
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 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 54/166
FCOM 19 AUG 10
ELEC EMER CONFIG (Cont'd)
(GEN NOT RECOVERED OR APU GEN NOT AVAILABLE)
LAND ASAP
EMER ELEC PWR.................................................................................................................MAN ON
L2 Display only if EMER GEN not automatically coupled.
L1ALL GEN..................................................................................................................... OFF THEN ON
L2 If at any time GEN 1 or/and GEN 2 recover, or if the APU GEN is available, Refer to
PRO-ABN-24-AJ ELEC EMER CONFIG (GEN 1 or/and GEN 2 Recovered or APU GEN Available)
or Refer to PRO-ABN-24-AJ ELEC EMER CONFIG (GEN 1 or/and GEN 2 Recovered or APU GEN
Available) - FWSPAGE for the applicable ECAM procedure and status.
L1BUS TIE.......................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates both generator channels.
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A330/A340機組操作手冊 FLIGHT CREW OPERATING MANUAL FCOM 6(162)