PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
Engine Instrument and Crew Alerting System (EICAS)
5-6
DISPLAYS
EICAS Display
The engine instrument and caution advisory display is divided into five
functional areas, as shown in figure 5--4. The areas include the
following:
D
Primary Engine Display
D
Crew Alerting System
D
Gear/Flaps/Spoiler
D
Cabin Pressurization and Auxiliary Power Unit (APU) Status
D
Pitch/Roll/Yaw Trim Display.
PRIMARY
ENGINE
DISPLAYS
CREW
ALERTING
SYSTEM
GEAR/
FLAPS/
SPOILER
CABIN
PRESSURIZATION
AND
APU STATUS
PITCH/ROLL
YAW
TRIM
DISPLAY
AD--50959--R1@
EICAS Display Functional Divisions
Figure 5--4