Garmin 0104400 TRAFFIC ADVISORY SYSTEM (TAS) PROCESSOR User Manual coverRev4TP
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GTS 8XX/GPA 65 Installation Manual (Includes the GA 58 Antenna) 190-00587-00 April, 2009 Revision 4TP © Copyright 2009 Garmin Ltd. or its subsidiaries All Rights Reserved Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express prior written consent of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed and to print one copy of this manual or of any revision hereto, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin International, Inc. 1200 E. 151st Street Olathe, KS 66062 USA Telephone: 913-397-8200 Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482 www.garmin.com Garmin (Europe) Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton, SO40 9RB, UK Telephone: +44 (0) 8708501241 RECORD OF REVISIONS Revision 1TP 2TP 3TP 4TP Revision Date 08/06/08 9/17/08 2/18/09 Description 1TP Release Updated manual with various engineering changes Updated manual with various engineering changes Updated manual with various engineering changes DOCUMENT PAGINATION Page A Revision 4TP Section Page Range Table of Contents Section 1 Section 2 Section 3 Section 4 Appendix A Appendix B i – vi 1-1 – 1-10 2-1 – 2-16 3-1 – 3-20 4-1 – 4-14 A-1 – A-14 B-1 – B-18 GTS 8XX/GPA 65 Installation Manual 190-00587-00 This manual reflects the operation of software version X.XX. Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions. INFORMATION SUBJECT TO EXPORT CONTROL LAWS This document may contain information which is subject to the Export Administration Regulations (“EAR”) issued by the United States Department of Commerce (15 CFR, Chapter VII Subchapter C) and which may not be exported, released or disclosed to foreign nationals inside or outside the United States without first obtaining an export license. The preceding statement is required to be included on any and all reproductions in whole or in part of this manual. NOTE Throughout this document references made to the GTS 8XX shall equally apply to the GTS 800, 820, and 850 except where specifically noted. WARNING This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This Notice is being provided in accordance with California's Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page i Revision 4TP This page intentionally left blank Page ii Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 TABLE OF CONTENTS PARAGRAPH PAGE 1.1 1.2 1.3 1.4 1.5 1.6 1.7 GENERAL DESCRIPTION..............................................................................................................1-1 Introduction........................................................................................................................................1-1 Equipment Description ......................................................................................................................1-1 Interface Summary.............................................................................................................................1-1 Technical Specifications ....................................................................................................................1-2 Certification .......................................................................................................................................1-4 Reference Documents ........................................................................................................................1-8 Limited Warranty...............................................................................................................................1-9 2.1 2.2 2.3 2.4 2.5 2.6 INSTALLATION OVERVIEW ........................................................................................................2-1 Introduction........................................................................................................................................2-1 Installation Considerations ................................................................................................................2-3 Electrical Bonding .............................................................................................................................2-5 Cabling and Wiring............................................................................................................................2-5 Cooling Requirements .....................................................................................................................2-15 Mounting Requirements ..................................................................................................................2-16 3.1 3.2 3.3 3.4 3.5 3.6 3.7 3.8 INSTALLATION PROCEDURE......................................................................................................3-1 Unpacking Unit..................................................................................................................................3-1 Wiring Harness Installation ...............................................................................................................3-1 QMA Connector Insertion and Removal ...........................................................................................3-3 Backshell, Pigtail Circular Connector, and Configuration Module Assemblies................................3-5 Unit Installation .................................................................................................................................3-5 GA 58 Antenna Installation .............................................................................................................3-19 GPA 65 PA/LNA Installation ..........................................................................................................3-20 Continued Airworthiness .................................................................................................................3-20 4.1 4.2 4.3 4.4 4.5 4.6 4.7 SYSTEM INTERCONNECTS..........................................................................................................4-1 GTS 8XX Pin Function List ..............................................................................................................4-1 GPA 65 Pin Function List..................................................................................................................4-6 Power .................................................................................................................................................4-7 Serial Data .........................................................................................................................................4-9 Configuration ...................................................................................................................................4-12 Analog/Discrete ...............................................................................................................................4-12 Mutual Suppression Bus ..................................................................................................................4-14 APPENDIX A: OUTLINE & INSTALLATION DRAWINGS .............................................................. A-1 APPENDIX B: INTERCONNECT EXAMPLE...................................................................................... B-1 GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page iii Revision 4TP LIST OF ILLUSTRATIONS FIGURE PAGE 2-1 GTS 800 Installation with Top and Bottom Directional Antennas....................................................2-7 2-2 GTS 800 Installation with Top and Bottom Monopole Antennas .....................................................2-8 2-3 GTS 800 Installation with Top Directional Antennas and no Bottom Antenna ................................2-8 2-4 GTS 820/GTS 850 Installation Top and Bottom Directional Antennas ............................................2-9 2-5 GTS 820/GTS 850 Installation with Top Directional and Bottom Monopole Antenna ..................2-10 2-6 GTS 820/GTS 850 Installation with Top Directional and no Bottom Antenna...............................2-10 2-7 RG-400/RG-142 Coaxial Cable Stripping Dimensions ...................................................................2-14 2-8 Ferrule and Crimp Die Positioning ..................................................................................................2-14 2-9 Heat Shrink Positioning ...................................................................................................................2-15 2-10 GTS 8XX Vertical Installation Rack (Garmin P/N 115-00781-00) ................................................2-16 2-11 GTS 8XX Horizontal Installation Rack (Garmin P/N 115-00784-00) ............................................2-16 3-1 Engaging QMA Connectors...............................................................................................................3-3 3-2 Disengaging QMA Connectors..........................................................................................................3-4 3-3 GTS 8XX Install Tool – Normal Tab ................................................................................................3-7 3-4 GTS 8XX Install Tool – Configuration Tab (GTS 800)....................................................................3-8 3-5 GTS 8XX Install Tool – Configuration Tab (GTS 820 and GTS 850)..............................................3-9 3-6 GTS 8XX Install Tool – Upload Tab...............................................................................................3-12 3-7 Self Test ...........................................................................................................................................3-15 3-8 Ground Test .....................................................................................................................................3-16 A-1 GTS 8XX Vertical Outline Drawing ................................................................................................ A-1 A-2 GTS 8XX Vertical Installation Drawing .......................................................................................... A-3 A-3 GTS 8XX Horizontal Outline Drawing ............................................................................................ A-5 A-4 GTS 8XX Horizontal Installation Drawing ...................................................................................... A-7 A-5 GPA 65 Outline Drawing ................................................................................................................. A-9 A-6 GPA 65 Installation Drawing ......................................................................................................... A-11 A-7 GA 58 Antenna Outline Drawing ................................................................................................... A-13 B-1 Notes ................................................................................................................................................. B-1 B-2 GTS 820/850/GPA 65 Example Interconnect................................................................................... B-3 B-3 GTS 800 Example Interconnect........................................................................................................ B-5 B-4 GTS 8XX G1000 Example Interconnect .......................................................................................... B-7 B-5 GTS 8XX GNS 4XX/GNS 5XX/GMX 200 Example Interconnect ................................................. B-9 B-6 GTS 8XX/GMA/Altimeter Example Interconnect ......................................................................... B-11 B-7 GTS 8XX Dongle Cable (Non-G1000 Installations Only)............................................................. B-13 B-8 GTS 8XX Discrete Interconnects ................................................................................................... B-15 B-9 GTS 8XX Config Module Example Interconnect .......................................................................... B-17 Page iv Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 LIST OF TABLES TABLE PAGE 2-1 2-2 2-3 2-4 3-1 3-2 3-3 3-4 GPA 65 Minimum Wiring Requirements ..........................................................................................2-6 Cable Types and QMA Connectors .................................................................................................2-11 Recommended Coaxial Length........................................................................................................2-12 Coaxial Cable Set Length Tolerance ...............................................................................................2-13 Socket and Pin Contact part Numbers ...............................................................................................3-1 Socket Contact MIL SPEC M39029/5-115 Crimp Tooling...............................................................3-1 Pin Contact GPN 336-00021-00 MIL SPEC M39029/58-360 Crimp Tooling .................................3-2 Pin Socket Contacts GPN 336-00022-00 MIL SPEC M39029/63-368 and GPN 336-00023-00 Crimp Tooling...............................................................................................................................................3-2 3-5 Self Test ...........................................................................................................................................3-15 GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page v Revision 4TP GTS 8XX HARDWARE MOD LEVEL HISTORY The following table identifies hardware modification (Mod) Levels for the GTS 8XX. Mod Levels are listed with the associated service bulletin number, service bulletin date, and the purpose of the modification. The table is current at the time of publication of this manual (see date on front cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers are encouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer Resource web site at www.garmin.com using their Garmin-provided user name and password. APPLICABLE LRU PART NUMBER Page vi Revision 4TP MOD LEVEL SERVICE BULLETIN NUMBER SERVICE BULLETIN DATE PURPOSE OF MODIFICATION GTS 8XX/GPA 65 Installation Manual 190-00587-00 1 1.1 GENERAL DESCRIPTION Introduction This manual presents mechanical and electrical installation requirements for installing the GTS 8XX/GPA 65 Traffic Advisory System (TAS) and Traffic Collision Avoidance System (TCAS I). 1.2 Equipment Description The GTS 8XX is a microprocessor-based Line Replaceable Unit (LRU) that uses active interrogations of Mode S (GTS 820 and GTS 850 only) and Mode C transponders to provide Traffic Advisories to the pilot. The GTS 820 and GTS 850 include a GPA 65 power amplifier/low-noise amplifier (PA/LNA) module, which allows for up to 40 nm of active surveillance range as well as Mode S interrogation capability. When installed with a 1090 MHz ADS-B transmit class of equipment the GTS 8XX also utilizes passive surveillance. Traffic is displayed on an external MFD via ARINC 429 and/or Ethernet High Speed Data Bus (HSDB). An aural alert is also provided to inform the crew a traffic advisory (TA) will be displayed. A top-mounted directional antenna is used to derive bearing of the intruder aircraft, which is displayed with relative altitude to own aircraft. Top antenna transmitted interrogations are directional, reducing the number of transponders that receive the interrogation thus reducing potential garble on the 1090 MHz band. Optional bottom antenna transmit interrogations are omni directional, using a monopole antenna (recommended for fixed gear installations) or a directional antenna (recommended for retractable gear installations). A bottom directional antenna installation gives the benefit of intruder bearing visibility for targets that are shaded from the top directional antenna. 1.2.1 GTS 8XX Model Differences GTS 800 GTS 820 GTS 850 1.3 011-01356-00 011-01446-00 011-01553-00 Transmit Power (Watts) GPA 65 PA/LNA 1090 ES ADS-B Receiver Traffic Collision Avoidance System (TCAS I) Traffic Advisory System (TAS) The following table summarizes the differences between the various GTS 8XX models documented in this manual. 40 200 200 Interface Summary The GTS 8XX is designed as an open architecture system that uses typical ARINC 429, RS-232, and Ethernet communications interfaces. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 1-1 Revision 4TP 1.4 Technical Specifications 1.4.1 Environmental Qualification Form It is the responsibility of the installing agency to obtain the latest revision of the GTS 8XX/GPA Environmental Qualification Form. This form is available directly from Garmin under the following part number: GTS 8XX Environmental Qualification Form, Garmin part number 005-00323-02 GPA 65 PA/LNA Environmental Qualification Form, Garmin part number 005-00323-22 GA 58 Antenna Environmental Qualification Form, Garmin part number 005-00232-23 To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site (www.garmin.com). 1.4.2 Physical Characteristics Characteristics GTS 8XX Width GTS 8XX Height GTS 8XX Depth w/Connector Kit GPA 65 Width GPA 65 Height GPA 65 Depth Not Including Connector And Cable GPA 65 Depth w/Connector And Cable Fully Extended GTS 8XX Unit Weight w/out Connector Kit GTS 8XX Unit Weight with Connector Kit/w Vertical Rack GTS 8XX Unit Weight with Connector Kit/w Horizontal Rack GPA 65 PA/LNA Unit Weight with Pigtail Connector Kit* GA 58 TAS/TCAS Antenna w/screws and o-ring QMA straight connector kit, 4 pcs QMA straight connector kit, 1 pc QMA right angle connector kit, 4 pcs QMA right angle connector kit, 1 pc QMA termination connector kit *Used with the GTS 820 and 850. Page 1-2 Revision 4TP Specifications 2.81 inches (7.14 cm) 6.94 inches (17.63 cm) 14.78 inches (37.54 cm) 4.25 inches (10.80 cm) 1.00 inches (2.54 cm) 7.96 inches (20.22 cm) 16.83 inches (42.75 cm) 9.0 lbs. (4.08 kg) 10.7 lbs. (4.85 kg) 11.5 lbs. (5.22 kg) 1.9 lbs. (0.86 kg) 0.82 lbs. (0.37 kg) 0.10 lbs. (0.05 kg) 0.03 lbs. (0.01 kg) 0.18 lbs. (0.08 kg) 0.05 lbs. (0.02 kg) 0.07 lbs. (0.03 kg) GTS 8XX/GPA 65 Installation Manual 190-00587-00 1.4.3 General Specifications The table below contains general specifications. For detailed environmental specifications, see the Environmental Qualification Form. Characteristics Specifications Operating Temperature Range -55°C to +70°C. Humidity 95% non-condensing Altitude Range -1,500 ft to 55,000 ft Software Compliance RTCA/DO-178B levels B, C, and D Hardware Compliance RTCA/DO-254 Level C Environmental Compliance RTCA/DO-160E 1.4.4 Power Requirements Characteristics GTS 8XX Power Requirements Specifications GTS 800 Power Consumption 14/28 Vdc. See the Environmental Qualification Form for details on surge ratings and minimum/maximum operating voltages. 1.1 +/- 0.2 A typical 1.5 A max operating @ 28 Vdc GTS 820/850 Power Consumption 2.2 +/- 0.2 A typical 2.6 A max operating @ 14 Vdc 1.3 +/- 0.2 A typical 1.6 A max operating @ 28 Vdc GTS 8XX Boot-up Current Draw GTS 8XX/GPA 65 Installation Manual 190-00587-00 2.7 +/- 0.3 A typical 3.2 A max operating @ 14 Vdc 4.0 A @ 28 Vdc for 70 ms 5.6 A @ 14 Vdc for 100 ms Page 1-3 Revision 4TP 1.5 Certification The conditions and tests required for TSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO standards. TSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. The following table provides a list of applicable TSO/ETSOs for the GTS 8XX/GPA 65. 1.5.1 TSO/ETSO Compliance Applicable LRU Function TSO/ETSO GTS 850 GPA 65 Traffic Alert and Collision Avoidance System (TCAS I) Airborne Equipment TSO-C118 ETSO-C118 GTS 800 GTS 820 GPA 65 Traffic Advisory System (TAS) Airborne Equipment TSO-C147 ETSO-C147 GTS 800 GTS 820 GTS 850 Extended Squitter Automatic Dependent Surveillance – Broadcast (ADS-B) and Traffic Information Service – Broadcast (TIS-B) Equipment Operating on the Radio Frequency of 1090 Megahertz (MHz) Category Class A Applicable LRU SW Part Numbers Applicable CLD Part Numbers 006-B0551-() 006-C0081-()** 006-C0092-()*** 006-B0551-() 006-C0081-()** 006-C0092-()*** 006-B0551-() 006-C0081-()** Class A0/Type 1 Receiving Only* TSO-C166a Class A1/Type 1 Receiving Only* * Equipment is Class A0 when installed with a single antenna, Class A1 when installed with diversity antennas. **GTS 8XX only ***GPA 65 only Page 1-4 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 1.5.2 TSO/ETSO Deviations 1.5.2.1 GTS 800 TSO/ETSO TSO-C147 RTCA DO-197A RTCA DO-185A RTCA DO-260A Deviation 1. Garmin was granted a deviation from TSO-C147 section 1.c to use RTCA DO-160E, instead of RTCA DO-160D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 1. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185A section 2.2.3.3 instead of the requirement of RTCA DO197A section 2.2.3.2.1 3. Garmin was granted a deviation from RTCA DO-197A section 2.2.9.1 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity. 4. Garmin was granted a deviation from RTCA DO-197A section 2.2.11 to use the suppression pulse on the aircraft suppression bus specified by RTCA DO-185A section 2.2.3.12 (70 +/-1 µs from top antenna and 90 +/-1 µs from bottom antenna) instead of 100 +/-5 µs. 1. Garmin was granted a deviation to use DO-185A as modified by Appendix 1 of TSO-C119B and ‘RWG Recommended Modification 2.0 to TSO-C119B.’ 2. Garmin was granted a deviation from RTCA DO-185A section 2.2.3.8.2 Mode S signal definition. 3. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.b to use the Enhanced Preamble Detection method of RTCA DO-260A Appendix I section I.4.1. 4. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.c to use the Baseline Multi-sample bit and confidence declaration technique of RTCA DO-260A Appendix I section I.4.2.3.1. 