PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
5-5
Engine Instrument and Crew Alerting System (EICAS)
CONTROLS
EICAS Bezel Controller
The EICAS bezel controller is shown in figure 5--2. The rotary knob is
used to scroll the amber and cyan CAS messages.
AD--50957--R2@
EICAS Bezel Controller
Figure 5--2
Master Warning and Caution Annunciation Switches
The master caution and warning annunciation switches are located on the
glare shield adjacent to the display controllers (DC). These switches,
shown in figure 5--3, are used to acknowledge the display of a warning or
caution message. The messages are shown on the EICAS display.
AD--50958@
Master Warning and Caution
Annunciation Switches
Figure 5--3
The display of a warning crew advisory system (CAS) message causes
WARN to flash in red. A caution CAS message causes CAUT to flash
in amber.