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ECAM sound Symbology
Warning signal
Continuous
repetitive chime
Single chime
Click
Cricket
Intermittent buzzer
Continuous buzzer
‘C’ chord
Auto call-out
(synthetic voice)
Ground proximity
warning
(synthetic voice)
Red warnings
Condition Duration
Permanent
Amber caution
A/P disconnection by take-over pb
A/P disconnection due to failure
Landing capability change
Stall
SELCAL call
Cabin call
Altitude alert
Height announcement
below 400ft
GWPS warning
1 / 2 second
1.5 second
Permanent
½ second (three pulses)
Permanent
Permanent
Permanent
1.5 second or Permanent
Permanent
Permanent
Cavalry change
STL 945.7136/97 12.14
A319/A320/A321 EIS - ECAM upper display
Fuel quantity indication
Flap / slats position
indication
Primary engine
indications
MEMO :
landing
STL 945.7136/97 12.15
A319/A320/A321 EIS - ECAM upper display
􀁺 The ECAM upper DU can provide the following
memo items for systems which can be use
temporarily and for which no dedicated
annunciator lights are provided.
􀁺 Specific memos for take-off and landing are also
available when appropriate.
IRS IN ALIGN X MIN
IRS ALIGNED
SEA BELTS
NO SMOKING
REFUEL G
OUTR CELL FUELXFRD
STROBE LT OFF
N. WHEEL STEERG DISC
IGNITION
GND SPLRS ARMED
GPWS FLAP MODE OFF
SPEED BRK
PARK BRK
HYD PTU
RAT OUT
EMER GEN
RAM AIR ON
ACARS CALL
ACARS MSG.
ENG A.ICE
WING A.ICE
APU AVAIL
APU BLEED
LDG LT
BRK FAN
AUDIO 3 X FRD
SWITCHING PNL
GPWS FLAP 3
ACARS STBY
MAN LDG ELEV
CRT TK FEEDG
FUEL X FEED
T.O. INHIB
LDG INHIB
LAND ASAP
AUTO BRK
OFF
LO
MED
MAX
TO MEMO LDG MEMO
AUTO BRK…….MAX
SIGNS …………ON
SPLRS …………ARM
FLAPS …………TO
TO CONFIG ….. TEST
CABIN …………READY
LDG GEAR…….DN
SIGNS …………ON
SPLRS …………ARM
FLAPS …………FULL
or
CONFIG 3
STL 945.7136/97 12.16
A319/A320/A321 EIS - ECAM lower DU
Cruise page Electrical system page with advisory
Title of the
system page
pulsing
Value pulsing
STL 945.7136/97 12.17
A319/A320/A321 EIS - ECAM lower DU
􀁺 The ECAM lower DU presents either (one of twelve)
system pages or status pages.
􀁺 Selection of System page is :
- either manual from the ECAM control panel,
- or automatic
in association with a warning/caution message,
with an advisory pulse message when a
parameter drifts out of range
according to flight phase.
􀁺 12 available pages :
Air bleed,
Air conditioning,
Cabin pressurization,
Electrical power supply – AC / DC,
Flight controls,
Fuel,
Hydraulics,
APU,
Engine monitoring,
Doors / oxygen,
Braking (wheel, ground spoiler),
Cruise.
••
•
STL 945.7136/97 12.18
A319/A320/A321 EIS - ECAM system pages
Cruise page Engine page Air bleed page Cabin pressurization page
Electric page Hydraulic page Fuel page APU page
Air conditioning page Doors/oxygen page Wheel page Flight controls page
STL 945.7136/97
Engine**
start
System
pages
Flight
phases
(FWC)
12.19
A319/A320/A321 EIS - ECAM lower display – auto flight phase
APU**
1 2 3 4 5 6 7 8 9 10
Door Wheel Engine Cruise Wheel Door
S/F extended
To PWR
Phase 6
1 MIN L/G
extended
and altitude < 10000ft
* FLT
CTL
Electrical power
1st engine starded
1st engine TO power
80 kt
1500 ft
800 ft
Touchdown
80 kt
2nd engine shutdown
5 minutes after
* FLT CTL page replaces wheel page for 20 seconds when either sidestick is moved or when rudder deflection is
above 22°.
** APU page or EBG START page automatically displayed during start sequence.

STL 945.7136/97 12.21
A319/A320/A321 EIS – ECAM lower display
Status page
The operational summary of the aircraft status after a
failure is displayed on the lower ECAM DU and includes :
(a) Postponable procedures not displayed on first page
　
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