SPZ--8000 Digital Integrated Flight Control System
A28--1146--055
REV 2
Modes of Operation
8-10
When the aircraft satisfies VOR track conditions, the course error signal
is removed from the lateral steering command. This leaves radio
deviation, roll attitude, and lateral acceleration 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 up to 45
course error . Figure 8--8 shows the cockpit displays for VOR tracking.
AD--58115@
AD--58116@
SRP
VOR (NAV) Mode Track
Figure 8--8