PRIMUS
r
1000 Integrated Avionics System
A28--1146--112--00
8-13
Modes of Operation
20
20
30
30
30
30
M
--2000
AD--50980--R1@
Localizer Mode Arm Display
Figure 8--10
With the aircraft approaching the selected course intercept, as shown
in figure 8--11, the LBS monitors localizer beam deviation, beam rate,
and TAS. At the computed time, the lateral beam sensor (LBS) trips and
captures localizer signal. The flight director drops the heading select
mode and generates the proper roll command to bank the aircraft
toward the localizer beam center. When the LBS trips, the PFD displays
LOC in green, as shown in figure 8--12. LOC is enclosed in a white box
for 5 seconds.