SYSTEM INSTALLATION MANUAL
89000016
GENERAL INFORMATION
1.
Introduction
A.
General
(1)
This document contains installation data and specifications about the BendixKing KGX series
product line. Table 1 specifies the applicable part numbers.
Table 1. Installation Manual Applicability
Honeywell Part Number
Component
89000016-130
KGX 130T ADS-B TRANSCEIVER WITHOUT INTERNAL GPS
89000016-131
KGX 130R ADS-B RECEIVER WITHOUT INTERNAL GPS
89000016-150
KGX 150R ADS-B RECEIVER WITH INTERNAL GPS
89000016-151
KGX 150T ADS-B TRANSCEIVER WITH INTERNAL GPS
89000016-001
KGX CONTROL PANEL (OPTIONAL)
89000016-002
KGX WiFi MODULE (OPTIONAL)
89000016-004
KGX 150/130 INSTALLATION KIT
89000016-017
WiFi MODULE INSTALLATION KIT
2.
General System Description
A.
General
(1)
The KGX 150T/130T transceiver provides both UAT transmit (ADS-B Out) and UAT receive
(ADS-B In) capability. The KGX 150R/130R receiver provides UAT receive (ADS-B In)
capability only and are intended for use with external ADS-B Out transmitters, including
Mode-S transponders with built-in ADS-B Out. The KGX series satisfy the TSO requirements
and the associated MOPS for UAT ADS-B class A1H/A1S/B1S equipment.
(2)
The KGX 150T/130T transceiver transmits aircraft position, velocity, and other flight data to
other aircraft and ground station equipment through a UAT data link once each second (ADS-B
Out). The KGX 150/130 transceivers and receivers receive aircraft position, velocity, and other
flight data from other aircraft and ground station equipment through a UAT data link (ADS-B
In). GPS data, pressure altitude data, TCAS, and pilot control inputs are received by the KGX
150/130 transceivers and receivers through configurable RS-232/422 serial, ARINC 429,
and/or discrete interfaces. ADS-B and TCAS Traffic, FIS-B (NEXRAD, METARs, NOTAMs,
SIGMETs, etc.) information, system health/status, etc. are output on multiple configured serial
links and/or discrete signals to be connected to pilot displays.
(3)
In Figure 1, the installation shows a display controller, KGX 150 transceiver, two UAT antennas,
and a GPS antenna. Additionally, connections are shown to an external altitude sensor (shared
with the transponder), the transponder suppression bus, and an air/ground detection switch.
The GPS data can optionally be provided by an existing aircraft GPS source if it meets the
interface requirements of the KGX (RS-232 or RS-422) such as the FreeFlight Systems 1201,
Garmin Series 400/500 with GPS ADS-B Plus Interface, or ARINC 743A compatible GPS (e.g.
1203/1203C) through an ARINC 429 bus, or serial connection.
EFFECTIVITY
ALL
Page 1
22 Dec 2016
© Honeywell International Inc. Do not copy without express permission of Honeywell.