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DESCRIPTION
Mode 2 − Excessive Terrain Closure Rate 17−10−34
Mode 3 − Altitude Loss After Takeoff
17−10−36
Mode 4 − Unsafe Terrain Clearance 17−10−37
Mode 5 − Descent Below Glideslope 17−10−40
Mode 6 − Callouts 17−10−40
Mode 7 − Windshear Warning 17−10−42
Windshear Flight Director Mode Annunciations 17−10−43
Windshear Escape Guidance 17−10−43
Terrain Awareness Alerting 17−10−44
Annunciations 17−10−47
Terrain Clearance Floor (TCF) 17−10−47
EGPWS Schematic 17−10−48
Flight Management System (FMS) 17−10−49
FMS Display Unit 17−10−49
Annunciators 17−10−51
Brightness Control 17−10−54
Line Select Keys 17−10−55
Legend 17−10−56
Function Keys 17−10−56
Scratchpad 17−10−62
Alphanumeric Keys 17−10−62
Clear (CLR) Key 17−10−62
Delete (DEL) Key 17−10−62
FMS Update 17−10−63
Position Initialization (POS INIT) 17−10−64
Flight Plan 17−10−65
Flight Plan (stored) 17−10−65
Flight Plan (Manual) 17−10−66
Departures 17−10−67
Performance Initialization 17−10−69
FMS Schematic 17−10−70
Navigation Display Unit (if installed) 17−10−71
ON Key 17−10−71
Data Entry Keyboard 17−10−72
Special Function Keyboard 17−10−72
System Select Keys 17−10−72
Data Select Keyboard 17−10−73
Displays 17−10−74
Fault Annunciator 17−10−74
NDU Update 17−10−75
Power On 17−10−75
NAVIGATION
TABLE OF CONTENTS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−00−2
Page
DESCRIPTION
Test 17−10−75
Position Entry 17−10−76
NDU Schematic 17−10−78
Global Positioning System (GPS) 17−10−79
Modes of Operation: 17−10−79
GPS Access 17−10−80
GPS Status 17−10−80
GPS Schematic 17−10−82
Navigation System EICAS Messages 17−10−83
EMS CIRCUIT PROTECTION
CB − NAV System 17−20−1
NAVIGATION
TABLE OF CONTENTS
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−00−3
Page
NAVIGATION
TABLE OF CONTENTS
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−00−4
THIS PAGE INTENTIONALLY LEFT BLANK
GENERAL
The navigation system includes those units and components which provide the following data to the
flight crew:
· Position Systems − Dual VHF navigation systems (providing VOR, LOC, GS and MB signals),
FMS, ADF, DME and ATC transponder systems.
· Independent Position Systems − Weather radar, TCAS.
The navigation receivers are tuned by the Radio Management Units (RMU) and navigation data is
displayed on the PFDs and MFDs.
MFD control panels (located on the pedestal) permit control over MFD format. PFD control panel
(located on the glareshield) permits control over navigation source and bearing source display.
The partial compass rose on the PFDs echos the MFD bearing information for the navigation aid
selected on the PFD control panel and tuned by the RMUs.
VOR, DME, ADF and MB audio selection and monitoring is provided at the audio control panels
(located on the pedestal).
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−4
1 TA/RA
RANGE:
121.82
118.02
MEMORY−1
117.45
110.00
1200
ADF
1799.5
6
NORMAL 15600
15423
LV
FMS
RMU
PFD Control Panel
MFD Control Panel
Audio Control Panel
GF1710_001
ACTIVE FLT PLAN
ORIGIN
KPHX
055 154 NM CLS
1/4
SJN 00 + 21 .75M/1 0 0 0 0 A
059 121 NM
00 + 15 .75M/FL350
T.0.INIT
ABQ
DEPARTURE
0
0
COMPARE FUEL QUANTITY
RAD BARO
MINIMUMS NAV SCR BARO SET
PUSH STD
IN HPa
NAVIGATION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−10−1
AUDIO CONTROL PANEL
The audio control panels, located on the pedestal, are used to select radios or PA for transmission
　
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