Garmin ADS-B Out System Installation - Page 4
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Elliott Aviation Technical Products Development, Inc.
th
6601 74
Ave Building A
Milan, IL 61264
Instructions for Continued Airworthiness For Garmin ADS-B System Installation
1.1
Scope/Purpose/Applicability/Distribution
The Instructions for Continued Airworthiness (ICA) described herein are applicable only to those aircraft modified
by FAA STC
procedures for the installation of Garmin ADS-B System.
The maintenance information provided by this document must be included in the operator's Aircraft Maintenance
Manual and the operator's Aircraft Scheduled Maintenance Program. All documents listed in the required
documents section must be maintained with this document. FAA accepted revisions to this document will be
distributed by mail to the applicable certifying authorities and operators of legally modified aircraft.
1.2
System Description
The features of this modification include the installation of Garmin GTX 3000 transponders, reusing existing aircraft
wiring, and two installed Shadin AMC Converters connecting the transponders to the RCZ Com units and the
remaining RSB bus. This modification also includes a Garmin GDL 88 GPS / UAT and optional Flight Stream 110
Bluetooth FIS-B installation. A GPS and UAT-SBS antenna is installed. Annunciation is added for ADS-B status.
New circuit breakers are installed in the copilot's circuit breaker panel. New wiring is added to supply the GTX
3000 transponders with GPS position for the GDL 88. The Flight Stream 110 (if installed) supports properly
equipped FIS-B capable Bluetooth devices
1.3
Required Data
All requited data is located in Appendix A of this document.
1.4
Referenced Garmin/Shadin documents:
Nomenclature
GTX 3000 Transponder Installation Manual
GDL 84/88 TSO Installation Manual
Flight Stream 110/210 TSO Installation Manual
ARINC to Manchester Converter
1.5
Systems Control:
1.5.1 The GTX 3000 transponders replace the Honeywell transponder modules. All control is via the existing
Honeywell RMU. No changes to operational control are imposed by this STC.
1.5.2 The Shadin AMC Converters convert RSB databus into ARINC 429. The AMC has no external control.
1.5.3 The GDL 88 is a GPS sensor and FIS-B UAT receiver. The GDL 88 has no external control.
1.5.4 The Flight Stream 110 is a Bluetooth repeater for the GDL 88 FIS-B products and has no external control.
1.6
Document administration:
1.6.1 This document will be revised by Elliott Aviation Engineering when revisions to descriptive or approval data
warrant.
1.6.2 When this document is revised, all pages will be revised to indicate the current level. Chapter 10 will have its
own revision status embedded. FAA approved revisions to the document will be distributed by mail to the
applicable certifying authorities and operations of legally modified aircraft.
INTRODUCTION
ST04272CH
. These ICA describe the recommended and required maintenance
Chapter 1
Drawing Number
190-00926-01
190-01122-00
190-01700-00
M833520-00
Report No.: ICA-3832-560
Revision: IR
Dated 01/23/2018
4 of 21
Rev
Date
P
Apr 2017
L
Nov 2017
F
Aug 2017
A
Dec 2017