Honeywell SPZ-8000 Maintenance Manual page 421

Digital automatic flight control system for gulfstream iv
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2.
D.
(4)
(a) Aircraft Symbol - The white aircraft
cue to aircraft position relative to
and selected course.
symbol provides a visual
heading, selected heading,
(b) Heading Display - The displayed compass rose rotates through
360 degrees of aircraft heading, is marked in 5-degree
increments, and is 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 217).
(c) Heading MAG/TRU Annunciations - TheMAG/TRU annunciation
operation and location is identical to the MAP mode (paragraph
2.D.(2)(d))
as
previously discussed.
(d) Heading Bug with Readout - The heading bug operation and
identification is as previously discussed in the MAP mode
(paragraph 2.D.(2)(e)).
(e) Wind Display - The wind format is displayed in white in either
an X-Y (Figure 217) or vector (Figure 218) format as selected
through the display controller. The wind display abeams the
aircraft symbol to the left, above the heading select digital
readout. This data is displayed from the selected ND FMS
source.
22-14-00
Page 247
Aug-15/91
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