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LX
LUF
+10
KLAX
−04
TERR
OFF
345
234
−40
−56
1+36
12.5
KDVT
KDVT
TRU FMS1
N
50 50
KPHX
TOC
KSRP
KLAX
ETE
NM
6
HDG
ETE
NM
FMS1
N
50 50
KPHX
TOC
KSRP
6
Range Arc
TCAS Zoom
GSPD
TAT
TAS
SAT GSPD
TAT
TAS
SAT
30
6
33
3
GF1710_024
UP Button DOWN Button
NAVIGATION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−10−16
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D)
TCAS Traffic Display (MAP Format)
TCAS display can also be enabled on MAP format and is selected through the TCAS button on the
MFD control panel. TCAS cannot be displayed on PLAN format.
315
TERR
OFF
−40
LX
360
LUF
WX
234
−56
1+36
12.5
KDVT
KDVT
KDVT
4000
345
FMS1
The button sequence is as follows:
OFF − TCAS − TCAS MAP − OFF
HDG
ETE
NM
N
20 20
KPHX
KPHX
TOC
TOC
KSRP
4000
FL180
KSRP
GSPD
TAT
TAS
SAT
30
6
33
3
GF1710_025
−04
+12
315
LX
360
LUF
WX
1+36
12.5
KDVT
KDVT
KDVT
4000
GSPD
TAT
TAS
−40
234
345
SAT −56
TERR
IOFF
HDG FMS1
ETE
NM
N
20 20
KPHX
KPHX
TOC
TOC
KSRP
4000
FL180
KSRP
+10
30
6
33
3
NAVIGATION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−10−17
TCAS SCHEMATIC
FLIGHT
DATA
RECORDER
ADVISORY
DISCRETES
ATC
TRANSPONDER
1, 2
RADIO
ALTIMETER
SYSTEM
OMNI−DIRECTIONAL
ANTENNA
AUDIO
INTEGRATING
SYSTEM
IAC 1, 2, 3
DIRECTIONAL
ANTENNA
TCAS
RECEIVER/TRANSMITTER WOW
SYNTHESIZED
VOICE
TA/RA DISPLAY DATA 1
TA/RA DISPLAY DATA 2
DAU 4
EICAS
ADC 1, 2, 3
AIR DATA COMPUTER
SYSTEM
ALT>15000FT
VHF COM SYSTEM
GF1710_026
NAVIGATION
Flight Crew Operating Manual REV 41, Jul 08, 2004
CSP 700−6
Volume 2
17−10−18
AUTOMATIC DIRECTION FINDER (ADF)
The two ADF receivers (ADF1 and ADF2) provide relative bearing between the airplane and a
selected ground station for display on the PFDs. ADF operations are controlled by the adjacent line
select keys and the tuning knobs. For more information, see Chapter 6 COMMUNICATIONS.
NB
6
NORMAL
1 ATC ALT ADF
LV
118.02
RANGE:
ATC/TCAS ADF1
TCAS DSPY 1 HF1
COM1 NAV1
121.82 108.30
1200 1799.5
15423
15600
DME IZZ
111.90
GF1710_027
The receivers operate in the following modes and are controlled by the adjacent line select keys or
the tuning knobs.
118.02
RANGE:
NB
6
NORMAL
1 ATC ALT
LV
ADF
ATC/TCAS ADF1
TCAS DSPY 1 HF1
COM1 NAV1
121.82 108.30
1200 1799.5
15423
15600
DME IZZ
111.90
GF1710_028
VOICE Maximum audio clarity and
fidelity, no bearing.
BFO ADF adds a beat frequency
oscillator (BFO) for detection of
ADF Bearing determination. Some
loss of received audio range
and sensitivity.
ANT Maximum sensitivity and range.
Aural beacon ident and voice
only, no bearing.
cw signals.
NAVIGATION
REV 41, Jul 08, 2004 Flight Crew Operating Manual
CSP 700−6
Volume 2
17−10−19
BEARING (BRG) SOURCE
Bearing information, VOR1, ADF1 or FMS1 and bearing information VOR2, ADF2 or FMS2, is
selected on either the pilot’s and/or the copilot’s PFD control panel, located on the glareshield.
VOR1
ADF 1
FMS 1
VOR2
ADF 2
FMS 2
NOTE
Pushing BRG button (s) will
toggle the following in sequence:
− VOR
− ADF
− FMS
− Blank
GF1710_029
PFD Control Panel
HDG
030
VOR1
CRS
360
VOR 2
3
N
6
33
E
W
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