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and the pitch trim value calculed by the FCMC,
based on the CG.
SINGLE
CHIME
MASTER
CAUT
F/CTL NIL
1, 4, 5, 6,
7, 8, 10
CONFIG R (L) SIDESTICK FAULT (BY TAKE
OVER)
L or R sidestick is inoperative (deactivated by
takeover pb) when thrust levers are set at TO or
Flex TO, or when pressing TO CONFIG. pb.
NIL
Red
(1)SIDESTICK
PRIORIRY lt
4, 5, 6, 7, 8
L + R ELEV FAULT
Loss of both elevators.
CRC MASRER
WARN
PFD message
L (R) SIDESTICK FAULT
Transducers on pitch or roll axis are failed on one
sidestick.
NIL
NIL
PRIM 1 (2)(3) FAULT
Failure of 1 primary computer.
FAULT lt
on PRIM pb 3, 4, 5, 7, 8
SEC 1 (2) FAULT
Failure of one secondary computer.
FAULT lt
on SEC pb 3, 4, 5
FCDC 1 + 2 FAULT
Failure of both FCDCs. NIL 4, 5, 7
DIRECT LAW
Direct law is active.
SINGLE
CHIME
MASTER
CAUT
F/CTL
PFD message 4, 5, 7, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-27-20-40 P 2/10
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
ALTN LAW
Alternate law is active. NIL
DUAL INPUT
Both sidesticks are moved simultaneously.
Synthetic
voice repeated
every 5 s
NIL
NIL SIDESTICK
Priority light NIL
GND SPLR FAULT
Loss of ground spoiler function in all PRIM
computers.
SPD BRK DISAGREE
Position disagree between surfaces and handle
position.
SPD BRK FAULT
Spdbrake lever transducers to all PRIM failed.
F/CTL 3, 4, 5
SPD BRK STILL OUT
The SPEED BRK memo has been amber for
more than 30 s .
NIL 1 to 5
8 to 10
STAB CTL FAULT
Loss of the electrical control of the stabilizer.
L (R) ELEV FAULT
Loss of both servojacks on one elevator.
L (R) OUTR (INR) AIL FAULT
Loss of both servojacks on one aileron.
4, 5
SPLR FAULT
Loss of one or more spoilers. 3, 4, 5, 7
RUD TRIM FAULT
Rudder trim 1 + 2 fault. 4, 5, 7, 8
RUD TRV LIM FAULT
travel limiter 1 + 2 failure.
F/CTL
4, 5
YAWDAMPER FAULT
yaw damper 1 + 2 fault. 4, 5, 7, 8
ELEV REDUND LOST
Loss of elevator redundancy for which a
subsequent failure would lead to a degraded pitch
control or pitch mechanical backup.
1, 4, 5,
7, 8, 10
SENSOR FAULT
loss of any sensor of F/CTL sys
SINGLE
CHIME
MASTER
CAUT
NIL
4, 5, 6, 7, 8
ELEV SERVO FAULT
Loss of one servojack on one elevator. 3, 4, 5
AIL SERVO FAULT
Loss of one servojack on one aileron.
F/CTL
FCDC 1 (2) FAULT
NIL NIL
NIL
NIL
3, 4, 5, 7, 8
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
A330/A340 FLEET DSC-27-20-40 P 3/10
FCOM 19 AUG 10
Continued from previous page
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
YAWDAMPER 1 (2) 3, 4, 5,
7, 8, 10
RUD TRIM 1 (2) FAULT
RUD TRV LIM 1 (2) 3, 4, 5, 7, 8
RUD B (Y) (G) SERVO JAM 3 to 8
SEC 1(2) PITCH FAULT 3 to 8
PRIM 1(2)(3) PITCH FAULT 3, 4, 5, 7, 8
TURB DAMP FAULT
longitudinal or lateral turbulence damping lost due
to accelerometer failure.
3, 4, 5, 7, 8
(1) The red SIDESTICK PRIORITY lt is illuminated as soon as the sidestick is inoperative.
MEMO
The "‐ SPEED BRK" memo display logic :
• When the speedbrakes are extended, in Flight Phases 2, 3, 4, and 5, the "SPEED BRK"
memo flashes amber.
• When the speedbrakes are extended, in Flight Phase 6 and 7, the "SPEED BRK" memo is
displayed in green. It flashes amber, after 50 s, if at least one engine is above idle.
‐ The "GND SPLRS ARMED" message appears in green, when the ground spoilers are armed.
‐ The "TURB DAMP OFF" message is displayed in green when the TURB DAMP pushbutton is
switch is selected OFF.
WARNINGS AND CAUTIONS
Applicable to:
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
　
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