5. Garmin was granted a deviation from RTCA DO-185A section 2.4.2.1.1.4. 1. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.3.4.7.3.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 2. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.4.2 to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 3. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.5.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 1-5 Revision 4TP 1.5.2.2 GTS 820 TSO/ETSO TSO-C147 RTCA DO-197A RTCA DO-185A RTCA DO-260A Page 1-6 Revision 4TP Deviation 1. Garmin was granted a deviation from TSO-C147 section 1.c to use RTCA DO-160E, instead of RTCA DO-160D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 2. Garmin was granted a deviation from TSO-C147 Appendix 1 section 1.6 to use selective Mode S interrogations as specified by RTCA DO-185A section 2.2.3.8.1 and 2.2.3.9 following all the applicable protocols for Mode-S surveillance interrogations in the NAS as stated in DO-185A and DO-181C. 1. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185A section 2.2.3.3 instead of the requirement of RTCA DO197A section 2.2.3.2.1 2. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.5 to use the “Mode C Only All-Call” format specified by RTCA DO-185A section 2.2.3.8.1 instead of the “Mode C” format for ATCRBS interrogations. 3. Garmin was granted a deviation from RTCA DO-197A section 2.2.9.1 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity. 4. Garmin was granted a deviation from RTCA DO-197A section 2.2.11 to use the suppression pulse on the aircraft suppression bus specified by RTCA DO-185A section 2.2.3.12 (70 +/-1 µs from top antenna and 90 +/-1 µs from bottom antenna) instead of 100 +/-5 µs. 1. Garmin was granted a deviation to use DO-185A as modified by Appendix 1 of TSO-C119B and ‘RWG Recommended Modification 2.0 to TSO-C119B.’ 2. Garmin was granted a deviation from RTCA DO-185A section 2.2.3.8.2 Mode S signal definition. 3. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.b to use the Enhanced Preamble Detection method of RTCA DO-260A Appendix I section I.4.1. 4. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.c to use the Baseline Multi-sample bit and confidence declaration technique of RTCA DO-260A Appendix I section I.4.2.3.1. 5. Garmin was granted a deviation from RTCA DO-185A section 2.4.2.1.1.4. 1. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.3.4.7.3.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 2. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.4.2 to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 3. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.5.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. GTS 8XX/GPA 65 Installation Manual 190-00587-00 1.5.2.3 GTS 850 TSO/ETSO TSO-C118 RTCA DO-197A RTCA DO-185A RTCA DO-260A Deviation 1. Garmin was granted a deviation from TSO-C118 section a.(2) to use RTCA DO-160E, instead of RTCA DO-160B as the standard for Environmental Conditions and Test Procedures for Airborne Equipment. 1. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185A section 2.2.3.3 instead of the requirement of RTCA DO197A section 2.2.3.2.1. 2. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.5 to use the “Mode C Only All-Call” format specified by RTCA DO-185A section 2.2.3.8.1 instead of the “Mode C” format for ATCRBS interrogations. 3. Garmin was granted a deviation from RTCA DO-197A section 2.2.6 to use selective Mode S interrogations following all the applicable protocols for Mode-S surveillance interrogations in the NAS as stated in DO-185A and DO-181C. 4. Garmin was granted a deviation from RTCA DO-197A section 2.2.9.1 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity. 5. Garmin was granted a deviation from RTCA DO-197A section 2.2.11 to use the suppression pulse on the aircraft suppression bus specified by RTCA DO-185A section 2.2.3.12 (70 +/-1 µs from top antenna and 90 +/-1 µs from bottom antenna) instead of 100 +/-5 µs. 1. Garmin was granted a deviation to use RTCA DO-185A as modified by Appendix 1 of TSOC119B and ‘RWG Recommended Modification 2.0 to TSO-C119B’. 2. Garmin was granted a deviation from RTCA DO-185A section 2.2.3.8.2 Mode S signal definition. 3. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.b to use the Enhanced Preamble Detection method of RTCA DO-260A Appendix I section I.4.1. 4. Garmin was granted a deviation from RTCA DO-185A section 2.2.4.4.2.2.c to use the Baseline Multi-sample bit and confidence declaration technique of RTCA DO-260A Appendix I section I.4.2.3.1. 1. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.3.4.7.3.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 2. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.4.2 to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. 3. Garmin was granted a deviation from RTCA DO-260A section 2.2.4.5.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260A section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185A. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 1-7 Revision 4TP 1.6 Reference Documents The following publications are sources of additional information for installing the GTS 8XX. Before installing the GTS 8XX, the technician should read all referenced materials along with the manual. Part Number 190-00313-11 190-00303-00 190-00303-04 190-00903-00 190-00907-00 Page 1-8 Revision 4TP Document Jackscrew Backshell Installation Instructions G1000 System Installation Manual G1000 Line Maintenance and Configuration Manual G1000 System Maintenace Manual LJ/VLJ G1000 System Maintenance Manual Standard Piston/Turboprop Aircraft GTS 8XX/GPA 65 Installation Manual 190-00587-00 1.7 Limited Warranty This Garmin product is warranted to be free from defects in materials or workmanship for two years from the date of purchase. Within this period, Garmin will at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided that the customer shall be responsible for any transportation cost. This warranty does not cover failures due to abuse, misuse, accident or unauthorized alteration or repairs. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES EXPRESS OR IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE, OR INABILITY TO USE THIS PRODUCT OR FROM DEFECTS IN THE PRODUCT. Some states do not allow the exclusion of incidental or consequential damages, so the above limitations may not apply to you. Garmin retains the exclusive right to repair or replace the unit or software or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, call Garmin Customer Service at one of the numbers shown below. Products sold through online auctions are not eligible for rebates or other special offers from Garmin. Online auction confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace missing components from any package purchased through an online auction. Garmin International, Inc. 1200 E. 151st Street Olathe, KS 66062, U.S.A. Phone: 800/800.1020 FAX: 913/397.0836 GTS 8XX/GPA 65 Installation Manual 190-00587-00 Garmin (Europe) Ltd. Liberty House Bulls Copse Road Hounsdown Business Park Southampton, SO40 9RB, UK Telephone: 44 (0) 8708501241 Page 1-9 Revision 4TP This page intentionally left blank Page 1-10 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 2 2.1 INSTALLATION OVERVIEW Introduction This section provides hardware equipment information for installing the GTS 8XX/GPA 65 and related hardware. Installation of the GTS 8XX/GPA 65 should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B and AC 43.13-2A, where applicable, may be found useful for making retro-fit installations that comply with FAA regulations. 2.1.1 Unit Configurations The GTS 8XX and GPA 65 are available under the following part numbers: Applicable LRU Software Part Numbers Applicable Custom Logic Device Part Numbers Garmin P/N GTS 800, (011-01356-00) 006-B0551-() 006-C0081-() 010-00519-00 GTS 820, (011-01446-00) 006-B0551-() 006-C0081-() 010-00562-00 GTS 850, (011-01553-00) 006-B0551-() 006-C0081-() 010-00563-00 GPA 65, (011-01347-00) 006-B0551-() 006-C0092-() 010-10721-00 Item 2.1.2 Required Accessories NOTE Refer to the Dealer’s Only portion of www.garmin.com for instructions on determining what accessories are needed. Each of the following accessories are provided separately from the GTS 8XX and GPA 65 unit and are required to install the unit. Installation Racks* Garmin P/N GTS 8XX Vertical Installation Rack 115-00781-00 GTS 8XX Horizontal Installation Rack 115-00784-00 * Only one is required. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-1 Revision 4TP For a GTS 800 installation with a single GA 58 directional antenna, two QMA Connector Kits (4 pieces, either straight or right angle) are required. For a GTS 800 installation with dual GA 58 directional antennas, four QMA Connector Kits (4 pieces, either straight or right angle) kits are required. For a GTS 800 installation with a single GA 58 directional antenna and a monopole antenna, two QMA Connector Kits (4 pieces, either straight or right angle) and one QMA Connector Kit (1 piece, either straight or right angle) are required. For GTS 820 and 850 installations, add two QMA Connector Kits (4 pieces, either straight or right angle) for the GPA 65 connections. One QMA Termination Connector Kit (4 pieces) is required for single antenna installations. Connector Kits Garmin P/N QMA Right Angle Connector Kit (4 pieces) 011-01364-00 QMA Straight Connector Kit (4 pieces) 011-01364-01 QMA Right Angle Connector Kit (1 piece) 011-01364-02 QMA Straight Connector Kit (1 piece) 011-01364-03 QMA Termination Connector Kit (4 pieces) 011-01364-04 GTS 8XX Connector Kit 011-01360-00 GPA 65 Circular Connector Kit 011-01365-00 USB-B Pigtail (non-G1000 installations only) 011-01782-00 Antennas GA 58 Directional Antenna, (011-01346-00) Monopole Antenna Garmin P/N 010-10720-00* 010-10160-00 or L-Band Monopole Antenna that meets TSO-C74c *010-10720-00 includes mounting screws and o-ring, unless specifically requested to exclude. Configuration Module Garmin P/N Configuration Module (non-G1000 installations only) 011-00979-20 Page 2-2 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 2.2 Installation Considerations Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are required for installation of the GTS 8XX/GPS 65. 2.2.1 Antenna Considerations Antenna installations on pressurized cabin aircraft require FAA approved installation design and engineering substantiation data whenever such antenna installations incorporate alteration (penetration) of the cabin pressure vessel by connector holes and/or mounting arrangements. For needed engineering support pertaining to the design and approval of such pressurized aircraft antenna installations, it is recommended that the installer proceed according to any of the following listed alternatives: 1. Obtain approved antenna installation design data from the aircraft manufacturer. 