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L1 ELAC 1........................................................................................................................ OFF THEN ON
L2Note: When the ELAC 1 computer is reset on ground, the pitch trim returns to the ground setting
position (0 °).
L1 ELAC 2........................................................................................................................ OFF THEN ON
�� If the warning disappears:
CAPT TAKE OVER pb..................................................................... PRESS (at least 3 seconds)
L2Check that the :
Aural ‐ “priority left” message is activated.
‐ F/O red arrow light is on.
L1CAPT TAKE OVER pb..................................................................................................RELEASE
F/O TAKE OVER pb.........................................................................PRESS (at least 3 seconds)
L2Check that the:
‐ Aural “priority right” message is activated
‐ CAPT red arrow light is on.
L1 F/O TAKE OVER pb..................................................................................................... RELEASE
L2Check that the warning does not reappear.
Note: There is no need to move the sidestick for the check.
L1�� If the warning does not disappear, or if the warning reappears after the above check:
L2Maintenance action is due.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 126/146
FCOM 19 AUG 10
F/CTL STABILIZER JAM
Applicable to:
L2When the Flight Control Computers detect a loss of electrical control of the stabilizer, pitch control
law reverts to alternate law. Depending on the type of failure, the MAN PITCH TRIM may still be
available.
L1MAN PITCH TRIM................................................................................................................... CHECK
L2 The force needed on the PITCH TRIM wheel may be higher than during pre-takeoff manual setting.
L1�� IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
L2 If manual pitch trim is available, trim to maintain the elevator at the zero position (indications on
ECAM F/CTL page).
L1
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
MAX SPEED...........................................................................................................................320 KT
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 127/146
FCOM 19 AUG 10
F/CTL STABILIZER JAM (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC:
FOR LDG...................................................................USE FLAP 3
Do not select configuration FULL, so as not to degrade the
handling qualities.
GPWS LDG FLAP 3................................................................. ON
Will be displayed when flaps in CONF 3
�� IF MAN TRIM NOT AVAIL:
�� WHEN CONF 3 AND VAPP:
L/G................................................................................DN
Landing gear extension is delayed, in order to delay the
switching to direct law.
APPR SPD:............................................................ VREF + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as
well as in roll. Refer to PRO-ABN-27-J F/CTL DIRECT LAW.
CAT 1 ONLY
INOP SYS
F/CTL PROT
STABILIZER
ELAC PITCH
AP 1 + 2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 128/146
FCOM 19 AUG 10
F/CTL STABILIZER JAM
Applicable to: ,
L2When the Flight Control Computers detect a loss of electrical control of the stabilizer, pitch control
law reverts to alternate law. Depending on the type of failure, the MAN PITCH TRIM may still be
available.
L1MAN PITCH TRIM................................................................................................................... CHECK
L2 The force needed on the PITCH TRIM wheel may be higher than during pre-takeoff manual setting.
L1�� IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
L2 If manual pitch trim is available, trim to maintain the elevator at the zero position (indications on
　
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