Honeywell PRIMUS 1000 - Page 103

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
4-63
Electronic Flight Instrument System (EFIS)
3030
3030
3
00
M
AD--50929--R1@
PFD Caution Indications for Vertical and
Course Deviation
Figure 4--35
D Autopilot Status Annunciations -- These annunciations display
the engage status of the autopilot. The annunciation is displayed
above and left of centerof theattitudesphere.Refertotable4--3 for
annunciations and colors.
D Yaw Damper Status Annunciations --Displaystheengage statusof
the yaw damper. The annunciation is displayed above and right of
centeroftheattitudesphere.Refertotable4--18forannunciationsand
colors.