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The flight crew can display the system/status page by :
Using the “ECAM/ND XFR“ switch, on the SWITCHING panel, ‐ to move it to a Navigation Display
Unit (NDU), or
‐ Pushing and holding (for a maximum of 3 min) the related system page pushbutton, on the ECAM
control panel, to temporarily display it on the lower ECAM DU (instead of the engine/warning
page).
FAILURE OF LOWER ECAM DU (OR CTL/BRIGHTNESS KNOB TURNED TO OFF)
Applicable to: ALL
If the lower ECAM display fails, or is switched off, the flight crew can display the system/status page
by :
‐ Using the "ECAM/ND XFR" switch, on the SWITCHING panel, to display it on the NDU, or
‐ Pushing and holding (for a maximum of 3 min) the related system page pushbutton, on the ECAM
control panel, to temporarily display it on the upper ECAM DU (instead of the engine/warning
page).
FAILURE OF BOTH ECAM DUs
Applicable to: ALL
If both ECAM displays fail, the flight crew may :
‐ Use the "ECAM/ND XFR", on the SWITCHING panel, to display the engine/warning page on a
navigation display and, if needed,
‐ Push and hold (for a maximum of 3 min) the related system page pushbutton, on the ECAM
control panel, to temporarily display the system/status page on an ND.
PFDU/NDU RECONFIGURATION
Applicable to: ALL
If a PFDU fails, the system automatically transfers the PFD image to the NDU.
The pilot can also make this transfer manually by :
‐ turning the PFD ON-OFF/brightness control OFF, or
‐ pressing the PFD/ND/XFR pushbutton, which cross-changes the images between the PFDU and
the NDU.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
EIS GENERAL - RECONFIGURING DUS
A318/A319/A320/A321 FLEET DSC-31-05-60 P 2/2
FCOM 19 AUG 10
If an NDU fails, the pilot can use the PFD/ND/XFR pushbutton to transfer the ND image to the PFDU.
DU RECONFIGURATION
Applicable to: ALL
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
ECAM DESCRIPTION
A318/A319/A320/A321 FLEET DSC-31-10 P 1/16
FCOM 19 AUG 10
ECAM DU ARRANGEMENT
Applicable to: MSN,
The ECAM has two display units :
one for the ‐ engine/warning display (E/WD).
‐ one for the system/status display (SD).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
ECAM DESCRIPTION
A318/A319/A320/A321 FLEET DSC-31-10 P 2/16
FCOM 19 AUG 10
ECAM DU ARRANGEMENT
Applicable to:
,
,
MSN,,,,
The ECAM has two display units :
‐ one for the engine/warning display (E/WD).
‐ one for the system/status display (SD).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
INDICATING / RECORDING SYSTEMS
ECAM DESCRIPTION
A318/A319/A320/A321 FLEET DSC-31-10 P 3/16
FCOM 19 AUG 10
COLOR CODE
Applicable to: ALL
The ECAM display uses a color code that indicates the importance of the failure or the indication.
RED : The configuration or failure requires immediate action.
AMBER : The flight crew should be aware of the configuration or failure, but need not take
immediate action.
GREEN : The item is operating normally.
WHITE : These titles and remarks guide the flight crew, as they execute various
procedures.
BLUE : These are actions to be carried out, or limitations.
MAGENTA : These are particular messages that apply to particular pieces of equipment or
situations (inhibition messages, for example).
WARNING/CAUTION CLASSIFICATION
Applicable to: ALL
LEVEL SIGNIFICATION AURAL VISUAL
Level 3 Red warning : The configuration, or
failure requires immediate action :
Aircraft in dangerous ‐ configuration,
or limit flight conditions (eg: stall,
o/speed)
‐ System failure altering flight safety
(eg : Eng fire, excess cab alt)
Continuous
Repetitive
Chime (CRC) or
specific sound or
synthetic voice
‐ MASTER WARN
light red flashing or
specific red light
‐ Warning message
(red) on E/WD
‐ Automatic call of
the relevant system
page on the S/D (1).
FAILURE MODE
Level 2 Amber caution :
The flight crew should be aware of the
configuration or failure, but does not
need to take any immediate action.
However, time and situation permitting,
these cautions should be considered
without delay to prevent any further
degradation of the affected system :
‐ System failure without any direct
consequence on the flight safety
(eg: HYD G SYS LO PR)
　
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