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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.
�� AT 3 MIN OR FT BEFORE LDG:
Restore all generators only 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.
GEN 2......................................................................................................................ON
EMER ELEC GEN 1 LINE...................................................................................... ON
�� WHEN A/C IS STOPPED:
ALL GEN................................................................................................................OFF
�� 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
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 145/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
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
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.
FAC 1......................................................................................................... OFF THEN ON
Rudder trim is recovered, despite the fact that no indication is available.
�� 3MN/2000 FT BEFORE LDG:
Restore all generators only 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.
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
protection).
MAX SPEED............................................................................................................320 KT
Note: The “EPR MODE FAULT N1 DEGRADED MODE” warning is triggered.
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 146/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
ECAM lower display is not available. STATUS SD page is displayed on the upper ECAM display, as
long as the STATUS pb is pressed.
STATUS
MIN RAT SPEED..................................................... 140 KT
MAX SPEED............................................................ 320 KT
MAX BRK PR........................................................1000 PSI
FOR LDG................................................................ USE FLAPS 3
GPWS LDG FLAP 3................................................................. ON
APPR SPD...............................................................VREF +10 KT
　
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