Vor/Ils/Marker/Dme Past; Vor/Ils/Marker/Dme Past Procedure - Honeywell PRIMUS 1000 Pilot's Manual

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
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:
After 2 seconds, marker lamps and tones annunciate in
D
the order of 400 Hz (outer); 1300 Hz (middle); and 3000
Hz (inner).
Localizer and glideslope deviation bars indicate a
D
centered course for approximately 2 seconds with flags
out of view.
Localizer and glideslope deviation bars deflect left
D
(localizer) and up (glideslope) one dot deflection, for
approximately 2 seconds with flags out of view.
If course selector is on zero, VOR deviation bar centers
D
on a course of 0°and RMI indicates zero degree north
for approximately 5 seconds with flags out of view.
The RMU annunciates VOR PASS in green, or VOR
D
ERR in red.
4 DME PAST Results:
TEST is displayed as Ident on DME indicator and EFIS.
D
10.0 NM on DME indicator and EFIS
D
RMU annunciates DME PASS in green or DME ERR in
D
red.

VOR/ILS/Marker/DME PAST Procedure

A28--1146--112--00
120 KTS
5 MIN
Table C--10
PRIMUSr1000 Integrated Avionics System
Procedure
PRIMUS
â
II Radio System
C--31