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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 95/176
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.
FAC 1......................................................................................................... OFF THEN ON
Rudder trim is recovered, despite the fact that no indication is available.
�� 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
protection).
MAX SPEED............................................................................................................320 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 96/176
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
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ENG 1+2 APPR IDLE ONLY
ENG 1+2 N1 DEGRADED MODE
(IAE-powered aircraft �� )
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
CTR TK �� FUEL UNUSABLE
INCREASED FUEL CONSUMP
SLATS/FLAPS SLOW
APPR PROC
�� BEFORE L/G EXTENSION:
GEN 2.................................................................................ON
EMER ELEC GEN 1 LINE..................................................ON
�� After recovery of normal electrical supply, the following
STATUS will be displayed:
MIN RAT SPEED......................................................... 140 KT
Will disappear at landing gear extension.
MAX SPEED................................................................ 320 KT
FOR LDG..........................................................USE FLAPS 3
GPWS LDG FLAP 3...........................................................ON
Will be displayed when flaps in CONF 3.
INOP SYS
Refer to 99 Duref Cible FCOM
ELEC EMER CONFIG SYS
REMAINING (except for fuel
pumps)
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 97/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL (Cont'd)
APPR SPD........................................................ VREF +10 KT
LDG DIST PROC......................................................... APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
See (1)
WHEN L/G DN: DIRECT LAW
See (2)
(1) Flight controls remain in alternate law, due to the loss of IR 2 and 3.
(2) At landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
　
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