Honeywell PRIMUS 1000 - Vor;Ils;Marker;Dme Past; Vor;Ils;Marker;Dme PAST Procedure

PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
C--31
PRIMUS
â
II Radio System
VOR/ILS/MARKER/DME PAST
Refer to table C--10 for the VOR/ILS/marker/DME PAST procedures.
NOTE: While in flight, this test may be inhibited by other aircraft
systems (e.g., by autopilot while on approach tracking).
Step Procedure
1 Adjust the selected course for zero degree.
2 Position cursor in NAV window. Verify that AUX ON is not
present. Push and hold the TST button. VOR TEST and
DME TEST are displayed in the NAV window.
3 VOR/ILS/MARKER PAST Results:
D After 2 seconds, marker lamps and tones annunciate in
the order of 400 Hz (outer); 1300 Hz (middle); and 3000
Hz (inner).
D Localizer and glideslope deviation bars indicate a
centered course for approximately 2 seconds with flags
out of view.
D Localizer and glideslope deviation bars deflect left
(localizer) and up (glideslope) one dot deflection, for
approximately 2 seconds with flags out of view.
D If course selector is on zero, VOR deviation bar centers
on a course of 0° and RMI indicates zero degree north
for approximately 5 seconds with flags out of view.
D The RMU annunciates VOR PASS in green, or VOR
ERR in red.
4 DME PAST Results:
D TEST is displayed as Ident on DME indicator and EFIS.
D 10.0 NM on DME indicator and EFIS
120 KTS
5 MIN
D RMU annunciates DME PASS in green or DME ERR in
red.
VOR/ILS/Marker/DME PAST Procedure
Table C--10