PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
5-23
Engine Instrument and Crew Alerting System (EICAS)
The CAS display is in the upper right half of the EICAS display. The color
convention and displayed priority for messages on the CAS display are
defined in table 5--17.
Color
Message
Red
Warnings (top of the message stack)
Amber
Cautions (middle of the message stack)
Cyan
Advisories and status (bottom of the message
stack)
Message Color Conventions
Table 5--17
Amber and cyan messages can be scrolled off the display with the
EICAS bezel controller knob. The quantity of scrolled messages is
displayed at the bottom of the CAS area.
NOTES:
1. Red (warning) messages cannot be scrolled.
2. No messages can be scrolled if any amber messages
that are displayed have not been acknowledged
through the caution annunciator.
3. The END message cannot be scrolled off the display.
CAS Messages
WARNING MESSAGES (RED)
When a red message becomes active, the following indications are
given:
D
Red message displayed flashing on the CAS display
D
Red WARN annunciator on the warning/caution annunciator is lit.
When the warning/caution annunciator/pushbutton is pushed on the
warning panel, the red annunciator is extinguished and the red
message is displayed steadily on the CAS display.
If there are red messages already on the CAS display when a new red
message becomes active, the new message is put at the top of the red
message stack. Messages are removed from the CAS display when the
condition causing the message is remedied. Table 5--18 lists the
warning messages.