2. Obtain an FAA approved STC, pertaining to, and valid for the antenna installation. 3. Contact the FAA Aircraft Certification Office in the appropriate Region and request identification of FAA Designated Engineering Representatives (DERs) who are authorized to prepare and approve the required antenna installation engineering data. 4. Obtain FAA Advisory Circular AC-183C and identify a DER from the roster of individuals in it. 5. Contact an aviation industry organization such as the Aircraft Electronics Association for assistance. For all composite aircraft, antenna installation requires that a ground plane be fabricated on the internal surface of the aircraft directly under the antenna. The TAS/TCAS antenna pattern is dependent upon a ground plane under the antenna. The minimum recommended antenna ground plane dimensions are 18” x 18” for composite aircraft. A fabricated doubler plate assembly supplied by the installing agent or antenna vendor may be required inside the fuselage to complete the antenna hardware installation. NOTE For all GTS 8XX installations, a monopole antenna is recommended if installing an optional bottom mounted antenna on a fixed-gear aircraft, while retractable-gear aircraft may use either a monopole or a directional bottom mounted antenna. The target bearing accuracy may be degraded for bottom directional antenna installations on aircraft with fixed gear. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-3 Revision 4TP 2.2.1.1 TAS/TCAS Antenna Location To achieve proper interrogation and surveillance volumes the following GTS 8XX antenna installation guidelines should be followed. The GTS 8XX requires a top-mounted directional antenna. An optional bottom mounted directional or L-band monopole antenna can be installed in conjunction with the top-mounted directional antenna. Antenna locations are critical to maintain the surveillance coverage across all azimuth and elevation angles. Locations shall be chosen so the top mounted and bottom mounted antenna will represent same range and bearing to an intruder. The mounting location, geometry, and surroundings of the antenna can affect the system performance. The following guidance provides information to aid the installer in ensuring that the most optimum location is selected for the installation of the antenna. Because meeting all of these installations guidelines may not be possible on all aircraft, these guidelines are listed in order of importance to achieve optimum performance. The installer must use best judgment to balance the installation guidelines. Installations must be thoroughly tested to verify that performance degradation as a result of antenna placement is not an issue for the TAS/TCAS system as well as other systems. 1. As far as physically possible, the top directional antenna shall be mounted at the most forward location. 2. The TAS/TCAS antenna(s) shall be mounted on the aircraft skin so that the horizontal base is horizontal to within +/-5° in longitudinal and lateral axes when the aircraft is in level flight. 3. The TAS/TCAS antenna(s) shall be mounted on a flat section of the fuselage to reduce the gap formed between the base plate and the fuselage when normal mounting torque is applied. 4. It is recommended that all antennas be mounted at least 20 inches away (measured from center to center) from the TAS/TCAS antenna(s). 5. Ground plane considerations shall include minimization of any discontinuities such as overlapped un-riveted airframe skins, cowlings, or hatches. It is recommended that all such discontinuities be at least 18 inches from the nearest edge of the TAS/TCAS antenna. 6. For installations using a bottom mounted antenna, it is recommended that the top and bottom antennas be located near the same vertical line through the aircraft such that they represent the same range and bearing to an intruder. 7. The top and bottom mounted TAS/TCAS Antenna shall be as close as possible to the aircraft centerline. 8. It is recommended that no antenna be mounted in front of the TAS/TCAS antenna(s). Page 2-4 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 2.3 Electrical Bonding Electrical equipment, supporting brackets, and racks should be electrically bonded to the aircraft’s main structure. Refer to SAE ARP 1870 section 5 when surface preparation is required to achieve electrical bond. The electrical bond should achieve direct current (DC) resistance less than or equal to 2.5 milliohms to local structure to where the equipment is mounted. Compliance should be verified by inspection using a calibrated milliohm meter. An equivalent OEM procedure may also be substituted. There may be OEM-specific reasons for electrically isolating equipment or having a higher bond resistance. These reasons should be rationalized upon installation approval. In general, Garmin recommends that all GTS 8XX equipment be electrically bonded. The antenna ground plane and doubler plate must be electrically bonded to the antenna baseplate. The electrical bond must achieve direct current (DC) resistance less than or equal to 2.5 milliohms. For composite aircraft, the antenna baseplate must be electrically bonded to the common ground of other installed equipment for lightning purposes. This can be achieved through the antenna mounting screws. 2.4 Cabling and Wiring Use #24 AWG or larger diameter wire for all connections unless otherwise specified. The minimum diameter wire size for all GTS 8XX installation wiring is #24 AWG, except in the case of Aircraft Power and Aircraft Ground and both shall be a minimum of #18 AWG. Refer to Table 2-1 for GPA 65 wiring specifications. A single circuit breaker shall be dedicated to the GTS 8XX unless specifically approved by the manufacturer on a case by case basis, or allowed by the STC. Do not attempt to combine more than one unit on the same circuit breaker unless it is specified on an aircraft manufacturer approved drawing, or STC documentation, for the specific installation requiring a combined configuration. The current rating for each standard density 37-pin D-sub connector pin is 5 Amps, and the current rating for each high density 78-pin D-sub connector pin is 2 Amps. A 14 Vdc installation requires a minimum of two Aircraft Power and two Aircraft Ground wires in the harness. A 28 Vdc installation requires a minimum of one Aircraft Power and one Aircraft Ground wires in the harness. It is the responsibility of the installing agency to take into account wire sizing based on the length and number of wires, current draw of the unit, D-sub connector pin current rating, and the unit’s internal protection requirements. NOTE GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-5 Revision 4TP The maximum wiring length from the GTS 8XX to the GPA 65 is 45 feet. Table 2-1. GPA 65 Minimum Wiring Requirements Line Number of Pins/Wires Length of Wire Wire Gauge Specification +35V Up To 45' #24 AWG Up To 45' #24 AWG Up To 30' #22 AWG Up To 20' #24 AWG Up To 45' #24 AWG Up To 30' #22 AWG Up To 20' #24 AWG Up To 45' #24 AWG +6V -5V Ground The contacts used to facilitate the use of #18 AWG wire for Aircraft Power and Aircraft Ground have expanded-diameter barrels that extend out from the back of the standard D-sub connector body to accommodate the larger diameter wire. Appropriate heat shrink tubing should be utilized to provide sufficient insulation from surrounding contacts. Ensure that routing of the wiring does not come in contact with sources of heat, RF or EMI interference. Check that there is ample space for the cabling and mating connectors. Avoid sharp bends in cabling and routing near aircraft control cables. NOTE All appliance to antenna cabling shall bundle top channels as a group and bottom channels as a group to prevent incorrect wiring between top and bottom channels. A visual inspection shall be performed to verify that all coaxial cables are connected properly, before attempting to operate the equipment. Page 2-6 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 2.4.1 Coaxial Cable The GTS 800 requires two sets of coaxial cable assemblies and the GTS 820/850 requires three sets of coaxial cable assemblies when a directional GA 58 antenna (or other Garmin approved antenna) is used for both top and bottom. Each set consists of four coaxial cable assemblies. Each set of four cables must be assembled using the same type of coaxial cable in order to meet phase and attenuation matching requirements. In order for the system to operate in compliance with manufacturer specifications, the coaxial cable assemblies must not exceed the attenuation specifications as stated in this document. This section explains in further detail the coaxial cable and termination requirements. 2.4.1.1 GTS 800 Installations NOTE A monopole antenna is required if installing an optional bottom mounted antenna on all fixed-gear aircraft. Retractable-gear aircraft can use either a monopole or a directional bottom mounted antenna. A GTS 800 installation with both top and bottom mounted directional antennas uses one set of coaxial cables for the four GTS 800 TOP jacks (J1 TOP, J2 TOP, J3 TOP, J4 TOP) that are connected to the corresponding top antenna jacks J1, J2, J3 and J4. A second set of coaxial cables are used for the four GTS 800 BTM jacks (J1 BTM, J2 BTM, J3 BTM, J4 BTM) that are connected to the corresponding bottom antenna jacks J1, J2, J3 and J4. Each cable assembly shall not exceed the maximum attenuation of 2.5dB at 1090MHz as shown in Figure 2-1. Figure 2-1. GTS 800 Installation with Top and Bottom Directional Antennas If an optional bottom mount monopole antenna is installed, a single coaxial cable must be used to connect the GTS 800 bottom jack J1 BTM to the monopole antenna jack. The coaxial cable assembly shall not exceed the maximum attenuation of 2.5dB at 1090MHz as shown in Figure 2-2 and stated in Table 2-4. Each of the remaining GTS 800 bottom jacks (J2 BTM, J3 BTM, J4 BTM) are to be terminated using a QMA 2 watt termination as specified in Table 2-2. