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KDVT
WX
T5 . 0
LX
LUF
360
234
−40
−56
+12
−02
WX
T5 . 0
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_024a
UP Button DOWN Button
NOTE
The TCAS zoom window shall be restored after menu usage,
if the TCAS zoom window was previously in use.
Plan Format Map Format
NAVIGATION
Rev 3, Apr 25, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
17−10−15
TRAFFIC ALERT AND COLLISION AVOIDANCE SYSTEM (TCAS) (CONT'D)
TCAS Traffic Display (MAP Format)
The TCAS overlay is the default condition on the MFD during powerup.
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:
not shown − TCAS zoom window − TCAS overlay − TCAS zoom window − not shown
HDG
ETE
NM
N
20 20
KPHX
KPHX
TOC
TOC
KSRP
4000
FL180
KSRP
GSPD
TAT
TAS
SAT
30
6
33
3
−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
GF1710_025a
NOTE
TCAS STBY, TA ONLY, TCAS, TCAS FAIL (amber), TCAS TEST (red)
are available annunciations.
TCAS not shown TCAS overlay
NOTE
TCAS STBY msg displayed on MFD and PFD when TCAS is
selected with transponder in STBY.
NAVIGATION
Flight Crew Operating Manual Rev 3, Apr 25, 2005
CSP 700−5000−6
Volume 2
17−10−16
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
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual
CSP 700−5000−6
Volume 2
17−10−17
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
Flight Crew Operating Manual Rev 2A, Apr 11, 2005
　
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