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INHIB
L (R) SIDESTICK FAULT
Transducers, on pitch or roll axis, are failed on one
sidestick.
NIL
ELAC 1 (2) FAULT
Failure of ELAC.
FAULT lt on
ELAC pb
ELAC 1 (2) FAULT
One sidestick transducer fault. NIL
3, 4, 5, 7, 8
SEC 1 (2) (3) FAULT
Failure of one SEC.
FAULT lt
on SEC pb 3, 4, 5
FCDC 1 + 2 FAULT
Failure of both FCDCs. NIL 4, 5, 7
DIRECT LAW
Direct laws are active.
PFD
message
ALTN LAW
Alternate laws are active.
SINGLE
CHIME
MASTER
CAUTION
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
SEC 1 + 3 or 1 + 2 or 2 + 3 or 1 + 2 + 3.
SPD BRK DISAGREE
Position disagree between surfaces and lever
position.
SPD BRK FAULT
Speedbrake lever transducers to SEC 1 and 3
failed.
F/CTL 3, 4, 5
SPD BRK STILL OUT
Speedbrake out with at least one engine not at
idle.
NIL 1, 2, 3, 4,
5, 8, 9, 10
STABILIZER JAM
Stabilizer jammed.
L (R) ELEV FAULT
Loss of both servojacks on one elevator, or
activation of elevator flutter protection in ELAC.
L (R) AIL FAULT
Loss of both servojacks on one aileron.
4, 5
SPLR FAULT
Loss of one or more spoilers.
SINGLE
CHIME
MASTER
CAUTION
F/CTL
NIL
3, 4, 5, 7
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-27-20-40 P 5/8
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
ELAC 1 PITCH FAULT
Failure of pitch channel in ELAC 1.
ELAC 2 PITCH FAULT
Failure of pitch channel in ELAC 2, or loss of one
or both ELAC 2 rudder pedal transducers.
3, 4, 5, 7, 8
GND SPLR 1 + 2 (3 + 4)
Ground spoiler channel failed in SEC 3 (1).
ELEV SERVO FAULT
Loss of one servojack on one elevator.
3, 4, 5
SPD BRK 2 (3 + 4) FAULT
Speedbrake lever transducers to SEC 3 (1) failed.
AIL SERVO FAULT
Loss of one servojack on one aileron, or loss of
one or both ELAC 1 rudder pedal transducers.
FCDC 1 (2) FAULT
3, 4, 5, 7, 8
SIDESTICK PRIORITY
Failure in a sidestick priority logic circuit.
NIL NIL
NIL 3, 4, 5,
6, 7, 8, 9
(1) The red SIDESTICK PRIORITY light comes on, as soon as the sidestick becomes inoperative.
MEMO DISPLAY
The “SPEED ‐ BRK” memo display logic :
• When the speedbrakes are extended in Flight Phases 2, 3, 4, and 5, the “SPEED BRK”
memo flashes in amber.
• When the speedbrakes are extended in Flight Phases 6 and 7, the “SPEED BRK” memo
appears in green. It flashes in 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.
WARNINGS AND CAUTIONS
Applicable to:
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLIGHT CONTROL SYSTEM - WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-27-20-40 P 6/8
FCOM 19 AUG 10
E/WD: FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT PHASE
INHIB
CONFIG NIL
• SLATS/FLAPS NOT IN T.O CONFIG, or
• SPD BRK NOT RETRACTED, or
• PITCH TRIM NOT IN TO RANGE, or
• RUD TRIM NOT IN T.O RANGE
A/C not in TO configuration when thrust levers
are set at TO, or Flex TO, or when pressing TO
CONFIG. pb.
F/CTL NIL
CONFIG R (L) SIDESTICK FAULT (BY TAKE
OVER) L or R sidestick is inoperative (takeover pb
pressed more than 30 s) when thrust levers are set
at TO, or Flex TO, or when pressing TO CONFIG
pb.
NIL
Red
(1)SIDESTICK
PRIORITY lt
5, 6, 7, 8
L + R ELEV FAULT
Loss of both elevators.
CRC MASTER
WARN
PFD
message
L (R) SIDESTICK FAULT
Transducers, on pitch or roll axis, are failed on one
sidestick.
NIL
NIL
ELAC 1 (2) FAULT
Failure of ELAC.
FAULT lt on
ELAC pb
ELAC 1 (2) FAULT
One sidestick transducer fault. NIL
　
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