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-7 Revision 4TP Figure 2-2. GTS 800 Installation with Top and Bottom Monopole Antennas If no bottom mount antenna is installed, each of the GTS 800 bottom jacks (J1 BTM, J2 BTM, J3 BTM and J4 BTM) must be terminated with a QMA 2 watt termination as specified in Table 2-2 and shown in Figure 2-3. Figure 2-3. GTS 800 Installation with Top Directional Antennas and No Bottom Antenna Page 2-8 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 2.4.1.2 GTS 820 and GTS 850 Installations GTS 820 and GTS 850 installation with both top and bottom mount directional antennas use one set of coaxial cables for the four GTS 820 or GTS 850 TOP jacks (J1 TOP, J2 TOP, J3 TOP, J4 TOP) that are connected to the corresponding GPA 65 processor unit jacks (J1U, J2U, J3U, J4U). Each top cable assembly shall not exceed the maximum attenuation of 3.0dB at 1090MHz as shown in Figure 2-4 and stated in Table 2-3. Each bottom cable assembly shall not exceed the maximum attenuation of 2.5dB at 1090MHz as shown in Figure 2-4 and stated in Table 2-3. A second set of coaxial cables are used to connect the four GPA 65 antenna jacks (J1A, J2A, J3A, J4A) to the corresponding top antenna jacks (J1, J2, J3, J4). Each cable assembly shall not exceed the maximum attenuation of 0.4dB at 1090MHz as shown in Figure 2-4 and stated in Table 2-3. A third set of coaxial cables are used to connect the four LRU BTM jacks (J1 BTM, J2 BTM, J3 BTM, J4 BTM) to the corresponding bottom antenna jacks (J1, J2, J3, J4). Each cable assembly shall not exceed the maximum attenuation of 2.5dB at 1090MHz as shown in Figure 2-4. Figure 2-4. GTS 820 and GTS 850 Installation with Top and Bottom Directional Antenna If an optional bottom mount monopole antenna is installed, a single coaxial cable must be used to connect the GTS 820 or GTS 850 J1 BTM jack to the monopole antenna jack. The cable assembly shall not exceed the maximum attenuation of 2.5dB at 1090MHz as shown in Figure 2-5 and stated in Table 2-3. Each of the remaining GTS 820 or GTS 850 bottom jacks (J2 BTM, J3 BTM, J4 BTM) are to be terminated using a QMA 2 watt termination as specified in Table 2-2. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-9 Revision 4TP Figure 2-5. GTS 820 and GTS 850 Installation with Top Directional and Bottom Monopole Antenna If no bottom mount antenna is installed, each of the GTS 820 or GTS 850 bottom jacks (J1 BTM, J2 BTM, J3 BTM and J4 BTM) shall be terminated with a QMA 2 watt termination as specified in Table 2-2 and shown in Figure 2-6. Figure 2-6. GTS 820 and GTS 850 Installation with Top Directional and No Bottom Antenna Page 2-10 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 NOTE Any QMA terminations used other than those specified in Table 2-2 will constitute the installation as being non-compliant with the manufacturer’s installation standards. 2.4.1.3 Fabrication of Coaxial Cable Assemblies The installing agency may fabricate cable assemblies by terminating either M17/128-RG400 or M17/60-RG142 coaxial cable with available QMA connector kits. Table 2-2 lists recommend cable types to be used with specified QMA connectors for the GTS 8XX. Table 2-2. Cable Types and QMA Connectors Connector Type QMA Right Angle Cable Type Manufacturer Connector Part Number RG 400, RG 142, ECS 311901 Amphenol 930-189P-51A Garmin 330-00500-00 Amphenol 930-191P-51A ECS 930-191P-51A PIC 110477 Amphenol 930-192P-51S Garmin 330-00500-01 Amphenol 930-190P-51S ECS 930-190P-51S PIC 110476 Amphenol 930-187P-51T ECS 311501, ECS 311601, ECS 421601, PIC S67163 RG 400, RG 142, ECS 311901 QMA Straight QMA 50 Load Termination ECS 311501, ECS 311601, ECS 421601, PIC S67163 Garmin Order Number 4 Piece Kit 1 Piece Kit 011-01364-00 N/A 011-01364-01 N/A 011-01364-03 N/A 011-01364-04 Garmin 011-01364-02 N/A 330-00500-02 The recommended coaxial cable lengths in Table 2-3 are for reference only. Along with standard MIL-C17/128-RG400 or MIL-C-17/60-RG142, Table 2-3 lists recommended antenna cable vendors along with the cable type that each specific vendor offers. The recommended coaxial cable lengths are defined as the end to end length of a non-terminated coaxial cable. The attenuation values listed in Table 2-3 include the maximum attenuation of both the maximum length of coaxial cable and two RF coaxial connectors at a frequency of 1090 MHz. It is the installing agencies responsibility to ensure that the coaxial cable assemblies built meet the manufacturer’s attenuation specifications in order to comply with the manufacturer’s installation standards. NOTE Any in-line or bulkhead penetrations must be evaluated separately. It is the installing agency’s responsibility to show airworthiness of the installed fabricated or purchased coaxial cable assemblies. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-11 Revision 4TP Table 2-3. Recommended Coaxial Length Loss of 2.5 dB Loss of 3.0 dB RG Type 1' 10" [0.55m] 2' 7" [0.79m] 9' 0" [2.74m] 12' 0" [3.66m] 15' 5" [4.70m] 18' 8" [5.68m] 15.5 M17/128 -RG400 RG-400 2' 0" [0.60m] 2' 9" [0.84m] 10' 5" [2.94m] 13' 0" [3.96m] 16' 6" [5.03m] 20' 1" [6.12m] 14.45 M17/60RG142 RG-142 2' 5" [0.74m] 3' 4" [1.02m] 11' 6" [3.50m] 15' 5" [4.70m] 19' 6" [5.94m] 23' 10" [7.26m] 12.16 311901 3' 3" [0.99m] 4' 6" [1.37m] 15' 8" [4.77m] 21' 0" [6.40m] 26' 8" [8.13m] 32' 7" [9.93m] 8.93 421601 3' 5" [1.04m] 4' 6" [1.37m] 16' 1" [4.90m] 21' 5" [6.55m] 27' 6" [8.38m] 33' 6" [10.21m] 8.7 311601 M17/127 -RG393 RG-393 4' 2" [1.27m] 5' 7" [1.70m] 19' 8" [5.99m] 26' 5" [8.05m] 33' 5" [10.19m] 40' 10" [12.44m] 7.12 311501 4' 0" [1.21m] 5' 5" [1.60m] 18' 5" [5.61m] 25' 0" [7.62m] 31' 6" [9.60m] 38' 3" [11.65m] 7.5 Supplier Information Page 2-12 Revision 4TP PIC Type Loss of 2.0 dB ECS Type Loss of 1.5 dB (dB/100ft) Loss of 0.5 dB Attenuation Loss of 0.4 dB MIL-C-17 Type Attenuation S67163 Vendor: Electronic Cable Specialists Vendor: PIC Wire and Cable 5300 W. Franklin Drive Franklin, WI 53132 Tel: 800327-9473 414-4215300 Fax: 414421-5301 N53 W24747 Corporate Circle Sussex, WI 530890330 Tel: 800742-3191 262-2460500 Fax: 262246-0450 www.ecsdirect.c om www.picwire.c om See current issue of Qualified Products List QPL-17. RG types are obsolete and are shown for reference only; replaced by M17 type numbers. GTS 8XX/GPA 65 Installation Manual 190-00587-00 The coaxial cable lengths in each coaxial cable assembly set used to connect the GTS 800 TOP and BOTTOM jacks to the top and bottom antenna jacks, the TOP GTS 820 or GTS 850 jacks to the GPA 65 jacks, and the BOTTOM GTS 820 or GTS 850 jacks to the directional antenna jacks, shall be within 2 inches of each other. The coaxial cable assembly lengths in each coaxial cable assembly set between the GPA 65 jacks and directional antenna jacks for the GTS 820 or GTS 850 shall be within 0.25 inches of each. Table 2-4. Coaxial Cable Set Length Tolerance Coaxial Cable Set Length Tolerance* GTS 800 TOP/BOTTOM to top and bottom antenna 2" of each other GTS 820 and/or 850 TOP to GPS 65 2" of each other GTS 820 and/or GTS 850 BOTTOM to directional antenna 2" of each other GPA 65 to directional antenna (for the GTS 820 and/or GTS 850 0.25" of each other * Ensure cables do not exceed the maximum lengths as stated in Table 2-3. NOTE It is recommended that a color band be placed on both ends of each cable to match the color marking designating the mating jack connector. NOTE It is recommended that the nominal end to end coaxial cable (non-terminated) length for each set be recorded for the specific installation in the event that a particular coaxial cable assembly associated with an installed set should require replacement. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-13 Revision 4TP 2.4.1.4 Coaxial Cable Assembly Instructions The following assembly instructions apply to coaxial cables assemblies using QMA connectors specified in Table 2-2 for use with RG-400 or RG-142 cable types: 1. Slide the heat shrink sleeve and crimp ferrule onto the cable. 2. Strip the cable to the dimensions shown in Figure 2-7. Figure 2-7. RG-400/RG-142 Coaxial Cable Stripping Dimensions 3. Slide the center contact onto the center conductor of the cable. Ensure the center conductor of the cable is visible through the inspection hole of the center contact and crimp using Tyco tool 354940-1 and die assembly 220189-3, or Tyco tool 354940-1 and die assembly 91901-1, or Tyco tool 69478-1. 4. Expand the shielding braid and insert the crimped center contact into the connector body until the cable dielectric is flush with the dielectric inside the connector body. Insure the shield braid does not enter the connector body. Figure 2-8. Ferrule and Crimp Die Positioning 5. Slide the crimp ferrule over the shielding braid to the back of the connector body. Position the crimp tool flush with the back of the connector body and crimp using Tyco tool 35940-1 and die assembly 220189-3, or Tyco tool 354940-1 and die assembly 91901-1, or Tyco tool 69478-1. The crimp tool should be positioned such that a “bellmouth” (see figure 2-8) is present in the crimp ferrule on the coaxial cable side of the crimp after crimping. 6. Slide heat shrink sleeve to back of connector body and shrink in place. Ensure that the heat shrink does not protrude past the connector body back end once it is shrunk into place. It is recommended that the color-coded heat shrink tubing provided in the kit be used. Page 2-14 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 Figure 2-9. Heat Shrink Positioning NOTE Use of QMA connectors other than those specified in Table 2-2 for coaxial cable assemblies fabricated by the installing agency using either M17/128-RG400 or M17/60-RG142 coaxial cable will constitute the cable assemblies as being non-compliant with the manufacturer’s installation standards. 2.4.1.5 Coaxial Cable Assembly Repair and Rework In the event that an individual coaxial cable assembly requires rework, between a GTS 800 jack and antenna jack, a TOP GTS820/850 jack and GPA 65 jack or a BTM GTS 820/850 jack and antenna jack, the repairable coaxial cable may be reduced in length a maximum of two inches. In the event that rework is required on a coaxial cable assembly between a GPA 65 jack and antenna jack on a GTS 820/850 installation, complete replacement of the cable assembly shall be required in lieu of rework. Refer to Table 2-3 for recommended maximum cable assembly lengths for cable assemblies fabricated by the installer. 2.5 Cooling Requirements The GTS 8XX and GPA 65 meet all TSO requirements without external cooling. A 5/8” diameter air fitting is provided on the rear of the GTS 8XX for the purpose of admitting cooling air if desired. If a form of forced air cooling is installed, make certain that rainwater cannot enter and be sprayed on the equipment. For G1000 installations refer to the G1000 System Installation manual, Garmin part number 190-00303-00, for more information on cooling requirements. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 2-15 Revision 4TP 2.6 Mounting Requirements The GTS 8XX can be mounted vertically or horizontally using the installation racks shown below. Refer to Appendix A for outline and installation drawings. Figure 2-10. GTS 8XX Vertical Installation Rack (Garmin P/N115-00781-00) Figure 2-11. GTS 8XX Horizontal Installation Rack (Garmin P/N115-00784-00) Page 2-16 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 3 INSTALLATION PROCEDURE 3.1 Unpacking Unit Carefully unpack the equipment and make a visual inspection of the unit for evidence of damage incurred during shipment. If the unit is damaged, notify the carrier and file a claim. To justify a claim, save the original shipping container and all packing materials. Do not return the unit to Garmin until the carrier has authorized the claim. Retain the original shipping containers for storage. If the original containers are not available, a separate cardboard container should be prepared that is large enough to accommodate sufficient packing material to prevent movement. 