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NOT IN CLIMB:
T TANK MODE..........................................................FWD
Note: Fuel consumption is increased by
approximately 1 %.
DIRECT LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 61/142
FCOM 19 AUG 10
F/CTL DIRECT LAW (Cont'd)
(PROT LOST)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 330/.80
MANEUVER WITH CARE
APPR PROC
FOR LDG...................................................................USE FLAP 3
MAN PITCH TRIM...................................................................USE
(except if B + Y HYD LO PR)
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
Note: If trim tank transfer is unavailable, consider
descending to a lower altitude, where
controllability is improved.
�� If the trim tank pump is inoperative:
�� IF CG AFT 32 % AND WHEN SPEED > 270 KT AND
NOT IN CLIMB:
T TANK MODE..........................................................FWD
Note: If trim tank transfer is unavailable, consider
descending to a lower altitude, where
controllability is improved.
DIRECT LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 62/142
FCOM 19 AUG 10
F/CTL DIRECT LAW
(PROT LOST)
Applicable to:
L2 PFD displays «USE MAN PITCH TRIM» in amber.
L1 SPD BRK.......................................................................................................................DO NOT USE
MAX SPEED...........................................................................................................................330/.80
L2Note: In case of EGPWS alerts, since protections are lost, respect stall warning when applying
the EGPWS procedure.
Speed is limited due to the loss of high speed protection.
Do not exceed M 0.80 so as not to degrade handling qualities.
L1MAN PITCH TRIM (EXCEPT IF B + Y HYD 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�� If the trim tank pump is operative:
�� IF CG AFT 32%:
T TANK MODE................................................................................................................FWD
L2Note: Fuel consumption is increased by approximately 1 %.
L1�� If the trim tank pump is inoperative:
�� IF CG AFT 32% AND WHEN SPEED > 270KT AND NOT IN CLIMB:
T TANK MODE................................................................................................................FWD
L2Note: Fuel consumption is increased by approximately 1 %.
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A330/A340 FLEET PRO-ABN-27 P 63/142
FCOM 19 AUG 10
F/CTL DIRECT LAW (Cont'd)
(PROT LOST)
L12
STATUS
SPD BRK.......................................................DO NOT USE
MAX SPEED............................................................ 330/.80
MANEUVER WITH CARE
APPR PROC
FOR LDG...................................................................USE FLAP 3
MAN PITCH TRIM...................................................................USE
(except if B + Y HYD LO PR)
�� If the trim tank pump is operative:
�� IF CG AFT 32 %:
T TANK MODE..........................................................FWD
Note: If trim tank transfer is unavailable, consider
descending to a lower altitude, where
controllability is improved.
�� If the trim tank pump is inoperative:
�� IF CG AFT 32 % AND WHEN SPEED > 270 KT AND
NOT IN CLIMB:
T TANK MODE..........................................................FWD
Note: If trim tank transfer is unavailable, consider
descending to a lower altitude, where
controllability is improved.
DIRECT LAW: PROT LOST
INOP SYS
F/CTL PROT
AP 1 + 2
CAT 2
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
　
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