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(R) Red warning
(A) Amber caution
CONFIGURATION WARNINGS
Applicable to: MSN
4566,,,
The following warnings and cautions appear in the lower part of the E/WD if the aircraft is not in
takeoff configuration when the pilot presses the T.O. CONFIG pushbutton on the ECAM control panel
or applies takeoff power.
WARNINGS/CAUTIONS TO CONFIG TEST TO POWER
SLATS/FLAPS
NOT IN TO CONFIG (R)
PITCH TRIM
NOT IN TO RANGE (R)
RUD TRIM
NOT IN TO RANGE (R)
SPD BRK
NOT RETRACTED (R)
SIDESTICK FAULT (R)
(BY TAKE OVER)
BRAKES HOT (A)
DOORS (A)
TRIGGERED
ENG 1(2) OIL LO TEMP (A)
TRIGGERED
NOT TRIGGERED
PARK BRAKE ON (R)
THR LEVERS NOT SET (A) NOT TRIGGERED TRIGGERED
(R) Red warning
(A) Amber caution
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
INDICATIONS ON SD
A318/A319/A320/A321 FLEET DSC-31-20 P 1/12
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The system/status display (SD) uses the lower ECAM DU to display :
pages showing synoptic diagrams ‐ of the aircraft systems, or
‐ the status page.
SYSTEM PAGES
Applicable to:
The lower ECAM DU can display 12 system pages (For description see relevant FCOM chapter) :
‐ ENGINE (secondary engine parameters)
‐ BLEED (air bleed)
‐ CAB PRESS (cabin pressurization)
‐ ELEC (electric power)
‐ HYD (hydraulic)
‐ FUEL (fuel)
‐ APU (auxiliary power unit)
‐ COND (air conditioning)
‐ DOOR/OXY (doors/oxygen)
‐ WHEEL (landing gear, braking, ground spoilers, etc.)
‐ F/CTL (flight controls)
‐ CRUISE (cruise)
The pilot may manually call up a system page for display on the lower ECAM DU, or the system may
automatically display a page.
‐ Manual :
• The pilot can, at any time, use the pushbutton on the ECAM's control panel to call up and
display any system page, except the CRUISE page.
• The corresponding pushbutton on the ECAM control panel lights up.
• A failure-related or advisory display automatically replaces a page the pilot has manually called
up.
‐ Automatic, related to a failure :
• The relevant system page automatically appears, as soon as any fault or malfunction triggers a
caution or warning message.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
INDICATIONS ON SD
A318/A319/A320/A321 FLEET DSC-31-20 P 2/12
FCOM 19 AUG 10
‐ Automatic, advisory :
• The relevant system page automatically appears, when a parameter drifts out of its normal
range.
• The value (shown in green) pulses, as long as it is outside its limits.
• The advisory mode is inhibited in some flight phases.
Note: If an advisory is triggered, when the ECAM is in the single-display configuration, an
advisory message appears on the upper part of the E/WD, and the associated key on
the ECAM control panel flashes to identify the appropriate system page.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
INDICATIONS ON SD
A318/A319/A320/A321 FLEET DSC-31-20 P 3/12
FCOM 19 AUG 10
‐ Automatic, flight phase mode
• If no other mode is engaged, the SD displays the system page related to the present flight
phase, as shown in the following diagram.
• Phase 2 : The F/CTL page replaces the WHEEL page for 20 s when either pilot moves his
sidestick (more than 3 ° in pitch or roll) or when the rudder pedal deflection is more than 22 °.
• The APU page appears when the APU MASTER switch is ON. It disappears when APU RPM
has been above 95 % for 10 s, or when the APU MASTER switch is switched OFF.
• The ENGINE page appears at the beginning of start sequence or when a pilot selects “CRANK”.
It disappears 10 s after the end of the start sequence, when the ENG MODE sel is set to
NORM.
For a description of the ENGINE and AIR indications that appear when the SD is displaying the
CRUISE page, see the relevant FCOM chapter.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
INDICATIONS ON SD
A318/A319/A320/A321 FLEET DSC-31-20 P 4/12
FCOM 19 AUG 10
SYSTEM PAGES
Applicable to:
,
,
MSN,,,,
The lower ECAM DU can display 12 system pages (For description see relevant FCOM chapter) :
ENGINE (‐ secondary engine parameters)
‐ BLEED (air bleed)
‐ CAB PRESS (cabin pressurization)
‐ ELEC (electric power)
　
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