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Figure 18--70--6 Traffic Alert and Collision Avoidance System --
MFD Indications 18--70--7
GROUND PROXIMITY WARNING SYSTEM
Figure 18--80--1 Ground Proximity Warning System
Interface Diagram 18--80--7
Figure 18--80--2 Ground Proximity Warning System -- Controls 18--80--8
Figure 18--80--3 Ground Proximity Warning System --
Windshear Detection and Alerting 18--80--9
Figure 18--80-- Ground Proximity Warning
System Status Page 18--80--12
WEATHER RADAR SYSTEM
Figure 18--90--1 Weather Radar System 18--90--2
Figure 18--90--2 Weather Radar System Control Panel 18--90--3
Figure 18--90--3 Weather Radar System -- MFD Indications 18--90--4
Figure 18--90--4 Weather Radar System -- MFD Indications 18--90--6
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NAVIGATION SYSTEMS
Table of Contents
Flight Crew Operating Manual MASTER
CSP A--013
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NAVIGATION SYSTEMS
Introduction
Flight Crew Operating Manual
CSP A--013
MASTER
1. INTRODUCTION
The aircraft is equipped with the following navigation systems:
S Flight Management System (FMS)
S VHF Navigation
S Automatic Direction Finder (ADF)
S Distance Measuring Equipment (DME)
S Air Traffic Control (ATC) Transponder System
S Traffic Alert and Collision Avoidance System (TCAS)
S Ground Proximity Warning System (GPWS)
S Enhanced Ground Proximity Warning System (EGPWS) <0040>
S Weather Radar System
Two separate VHF systems are provided for radio navigation and are designed and installed
so that the failure of one system does not prevent the operation of the other. Both systems
are connected to the onside and cross-side flight compartment displays and controls.
The navigation receivers are tuned by two radio tuning units and navigation data is
displayed on the primary flight displays (PFD’s) and multifunctional displays (MFD’s).
Frequency selection is accomplished through the two radio tuning units. In the event of a
failure of one or both radio tuning units, radio communication and navigation can be
controlled by the backup tuning unit.
Display control panels permit control over the multifunctional display formats, navigation
source and bearing source display.
Audio monitoring is provided by three audio control panels.
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Introduction
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NAVIGATION SYSTEMS
Flight Management System
Flight Crew Operating Manual
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MASTER
1. FLIGHT MANAGEMENT SYSTEM
The flight management system (FMS) is an integrated navigation system that provides
worldwide point--to--point and great circle navigation. The FMS can be used for:
S NAV Sensor Control (VOR/DME, AHRS)
S NAV Sensor Control (VOR/DME, AHRS and GPS) <0027><0047>
S NAV Sensor Control (VOR/DME, IRS and GPS) <0025><0027><0047>
S NAV Sensor Control (VOR/DME, and IRS) <0025>
S Dead Reckoning (DR)
S N1 Thrust Settings and Computation
S Secondary Radio Tuning
S MFD Control Menus
S Lateral Flight Plan Point--to--Point Navigation
S Flight Parameter Computations
S Fuel and Time Predictions
S Lateral Steering Command Outputs (flight control systems)
S Vertical Steering advisories
S Non-precision approaches
The FMS consists of a flight management computer, located in the avionics compartment,
and a control display unit located in the center console. The flight management computer
collects information from the navigation sensors and performs all computations, control and
command functions. The control display unit provides the pilot interface for data input and
control functions, and provides display of functions, modes and flight data. Pictorial data is
displayed on the multifunctional displays. <0050>
The FMS consists of two flight management computers, located in the avionics
compartment, and two control display units located in the center console. The flight
management computers collect information from the navigation sensors and perform all
computations, control and command functions. The control display units provides the pilot
interface for data input and control functions, and provides display of functions, modes and
flight data. Pictorial data is displayed on the multifunctional displays. <0024>
A portable data loader is used to transfer data to and from the FMS and maintenance
diagnostic computer (MDC).
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