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arrow pointer and the BRG2 pointer is a double
cyan line with an open arrow pointer. If a
bearing pointer is selected for display, a white
circle appears in the center of the compass card
to separate the bearing pointer(s) from the CDI.
Bearing pointers never override the CDI.
The BRG1 window is at the lower left corner
of the compass display and the BRG2 window
is at the lower right corner of the compass
display. Each window indicates:
• Distance to the station/waypoint
• Station/waypoint identifier (or frequency)
• Source for the bearing (NAV1, NAV2,
GPS, or automatic direction finder [ADF])
• Arrow icon matching the bearing pointer
OBS Mode
OBS mode is useful for holding and for intercepting
a course to a waypoint. Enabling
omni bearing selector (OBS) mode is useful
for holding and for intercepting a course to
a waypoint. OBS mode with the OBS softkey
suspends the automatic sequencing of
waypoints in a GPS flight plan, but retains
the active-to waypoint as the navigation reference
even after passing the waypoint. When
OBS is disabled by pressing the OBS softkey
again, the GPS returns to normal opera
t i o n , with automatic sequencing of
waypoints. OBS mode also allows a desired
course TO/FROM a waypoint to be set (with
a CRS knob); pressing the CRS knob recenters
the CDI and returns the course point TO
the waypount bearing.
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S
15
12
N
33
0
VOR2
158°
21
S
15
3
N
33
GPS ENR
360°
LOI
12
E
30
W
GPS TERN
283°
SUSP
21
S
15
3
N
33
LOC1
180°
Figure 16-20. Navigation Sources
SUSPend Mode
SUSPend mode is automatically activated
when appropriate during approach operations.
As the aircraft crosses the missed approach
point (MAP), automatic approach waypoint sequencing
is suspended. SUSP appears on the
HSI (to the lower right of the aircraft symbol)
in place of OBS and the OBS softkey label
changes to SUSP. Also suspends when on vectors
to an approach or while in a hold.
Glide Slope
During precision approach operations, glideslope
position is indicated by a diamond on a
glide-slope scale, which is on the left edge of the
altitude display (Table 16-4 and Figure 16-21).
Marker Beacon
When passing over a marker beacon, a small
box appears at the top left of the altitude display
(Figure 16-22). The box appears differently
for different beacons:
• Outer marker—Blue box with black
letter “O”
• Middle marker—Amber box with black
letter “M”
• Inner marker—White box with black
letter “I”
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1800
0
1700
1600
1400
1300
15 20
40
00
G
M
29.92IN
MARKER
BEACON
ANNUNCIATION
GLIDE-SLOPE
INDICATOR
Figure 16-21. Glide-Slope Indicator
INDICATOR G G V
BUG ICON
(GLIDESLOPE) (GLIDEPATH) (VERTICAL DEVIATION)
Table 16-4. VERTICAL DEVIATION
DISPLAY
FLIGHT PHASE ANNUNCIATION AUTO CDI SCALING
DEPARTURE DPRT 0.3 NM
OCEANIC OCN 2.0 NM
ENROUTE ENR 2.0 NM
TERMINAL MODE TERM 1.0 NM
APPROACH LNAV 1.0 NM DECREASING TO
(NON-PRECISION) 350 FT DEPENDING ON
VARIABLES
APPROACH LNAV +V 1.0 NM DECREASING TO
(VERTICAL 350 FT DEPENDING ON
GUIDANCE) VARIABLES
APPROACH L/V NAV 1.0 NM DECREASING TO
(LNAV/VNAV) 350 FT DEPENDING ON
VARIABLES
APPROACH LPV 1.0 NM DECREASING TO
(LPV) 350 FT DEPENDING ON
VARIABLES
MISSED APPROACH MAPR 0.3 NM
Table 16-3. Flight Phases and CDI Scaling
Vertical Speed
Vertical Speed Indication
The vertical speed indication is through a
fixed index scale on the right side of the altitude
scale, and through a moving black pointer
box with white digits indicating current vertical
speed (when greater than 100 fpm up or
down) (Figure 16-23). A negative number indicates
descent. The vertical speed indication
displays in 50-foot increments.
Vertical Speed Reference Box and
Bug
A reference vertical speed set through the
AFCS indicates on the vertical speed scale by
a notched cyan bug on the scale and a vertical
speed indicated with cyan digits in a box at the
top of the scale.
INSET MAP
The pilot may activate a small moving map or
　
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