曝光台 注意防骗
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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 68/176
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 69/176
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
00011770 **Not found**).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FIRE PROTECTION
A318/A319/A320/A321 FLEET PRO-ABN-26 P 70/176
FCOM 19 AUG 10
SMOKE/FUMES/AVNCS SMOKE - GENERAL
Applicable to:
This paper procedure includes all the steps of the AVIONICS SMOKE ECAM procedure.
Apply this paper procedure when:
The flight (cabin) crew suspect that smoke is coming ‐ from the avionics, and/or the air
conditioning, and/or the cabin equipment.
‐ The AVIONICS SMOKE ECAM caution is triggered, or, at the latest, after completing the
immediate actions of the AVIONICS SMOKE ECAM procedure (before reaching the 5–minutes
countdown procedure line)
There is a smell of smoke/fumes in the cockpit:
• If the smell is similar to that of orange peels, suspect a toxic leak of rain repellent fluid.
• If the smell is similar to that of pine needles, suspect a non-toxic leak.
If any other ECAM SMOKE alert triggers (CARGO, ...), the crew must first apply the ECAM
procedure, then consider applying this paper procedure.
Note that these ECAM alerts may be caused by another source, that should usually first be
detected by the flight crew/cabin crew/avionics smoke detectors.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(33)
