INSTALLATION MANUAL
89000007
Page 4-2
15 Nov 2013
© Honeywell International Inc. Do not copy without express permission of Honeywell.
The script will prompt for the following configuration items:
Aircraft
registration
Mode S address
VFR squawk code
Aircraft maximum airspeed
Aircraft
category
Squat switch source, if fitted
ARINC TIS-A output format, if used
RS232 TIS-A output format, if used
GPS position source, if fitted, and ADS-B parameters
Measurement
units
Aircraft length and width
GPS reference offset
Audio output volume
LCD dimming settings.
It will then run some simple installation diagnostics, including an external interface
check, a check of the altitude encoder interface, and a check of the lighting bus input.
All the programming is accomplished using the numeric buttons 2 (back), 6 (down), 7
(up), and the ENT and FUNC buttons. Pressing the ENT button accepts the current
input. Pressing the 2 (back) button goes back to the previous page. Pressing 6 or 7
buttons allows the user to move up and down the menu options. Pressing the FUNC
button also accepts the selection and moves directly to the next screen. Refer to
Figure 4-1.
Figure 4-1. KT 74 Transponder