Honeywell PRIMUS 1000 - Introduction

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
1-1
Introduction
1. Introduction
This document describes the operation, components, typical flight
applications, and operating procedures for the PRIMUS
R
1000
IntegratedAvionicsSystemshown aspartof thecockpitlayout infigure
1--1, in the Embraer145 aircraft. Subsystems describedin this manual
include:
D PRIMUS
R
1000 Flight Guidance System (FGS)
D Electronic Display System (EDS)
D ADZ--850 Air Data System (ADS)
D AHZ--800 Attitude and Heading Reference System (AHRS)
D SRZ--850 PRIMUS
R
II Integrated Radio System
D PRIMUS
R
660 Weather Radar System
D AA--300 Altimeter System.
The traffic alert and collision avoidance system (TCAS) is covered in
another manual. Optional systems, including the PRIMUS
R
880
WeatherRadarSystemsandtheNZ--2000FlightManagementSystem
(FMS) are described in separate pilot’s manuals. These manuals are
listed in table 1--1. The equipment covered in this manual is listed in
table 1--2.
System Publication No.
Traffic Alert and Collision
Avoidance System (TCAS)
A28--1146--070
PRIMUS
R
880 Weather Radar
System
A28--1146--102
NZ--2000 Series Flight
Management System (FMS)
Refer to aircraft supplemental
flight manual for current
software versions.
Supplemental Pilot’s Manuals
Table 1--1