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Brightness Knob
Line Select Keys
Function Keys
Data Entry Keys
Function Keys
Position Knob
Data Entry Keys
Line Select Keys
POS BRT
Vol. 1 18--20--4
NAVIGATION SYSTEMS
Flight Management System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Flight
Management
System
Control
Display Unit
CDU 1 DC BUS 1 1 H9
Vol. 1 18--25--1
NAVIGATION SYSTEMS
Global Positioning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. GLOBAL POSITIONING SYSTEM <1027>
The Global Positioning System (GPS) is a satellite navigation system that computes the
position of the aircraft relative to orbiting satellites. The GPS provides highly accurate
three-dimensional position, velocity and time information to the integrated avionics processor
system (IAPS).
The GPS consists of two antennas and two receivers. The antennas supply signals to their
respective receivers. The receivers process the signals and supply continuous navigation
updates to the inertial reference system (IRS) and to the flight management system (FMS).
The FMS uses the GPS and other available navigation and position sensors to provide
navigation, position information and guidance. <1212><1025><1027>
The FMS control display units provides the pilots with access to GPS data and control
settings. GPS information is displayed on the multifunctional displays. For more
information, refer to the FMS Pilot’s Guide. <1214>
Vol. 1 18--25--2
NAVIGATION SYSTEMS
Global Positioning System REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
Dual Global Positioning System <1025,1027,1212>
Figure 18---25---1
GPS
IAPS FMS
IRS
ADC 1 ALT AID
1 2 3
4 5 6
7 8 9
· 0 +/--
A
F
K
P
U
Z
B
G
L
Q
V
SP
C
H
M
R
W
DEL
D
I
N
S
X
/
E
J
O
T
Y
CLR
LABEL 1L
LABEL 2L
LABEL 3L
LABEL 4L
LABEL 5L
LABEL 6L
LABEL 1R
LABEL 2R
LABEL 3R
LABEL 4R
LABEL 5R
LABEL 6R
DATA1L DATA1R
DATA2L DATA2R
DATA3L DATA3R
DATA4L DATA4R
DATA5L DATA5R
DATA6L DATA6R
TITLE LINE 1 / 3
[ SCRATCHPAD ]
MSG EXEC
MOD BRT
MSG DIR
INTC
PREV
FPLN PAGE NEXT
PAGE
EXEC
MDCU
LEGS MENU
HOLD
VNAV
DEP
ARR
SEC
FPLN
RADIO
PERF
MFD
MENU
PROG
MFD
ADV
MFD
DATA
INDEX FIX 28 VDC
BUS 1
G--11
GPS
1
ANTENNA
28 VDC
BUS 2
G--11
GPS
2 GPS
ANTENNA
Vol. 1 18--25--3
NAVIGATION SYSTEMS
Global Positioning System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
A. System Circuit Breakers
SYSTEM SUB--SYSTEM CB NAME BUS BAR CB
PANEL
CB
LOCATION
NOTES
Global
Positioning
Receiver
GPS 1 DC BUS 1 1 G11
System
GPS 2 DC BUS 2 2 G11 <1027>
Vol. 1 18--25--4
NAVIGATION SYSTEMS
Global Positioning System Sep 09/02
Flight Crew Operating Manual
CSP C--013--067
THIS PAGE INTENTIONALLY LEFT BLANK
Vol. 1 18--30--1
NAVIGATION SYSTEMS
VHF Navigation REV 3, May 03/05
Flight Crew Operating Manual
CSP C--013--067
1. VHF NAVIGATION
There are two VHF navigation systems installed on the aircraft and are identified as
VHF/NAV 1 and VHF/NAV 2. The systems provide the following functions:
S VHF omnidirectional range (VOR)
S Localizer/glideslope (LOC/GS)
S Marker beacon (MB)
The VHF/NAV receivers are installed in the avionics compartment and contain the logic to
control the VOR/LOC receiver, glideslope receiver and the marker beacon receiver.
Frequency tuning and mode selection is done by two radio tuning units (RTU), a single
backup tuning unit or the FMS control display unit. The radio tuning units are the primary
radio communication system radio tuning source (Refer to Chapter 05--30--01 for additional
information).
The VOR/LOC receivers operate in the following frequency ranges:
S VOR frequencies -- All even frequencies from 108.00 to 111.90 MHz and all frequencies
from 112.00 to 117.95.
S LOC frequencies -- All odd frequencies from 108.10 to 111.95 MHz
　
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