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AVNCS/ELECTRICAL SMOKE SUSPECTED:
Consider shedding the AC BUS bar on one side. Then, if unsuccessful, on the other. When it is
clear that the shedded side is not involved, reconnect it.
Shed AC BUS 1 as follows:
GEN 2...................................................................................................................CHECK ON
ECAM/ND SEL.................................................................................................................. F/O
The ECAM SD will be lost during the sequence. Switching is necessary to allow ELEC
page monitoring.
ELEC/AC page.......................................................................................................... SELECT
BUS TIE........................................................................................................................... OFF
The BUS TIE OFF caution is triggered after 5 s.
AC ESS FEED............................................................................................................... ALTN
Avoids autopilot and autothrust disconnection during electrical transients.
GEN 1..............................................................................................................................OFF
The ECAM SD is lost.
Note: If this electrical configuration is maintained, the Captain’s Total Air Temperature
and angle-of-attack, standby angle-of-attack, and pitot are not deiced. PFD1 and
STBY instruments may display erroneous data in icing conditions. Use PFD2.
SMOKE DISSIPATION............................................................................................... CHECK
If smoke continues:
GEN 1.............................................................................................................................. ON
AC ESS FEED..............................................................................................................NORM
ECAM/ND SEL............................................................................................................. NORM
Shed AC BUS 2 as follows:
GEN 1.........................................................................................................................CHECK ON
BUS TIE.................................................................................................................... CHECK OFF
AC ESS FEED...................................................................................................... CHECK NORM
ECAM/ND SEL......................................................................................................CHECK NORM
GEN 2................................................................................................................................... OFF
PFD2 and ND2 are lost.
SMOKE DISSIPATION......................................................................................................CHECK
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 100/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
If smoke continues:
GEN 2.............................................................................................................................. ON
BUS TIE.........................................................................................................................AUTO
SMOKE/FUMES REMOVAL....................................................................................... CONSIDER
ELEC EMER CONFIG................................................................................................ CONSIDER
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 101/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
IF SMOKE SOURCE CANNOT BE DETERMINED AND STILL PERSISTS OR
AVNCS/ELECTRICAL SMOKE SUSPECTED:
Consider shedding the AC BUS bar on one side. Then, if unsuccessful, on the other. When it is
clear that the shedded side is not involved, reconnect it.
Shed AC BUS 1–1 + 1–2 as follows:
GEN 3+4.............................................................................................................. CHECK ON
ECAM/ND SEL.................................................................................................................. F/O
The ECAM SD will be lost during the sequence. Switching is necessary to allow ELEC
page monitoring.
ELEC/AC page.......................................................................................................... SELECT
BUS TIE........................................................................................................................... OFF
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 7(62)
