Honeywell SPZ-8000 Maintenance Manual page 409

Digital automatic flight control system for gulfstream iv
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2.
D.
(2) Map (MAP)
Mode
The map mode is comprised of the follow.
.
120-Degree Compass Rose
Digital Heading Readout
. Magnetic/True Annunciation
. Heading Bug with Digital Readout
. Actual Track Line
. Wind Display in Vector or X-Y Formats
FMS 1/2 Source Annunciation
Bearing Pointers Circle/Diamond
.
Bearina Pointer Source Annunciation
ng funct"ons:
.
Flight-Management System (FMS) Mode Annunciations
.
FMS Waypoint, Airport, and Navaid Display Provisions
.
FMS Desired Track Lines
. Map/Weather Radar Range Rings
. Joystick Slewable Waypoints
Vertical Profile Presentation
. Weather Radar Display
(a)
(b)
(c)
Aircraft Symbol - The white aircraft symbol provides a visual
cue to aircraft position relative to actual heading and
selected heading.
Actual Track Vector - Actual track from the IRS is displayed
from the nose of the aircraft symbol to the map lubber line as
a magenta, dashed line. The selected IRS
source
provides
this
data
(Figure
212).
Heading
Display
- The
displayed
compass
rose
consists
of
an
expanded
120-degree
arc
that
is divided
into
5-degree
increments
and
labeled
every
30 degrees.
The
compass
rose
rotates
about
the
stationary
aircraft
symbol
to
provide
actual
heading
information.
The
compass indices and labels are
displayed
in white. The display is augmented with a white
digital readout of actual heading above the compass lubber-line
(Figure 212).
22-14-00
Page 235
Aug 15/91
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