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Elliott Aviation Technical Products Development, Inc. 

Report No.: ICA-3832-560 

6601 74

th

 Ave Building A

Revision: A 

Milan, IL 61264 

Dated 01/15/2018 

A1 

Instructions for Continued Airworthiness For Garmin ADS-B System Installation 

APPENDIX A 

ATTACHMENTS 

All documents listed in the table below must be attached to this document and maintained in accordance with Chapter 

one. 

ATTACHMENTS 

DOCUMENT NO. 

TITLE 

REV 

PAGES 

CFG-3832-560 

Configuration Instructions for Garmin ADS-B Out System Installation 

A 

14 

237-3832-E0560-000 

GTX3000 Transponders and GDL88 ADS-B System 

A 

8 

237-3832-M0560-050 

Wire Routing Installation 

IR 

4 

Summary of Contents for ADS-B

Page 1: ...HNICAL PRODUCTS DEVELOPMENT INC Elliott Aviation Technical Products Development Inc reserves the copyright of all information and illustrations in this publication which is provided in confidence and which may not be used for any purpose other than for which it was originally supplied The publication may not be reproduced in part or in whole without the consent in writing of Elliott Aviation Techn...

Page 2: ...A 3832 560 6601 74 th Ave Building A Revision IR Milan IL 61264 Dated 01 23 2018 2 of 21 Instructions for Continued Airworthiness For Garmin ADS B System Installation REVISIONS PAGE Rev Description Page S Date Approved By IR Initial Release ALL 01 23 2018 R Woolums ...

Page 3: ...m Installation TABLE OF CONTENTS COVER PAGE 1 REVISIONS PAGE 2 TABLE OF CONTENTS 3 Chapter 1 Introduction 4 Chapter 2 Maintenance Instructions and Shedules 6 Chapter 3 Access 13 Chapter 4 Lifting and Shoring 14 Chapter 5 Leving and Weighing 14 Chapter 6 Towing and Taxing 15 Chapter 7 Parking and Moring 15 Chapter 8 Placards and Markings 15 Chapter 9 Servicing 15 Chapter 10 Airworthiness Limitation...

Page 4: ...s 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 Drawing Num...

Page 5: ... explanation Latency The total time between when the position is measured and when the position is transmitted by the aircraft A 14 CFR 91 227 performance requirement for ADS B broadcast systems The collection of specific equipment interface and testing represented by this STC comprises an approved Latency OEM Original Equipment Manufacturer SBS Surveillance and Broadcast Service Provided by the F...

Page 6: ...Z 8000 altitude reporting equipment connected to the Garmin ADS B transponders must comply with all applicable 14 CFR 91 217 91 411 and part 43 appendix E test and inspection requirements If the altimetry system is compliant with the Reduced Vertical Separation Minimum RVSM standards the requirements and tolerances stated in the approved RVSM maintenance program must be met ADS B installation does...

Page 7: ...setup and configuration GPS reception must be confirmed using the diagnostic page Use known GPS position to validate the GDL 88 diagnostic position readout such as the aircrafts navigation GPS This information is presented on the Pro Line 4 cockpit control display unit under the IDX pages Sample page below show typical GDL 88 GPS data 2 3 1 5 After GPS reception is verified aircraft maybe returned...

Page 8: ... approval 2 3 2 3 While using the Elliott Configuration Instructions access to the GTX 3000 status is available Real time information is presented 2 3 2 4 For setup and configuration the following items must be verified GPS Position Magnetic Weight on wheels is operating correctly ADS B mode indicated 4096 code agrees with RMU ATC settings Flight ID agrees with RMU ATC settings note Dynamic pilot ...

Page 9: ...ort No ICA 3832 560 6601 74 th Ave Building A Revision IR Milan IL 61264 Dated 01 23 2018 9 of 21 Instructions for Continued Airworthiness For Garmin ADS B System Installation GTX 3000 Configuration GPS Sample page GTX 3000 Configuration Heading Sample page ...

Page 10: ...ed for the Flight Crew presentations The GTX 3000 is not field serviceable If faulty the GTX 3000 line replaceable unit may only be repaired by Garmin 2 3 2 12 For troubleshooting an in service system the above may be confirmed using this Status page Weight on wheels is operating correctly squat switch wiring and config ADS B mode indicated GDL 88 valid 429 data wiring and config 4096 code agrees ...

