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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
INOP SYS
L+R ELEV
ELAC PITCH
AP 1+2
CAT 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
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 96/146
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
INOP SYS
L + R ELEV
ELAC PITCH
LAF (A320 with LAF only)
AP 1 + 2
CAT 2
F/CTL L+R ELEV FAULT
Applicable to: ,
MSN,
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 97/146
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
INOP SYS
L + R ELEV
ELAC PITCH
LAF (A320 with LAF only)
AP 1 + 2
CAT 2
F/CTL L+R ELEV FAULT
Applicable to: MSN
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.
　
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本文鏈接地址：A320機(jī)組操作手冊(cè)FLIGHT CREW OPERATING MANUAL 9(100)