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is coming from this equipment.
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 56/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
�� IF AIR COND SMOKE SUSPECTED:
APU BLEED..........................................................................................................................OFF
VENT EXTRACT..................................................................................................................AUTO
Note: When VENT EXTRACT is in the OVRD position, a single pack may not be able to
maintain cabin pressure.
CARGO BULK ISOL VALVES................................................................................................OFF
To prevent a cargo smoke warning from being triggered due to cabin smoke.
PACK 1................................................................................................................................. OFF
�� If smoke continues:
PACK 1.............................................................................................................................. ON
PACK 2.............................................................................................................................OFF
�� If smoke still continues:
PACK 2........................................................................................................................ON
If the crew suspects that the smoke does not come from Pack 2, normal pack
configuration can be restored.
VENT EXTRACT.................................................................................................... OVRD
SMOKE/FUMES REMOVAL....................................................................................... CONSIDER
�� IF CABIN EQUIPMENT SMOKE SUSPECTED:
�� If smoke continues:
EMER EXIT LT.................................................................................................................. ON
To recover minimum cabin lighting when the COMMERCIAL is switched OFF.
COMMERCIAL..................................................................................................................OFF
SMOKE DISSIPATION............................................................................................... CHECK
FAULTY EQPT.........................................................................................SEARCH/ISOLATE
Cabin lights, reading lights, passenger system, and galleys have dedicated control or C/B
in the cabin or cockpit.
�� If smoke still continues or when faulty equipment confirmed isolated:
COMMERCIAL..............................................................................................................NORM
SMOKE/FUMES REMOVAL....................................................................................... 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 57/132
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
�� IF SMOKE SOURCE CANNOT BE DETERMINED AND STILL CONTINUES 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 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
　
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