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ADF main page. During the test, the bearing pointer rotates 90 degrees
counterclockwise and the tone generator activates. The self-test is completed when the
bearing pointer returns to its original bearing.
Controls and Indicators
The figures that follow outline the controls and indications relevant to ADF
navigation. Refer to Chapter 6 Communications and Chapter 11 Flight Instruments for
additional information on the Radio Tuning Unit (RTU) and EFIS displays.
NAVIGATION SYSTEMS
17-70 For Training Purposes Only
Jan 04
P I LOT T R A I N I N G GU I D E
ADF Bearing Display (PFD)
Figure 17-50
No. 1 Bearing Pointer
Source Switches
Push to select No.1 source:
-OFF
-VOR 1
-ADF 1
-FMS 1
-(FMS 3)
Source indicated on
PFD/MFD.
BRT
N
33
30
W
24
E
6
3
20
10
10
20
260
220
240
280
000
900
800
100
200
19000
ADF1
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
ADF2
ALTS PATH GS
10000
NAV
SOURCE
FORMAT RANGE
BRG TERR WX TFC
PUSH
X -SI DE
PRIMARY FLIGHT DISPLAY
DISPLAY CONTROL PANELS
No. 1 Bearing Source
Indicator
Indicates navigation source
selected to obtain No. 1
bearing
No. 2 Bearing Source
Indicator
Indicates navigation source
selected to obtain No. 2
bearing
No. 1 Bearing Pointer
Indicates bearing to VOR,
ADF or FMS navigation
source selected on display
control panel. Pointer
removed if navigation source
failed
No. 2 Bearing Pointer
Indicates bearing to VOR,
ADF navigation
source selected on display
control panel. Pointer
removed if navigation source
failed
or FMS
VOR 1
ADF 1
FMS 1
FMS 3
VOR 2
ADF 2
FMS 2
FMS 3
VOR 1
ADF 1
FMS 1
FMS 3
VOR 2
ADF 2
FMS 2
FMS 3
PFD 1 PFD 2
BEARING POINTER
P604_17_029
No. 2 Bearing Pointer
Source Switches
Push to select No.2
(single/dual bar) source:
-OFF
-VOR 2
-ADF 2
-FMS 2
-(FMS 3)
Source indicated on
PFD/MFD.
NAVIGATION SYSTEMS
For Training Purposes Only
May 03
17-71
P I LOT T R A I N I N G GU I D E
ADF Bearing Display (MFD)
Figure 17-51
DBQ
ALO
CID
30
33 340 N
3
50
ADF 1 ADF 2
100
LX/WX+TRB+GCS G+3 USTB T+10.7
UTC 11:42 TAS 250 GS 254 SAT 12 C TAT -15 C
VOR1
CID
CRS 350
30.0NM
FMS2
VIN
DTK 030
104 NM
TTG :07 TTG :26 No. 2 Bearing
Pointer
No. 2 Bearing
Source
Indicator
No. 2 Bearing
Pointer
Indicator
HSI MODE NAV SECTOR MAP MODE
No. 1 Bearing
Pointer
No. 1 Bearing
Source
Indicator
No. 1 Bearing
Pointer
Indicator
340
ADF 1 ADF 2
WX
UTC 11:42 TAS 250 GS 254 SAT 12 C TAT -15 C
VOR1
CID
CRS 350
30.0NM
FMS2
VIN
DTK 030
104 NM
TTG :07 TTG :26
33
30
21
S
15
12
6
3
N
E
W
24
Cross-side
Course
Pointer
P604 17 030
NAVIGATION SYSTEMS
17-72 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
ADF Controls (RTU / Audio Control Panel)
Figure 17-52
Tone Key
ON
Selects tone circuit either on or
off.
– Superimposes an aural
signal on unmodulated carrier
waves to aid in precise
frequency selection.
1 - DME - 2
1 - NAV - 2 1 - MKR - 2
1 - ADF - 2
R/T
I/C
VOICE
BOTH
SPKR MASK
BOOM
EMER
NORM
PA
IDENT
DME-H
1/2
BRT
BRT
108.50
ACT PRE
109.00
NAV1
ACT PRE
123.45 134.92
COM1
195.5
ADF1 TCAS
AUTO REL
ATC
NEXT
PAGE 4567
STBY
TONE
IDENT
DME-H
1/2
BRT
BRT
MODE
238.0
ADF1
RETURN
TONE
TONE
TEST
ADF ANT
OFF ON
Top Level Page
ADF FREQ Readout
Indicates active ADF frequency
FREQ Change / Radio Page
Key
Tune
Radio Page
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