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ELEC EMER CONFIG................................................................................................ CONSIDER
As a last attempt, the flight crew can set the electrical emergency configuration to possibly
isolate or minimize the smoke source.
�� IF SMOKE disappears within 5 min:
NORMAL VENTILATION..............................................................................................RESTORE
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A318/A319/A320/A321 FLEET PRO-ABN-26 P 39/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
TO SET EMER ELEC CONFIG
EMER ELEC GEN 1 LIN.......................................................................................................... OFF
GEN 1 LINE contactor opens. GEN 1 remains running and supplies one fuel pump in each wing
tank. AC BUS 1 is supplied by GEN 2 through the bus tie contactor.
EMER ELEC PWR.............................................................................................................MAN ON
RAT is extended and the EMER GEN is connected to the aircraft network. Check emergency
generator parameters on the ELEC SD page (displayed automatically).
�� WHEN EMER GEN AVAIL:
APU GEN............................................................................................................................OFF
GEN 2............................................................................................................................... OFF
ELEC EMER CONFIG
Two different procedures can be displayed on the ECAM, depending on whether the
AVIONICS SMOKE ECAM caution is triggered or not before the flight crew sets the electrical
emergency configuration.
�� If AVIONICS SMOKE is not triggered
The ECAM displays the ELEC EMER CONFIG procedure described in Refer to 99 Duref
Cible FCOM.
The flight crew must apply the ECAM without performing the GEN 1+2 reset.
�� BEFORE L/G EXTENSION:
Restore all generators only few minutes before landing to minimize the possible
reactivation of a smoke source.
GEN 2......................................................................................................................ON
EMER ELEC GEN 1 LINE...................................................................................... ON
�� If AVIONICS SMOKE is triggered:
The ECAM displays a specific ELEC EMER CONFIG procedure. The flight crew must
apply the following ECAM procedure.
MIN RAT SPEED.....................................................................................................140 KT
Note: The electrical configuration is the same as for loss of both generators (except
that one fuel pump in each wing tank remains supplied).
VHF 1/HF 1/ATC 1.......................................................................................................USE
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A318/A319/A320/A321 FLEET PRO-ABN-26 P 40/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
Only VHF 1, HF 1 and ATC 1 are supplied in this configuration. Notify the ATC of the
nature of the emergency, and state intentions. If there is no contact with the ATC, switch
to code A7700, or transmit a distress message on one of the following frequencies: VHF
121.5 MHz, HF 2 182 kHz, or 8 364 kHz.
APU MASTER switch (if APU not running)..................................................................OFF
With the APU master pb-sw ON, the DC BAT BUS is supplied by the batteries.
FAC 1......................................................................................................... OFF THEN ON
Rudder trim is recovered, despite the fact that no indication is available.
LDG ELEV....................................................................................................MAN ADJUST
The LDG ELEV may be manually adjusted since, if the normal electrical supply is not
restored before landing gear extension, the FMGC is no longer supplied.
�� BEFORE L/G EXTENSION
Restore all generators only a few minutes before landing, to minimize possible
smoke source reactivation.
GEN 2......................................................................................................................ON
EMER ELEC GEN 1 LIN.........................................................................................ON
F/CTL ALTN LAW (PROT LOST)
Flight control normal laws and associated protections are lost. Only the load factor
limitation, and the high and low speed stability remain (ALTN law with reduced
　
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