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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: ,
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
CONFIG.
• SPD BRK NOT RETRACTED or
• PITCH TRIM NOT IN TO RANGE (-7 °, 0 °)
• RUD TRIM NOT IN TO RANGE (± 3 °)
aircraft not in TO configuration when thrust levers
are set at TO or Flex TO, or when pressing TO
CONFIG. pb
CRC MASTER
WARN 5, 6, 7, 8
PITCH TRIM/MCDU/CG DISAGREE
Disagreement between the real pitch trim value,
the pitch trim value calculated by the FCMC,
based in the CG, and the pitch trim value entered
in the MCDU.
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.
CRC MASTER
WARN NIL
Red
(1)SIDESTICK
PRIORITY lt
4, 5, 6, 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 7/10
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
L + R ELEV FAULT
Loss of both elevators. 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.
F/CTL
PFD message
ALTN LAW
Alternate law is active.
SINGLE
CHIME
MASTER
CAUT
NIL
4, 5, 7, 8
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
Appears :
In flight phase 6, ‐ when the SPEED BRK memo
is amber for more than 30 s .
‐ In final approach, below 800 ft , when
speedbrakes are extended for more than 5 s
(regardless of the landing configuration).
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.
SINGLE
CHIME
MASTER
CAUT
F/CTL
NIL
4, 5
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 8/10
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
SPLR FAULT
Loss of one or more spoilers. 3, 4, 5, 7
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
PEDAL SENSOR FAULT 3, 4, 5,
6, 7, 8
SENSOR FAULT
loss of any sensor of F/CTL sys
NIL
3, 4, 5,
6, 7, 8
RUD TRIM FAULT
Rudder trim 1+2 fault. 4, 5, 7, 8
RUDDER FAULT
RUD NORM CTL FAULT 1, 4, 10
RUD PEDAL FAULT 4, 5
ELEV SERVO FAULT
Loss of one servojack on one elevator. 3, 4, 5
AIL SERVO FAULT
Loss of one servojack on one aileron.
RUD B (Y) (G) SERVO FAULT
F/CTL
FCDC 1 (2) FAULT
3, 4, 5, 7, 8
RUD TRIM 1 (2) FAULT 3, 4, 5, 7, 8
RUD B (Y) (B) SERVO JAM 3 to 8
SEC 1(2) PITCH FAULT 3 to 8
　
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