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000
900
800
100
200
21
S
20
10
10
20
2
R
T
160
140
120
100
400
500
600
700
800
1
2
4
1
2
4
E
6
30
20
10
10
260
220
240
280
300
400
500
600
1
2
4
1
2
4
Selected VS
VS Pointer
Selected VS Bug
VS Digital Readout
VS Advisory
TCAS Resolution
Advisory
VS Pointer
VS Digital Readout
FLIGHT INSTRUMENTS
11-32 For Training Purposes Only
May 03
P I LOT T R A I N I N G GU I D E
Navigation Displays
Vertical Deviation Display (GS, FMS and VNAV)
The ILS glideslope vertical deviation display appears when all conditions are met. Use
the on-side DCP to select FMS or LOC as the active NAV source. If deviation data
becomes invalid, this display is replaced with a red GS (flag) annunciation. When
conducting a back course approach, the scale displays without a pointer or flag
annunciation.
With LOC selected as the active NAV source, glideslope deviation is shown by the
position of a diamond-shaped pointer relative to the deviation scale. The scale consists
of two dots above and two dots below center. When the pointer moves to the top or
bottom of the scale, it changes to a half diamond (triangle) pointing in the direction of
the glideslope. A star against the same scale displays FMS glideslope vertical
deviation.
Marker Beacon Annunciation
Marker beacon status is annunciated by a cyan boxed “OM” (Outer Marker), yellow
boxed “MM” (Middle Marker), or by an empty white box (Inner Marker).
Marker Beacon Annunciations
Figure 11-17
Horizontal Situation Indicator (HSI) Function
The PFD has a Horizontal Situation Indicator located at the bottom center. It consists
of an airplane symbol and a compass rose. The compass rose is graduated in fivedegree
marks, with numeric labels at every 10 degrees and letters at N, E, S and W.
Airplane heading is read against the fore lubber line. Selected heading is set by the
HDG knob on the Flight Control Panel, which moves a heading bug on both PFDs
together. The digital value is displayed at the top left of the HSI while turning the
HDG knob and remains displayed for a period of three seconds once HDG knob
rotation is stopped.
Selected course VOR, LOC or desired FMS track is digitally presented, and also
displayed by an arrow. Course or track deviation is displayed against a scale centered
on the airplane. Two bearing pointers are available to display bearing to navigation
stations or a flight plan TO waypoint.
20
10
OM
P604_11_050
20
10
MM
20
10
FLIGHT INSTRUMENTS
For Training Purposes Only
Jan 04
11-33
P I LOT T R A I N I N G GU I D E
PFD HSI Display
Figure 11-18
N
S
15
12
E
6
3
20
10
10
20
T
200
180
160
140
200
300
400
500
600
ADF1
29.96 IN
1/2BNK HDG DR GS
AP
1
2
4
1
2
4
0.6
190
2
MDA 580
M.452
LOC1
CRS
8.
IOW
9H
071
LOC1
0.9
VT 170
VSPD
GS
FD2
2500
VS
ALTS
2000FT
P604_11_038
N
33
S
15
12
E
6
3
20
10
10
20
T
200
180
160
140 300
400
500
600
700
ADF1
29.96 IN
LOC1 DR GS
AP
1
2
4
1
2
4
173
2
MDA 580
M.452
LOC1
CRS
7.0H
IOW
071
ALTS PATH GS
2500
2100FT
N
33
S
15
12
E
6
3
20
10
10
20
2
R
T
160
140
120
100
800
700
600
500
400
RWY
ADF1
29.96 IN
1/2BNK LNV1 DR VGP
AP
1
2
4
1
2
4
0.7
128
1
MDA 840
M.452
FMS1
DTK
3.8NM
RW07
GPS APPR
MSG
072
LOC1
25
ADF2
ALTS PATH GS
900
HDG 072
1200FT
Full Scale
Deflection of Glideslope
Glideslope
Captured
FMS VNAV
Glide Path
Captured
Heading
　
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