Amber Fail Annunciation; Radar Tilt; Target Alert (Tgt); Mid--Right Side - Honeywell PRIMUS 1000 Pilot's Manual

- AMBER FAIL ANNUNCIATION -- When the amber FAIL
annunciation is displayed (optional PRIMUS
System only), selecting the test mode displays the weather radar
system fault code data in place of the tilt information. Refer to the
PRIMUS
â
information on fault code interpretation.
NOTE:
- RADAR TILT -- Radar tilt is displayed in the form of a cyan number
with + (up) or -- (down) sign. If attitude compensated tilt (part of
the optional PRIMUS
A is displayed in this location.
- TARGET ALERT (TGT) -- TGT alert is shown above the tilt angle.
It overrides the display of variable gain. When armed, TGT is
displayed in green. When activated, TGT turns amber and
flashes.
- VARIABLE GAIN -- When radar gain is selected as a variable, it
displays a value for radar gain in proportion to the radar controller
gain setting.

Mid--Right Side

D
- MAP DESIGNATOR (if FMS is installed) -- This section of the
display, shown in figure 4--39, shows the cyan designator bearing
and distance position data. The designator is always cyan.
A28--1146--112--00
880 Weather Radar maintenance handbook for specific
The PRIMUS 660 and optional PRIMUS
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can also display plain English fault displays when the
TEST mode is selected.
880 Weather Radar only) is engaged, an
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PRIMUSr1000 Integrated Avionics System
â
Electronic Flight Instrument System (EFIS)
880 Weather Radar
880 radars
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4-71