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chapter for detailed description).
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EIS: ENGINE/WARNING DISPLAY PRESENTATION - UPPER AREA
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EIS: ENGINE/WARNING DISPLAY PRESENTATION
LEFT MEMO AREA
Take off or landing memo, normal memo, independent
failure messages, or primary failure messages and
actions to be performed are displayed in the left memo
area.
As soon as a failure is detected, the memo messages
are replaced by warning/caution messages.
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EIS: ENGINE/WARNING DISPLAY PRESENTATION - LEFT MEMO AREA
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EIS: ENGINE/WARNING DISPLAY PRESENTATION
RIGHT MEMO AREA
Normal memo and secondary failure messages are
displayed in the right memo area.
For example when an Engine Anti Ice P/B is set to ON,
ENG A.ICE appears on the right memo area.
During take off and landing, most of the warnings are
inhibited to avoid distraction of the crew.
For example, at take off, when the second engine is
set to take off power and until the aircraft has reached
1500 ft, TO INHIB is displayed.
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EIS: ENGINE/WARNING DISPLAY PRESENTATION - RIGHT MEMO AREA
TMUEIAD04-P04 LEVEL 1
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EIS: ENGINE/WARNING DISPLAY PRESENTATION
ADVISORY AND STATUS
Advisory and Status indications are ’attention
getters’ on the display.
ADV: Advisory appears in single display configuration,
pulsing to indicate that an A/C system parameter has
drifted.
STS: Status indicates that a status message is present
on the ECAM page.
Overflow arrow: only concerns the warning messages and
indicates that the messages exceed the capacity of the
display on the Left Memo Area. In this case, the heading
titles of the warning messages are displayed on the
Right Memo Area.
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EIS: ENGINE/WARNING DISPLAY PRESENTATION - ADVISORY AND STATUS
TMUEIAD04-P05 LEVEL 1
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SELF EXAMINATION
Where does a warning message appear?
A - Upper area
B - Left memo area
C - Right memo area
What does a warning message replace?
A - Memos
B - Slats/Flaps position
C - Fuel indication.
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31 - INDICATING/RECORDING SYSTEMS
31-67-00 EIS: SYSTEM DISPLAY PRESENTATION
CONTENTS:
General
System Pages
Status Page
Permanent Data
System Page Logic
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EIS: SYSTEM DISPLAY PRESENTATION
In this module, parameters are given for a CFM engine
(For an IAE engine, EPR replaces N1).
　
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