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1 - DME - 2
1 - NAV - 2 1 - MKR - 2
1 - ADF - 2
R/T
I/C
VOICE
BOTH
SPKR MASK
BOOM
EMER
NORM
PA
VHF 3 1 - HF - 2 INT/SVC
Navigation Source Knob
Rotate to select navigation
source:
-(FMS 3)
-FMS 1
-VOR 1 / LOC 1
-OFF
-VOR 2 / LOC 2
-FMS 2
-(FMS 3)
VOICE/BOTH Switch
VOICE
BOTH
– CW signals are
filtered out of VOR, ILS
and ADF
– Station
identification and voice
signals are audible
Navigation Receive
Switches
Press to monitor
respective navigation
receiver.
Press again to deselect.
Any number of audio
sources can be monitored
at the same time.
Rotate to adjust volume.
Marker Beacon Receive
Switches
3000 Hz
1300 Hz
400 Hz
Press to monitor marker
beacon audio signals:
- inner marker
- middle marker,
and
- outer marker
Press again to deselect.
Rotate to adjust volume.
Marker-receive sensitivity
and output volume are set
by MKR sens mode, on
NAV main page of RTU
AUDIO CONTROL PANEL
DISPLAY CONTROL PANEL
P604_17_024
Cross-side Course
Selection Pushbutton
Used only on MFD. In HSI
and NAV sector formats,
displays currently selected
cross-side course, along
with course deviation and
course labeling from
cross-side. Selection does
not remove existing data
from MFD. Push on/push
off.
NAVIGATION SYSTEMS
For Training Purposes Only
Jan 04
17-59
P I LOT T R A I N I N G GU I D E
Flight Control Panel Course Knobs
Figure 17-43
PFD Navigation Display
Figure 17-44
FLC
SPEED
NAV HDG APPR
1/2 BANK
HDG
B/C
ALT
CRS1 ALT CRS2
FD VS FD
VNAV
DOWN
UP
XFR
TURB AP DISC
AP ENG
PUSH
DI
RECTIAS/MACH
PUSH
SYNC
PUSH
CANCEL
PUSH
DIRECT
FLIGHT CONTROL PANEL
Course
Knob
Course
Knob
P604_17_089
N
33
30
W
24
E
6
3
VOR1
VOR1
CRS
29.4NM
VIN
310
VOR2
BRT
N
33
30
W
24
E
6
3
20
10
10
20
260
220
240
280
000
900
800
100
200
19000
VOR1
30.15 IN
HDG DR VS
AP
1
2
4
1
2
4
1.9
250
8
M.452
VOR1
CRS
29.4NM
VIN
310
VOR1
3.0
30
VOR2
ALTS PATH GS
10000
OM
Bearing
Source
Indicator
Station
Identifier
Course
Display
Navigation
Source
Indicator
Bearing
Pointer
Indication
Course
Pointer
Bearing
Pointers
Lateral
Deviation
Scale
Lateral
Deviation
Bar
Bearing
Pointer
Indicators
ILS G/S
Vertical
Deviation
Pointer
Vertical
Deviation
Scale
Vertical Deviation Display (G/S or FMS)
ILS G/S appears when all necessary conditions are met.
If deviation data becomes invalid, display replaced by red
GS flag. When back course selected, scale is presented
without pointer or flag annunciation. When pointer moves
to top or bottom of the display, diamond pointer changes to
a ½ diamond pointing in the direction of the deviation.
Excessive deviation causes the pointer to flash (amber).
Marker Beacon Indicator
Colored box is displayed as airplane passes over
applicable marker beacon and flashes to indicate:
-inner or airway marker (BLANK)(white)
-middle marker (MM) (yellow)
-outer marker (OM) (cyan).
FMS VNAV
Deviation
Pointer
P604_17_025
NAVIGATION SYSTEMS
17-60 For Training Purposes Only
Sept 04
P I LOT T R A I N I N G GU I D E
MFD Navigation Display
Figure 17-45
BRT
VOR1 VOR2
WX
UTC11 : 42
TTG11 : 07
VOR1
CID
CRS 350 FMS2 DTK 030
TAS 250 GS 240 SAT 12C TAT–15C
TGT
30.0NM VIN 104.7NM
TTG 11: 26
N
33
30
W
24
21
S
15
12
E
6
3
340
MULTIFUNCTION DISPLAY
PILOT'S AND COPILOT'S INSTRUMENT PANELS
MULTIFUNCTION DISPLAY
PILOT'S AND COPILOT'S INSTRUMENT PANELS
No. 1 Bearing Pointer
Pointer removed if bearing source failed.
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