曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
L2 Display only if EMER GEN not automatically coupled.
L1 ALL GEN..................................................................................................................... OFF THEN ON
L2 If at any time any GEN recover, or if the APU GEN is available, Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) and Refer to PRO-ABN-24-AI ELEC
EMER CONFIG (All GEN Recovered or APU GEN Available) - FWSPAGE for the applicable ECAM
procedure and status.
L1 BUS TIE.......................................................................................................................................OFF
L2 Setting BUS TIE pb-sw to OFF segregates all generator channel.
L1 ALL GEN..................................................................................................................... OFF THEN ON
VHF 1/ATC 1 (IF EMER GEN SUPPLIED BY ENG. HYD. PUMPS)........................................... USE
VHF 1 (IF EMER GEN SUPPLIED BY RAT)............................................................................... USE
L2 SELCAL is inoperative.
L1 VENT EXTRACT........................................................................................................................OVRD
L2 Switch EXTRACT pb-sw OVRD since extract fan and cabin fans are lost.
CAUTION In case of discrepancies between air speed indications on captain PFD and on
standby indicator, disregard standby indicator (probe not deiced).
L1LDG ELEV............................................................................................................................ ADJUST
L2 Landing elevation has to be manually set since both FMGCs are lost.
L1 AVOID 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 61/166
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.
L1LDG 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
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 6(165)
