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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 81/132
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 82/132
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
The BUS TIE OFF caution is triggered after 5 s.
AC ESS FEED............................................................................................................... ALTN
Avoids autopilot and autothrust disconnection during electrical transients.
GEN 1+2...........................................................................................................................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
　
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