SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Modes of Operation
8-16
With FMS selected as the navigation source, LNV capture occurs at
one of the following points:
D When the aircraft is within 2.5 miles of the desired track and moving
away from it, or
D At a calculated point, as a function of track error and groundspeed
if the aircraft is flying toward the desired track.
The two possible capture profiles are shown in Figure 8--12.
FMS Steering
Figure 8--12
The FMS LNV mode is cancelled by:
D Pushing the NAV button on the flight guidance controller
D Selecting go--around mode
D Selecting standby mode
D Selecting the heading lateral steering mode
D Coupling to the cross--side EHSI
D With the autopilot engaged, moving the turn knob out of detent
D Selecting a different NAV source.