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Values are given using the metric system.
The AIRCOND page is given as an example.
This may be different to your aircraft configuration.
GENERAL
The System Display is normally on the lower ECAM
Display Unit. It is divided into two areas.
The upper area displays system or status pages, the
lower area permanent data.
The system or status pages can be called automatically
after a failure or manually upon crew request by
pressing the related P/B on the ECAM control panel.
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SYSTEM PAGES
11 system pages can be displayed manually or
automatically. Refer to each chapter for detailed
description of the pages.
The 11 system pages are:
- Air bleed (BLEED)
- Air conditioning (COND)
- Cabin pressurization (PRESS)
- Electrical power supply (ELEC)
- Flight controls (F/CTL)
- Fuel (FUEL)
- Hydraulic power (HYD)
- APU (APU)
- Engine secondary parameters (ENG)
- Doors and oxygen (DOOR)
- Landing gear, wheels, brakes (WHEEL)
The cruise page is only automatically called in flight.
The cruise page displays main systems parameters to
be monitored during the flight:
- engine parameters such as fuel used, oil
quantity and vibrations
- cabin press parameters such as landing field
elevation, cabin vertical speed, cabin
altitude, cabin differential pressure.
- zone temperature.
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STATUS PAGE
The status page contains an operational summary of the
aircraft condition. This page is automatically called
when slats > 2 (in approach).
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PERMANENT DATA
At the bottom of the System Display, permanent data
is always displayed whatever the page presented.
Here Temperature, Time and Gross weight are always
displayed.
Total Air Temperature (TAT) and Static Air Temperature
(SAT) are digital values.
TAT:
+19 (green) when normal,
XX (amber) when data not available.
The same applies for SAT.
The Greenwich Mean Time (GMT), synchronized with the
cockpit clock, is displayed in green.
Two items of information can be displayed one at a
time on the display above GMT.
- The load factor (G LOAD) is displayed in amber
when the value is out of limits (above 1.4g or
below 0.7g).
- The altitude selected on the FCU is displayed
in green when the metric unit is selected
provided G LOAD parameter is not displayed.
The Gross Weight (GW) is shown in green. It is inhibited
before flight phase 2 and after flight phase 9.
SYSTEM PAGE LOGIC
The ECAM operates in four modes for the system page
presentation, with a priority order.
The four selection modes of system page presentation
are:
- the manual mode, which can override all other
modes,
- the failure mode,
- the advisory mode,
- the flight phase mode.
Manual mode: selection from ECAM Control panel.
Failure mode: automatic presentation due to a
warning/caution.
Advisory mode: automatic presentation due to a
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