AIRCRAFT
SA160
AIRCRAFTA I R C R A F T
Symphony
7.2 SYSTEM DESCRIPTION
The GNS 430 system consists primarily of the GNS 430 unit, a GPS
antenna,aVHFVOR/LOC/GSantenna,andaVHFCOMMantenna.
The GNS 430 unit contains the GPS Receiver, the VOR/ILS receiver, and
the VHF Communications Transceiver. The unit is mounted in the center
ofinstrumentpanel;intheavionicscolumn.
The GNS 430 system can be turned ON if the BAT switch and the
AVIONICSswitchareintheONposition.
SECTION 9
SUPPLEMENT 1
SECTION 7
DESCRIPTION AND OPERATION
7.1 GENERAL
The information contained in here supersedes the information on the
Bendix/King KX 125 VHF NAV/COM receiver-transmitter, provided in
the Description & Operation Section of the basic Pilot's Operating
HandbookandTCApprovedAirplaneFlightManual.
For a complete description of the GNS 430 system, refer to the GARMIN
GNS 430Pilot's Guide, P/N 190-00140-00, Rev. A, dated October, 1998, or
laterappropriaterevision.
Feb 25, 2005
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