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Electronic Display System (Eds) - Honeywell PRIMUS 1000 Pilot's Manual

Integrated avionics system for embraer 145
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PRIMUSr1000 Integrated Avionics System

ELECTRONIC DISPLAY SYSTEM (EDS)

The EDS includes the following components:
Display Symbol Generator (Inside each IAC)
D
Display Unit (DU) -- PFD, MFD, and EICAS
D
Bezel Controller
D
MFD/EICAS Bezel Controller
D
Display Controller
D
Data Acquisition Unit (DAU)
D
Reversionary Control Panel
D
EICAS Reversionary Panel
D
Remote Mounted Joystick (option).
D
In addition, the system outputs backup displays for the PRIMUS
RMUs as follows:
Navigation Display
D
Select engine instruments and data.
D
The EDS displays pitch and roll attitude, heading, course orientation,
flightpath commands, weather presentations, checklists, mode and
source annunciations, air data parameters, engine data, and fault
warning information. The displays are organized as follows:
Primary Flight Display -- The PFD integrates attitude, heading, air
D
data information, flight director modes and command bars, TCAS
resolution advisory (RA) commands, weather radar, and navigation
information.
Multifunction Display -- The MFD displays heading, navigation
D
maps, weather radar information, and checklist.
Engine Instrument and Crew Alerting System -- The EICAS
D
displays engine data, aircraft systems information, and warning/
caution/advisory messages.
The EDS displays essential display information from sensor systems,
automatic flight control, navigation performance, and caution--warning
systems in the pilot' s prime viewing area.
System Description
2-4
II
â
A28--1146--112--00

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