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L2 Automatic trim is inoperative in direct law.
L1MANEUVER WITH CARE
L2 Use small control inputs at high speed, since in direct law the controls are powerful. Use of manual
thrust is recommended. Avoid large thrust changes.
L1 USE SPD BRK WITH CARE
L2 At high Mach numbers, use speed brakes with care to avoid too strong nose up changes.
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 76/146
FCOM 19 AUG 10
F/CTL DIRECT LAW (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320/.77
MANEUVER WITH CARE
USE SPD BRK WITH CARE
APPR PROC
FOR LDG................................................................ USE FLAPS 3
GPWS LDG FLAP 3................................................................. ON
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.
DIRECT LAW
INOP SYS
F/CTL PROT
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 77/146
FCOM 19 AUG 10
F/CTL DIRECT LAW
Applicable to: ,
MSN,,,,
L2 PFD displays « USE MAN PITCH TRIM » in amber. Refer to PRO-SUP-27-50 Aircraft Trimming
L1 (PROT LOST)
L12
Note: In case of GPWS ( EGPWS ) alerts, since protections are lost, respect stall warning
when applying the GPWS (EGPWS ) procedure.
MAX SPEED...........................................................................................................................320/.77
L2 Speed is limited, due to the loss of high-speed protection. Do not exceed M 0.77, so as not to
degrade handling qualities.
L1MAN PITCH TRIM (EXCEPT IF HYD Y + G SYS LO PR).......................................................... USE
L2 Automatic trim is inoperative in direct law.
L1MANEUVER WITH CARE
L2 Use small control inputs at high speed, since in direct law the controls are powerful. Use of manual
thrust is recommended. Avoid large thrust changes.
L1 USE SPD BRK WITH CARE
L2 At high Mach numbers, use speed brakes with care to avoid too strong nose up changes.
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 78/146
FCOM 19 AUG 10
F/CTL DIRECT LAW (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320/.77
MANEUVER WITH CARE
USE SPD BRK WITH CARE
APPR PROC
FOR LDG................................................................ USE FLAPS 3
GPWS LDG FLAP 3................................................................. ON
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.
DIRECT LAW
INOP SYS
F/CTL PROT
CONFIG L (R) SIDESTICK FAULT
BY TAKE OVER
Applicable to: ALL
L2 The warning is triggered, when on the ground, if either stick is inoperative (takeover pushbutton
pressed more than 30 s).
L1 L (R) TAKEOVER .............................................................................................................. DEPRESS
L2 The affected stick becomes operative.
CONFIG PITCH TRIM NOT IN T.O RANGE
Applicable to: ALL
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 79/146
FCOM 19 AUG 10
F/CTL ALTN LAW
Applicable to:
L2 Refer to PRO-SUP-27-10 General for flight characteristics.
With autopilot engaged the FMGC (AP mode) controls the aircraft.
L1 (PROT LOST)
L2 All protections, except maneuver protections, are lost. Depending on the failure, static stability may
be introduced.
L1Note: In case of GPWS (EGPWS ) alerts, since protections are lost, respect stall warnings
when applying the GPWS (EGPWS ) procedure.
MAX SPEED...........................................................................................................................320 KT
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 9(95)
