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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+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
�� If smoke continues:
GEN 1+2............................................................................................................................ ON
AC ESS FEED..............................................................................................................NORM
ECAM/ND SEL............................................................................................................. NORM
�� Shed AC BUS 2–3 + 2–4 as follows:
GEN 1+2.....................................................................................................................CHECK ON
BUS TIE.................................................................................................................... CHECK OFF
AC ESS FEED...................................................................................................... CHECK NORM
ECAM/ND SEL......................................................................................................CHECK NORM
GEN 3+4............................................................................................................................... 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 102/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
�� If smoke continues:
GEN 3+4............................................................................................................................ 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 103/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
TO SET ELEC EMER CONFIG
EMER ELEC PWR.............................................................................................................MAN ON
�� WHEN EMER GEN AVAIL:
GEN 1+4............................................................................................................................. OFF
GEN 2+3............................................................................................................................. OFF
APU GEN............................................................................................................................OFF
ASSOCIATED PROCEDURES
ELEC EMER CONFIG
Two different procedures can be displayed on the ECAM, depending on whether the
SMOKE AVNCS VENT SMOKE ECAM warning is triggered or not before the flight crew
sets the electrical emergency configuration.
�� If SMOKE AVNCS VENT SMOKE is not triggered:
The ECAM displays the ELEC EMER CONFIG procedure described in Refer to
PRO-ABN-24-Z ELEC EMER CONFIG (GEN not Recovered or APU GEN not Available).
The flight crew must apply the ECAM without performing the ALL GEN reset.
�� AT 3 MIN OR 2000 FT BEFORE LDG:
Restore all generators 3 min before landing or at 2 000 ft AAL to recover normal
braking and normal flight control law, while minimizing possible reactivation of a
smoke source. Just before restoring all generators, switch First Officer Side on IR3,
since:
IR3 is not ‐ lost in EMER ELEC CONFIG,
‐ IR2 is recovered but faulty since not aligned, and PFD2 and ND2 are recovered
after that generators are on.
ATT HDG SWTG.......................................................................................... F/O ON 3
　
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