3.2 Wiring Harness Installation Allow adequate space for installation of cables and connectors. The installer shall supply and fabricate all of the cables. All electrical connections are made through two 78-pin high-density D subminiature connectors, one 37-pin standard density connector, and one 19-pin circular connector (GTS 820 and GTS 850 only). Section 4 defines the electrical characteristics of all input and output signals. Required connectors and associated hardware are supplied with the connector kit. See Appendix B for examples of interconnect wiring diagrams. Construct the actual harness in accordance with aircraft manufacturer authorized interconnect standards. Table 3-1. Socket and Pin Contact Part Numbers 78 Pin High Density D-Subminiature Connectors P8001 & P8002 37 Pin Standard Density D-Subminiature Connector P8003 19 Pin Circular Connector P651 Manufacturer High Density Pin (P8001 & P8002) Standard Socket (P8003) Circular Connector Socket (P651) Standard Socket (P8003) Garmin P/N 336-00021-00 336-00022-00 N/A 336-00023-00 Military P/N M39029/58-360 M39029/63-368 M39029/5-115 N/A Positronic FC6018D AMP 205090-1 ITT Cannon 031-1007-042 031-1007-054** *Identify manufacturer part number by MIL SPEC identification ** Use only positioner part numbers ITT Cannon 980-0005-722, Astro Tools 616245 and Daniels MFG K250 Table 3-2. Socket Contact MIL SPEC M39029/5-115 Crimp Tooling Manufacturer Hand Crimping Tool Positioner Insertion/Extraction Tool Tools Option 1 Military P/N M22520/1-01 M22520/1-02 M81969/14-11* Daniels AF8 TH1A M81969/14-11* Tools Option 2 Military P/N M22520/2-01 M22520/2-02 M81969/14-11* Daniels AFM8 K1S M81969/14-11* * Indicates plastic insertion/extraction tool GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-1 Revision 4TP Table 3-3. Pin Contact GPN 336-00021-00 MIL SPEC M39029/58-360 Crimp Tooling Manufacturer Hand Crimping Tool Positioner Insertion/Extraction Tool Military P/N M22520/2-01 M22520/2-09 M81969/1-04 Daniels AFM8 K42 M81969/1-04 Positronics 9507 9502-4 M81969/1-04 ITT Cannon 995-0001-584 M22520/2-09 274-7048-000* MIL SPEC M81969/14-01 Tyco-AMP 601966-1 601966-6 91067-1 MIL SPEC M81969/1-04 Astro 615717 615725 M81969/1-04 Amphenol 9507 9502-4 M81969/1-04 * Indicates plastic insertion/extraction tool Table 3-4. Pin Socket Contacts GPN 336-00022-00 MIL SPEC M39029/63-368 and GPN 336-00023-00 Crimp Tooling Manufacturer Hand Crimping Tool 22 AWG Socket Contact GPN 336-00022-00 (M39029/63-368) 18 AWG Socket Contact GPN 336-00023-00 Positioner Insertion/Extraction Tool Positioner Insertion/Extraction Tool Military P/N M22520/2-01 M22520/2-08 M81969/1-02 N/A M81969/1-02 Daniels AFM8 K13-1 M81969/1-02 K774 M81969/1-02 Positronics 9507 9502-5 M81969/1-02 9502-11 M81969/1-02 980-2000-426* 980-0005-722** or Daniels K250** N/A ITT Cannon 995-0001-584 995-0001-604 Tyco-AMP 601966-1 601966-5 91067-2 or M81969/1-02 N/A N/A ASTRO 615717 615724 M81969/1-02 616245** N/A Amphenol 9507 N/A N/A 9502-11 M81969/1-02 * Indicates plastic insertion/extraction tool ** Use only positioner part numbers ITT Cannon 980-0005-722, Astro Tools 616245 and Daniels MFG K250 for contact part number ITT Cannon 031-1007-001 Page 3-2 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 NOTES 1. Non-Garmin part numbers shown are not maintained by Garmin and consequently are subject to change without notice. 2. Extracting a contact used for #18 AWG requires that the wire barrel be cut off from the contact. It may also be necessary to push the pin out from the face of the connector when using and extractor due to the absence of the wire. A new contact must be used when reassembling the connector. 3. Contacts for #16 AWG and Contact Crimp Tooling: Contact Garmin for information regarding contacts and contact crimp tooling. Note 2 also applies. 4. Alternate Contacts for Use With #18 AWG: As an alternative to the Positronic contacts listed, and provided in the installation kit, if the need arises the installer may use contacts made by ITT Cannon under P/N 031-1007-001. The particular contact is not compatible with the Daniels MFG K774, Positronics 9502-11 or Amphenol 9502-11 positioners, though. Only use postioner part numbers Daniels MFG K250, ITT Cannon 980-0005-722 and Astro 616245. 3.3 QMA Connector Insertion and Removal To engage the QMA connectors, use the outer sleeve of the QMA plug to align the connectors and insert the plug onto the jack until it snaps into place. There will be an audible “snap” when the connectors are fully engaged, refer to Figure 3-1. No tools are required for the insertion of a QMA plug onto a QMA jack. Engage Outer Sleeve Figure 3-1. Engaging QMA Connectors GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-3 Revision 4TP CAUTION Do not pull on the cable when removing the QMA plug from the jack. To disengage the QMA connectors, pull back firmly on the outer sleeve of the QMA plug away from the jack connector (refer to Figure 3-2). This will disengage the locking mechanism that secures the plug connector to the jack connector. Pulling on or disengaging the QMA connectors in any other way is not recommended and may cause damage to both the connectors and coaxial cable. Disengage Outer Sleeve Figure 3-2. Disengaging QMA Connectors CAUTION Side-loading of the QMA connectors should be avoided during both the insertion and removal of the connectors. It is recommended service loops with adequate length of coaxial cable be used to insure that side-loading on the connectors is minimized once the cable is securely fastened in the aircraft. Excessive side-loading may result in damage or premature failure of the QMA connectors. Page 3-4 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 3.4 Backshell, Pigtail Circular Connector, and Configuration Module Assemblies The GTS 8XX connector kits includes three Garmin backshell assemblies. The backshell assembly houses the configuration module, if applicable. Garmin’s backshell also gives the installer the ability to easily terminate shield grounds at the backshell housing. Refer to the Jackscrew Backshell Installation Instructions (Garmin part number 190-00313-11) for backshell assembly instructions. Refer to the GPA 65 Pigtail Circular Connector Installation Instructions (Garmin part number 190-00313-XX) for pigtail assembly instructions. Refer to the Jackscrew Configuration Module Installation Instructions (Garmin part number 190-00313-10) for configuration module assembly instructions. 3.5 Unit Installation Refer to the outline and installation drawings shown in Appendix A of this manual GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-5 Revision 4TP 3.5.1 Post Installation Configuration & Checkout Before beginning the installation calibration, the installer must perform a visual inspection to verify the coaxial cables are installed correctly based upon the system and antenna configuration. NOTE Tests performed with a ramp tester should be performed away from buildings that may reflect the signal. Local air traffic control should be advised if the ramp tester has an altitude programmed into it that may cause interaction with other TCAS-equipped traffic. The following actions need to be performed after the equipment is installed: 1. GTS 8XX Configuration Options 2. CDTI (Cockpit Display of Traffic Information) Display setup and configuration 3. Calibration 4. Self test 5. Ramp test and return to service tests 6. Antenna verification 3.5.2 GTS 8XX Configuration Options GTS 8XX Configuration is performed using a computer (installed with Microsoft Windows XP or later) and the GTS 8XX Install Tool, Garmin part number 006-A0242-00. The tool is available for download from the Dealers Only portion of the Garmin website (www.garmin.com). G1000 Installations: When installed as part of the G1000 integrated flight deck, the GTS 8XX must have FAA approved configuration data. Configuration data is loaded to the GTS 8XX from an aircraft-specific G1000 software loader card. For basic configuration information refer to the G1000 Line Maintenance and Configuration Manual (190-00303-04), G1000 System Maintenance Manual LJ/VLJ (190-00903-00), or the G1000 System Maintenance Manual Standard Piston/Turboprop Aircraft (190-00907-00). For actual installation/checkout, use only aircraft manufacturer approved or STC checkout procedures. Non-G1000 Installations: Configuration and software uploading is accomplished by using a computer (installed with Microsoft Windows XP or later) and the GTS 8XX Install Tool. An optional USB pigtail installed in the wiring harness may be used. The GTS 8XX Install Tool allows for configuration, diagnostics, and upload of GTS 8XX software. The following GTS 8XX modes are accessible with the GTS 8XX Install Tool. • Normal Mode – Allows selection of Traffic Mode to Standby, Operate, or Test. Reports System Faults, Status Flags, and Operating Status. Allows Ground Test Mode to be Enabled or Disabled. • Configuration Mode – Allows selection of installation options • Upload Mode – Allows upload of software to GTS 8XX unit • Debug Mode – Runs system diagnostics Page 3-6 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 3.5.2.1 Normal System Mode Tab The Normal tab displays various faults, flags, and operational information. When the Normal tab is selected, the unit is commanded to Normal System Mode. Figure 3-3. GTS 8XX Install Tool – Normal Tab Normal Mode – System Faults: Red Bold text indicates that a fault is active. Gray text indicates that there is no active fault. (System Faults are described in the Self-Test section.) Status Flags: Black Bold text indicates that a flag is set. Gray text indicates that the flag is not set. (Status Flags are described in the Self-Test section.) Traffic Mode Status: Standby – Unit is not transmitting or receiving data Operate – Unit is interrogating and processing received data Test – Allows special transmit interrogation rates and data patterns to be initiated (Selected mode is active.) Ground Test: Enabled Disabled (Ground Test is described in the Ramp Test and Return to Service Tests section. