Honeywell SPZ-8000 - Introduction

SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
1-1
Introduction
1. 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:
D 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
R
650 or PRIMUS
R
870 Weather Radar (WX) System
D LASEREF
R
II or LASEREF
R
III Inertial Reference System (IRS)
D Lightning sensor system (LSS) (optional)
D Traffic alert and collision avoidance system (TCAS) (optional)
D Enhanced ground proximity warning system (EGPWS) (optional)