Introduction; Supplemental Pilot’ S Manuals - Honeywell PRIMUS 1000 Pilot's Manual

1.

Introduction

This document describes the operation, components, typical flight
applications, and operating procedures for the PRIMUS
Integrated Avionics System shown as part of the cockpit layout in figure
1--1, in the Embraer 145 aircraft. Subsystems described in this manual
include:
R
PRIMUS 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
D
PRIMUS R 660 Weather Radar System
D
AA--300 Altimeter System.
D
The traffic alert and collision avoidance system (TCAS) is covered in
another manual. Optional systems, including the PRIMUS
Weather Radar Systems and the NZ--2000 Flight Management System
(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
Traffic Alert and Collision
Avoidance System (TCAS)
R
PRIMUS 880 Weather Radar
System
NZ--2000 Series Flight
Management System (FMS)
A28--1146--112--00
R II Integrated Radio System
Supplemental Pilot' s Manuals
Table 1--1
PRIMUSr1000 Integrated Avionics System
Publication No.
A28--1146--070
A28--1146--102
Refer to aircraft supplemental
flight manual for current
software versions.
R
1000
R 880
Introduction
1-1