Table of Contents
R
PRIMUS
1000 Integrated Avionics System
D
Aircraft Symbol – The white aircraft symbol shows the aircraft's
position relative to the flight plan data. It is always oriented vertically.
D
Designator Range and Bearing – Bearing and distance from the
designator's anchor point to its present position are displayed in
cyan
in the lower right part of the MFD.
D
TAS (True Airspeed) Display – True airspeed is displayed in
digits on the lower right of the MFD with a white TAS label. It is
calculated by the MADC.
D
GSPD (Groundspeed) Display – Groundspeed is displayed in
magenta
digits below the TAS display. The GSPD label is white.
Groundspeed is calculated by the FMS.
D
Designator LAT/LON Annunciator – The designator's latitude
and longitude are displayed in
of the MFD, with a resolution of 0.1 minutes.
D
Variable Gain Display – When radar gain is selected as variable,
it displays
VAR
D
Radar Tilt Display – Radar tilt is displayed on line 3 of the 4–line
display area as a
is engaged, an
D
Weather Radar Mode Annunciator – Described in Table 3–26,
these modes are annunciated on the lower left of the MFD. The
number shown in the line column indicates the position of the
annunciator within the boxed 4–line display area.
Annunciator
WAIT
STBY
FSBY
TEST
FAIL
RCT
Weather Radar Mode Annunciators on MFD
Electronic Flight Instrument System (EFIS)
3-84
cyan
on line 2 of the 4–line display area.
green
number with
A
follows the number.
Line
1
Power–up, about 1 minute
1
Normal standby
1
Forced standby (weight–on–wheels)
1
Test mode and no faults
1
Test mode with faults detected
1
Normal weather with REACT (rain echo
attenuation compensation technique)
Table 3–26 (cont)
on the lower middle–left portion
+
–
(up) or
(down). If autotilt
Mode
green
A28–1146–134
REV 1 Jan/03
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