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-7 Revision 4TP 3.5.2.2 Configuration System Mode Tab The Configuration tab displays configuration data and allows the installer to change the installation configuration. When the Configuration tab is selected, the unit is commanded to Configuration System Mode. Figure 3-4. GTS 8XX Install Tool – Configuration Tab (GTS 800) Page 3-8 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 Figure 3-5. GTS 8XX Install Tool – Configuration Tab (GTS 820 and GTS 850) The Configuration tab displays installation configuration options. Changes made in the Configuration tab are not immediately committed to the GTS. Changed options will be colored yellow until ‘Set Active’ is selected. Configuration Mode – Barometric Altitude Source: Note: At least one source must be selected (same altitude source used for the transponder). Primary A429 RX Channels 1 - 6 or Disabled Secondary A429 RX Channels 1 - 6 or Disabled COM RS-232 Ports 1 - 5 or Disabled Magnetic Heading Source (optional): Primary A429 RX Channels 1 - 6 or Disabled Secondary A429 RX Channels 1 - 6 or Disabled Radio Altitude Source (optional): A429 A429 RX Channels 1 - 6 or Disabled Analog Disabled ARINC 552 ARINC 552A Bonzer MK10X Collins ALT50 Collins ALT55 King KRA10 King KRA405 Sperry AA100 Terra TRA3000 Terra TRA3500 GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-9 Revision 4TP GPS Position/Velocity/Time Source: Note: At least one source required for ADS-B IN functionality. Primary A429 RX Channels 1 - 6 or Disabled Secondary A429 RX Channels 1 - 6 or Disabled Traffic Display Destination: Note: At least one source is required. Primary A429 TX Channels 1 - 6 or Disabled COM RS-232 Ports 1 - 5 or Disabled Transponder 1 & 2 Communication: Note: At least Transponder 1 RX and TX required for GTS 820 and GTS 850. Primary should be configured for channels wired to Transponder 1. Secondary should be configured for channels wired to Transponder 2 in a dual transponder installation. Primary RX A429 RX Channels 1 - 6 or Disabled Primary TX A429 TX Channels 1 - 6 or Disabled Secondary RX A429 RX Channels 1 - 6 or Disabled Secondary TX A429 TX Channels 1 - 6 or Disabled Top Antenna: Model Cable loss (dB) Bottom Antenna: Model Cable loss (dB) None Monopole Garmin GA58 Sensor Systems 0.2 – 4.0 Note: Cable loss information is described in Fabrication of Coaxial Cable Assemblies section. None Monopole Garmin GA58 Sensor Systems 0.2 – 4.0 Note: Cable loss information is described in Fabrication of Coaxial Cable Assemblies section. Note: All A429 options have the ability to select High or Low speed. Note: Page 3-10 Revision 4TP 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. GTS 8XX/GPA 65 Installation Manual 190-00587-00 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. ADSB TX Capable: Indicate whether aircraft is equipped with ADS-B transmitter. Squat ‘on-ground’ Sense: Indicate type of sense switch. Mode S ID (HEX): Applicable to GTS 820 and GTS 850 only. 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 8XX. Revert Changes: Select to show current GTS 8XX settings. An incorrect configuration will be reverted back to previous settings. Note: Default is “disabled” for all inputs and outputs. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-11 Revision 4TP 3.5.2.3 Upload System Mode Tab The Upload tab displays version information for Boot Block, Region List, System, FPGA, Audio, Magnetic Variation. Boot Block updating is not allowed. For other files, select the appropriate image files and select upload. Figure 3-6. GTS 8XX Install Tool – Upload Tab 3.5.2.4 Debug Tab The Debug tab is reserved and not available for field installation use. Page 3-12 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 3.5.3 CDTI Display Setup and Configuration For configuration of the displays, refer to their respective installation manuals. • • • • • 3.5.4 500 Series Installation Manual (190-00181-02) GMX 200 Installation Manual (190-00607-04) GDU 620 Installation Manual (190-00601-04) G1000 Line Maintenance and Configuration Manual (190-00303-04) G1000 System Maintenance Manual LJ/VLJ (190-00903-00) Self Test A self-test feature tests the (aural) alarm, attempts self calibration, and activates each display element in a pre-determined sequential pattern to allow visual verification that display outputs issued by the digital processor can be correctly interpreted by the pilot. NOTE Self tests may be performed indoors but signal multi-path from building walls may be a factor. If problems are experienced, self tests should be performed outside away from buildings, and where local traffic is not a factor. With the GTS 8XX powered up and Standby indicated on the CDTI, cycle the GTS 8XX to Self Test. The self test feature of the GTS 8XX tests the following internal parameters as well as performs calibration of various components in the GTS 8XX: a) Calibration data fault – Stored factory calibration parameters are invalid. Return unit to Garmin for service. b) Configuration data fault – Stored system configuration parameters are invalid or Mode S address is invalid (All 0’s or F’s ). Fault will persist until configuration is corrected. Attempt configuration per the Configuration Section. c) FPGA fault – Check of the FPGA image failed. Fault will persist until valid FPGA image is loaded. If upload of FPGA image was recently attempted, retry the upload. Otherwise, return unit to Garmin for service. d) ROM fault – Internal non-volatile memory failure, or invalid data image detected. If upload of audio image or IGRF magnetic field image was recently attempted, retry the upload. Otherwise return unit to Garmin for service. e) Execution fault – CPU execution fault has occurred. Cycle power and retry self test. If fault persists, return unit to Garmin for service. f) Electrical fault – One of the internal electrical voltages are out of range. Fault will persist until power is cycled. Check aircraft power supply. If fault persists, return unit to Garmin for service. g) Whisper Shout fault – Transmitted power is out of tolerance. Check cable loss configuration, antenna installation and all cable connections and retry self test. If fault persists, return unit to Garmin for service. h) Transmit Power fault - One of the internal transmitter power source voltages are out of range. Fault will persist until power is cycled. Check aircraft power supply. If fault persists, return unit to Garmin for service. i) 1030 MHz Frequency Source fault - Transmit Frequency synthesizer is not locked. Cycle power and retry self test. If fault persists, return unit to Garmin for service. j) 1090 MHz Frequency Source fault - Receive Frequency synthesizer is not locked. Cycle power and retry self test. If fault persists, return unit to Garmin for service. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-13 Revision 4TP k) Receiver Calibration fault. Check antenna installation and all cable connections and retry self test. Ensure that self test occurs in area free of buildings and large objects that can reflect signals. If fault persists, return unit to Garmin for service. NOTE Receiver self-calibration is performed prior to the transmitter self-calibration. In the event that a receiver calibration fault occurs, a transmitter self-calibration will not be performed. l) Transmitter Calibration fault. Check antenna installation and all cable connections and retry self test. Ensure that self test occurs in area free of buildings and large objects that can reflect signals. If fault persists, return unit to Garmin for service. NOTE A transmitter self-calibration can only be performed after a successful receiver selfcalibration. m) Barometric Altitude Input fault – Own ship barometric altitude calculation is invalid or has timed out. Check wiring to source of barometric altitude and ensure that source is operating. Fault will clear as soon as valid barometric altitude data is received. n) Main Board Temperature fault – Main board temperature or RF receiver temperature is greater than 90° Celsius or less than -60° Celsius. Fault will persist until internal temperature returns to acceptable range. o) TCAS Equipage Timeout fault – TCAS Equipage data is not being received or has timed out for 800ms. Check wiring to TCAS Equipage data source and ensure that source is operating. Fault will clear as soon as valid TCAS Equipage data is received. The self test feature also checks the following external parameters: a) Mag Variation – Magnetic variation data (difference between ‘True’ North and Magnetic North) is available. b) GPS Status – GPS Position, Velocity and Time data is available c) Display #1 status - Check of Traffic display #1 discrete input is inactive for 2 or more seconds. d) Display #2 status - Check of Traffic display #2 discrete input is inactive for 2 or more seconds. e) Radio Altimeter Input status – Radio altimeter is installed and radio altimeter input status is inactive. f) Magnetic Heading Input status – Invalid magnetic heading data is received. g) Maintenance/Data logger Input status – Data logger is inhibited if active. h) Self Test Inhibit status – Self test is inhibited if active. Page 3-14 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 When the display receives an indication that a pilot initiated Self Test is in progress, this state is clearly annunciated on the traffic display and the following test patterns will be executed. Figure 3-7. Self Test Table 3-5. Self Test Intruder #1 (transmitted in intruder number field) 2.0 NM Vertical Rate = Climbing, relative altitude = –200 feet TA, Bearing = –90 degrees Intruder #2 (transmitted in intruder number field) 3.625 NM Vertical Rate = Descending, relative altitude = –1,000 feet Prox Traffic, Bearing = +33.75 degrees Intruder #3 (transmitted in intruder number field) 3.625 NM No vertical rate, relative altitude = +1,000 feet Other traffic, bearing = –33.75 degrees. Audio annunciation shall be: GTS 800/820 - “TAS system Passed” or “TAS system Failed” GTS 850 - “TCAS system Passed” or “TCAS system Failed” Any faults and flags are also displayed on the Normal tab of the GTS8XX Install Tool. Faults that occur will be colored in red and flags will be colored in black. If self test fails, refer to the diagnostics data to determine a cause. Insure that no Intruder appears at close range to own aircraft. NOTE If the intruder appears at close range to own aircraft, verify that the mutual suppression line is connected between GTS 8XX and other L-band equipment (transponder, DME, etc.). GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-15 Revision 4TP 3.5.5 Ramp Test and Return To Service Test Using a ramp tester, such as a TIC TR220 or equivalent, make the following setup and measurements to verify GTS 8XX operational and surveillance functional. To select a scenario that will properly converge and intercept the GTS 8XX, the GTS 8XX must be in Ground Test mode. To enable Ground Test mode, the aircraft must be on the ground and the GTS 8XX must be in Normal System mode and in Standby. Activate ground test mode by clicking ‘Enable’ in the Ground Test field on the Normal tab of the GTS 8XX Install Tool. Figure 3-8. Ground Test This simulates the GTS to be airborne at 50,000 ft with magnetic heading of 0°. NOTE The GTS 8XX will not accept the Ground Test command unless the unit is in Standby and the squat switch indicates the aircraft is on the ground. Position the test set directional antenna with a clear line of sight to the GTS 8XX antenna at 90 degrees. With the GTS 8XX powered up and in Standby mode indicated on the CDTI, cycle the GTS 800 to “Operate”. Select the following scenario: Set the intruder type as ATCRBS. Intruder Start Distance Intruder Start Altitude 10 NM 50,000 ft Vertical Speed 0 fpm. Velocity 360 Kts Initiate the intruder scenario and observe the following: • • • Page 3-16 Revision 4TP Traffic should be acquired at approximately 10 NM at 90 degree bearing and co-altitude. Observe intruder closes on own aircraft at a rate of .1 NM/sec. The intruder should transition from Other Traffic (displayed as an open diamond with 00 displayed above), to proximate traffic (displayed as a filled white diamond with 00 displayed above), to a Traffic Advisory (TA) alarm. The appropriate TA symbology (yellow filled circle with 00 displayed above, and an audio annunciation of "Traffic! 