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ELECTRONIC INSTRUMENT MENU
ECAM System 11/117
If failures occur Warning/Caution messages are
displayed in place of the memos. In the example shown
there is an amber caution message with a series of blue
action items. These action items are your electronic
checklist to respond to the particular abnormal
situation
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ELECTRONIC INSTRUMENT MENU
ECAM System 12/117
The SD is used to display particular system information. In the example
shown the CRUISE page is displayed. This is the page normally seen for the
majority of the time that the aircraft is airborne. Information, that is useful
during flight, from several systems is displayed.
The individual indications will be covered in the appropriate system
modules.
CRUISE
Page
ELECTRONIC INSTRUMENT MENU
ECAM System 13/117
The SD can also be used to display synoptic diagrams of
the aircraft systems, System pages. In the example shown
the hydraulics system page has been called.
You will see later how these system pages are called
either manually or automatically.
ELECTRONIC INSTRUMENT MENU
ECAM System 14/117
An aircraft STATUS page may be displayed on the SD to check the
state of the aircraft. A NORMAL message is displayed to indicate that the
aircraft state is normal and that there are no inoperative systems.
Let’s see what the STATUS page looks like when things are not normal,
for example, following a system failure.
ELECTRONIC INSTRUMENT MENU ECAM System 15/117
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ELECTRONIC INSTRUMENT MENU ECAM System 16/117
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Approach
Procedures
ELECTRONIC INSTRUMENT MENU ECAM System 17/117
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Approach
Procedures
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ELECTRONIC INSTRUMENT MENU
ECAM System 18/117
The information displayed on the STATUS page will vary depending on
the failure but as an example can include:
• Limitations,
• Approach procedures including actions and corrections,
• Information,
• Inoperative systems.
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Approach
Procedures
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ELECTRONIC INSTRUMENT MENU
ECAM System 19/117
The area at the bottom of any SD
contains permanent data:
• Total Air Temperature (TAT),
• Static Air Temperature (SAT),
• Time,
• Gross Weight.
ELECTRONIC INSTRUMENT MENU
ECAM System 20/117
Individual airlines can choose which units they wish to use for
certain parameters on the ECAM screens. In the examples shown we
have highlighted the areas on the screens where the units used differ.
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ELECTRONIC INSTRUMENT MENU
ECAM System 21/117
Because these indications are only mentioned in a few areas of the
ground school course, we will use boxes to indicate that the units may
differ depending on your airlines’ choice. The boxes mean that the
information in this area of the screen is irrelevant to the system being
studied. When a system, for example Fuel, is being studied then
appropriate unit values will be shown.
UUSSUUNNIITTSS MMEETTRRIICCUUNNIITTSS
ELECTRONIC INSTRUMENT MENU
ECAM System 22/117
Under normal conditions the
ECAM system provides the pilots
with the information that they “Need
to Know” for the particular phase of
flight, no more no less.
As an example during the
approach when the landing gear is
extended the ECAM WHEEL system
page is automatically displayed.
ELECTRONIC INSTRUMENT MENU
ECAM System 23/117
The ECAM system divides the various stages of a flight
into phases, from initial electrical power up until after
engine shutdown.
The ECAM system will avoid alerting the pilots
unnecessarily during the critical flight phases of take off and
landing. The warnings and cautions that can be delayed
until a less critical phase of flight will be inhibited.
Electrical
power up
After
shut down
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ELECTRONIC INSTRUMENT MENU
ECAM System 24/117
We will now look at the different
ways that the ECAM system advises
you when things are not going
exactly right. We will start with a
minor advice indication and work up
to a major fault, concentrating on the
two ECAM screens.
ELECTRONIC INSTRUMENT MENU
ECAM System 25/117
If a system parameter, for example an
engine vibration level, approaches a limit
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