Introduction; The Primus R 1000 Integrated Avionics System - Honeywell PRIMUS 1000 Pilot's Manual

1.

Introduction

THE PRIMUS
This document describes the components, operating procedures, and
typical flight applications for the PRIMUS
System in the Cessna Citation Encore (Model 560, SN 0539 and
above). Figure 1–1 shows a layout of the Encore cockpit.
Subsystems described in this manual include:
R
D
PRIMUS 1000 Integrated Avionics System's flight control system
D
Electronic flight instrument system (EFIS)
D
Air data system (ADS)
R
D
PRIMUS 660 Digital Weather Radar System.
R
The PRIMUS
R
PRIMUS II Integrated Radio System are described in separate
manuals.
Traffic alert and collision avoidance system (TCAS) and enhanced
ground proximity warning system (EGPWS) are optional subsystems
that interface with the PRIMUS
Table 1–1 lists the cockpit–mounted and remote–mounted equipment
described in this manual.
Model
Cockpit Mounted
DU–870 Display Unit (DU)
BL–870 Primary Flight Display (PFD)
Bezel Controller
BL–871 Multifunction Display (MFD)
Bezel Controller
A28–1146–134
REV 1 Jan/03
R
1000 INTEGRATED AVIONICS SYSTEM
880 Weather Radar System (optional) and the
R
Unit
Equipment List
Table 1–1 (cont)
R
PRIMUS 1000 Integrated Avionics System
R
1000 Integrated Avionics
1000 Integrated Avionics System.
Qty
3
2
1
Part No.
7014300–901
7014331–931
7014332–841
Introduction
1-1