EasyManua.ls Logo

Honeywell PRIMUS 1000 - VOR Navigation Mode Capture

Honeywell PRIMUS 1000
334 pages
To Next Page IconTo Next Page
To Next Page IconTo Next Page
To Previous Page IconTo Previous Page
To Previous Page IconTo Previous Page
Loading...
PRIMUSr 1000 Integrated Avionics System
A28--1146--112--00
8-7
Modes of Operation
30
30
30
30
AD--50973--R1@
VOR Navigation Mode Capture
Figure 8--6
When the aircraft meets the VOR track conditions the course error
signal is removed fromthelateralsteeringcommand.This leavesradio
deviation and DME gain programming (if available) to track the VOR
signal and to compensate for beam standoff in the presence of a
crosswind. The system automatically compensates for a crosswind of
upto45_courseerror.Figure8--7showsthePFDdisplayinthetracking
mode.
Cancel the VOR navigation mode with anyoneofthefollowingactions:
D Push the NAV button on the GC
D Select go--around
D Select another lateral mode
D Change the selected navigation or heading source.

Table of Contents

Related product manuals