PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-48
ALTIMETER DISPLAY
The altimeter display is shown in figure 4--25. Refer to the figure for the
location of annunciations described in the paragraphs that follow.
BAROMETRIC
ALTIMETER DISPLAY
IN
HPA
INCHES Hg
HECTOR PASCALS
AD--50919--R2@
145
00
29.92 IN
00
20
80
14500
143
14000
00
20
80
4500
43
50
00
29.92 IN
ALTITUDE ALERT
PRESELECT DISPLAY
CURRENT ALTITUDE
DIGITAL DISPLAY
LOW ALTITUDE
AWARENESS
SYMBOL
ALTITUDE SELECT
BUG
ALTITUDE TREND
VECTOR
ALTITUDE ANALOG
SCALE
ALTITUDE REFERENCE
LINE
Altimeter Display
Figure 4--25