PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-42
NOTES: 1. The APP and TERM annunciators are related to
FMS supplied approaches as described in table
4--12.
2. The INTEG annunciation indicates that the GPS
sensor does not meet the required integrity
calculations for the current phase of flight.
3. The MSG annunciator flashes until the FMS
condition is cleared.
FMS Annunciation Action
Full accuracy approach
(typically with stored
approaches)
APP Flashes for 10
seconds.
Normal RNAV accuracy
approach
APP Steady
annunciator
Enter the terminal area TERM Steady
annunciator
Approach and Terminal Annunciators
Table 4--12
D Weather Returns -- Weather radar returns can be displayed to
show the location of weather cells in relation to the range and
direction from the aircraft.
D WeatherRadar Range Ring Value -- Thehalfrangeringandvalue
are controlled by the weather radarcontroller. Normal range canbe
selected between 5--300 NM. FPLN (flight plan) range can be
selected up to 1000 NM.
D Weather -- When weather is selected on the DC, weather
information is displayed on the arc format. Each PFD can
independently display selected weather information. Depending on
the installed weather radar system, the mode annunciations
described in table 4--13aredisplayed to the left of the compassarc.
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