SYSTEM INSTALLATION MANUAL
89000016
SYSTEM INTERCONNECT DIAGRAMS
1.
Typical System Configurations
A.
General
(1)
This section contains general system interconnect and wiring diagram examples for popular
configurations. Each system interconnect contains a table of appropriate KGX settings.
(2)
The air/ground input varies on each aircraft depending on the equipment installed. Refer to the
aircraft manual to determine the appropriate input signal to the KGX. Light Aircraft can refer to
INSTALLATION, Paragraph 10.F. Step (2) for additional data about air/ground.
(3)
All ports (except MPI) not connected to equipment should be set to UNUSED.
NOTE:
The graphics that follow show system configuration from the Terminal MPI.
For corresponding KGX control panel or ADS-B MPI App settings, refer to
CONFIGURATION, CALIBRATION, AND CHECKOUT, and Paragraph 6.
NOTE:
Highlighted configuration options represent those that are unique to each aircraft.
Configuration options must be configured appropriately in accordance with
CONFIGURATION, CALIBRATION, AND CHECKOUT, Paragraph 5.C. and
Paragraph 6.
2.
System Interconnect Diagrams
A.
General
(1)
Refer to Table 2001 for a list of the system interconnect diagrams.
Table 2001. System Interconnect Diagrams
System
Figure Number
Garmin GNS 430W/530W Display and GPS, GTX-330
Transponder
Figure 2001
Chelton FlightLogic Display, GSL-71 Controller, No Transponder
Figure 2002
Aspen Display and Control, GTX 327 Transponder
Figure 2003
BendixKing KSN 765/770 Display and GPS, GTX-327
Transponder
Figure 2004
Mode A/C Transponder, KGX control panel
Figure 2005
Garmin GNS 480, SL-70 Transponder, TCAS
Figure 2006
Garmin MX-20 Display and Control, No Transponder
Figure 2007
Garmin GMX-200 Display, GTX-330 Transponder
Figure 2008
EFFECTIVITY
ALL
Page 2001
22 Dec 2016
© Honeywell International Inc. Do not copy without express permission of Honeywell.