Honeywell PRIMUS 1000 - ADF Bearing Pointer; Digital Heading; RMU Backup Navigation Display; VOR;ILS and ADF Frequency Display

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Electronic Flight Instrument System (EFIS)
4-98
MARKER BEACON
OM
MM
IM
AD--50954--R1@
RMU Backup Navigation Display
Figure 4--56
D ZADF Bearing Pointer -- The bearingpointer, and its legendand
digital position display are white. When the pointer (or its tail) is not
in view, a double white arrow is displayed above the compass arc,
on either the left or right side, indicating its location.
D VOR/ILS and ADF Frequency Display -- The VOR/ILS tuned
frequencyisshownintheupperleftandthe ADFfrequencyisshown
in the upper right of the display; both are white. When the RMUline
select key adjacent to the respective window is pushed, that
frequency is enclosed in the RMU yellow tuning box.The tuneknob
is used to select the desired frequency.
D Digital Heading -- This is the digital value of the current heading.
D fVOR Bearing Pointer -- The bearingpointer, andits legendand
digital position display are cyan. When the pointer (or its tail) is not
in view, a single cyan arrow is displayed abovethe compass arc, on
either the left or right side (as appropriate), indicating its location.