曝光臺 注意防騙 網曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費者

Control laws remains normal.
Note: When both FCDCs fails:
‐ F/CTL warning are not available on the ECAM.
‐ Stall warning may be triggered as in alternate or direct law (it may occur at speeds
greater than Vα max).
‐ Bank and pitch limits are no longer displayed on the PFD.
‐ Vα prot, Vα max are lost on the PFD.
‐ Vsw, displayed on the PFD, corresponds to the stall warning of the alternate or direct
law.
STATUS
F/CTL INDICATIONS LOST INOP SYS
FCDC 1 + 2
F/CTL AIL SERVO FAULT
Applicable to:
, ,
MSN,
4538,
L2 LAF is degraded (A320 only).
Crew awareness
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 89/146
FCOM 19 AUG 10
F/CTL AIL SERVO FAULT
Applicable to: MSN,
L2Crew awareness
F/CTL L (R) AIL FAULT
Applicable to:
L2 LAF is degraded and uses spoilers only (A320 only).
Crew awareness
L12
STATUS
INOP SYS
L (R) AIL
Note: With one or both
aileron fault(s),
fuel consumption
increases by
approximately
6 %.
F/CTL L (R) AIL FAULT
Applicable to: ,
L2 LAF is degraded and uses spoilers only (A320 only).
Crew awareness
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 90/146
FCOM 19 AUG 10
F/CTL L (R) AIL FAULT (Cont'd)
L12
STATUS
INOP SYS
L (R) AIL
Note: With one or both
aileron fault(s),
fuel consumption
increases by
approximately
6 %.
F/CTL L (R) AIL FAULT
Applicable to: MSN,
L2Crew awareness
L12
STATUS
INOP SYS
L (R) AIL
Note: With one or both
aileron fault(s),
fuel consumption
increases by
approximately
6 %.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 91/146
FCOM 19 AUG 10
F/CTL L (R) AIL FAULT
Applicable to: ,
MSN,,
L2 LAF is degraded and uses spoilers only (A320 only).
Crew awareness
L12
STATUS
INOP SYS
L (R) AIL
Note: With one or both
aileron fault(s),
fuel consumption
increases by
approximately
6 %.
F/CTL L+R ELEV FAULT
Applicable to:
MAX SPEED...........................................................................................................................320/.77
L2 Due to loss of high speed protections.
L1MAN PITCH TRIM........................................................................................................................ USE
L2 Only manual trim is available for pitch control.
L1 SPD BRK.......................................................................................................................DO NOT USE
L2 Do not use speed brakes, because it is difficult to control the induced pitch moment with manual
pitch trim only.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 92/146
FCOM 19 AUG 10
F/CTL L+R ELEV FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320/.77
SPD BRK.......................................................DO NOT USE
APPR PROC
FOR LDG...................................................................USE FLAP 3
Do not select CONF FULL, so as not to degrade handling
qualities.
GPWS LDG FLAP 3................................................................. ON
Will be displayed when flaps in CONF 3.
MAN PITCH TRIM...................................................................USE
APPR SPD......................................................................VREF+10
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
PITCH MECH BACK UP
ROLL DIRECT LAW
CAT 1 ONLY
INOP SYS
L+R ELEV
ELAC PITCH
LAF (A320 with LAF only)
AP 1+2
F/CTL L+R ELEV FAULT
Applicable to: ,
MAX SPEED...........................................................................................................................320/.77
L2 Due to loss of high speed protections.
L1MAN PITCH TRIM........................................................................................................................ USE
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機組操作手冊FLIGHT CREW OPERATING MANUAL 9(98)