SYSTEM INSTALLATION MANUAL
89000016
(c)
When the Warning page is displayed, the KGX control panel continually requests the
active system messages. The MSG icon remains shown as long as system messages
are still present.
(d)
Push the FN button again to exit this mode and return to normal operation.
(e)
A log of system messages can be accessed using the MPI.
(5)
Fault Annunciation
(a)
If the transponder detects a catastrophic internal failure the screen will indicate FAULT
with a brief statement of the problem. No ADS-B messages will be transmitted when a
fault has been detected.
2.
Preliminary Checkout
A.
Overview
(1)
Before the unit is installed and tested, verify that all cables are properly secured. With the KGX
and KGX control panel removed, turn on aircraft power and verify the following.
(a)
Verify that aircraft DC bus voltage is present on Pins 1 and 16 of P1.
(b)
Verify that ground is present on Pins 17 and 31 of P1.
(c)
Verify that the two UAT antenna coax center conductors are not shorted to its shield
or aircraft ground.
(2)
When the above conditions are verified, turn off the master power. Properly attach the external
connectors to the KGX and KGX control panel. Mount the KGX and KGX control panel in their
respective mounting locations. Turn on master power and then turn on the KGX control panel,
if installed. During initialization the KGX unit performs a comprehensive diagnostics test.
(3)
A system component failure will be annunciated by a "Warning Indication" on the KGX control
panel, if installed, or the display. Warnings concerning the GPS status may not be displayed
until 2.5 minutes after power on in order to give the GPS time to acquire satellites. Consult
the Pilot Guide for more information concerning warning messages. Detailed system status
can be observed using the maintenance port Interface as described in CONFIGURATION,
CALIBRATION, AND CHECKOUT.
(4)
The KGX aircraft installation must be verified to ensure compliant operation and configuration.
Reference the applicable STC installation verification instructions.
(a)
The FFS FT-9000 ramp tester can be used for this purpose (refer to INSTALLATION,
Table 1009 for more information). Use of the FFS STC data requires the use of the
FT-9000 for installation verification.
(5)
Refer to Pub. No. D201405000060, BendixKing KGX 150/130 ADS-B Certified Transceivers
and Receivers Pilot’s Guide for more information about System Messages.
3.
Installation Setup and Configuration
A.
General
(1)
System installation is configured using either:
• The MPI on serial Port 3 or Port 5 (typical) or,
• The KGX control panel, if installed, in a special configuration mode.
EFFECTIVITY
ALL
Page 3004
22 Dec 2016
© Honeywell International Inc. Do not copy without express permission of Honeywell.