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Honeywell PRIMUS 1000 - Page 206

Honeywell PRIMUS 1000
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PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
Modes of Operation
8-18
Step Procedure
6 Push the NAV button on the GC. With the aircraft outside
the normal back course localizer capture limits, and more
than 105_ off the localizer front course heading, the PFD
annunciates BC in white and HDG in green, as shown in
the display below.
2020
3030
3030
M
--2000
AD--50984--R1@
7 At back course capture, the PFD annunciates BC in green,
as shown in the display below. BC is enclosed in a white
box for 8 seconds.
30
30
30
30
3
2
1
0
1
2
3
M
--2000
AD--50986--R1@
Back Course Flight Procedure
Table 8--5

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