Honeywell PRIMUS 1000 Pilot's Manual page 114

Integrated avionics system for the citation encore
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D
Same Attitude Source – If both pilots are using normal on–side
attitude sources, the attitude source is not displayed. When a new
attitude source is selected, it is annunciated in white. If both pilots
have selected the same attitude source, it is annunciated in
on both PFDs.
NOTE:
If both pilots have selected the cross–side attitude source,
the attitude source is annunciated in white.
D
Common Symbol Generator – When the reversionary mode and
one symbol generator are driving both displays, an
indicates the information source.
upper left corner next to the sphere, indicating which symbol
generator is the source.
D
Below Minimums – When the radio altitude is within +100 feet of
minimums, a white box appears in the upper left of the altitude
display. When at or below minimums,
D
Same Air Data Source – Under normal conditions, the on–side
source annunciator is not displayed. When both pilots have selected
the same source, an
upper left corner of the PFD.
A28–1146–134
REV 1 Jan/03
R
PRIMUS
SG1
MIN
amber
source annunciator appears in the
Electronic Flight Instrument System (EFIS)
1000 Integrated Avionics System
amber
or
SG2
is displayed in the
is displayed in the box.
amber
warning
3-77

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