Introduction - Honeywell SPZ-8000 Pilot's Manual

Digital integrated flight control system
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Introduction

This manual describes the operation, components, typical flight
applications, and operating procedures for the Honeywell SPZ--8000
Digital Integrated Flight Control System (DIFCS) as factory installed in
the CANADAIR Challenger CL--601--3A and CL--601--3R aircraft.
Subsystems covered in this manual include the following:
Air data system (ADS)
D
Electronic flight instrument system (EFIS)
D
Multifunction display (MFD) system
D
Dual flight guidance system (FGS)
D
Flight management system (FMS)
D
Radio altimeter system
D
PRIMUS
650 or PRIMUS
R
D
LASEREF
II or LASEREF
R
D
Lightning sensor system (LSS) (optional)
D
Traffic alert and collision avoidance system (TCAS) (optional)
D
Enhanced ground proximity warning system (EGPWS) (optional)
D
A28--1146--055
REV 2
SPZ--8000 Digital Integrated Flight Control System
870 Weather Radar (WX) System
R
III Inertial Reference System (IRS)
R
Introduction
1-1

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