Page 11: ... 3 3 GTX 3000 N number Registration change 2 3 3 1 Obtain Elliott Configuration Instructions located in Appendix A Using sections 2 and 4 of the Configuration Instructions Access the Aircraft tab on the GTX 3000 configuration tool Modify the registration as needed and press enter to set the configuration Shutdown the configuration tool and verify registration number change using IFR 6000 or simila...

Page 12: ...t seen by flight crew report will come from ATC Ground Same as above for ADS B annunciation status Transponder reporting Mode C Observe or determine the Honeywell RMU annunciations If alternate GTX 3000 can be controlled using Honeywell RMU suspect the GTX 3000 LRU TCAS Honeywell MFD Observe status Use the Test button on the front of the TCAS processor and verify errors displayed on the LED lights...

Page 13: ...ght avionics bay upper equipment shelf A configuration module is also located inside the J811 connector 3 1 3 AMCs are located in the forward right and left avionics bays upper equipment shelf 3 1 4 Flight Stream 110 if installed is located on the outboard side of the Co Pilot s chart holder cabinet 3 1 5 ADS B 1 2 annunciator is located in the cockpit panel 3 1 6 GA 36 GPS Antenna is located on t...

Page 14: ... procedures described elsewhere in this document 3 2 1 4 Configuration Modules are located inside the J881 GDL 88 connector and inside each J3302 GTX 3000 connector Hand tools are required to gain access inside the backshell Retain hardware after removal To install secure retained hardware and Reconnect to applicable unit Conduct necessary checkout procedure described elsewhere in this document 3 ...

Page 15: ... 23 2018 15 of 21 Instructions for Continued Airworthiness For Garmin ADS B System Installation Chapter 6 TOWING AND TAXIING Not applicable this modification Chapter 7 PARKING AND MOORING Not applicable this modification Chapter 8 PLACARDS AND MARKINGS Not applicable this modification Chapter 9 SERVICING Not applicable this modification ...

Page 16: ......

Page 17: ... take effect from the date of installation Any existing inspection requirements established by the manufacturer for the affected structure are also applicable The connector and fastener holes should be inspected using eddy current inspection techniques according to the intervals outlined in the tables above 10 2 Inspection Procedures The inspection should include the following structural details M...

Page 18: ...requency eddy current inspection techniques around the connector and installation fastener holes Circle templates are provided at the end of this section to aid in the inspection 4 Make sure the bonding areas of the attachment screws and antenna mating surfaces are not damaged or contaminated Put the antenna in position and attached with screws Seal the periphery of the antenna and heads of screws...

Page 19: ...ed Airworthiness For Garmin ADS B System Installation 10 3 Inspection Procedures Aids Circle templates are provided report to aid in inspection Eddy Current Circle Templates Modification Hole Diameter 0 75 IN 0 201 IN Rivets GPS Antenna X X X UAT Antenna X X X For 0 75 inch hole Note Always confirm scale of final printed template FAA Approved Date _________________ FEB 09 2018 ...

Page 20: ...h Ave Building A Revision IR Milan IL 61264 Dated 01 23 2018 20 of 21 Instructions for Continued Airworthiness For Garmin ADS B System Installation For 0 201 inch hole For selected rivets Note Always confirm scale of final printed template FAA Approved Date ________________ FEB 09 2018 ...

Page 21: ...ditions are met 1 The maintenance check for the aircraft occurs before the threshold inspection interval indicated by the analysis in this report 2 Subsequent maintenance checks for the aircraft occur before the recurring inspection interval indicated by the analysis in this report If the maintenance checks for the aircraft exceed the threshold or recurring inspection intervals specified in this r...

Page 22: ... System Installation APPENDIX A ATTACHMENTS All documents listed in the table below must be attached to this document and maintained in accordance with Chapter one ATTACHMENTS DOCUMENT NO TITLE REV PAGES CFG 3832 560 Configuration Instructions for Garmin ADS B Out System Installation A 14 237 3832 E0560 000 GTX3000 Transponders and GDL88 ADS B System A 8 237 3832 M0560 050 Wire Routing Installatio...

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