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They become amber, if :
Both relevant hydraulic systems fail, unless the aircraft is ‐ on ground with both engines
stopped.
‐ The wingtip brakes are on.
‐ There is a slats or flaps fault.
(5) Selected surface position
These blue triangles indicate the position the pilot has selected.
(With the current standard display management computer, the blue triangles may disappear
before the slats and flaps are all completely in the selected position).
(6) F and S
“F” and “S” normally appear in green. They become amber, if :
‐ Both relevant hydraulic systems fail, unless the aircraft is on ground with both engines
stopped.
‐ The wingtip brakes are on.
‐ There is a slats or flaps fault.
“S (F) LOCKED” legend, appears in amber, in association with an ECAM caution, when the
wingtip brakes are applied, or when the system detects a non-alignment between two flaps.
The “A-LOCK” legend pulses in cyan, when the slat alpha/speedlock function is active.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLAPS AND SLATS - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-30-20 P 6/8
FCOM 19 AUG 10
ECAM UPPER DISPLAY
Applicable to:
,
,
MSN,,,,
(1) Position indexes
These white points indicate that the slats and flaps are in a selectable position. They do not
appear, when the aircraft is in clean configuration.
(2) F and S
“F” and “S” normally appear in white. They become amber, if :
Both relevant hydraulic systems fail, unless the aircraft is ‐ on ground with both engines
stopped.
‐ The wingtip brakes are on.
‐ There is a slats or flaps fault.
“S (F) LOCKED” legend, appears in amber, in association with an ECAM caution, when the
wingtip brakes are applied, or when the system detects a non-alignment between two flaps.
The “A-LOCK” legend pulses in cyan, when the slat alpha/speedlock function is active.
(3) Flaps/Slats’ actual position
These green boxes indicate the actual flaps/slats position.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLAPS AND SLATS - CONTROLS AND INDICATORS
A318/A319/A320/A321 FLEET DSC-27-30-20 P 7/8
FCOM 19 AUG 10
They become amber, if :
‐ Both relevant hydraulic systems fail, unless the aircraft is on ground with both engines
stopped.
‐ The wingtip brakes are on.
‐ There is a slats or flaps fault.
(4) Selected position
It is in blue, when the surfaces are in transit.
It disappears, when the selected position is reached.
(5) Flap lever position
The “0”, “1 + F”, “1”, “2”, “3”, or “FULL” legend appears.
‐ It is green, when the slats and flaps are in the selected position. “0” is not displayed, when
the aircraft attains clean configuration.
‐ It becomes cyan, when the slats and flaps are in transit.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLAPS AND SLATS - CONTROLS AND INDICATORS
Intentionally left blank
A318/A319/A320/A321 FLEET DSC-27-30-20 P 8/8
FCOM 19 AUG 10
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
FLIGHT CONTROLS
FLAPS AND SLATS - WARNINGS AND CAUTIONS
A318/A319/A320/A321 FLEET DSC-27-30-30 P 1/2
FCOM 19 AUG 10
WARNINGS AND CAUTIONS
Applicable to:
E/WD : FAILURE TITLE
conditions
AURAL
WARNING
MASTER
LIGHT
SD PAGE
CALLED
LOCAL
WARNING
FLT
PHASE
INHIB
CONFIG SLATS (FLAPS) NOT IN TO CONFIG
Slats or flaps are not in takeoff configuration,
when thrust levers are set at TO or FLEX TO, or
when pressing the TO CONFIG pb.
CRC MASTER
WARN 5, 6 (1), 7, 8
SLATS (FLAPS) FAULT
Failure of both slat or flap channels.
SLATS (FLAPS) LOCKED
Slats or flaps' wing tip brakes applied, or non
alignment detected between 2 flaps.
SINGLE
CHIME
MASTER
CAUT 4, 5, 8
SLATS SYS 1 (2) FAULT
Failure of slat channel in one SFCC.
FLAP SYS 1 (2) FAULT
Failure of flap channel in one SFCC.
SLAT (FLAP) TIP BRK FAULT
Failure of one wing tip brake on slats or flaps, or
failure of one wing tip brake solenoid on slats, or
flaps.
FLAPS ATTACH SENSOR
Failure of flap attachment's failure detection
sensor.
NIL NIL
NIL NIL
3, 4, 5, 7, 8
(1) The warning is automatically recalled by pressing the TO CONFIG pushbutton.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 3(47)
