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REPETITIVE CHIME RED WARNINGS PERMANENT Press (1)
MASTER WARN lt
SINGLE CHIME AMBER CAUTION 1/2 s
A/P DISCONNECTION
BY TAKE OVER pb 1.5 s Second push on
CAVALRY CHARGE (3) TAKE OVER pb A/P DISCONNECTION
DUE TO FAILURE PERMANENT Press MASTER WARN
lt or TAKE OVER pb
TRIPLE CLICK
Landing capability downgrade
or "GPS PRIMARY LOST" in
approach, or mode reversion
1/2 s (3 pulses)
CRICKET
+
“STALL” message
(synthetic voice)
STALL PERMANENT NIL
CABIN CALL 3 s NIL
EMER CABIN CALL 3 s REPEATED
BUZZER 3 TIMES NIL
MECH CALL (2)As long as outside pb pressed NIL
CONTINUOUS BUZZER (2) SELCAL CALL PERMANENT Press RESET key on ACP
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
ECAM DESCRIPTION
A318/A319/A320/A321 FLEET DSC-31-10 P 16/16
FCOM 19 AUG 10
Continued from previous page
WARNING SIGNAL CONDITION DURATION SILENCING (1)
“WINDSHEAR” (synthetic
voice) WINDSHEAR REPEATED 3 TIMES NIL
"GO AROUND WIND SHEAR
AHEAD" (synthetic voice)
Windshear ahead detected
during the landing phase PERMANENT NIL
"WINDSHEAR
AHEAD" (twice)
(synthetic voice)
Windshear ahead detected
during the takeoff phase PERMANENT NIL
"MONITOR RADAR
DISPLAY" (synthetic voice)
Windshear ahead
detected caution message PERMANENT NIL
C CHORD
ALTITUDE ALERT
(Refer to DSC-31-40
ALTITUDE ALERT)
1.5 s or PERMANENT
new ALTITUDE
selection or press
MASTER WARN pb
AUTO CALL OUT
(synthetic voice)
HEIGHT ANNOUNCEMENT
BELOW 2 500 ft
(Refer to DSC-34-40-10-A
AUTOMATIC CALL
OUT - GENERAL)
PERMANENT NIL
GROUND PROXIMITY
WARNING
(synthetic voice)
(Refer to DSC-34-70-10
DESCRIPTION) PERMANENT NIL
“PRIORITY LEFT” ”PRIORITY
RIGHT“ (synthetic voice) A/P TAKE OVER pb 1 s NIL
“RETARD"
(synthetic voice)
THRUST LEVER NOT
IN IDLE POSITION
FOR LANDING
PERMANENT THRUST LEVER
TCAS (synthetic voice) (Refer to 99 Duref
Cible FCOM) PERMANENT NIL
″RODDC+􀀃RODDC+􀀃RODDC″
(Synthetic voice)
Current thrust is not sufficient
to recover a positive flight
through pitch control
Every 5 s until
thrust is increased THRUST LEVER(s)
"DUAL INPUT"
(synthetic voice)
Both sidesticks are
moved simultaneously Every 5 s One sidestick deactivated
(1) The pilot can cancel any aural warning, by pressing :
The EMER CANC pushbutton on ‐ the ECAM control panel,
‐ The MASTER WARN pushbutton, except for OVERSPEED or L/G NOT DOWN warnings.
(2) The pilot can cancel the continuous buzzer, by pressing the MASTER CAUT pushbutton.
(3)When the flight crew presses the MASTER WARN pushbutton (following a warning that leads to an AP
disconnection), the Cavalry Charge sound is only inhibited when it has been emitted in order to avoid an unintended
cancellation.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
INDICATIONS ON E/WD
A318/A319/A320/A321 FLEET DSC-31-15 P 1/10
FCOM 19 AUG 10
GENERAL
Applicable to:
The Engine Warning Display (E/WD) appears on the ECAM's upper Display Unit (DU).
The ‐ upper part of this DU displays :
• Engine parameters (Refer to DSC-70-90-A ECAM - PRIMARY PARAMETER )
• Fuel On Board (FOB) (Refer to DSC-28-20 ECAM UPPER DISPLAY)
• Slats/Flaps' position (Refer to DSC-27-20-30 ECAM F/CTL PAGE)
‐ The lower part of this DU displays messages generated by the FWC :
• Warning and caution messages, when a failure occurs.
• Memos, when there is no failure.
The lower part, dedicated to ECAM messages, is divided into two sections of several lines each.
Bottom left : ‐ Primary or independent warnings and cautions, or
‐ Memo information.
Bottom right : ‐ Title of the system affected by a primary or independent warning or caution,
in case of overflow on the bottom left part, or
‐ Secondary failure, or
‐ Memo, or
‐ Special lines (such as “AP OFF”, “LAND ASAP”).
As soon as the FWC detects a failure, and if there is no flight phase inhibition active, the E/WD
displays the title of the failure and actions to be taken.
The action line automatically clears, when the flight crew has performed the required action.
Note: Certain actions lines will not disappear after being done.
　
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