User's Manual

Page 3-14 GTS Processor Installation Manual
Revision A 190-00587-50
Bottom Antenna:
Model None
Monopole
Garmin GA58
Sensor Systems
Cable loss (dB) 0.2 – 4.0
Note: Cable loss information is described in Fabrication of
Coaxial Cable Assemblies Section 2.4.1.2.
Note: All A429 options have the ability to select High or Low speed.
Note: If an input is inactive, a will be displayed.
If an input is active, a will be displayed.
If an input is in an unknown state, a will be displayed.
Volume Level:
Allows audio volume level selection from 0 to -63 dB in 0.5 dB increments.
Maximum audio output is at least 80 mW into a 600 Ohm load. (6.93 Vrms)
Voice Gender:
Enter voice preference selection.
Gear/Wheel:
Enter type of aircraft gear design.
Discrete ‘gear-down’ Sense:
Indicate the type of gear down sense switch for the Gear Down and Locked* discrete input.
See Appendix B (Note 7) and Figure B-9 for Gear Down and Locked* discrete input.
Note: Discrete ‘gear-down’ sense is only enabled when ‘Retractable’ Gear/Wheel design is
configured.
ADSB TX Capable:
Indicate whether aircraft is equipped with ADS-B transmitter.
Squat ‘on-ground’ Sense:
Indicate type of sense switch.
Note: For helicopter installations without a squat switch, the traffic system status valid discrete
output can be wired to the air/ground discrete input to prevent the GTS from going to standby mode
during extended hover. For such installations, configure squat ‘on-ground’ sense to ‘open’.
Mode S ID (HEX):
Enter Mode S transponder ID (must match the Mode S ID used by the transponder).
Set Active:
Must select Set Active to enable the settings on the GTS Processor.
Revert Changes:
Select to show current GTS Processor settings.
An incorrect configuration will be reverted back to previous settings.
Note: Default is “disabled” for all inputs and outputs.
DRAFT