Honeywell PRIMUS 1000 - Amber Fail Annunciation; MID-Right Side; Radar Tilt; Target Alert (Tgt)

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-71
Electronic Flight Instrument System (EFIS)
- AMBER FAIL ANNUNCIATION -- When the amber FAIL
annunciation is displayed (optional PRIMUS
â
880 Weather Radar
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
880 WeatherRadarmaintenance handbook for specific
information on fault code interpretation.
NOTE: ThePRIMUS
â
660andoptionalPRIMUS
â
880radars
can also display plain English fault displays when the
TEST mode is selected.
- RADARTILT--Radartiltisdisplayedintheformofacyannumber
with + (up) or -- (down) sign. If attitude compensated tilt (part of
the optional PRIMUS
â
880 WeatherRadar only) is engaged,an
A is displayed in this location.
- TARGETALERT(TGT)--TGTalert isshownabovethetiltangle.
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
displaysavalueforradargaininproportiontotheradarcontroller
gain setting.
D Mid--Right Side
- MAP DESIGNATOR (if FMS is installed) -- This section of the
display,showninfigure4--39,showsthecyandesignatorbearing
and distance position data. The designator is always cyan.