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Volume 2
17−00−4
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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 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
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
and/or receive communication/information from NAV, ADF, DME and MB. For more information, see
Chapter 6 COMMUNICATIONS.
NAV1, NAV2, NAV3 (if installed)
ADF1, ADF2
DME1, DME2
Receive Buttons
MKR Button
Controls onside
marker
beacon receiver sensitivity.
MUTE Button
Used to temporarily silence the
marker beacon audio (nonlatching).
GF1710_002
NAVIGATION
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
CSP 700−5000−6
Volume 2
17−10−2
RADIO MANAGEMENT UNIT (RMU)
The RMUs, located on the pedestal are used for frequency and mode control. With the exception of a
DME indicator, all navigation data is displayed on EFIS.
Each RMU controls the following functional modules:
· An Integrated Navigation Unit, incorporating a VHF NAV Transceiver Module, a DME
Transceiver Module and an ADF Receiver Module.
· An Integrated Communication Unit, incorporating a VHF COM Transceiver Module, a Mode S
Transponder Module and a TCAS Interface Module.
Any selectable parameter, such as VOR or ADF frequency, may be changed by pressing the
corresponding line select key, then by rotating the tuning knobs to set a desired value. For more
information, see Chapter 6 COMMUNICATIONS.
Pilot’s Windows
− COM1
− NAV1
− ATC/TCAS
− ADF1
− TCAS DSPY 1
− HF1
Copilot’s Windows
− COM2
− NAV2
− ATC/TCAS
− ADF2
− TCAS DSPY 2
− HF2
Main Tuning Page
Transfer Key
Line Select Keys
Function Keys
RMU 1 (Pilot’s)
Tuning Knobs
GF1710_003
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
NB
MEMORY−4
1 ATC ALT
ALT:
121.82
118.02
MEMORY−1
117.45
110.00
1200
ADF
1799.5
REL
NORMAL 15600
15423
LV
NAVIGATION
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
17−10−3
VHF NAVIGATION RECEIVERS
The two VHF Navigation receivers (NAV 1 and NAV 2) provide VHF omnirange (VOR), Localizer
(LOC), Glideslope (GS) and Marker Beacon (MB) signals to the navigation systems and flight crew.
The navigation receivers operate in the following ranges:
System Frequency Range Channel Spacing
VOR 108.00 to 117.9 MHz 50 kHz (160 chan)
LOC 108.10 to 111.95 MHz 50 kHz (40 chan)
GS 329.15 to 335.00 MHz 150 kHz (40 chan)
MB 75.00 MHz Preset
Frequency selection is through radio tuning units located on the pedestal.
COM1 NAV1
ATC/TCAS ADF1
TCAS DSPY 1 HF1
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