3 O'clock! At Altitude! 3 Miles!"), displayed when the intruder approaches within 3 NM. GTS 8XX/GPA 65 Installation Manual 190-00587-00 3.5.6 Antenna Verification The first step in antenna verification is to verify auto-calibration operates without indicating a fault. 1. With the GTS 8XX powered up and “Standby” indicated on the CDTI cycle the GTS 8XX to “Operate”. Each time the GTS 8XX transitions between these modes a self test of the antenna circuit is initialized. If the antenna connection is not correct the CDTI will display “Failure” indicating it will be necessary to recheck the antenna coaxial connections. If the CDTI displays “Operate” without indicating a fault, proceed to the next step of antenna verification. Using a ramp tester, such as a TIC TR220 or equivalent, make the following set up and measurements to assure the antenna is properly connected and the GTS 8XX is operational. 2. Position the test set directional antenna with a clear line of sight to the GTS8XX antenna. 3. Ensure that the transmitter or receiver (RX/TX) that you are testing is significantly closer to the ramp tester than another operating RX/TX, or erroneous and inaccurate results may occur. All four quadrants (forward, starboard, aft, and port) will be similarly tested to verify bearing of simulated intruder supplied via the ramp tester are correctly displayed on the CDTI. 4. Using the ramp tester, select the proper antenna gain and distance to aircraft. 5. Position ramp test set at 0 degrees. 6. Turn the test set on. 7. Connect the directional antenna to the ramp test set. 8. Set the multifunction test set to perform “TCAS” testing. Configure the GTS 8XX to the normal operating mode. 9. Program a static intruder per the following scenario: NOTE See ramp test set operators manual to set the following parameters Intruder Start Distance 2 NM Intruder Start Altitude 50,000 Vertical Speed 0 fpm. Velocity 0 Kts 10. Set the intruder type as ATCRBS. 11. Verify a target is annunciated on the GTS 8XX TAS/TCAS display at the correct bearing of approximately 0 degree azimuth at 2 NM and co-altitude (read as 00 above a filled diamond indicating proximate traffic). 12. Toggle intruder traffic to standby or off. 13. Reposition ramp test set and directional antenna to a starboard position of 90 degrees. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-17 Revision 4TP 14. Reengage the same intruder scenario as above. 15. Verify a target is annunciated on the GTS 8XX TAS/TCAS display at the correct bearing of approximately 90 degree azimuth at 2 NM and co-altitude. 16. Toggle intruder traffic to standby or off. 17. Reposition ramp test set and directional antenna to an aft position of 180 degrees. 18. Reengage the same intruder scenario as above. 19. Verify a target is annunciated on the GTS 8XX TAS/TCAS display at the correct bearing of approximately 180 degree azimuth at 2 NM and co-altitude. 20. Toggle intruder traffic to standby or off. 21. Reposition ramp test set and directional antenna to a port position of 270 degrees. 22. Reengage the same intruder scenario as above. 23. Verify a target is annunciated on the GTS 8XX TAS/TCAS display at the correct bearing of approximately 270 degree azimuth at 2 NM and co-altitude. 24. Toggle intruder traffic to standby or off. 25. If the bearing is not as anticipated, recheck the antenna coaxial connections and verify the correct antenna type is selected. NOTE If multiple targets are displayed during the antenna tests, recheck the antenna coaxial connections. Page 3-18 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 3.6 GA 58 Antenna Installation Refer to the GA 58 installation drawing shown in Appendix A of this manual. CAUTION Do not use construction grade RTV sealant or sealants containing acetic acid. These sealants may damage the electrical connections to the antenna. Use of these type sealants may void the antenna warranty. 1. Refer to the GA 58 installation drawing shown in Appendix A for the mounting cutout. 2. For composite aircraft, fabricate a ground plane under the antenna base plate on the internal surface of the aircraft with recommended minimum dimensions of 18” x 18”, with center of ground plane under the center of the antenna baseplate. Refer to notes in Antenna Considerations section and Electrical Bonding section of this document. 3. For metal skin aircraft, do NOT remove paint on outer skin of aircraft under the footprint of the antenna baseplate. The painted surface prevents corrosion. 4. Install a doubler plate to reinforce the aircraft skin as necessary. 5. Place the supplied O-ring, 251-00011-00, in the groove on the bottom surface of the antenna. 6. Mount the antenna to the airframe with the four supplied #8-32 stainless steel screws, 21160209-16. Washers and locking nuts (not provided, may be part of doubler plate) are required to secure the antenna. Apply torque evenly across all mounting screws. 7. Ensure that the antenna base and aircraft skin are in continuous contact. 8. Fillet seal the antenna and gasket to the fuselage using a good quality electrical grade sealant, MIL-S-8802B or equivalent. Run a bead of the sealant along the edge of the antenna where it meets the exterior aircraft skin. Use caution to ensure that the antenna connector is not contaminated with sealant. Seal the mounting screws with sealant. 9. Connect the four antenna cables ensuring each cable is connected to the correct antenna connector. Each antenna connector and cable has a matching color band. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 3-19 Revision 4TP 3.7 GPA 65 PA/LNA Installation Refer to the GPA 65 installation drawing shown in Appendix A of this manual. 1. Assemble the wiring harness and circular connector per Section 3.4. 2. Assemble the coaxial cables per Section 2.4.1. 3. Mount the unit to a suitable mounting location using #8-32 pan head screws (4 ea) (not provided). 4. Connect the circular connector and eight coaxial cables ensuring each coaxial cable is connected to the correct jack connector. Each jack connector and cable has a matching color band. 3.8 Continued Airworthiness Maintenance of the GTS 8XX and GPA 65 is “on condition” only. Page 3-20 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 4 SYSTEM INTERCONNECTS 4.1 GTS 8XX Pin Function List 4.1.1 P8001 (Digital) View of J8001 connector from back of unit 60 40 61 21 Pin 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 62 41 42 22 63 43 23 64 44 24 65 45 25 66 46 26 67 47 27 28 Pin Name CONFIG MODULE GROUND RS-232 OUT 1 RS-232 IN 1 SIGNAL GROUND RS-232 OUT 2 RS-232 IN 2 SIGNAL GROUND RS-232 OUT 3 RS-232 IN 3 SIGNAL GROUND RS-232 OUT 4 RS-232 IN 4 SIGNAL GROUND ARINC 429 OUT 1 A ARINC 429 OUT 1 B ARINC 429 IN 1 A ARINC 429 IN 1 B SIGNAL GROUND GPS PPS 1 IN SIGNAL GROUND CONFIG MODULE POWER OUT SIGNAL GROUND ARINC 429 OUT 2 A ARINC 429 OUT 2 B ARINC 429 IN 2 A ARINC 429 IN 2 B SIGNAL GROUND ARINC 429 OUT 3 A ARINC 429 OUT 3 B ARINC 429 IN 3 A ARINC 429 IN 3 B SIGNAL GROUND ARINC 429 OUT 4 A ARINC 429 OUT 4 B ARINC 429 IN 4 A ARINC 429 IN 4 B RS-422 IN A RS-422 IN B GTS 8XX/GPA 65 Installation Manual 190-00587-00 68 48 69 49 29 30 10 70 50 71 72 51 52 31 11 32 12 73 53 33 13 74 54 34 14 75 55 35 15 76 56 36 16 77 37 17 78 58 57 38 18 59 39 19 20 I/O -Out In -Out In -Out In -Out In -Out Out In In -In -Out -Out Out In In -Out Out In In -Out Out In In In In Page 4-1 Revision 4TP Connector P8001, continued Pin 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 Pin Name SIGNAL GROUND CONFIG MODULE DATA SIGNAL GROUND ARINC 429 OUT 5 A ARINC 429 OUT 5 B ARINC 429 IN 5 A ARINC 429 IN 5 B SIGNAL GROUND ARINC 429 OUT 6 A ARINC 429 OUT 6 B ARINC 429 IN 6 A ARINC 429 IN 6 B SIGNAL GROUND ETHERNET OUT A ETHERNET OUT B ETHERNET IN A ETHERNET IN B SIGNAL GROUND RS-422 OUT A RS-422 OUT B SIGNAL GROUND CONFIG MODULE CLOCK TOP PA/LNA DATA RS-422 OUT A TOP PA/LNA DATA RS-422 OUT B TOP PA/LNA DATA RS-422 IN A TOP PA/LNA DATA RS-422 IN B RESERVED RESERVED RESERVED RESERVED SPARE SPARE SPARE SPARE GPS PPS IN 2 HI GPS PPS IN 2 LO USB VBUS POWER USB DATA HI USB DATA LO USB GROUND Page 4-2 Revision 4TP I/O -I/O -Out Out In In -Out Out In In -Out Out Out Out -Out Out -Out Out Out In In --------In In In I/O I/O -- GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.1.2 P8002 (Analog/Discrete) View of J8002 connector from back of unit 60 40 61 21 Pin 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 38 39 40 41 62 41 42 22 63 43 23 64 44 24 65 45 25 66 46 26 67 47 27 68 48 28 69 49 29 30 10 70 50 71 72 51 52 31 11 32 12 73 53 33 13 34 14 Pin Name SIGNAL GROUND RESERVED RESERVED RESERVED SIGNAL GROUND AIR/GROUND* SPARE TRAFFIC DISPLAY 1 STATUS VALID* TRAFFIC DISPLAY 2 STATUS VALID* GEAR DOWN AND LOCKED* TA INHIBIT* 1 TA INHIBIT* 2 RESERVED SELF TEST INHIBIT PROGRAM* TA INTRUDER DISPLAY LIMIT 16 PROGRAM * TA INTRUDER DISPLAY LIMIT 8 PROGRAM * TA INTRUDER DISPLAY LIMIT 4 PROGRAM * TA INTRUDER DISPLAY LIMIT 2 PROGRAM * TA INTRUDER DISPLAY LIMIT 1 PROGRAM * RESERVED SIGNAL GROUND RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED RESERVED SIGNAL GROUND SIGNAL GROUND HEADING X HI GTS 8XX/GPA 65 Installation Manual 190-00587-00 74 54 75 55 35 15 76 56 36 16 77 37 17 78 58 57 38 18 59 39 19 20 I/O -----In -In In In In In -In In In In In In ---------------------In Page 4-3 Revision 4TP Connector P8002, continued Pin 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 Pin Name HEADING X LO (GROUND) SIGNAL GROUND HEADING Y HI HEADING Y LO (GROUND) SIGNAL GROUND SPARE EXTERNAL SUPPRESSION I/O SIGNAL GROUND TA DISPLAY ENABLE* AURAL TA ALERT* SPARE VISUAL TA ALERT* TRAFFIC SYSTEM STATUS VALID* RESERVED RESERVED SIGNAL GROUND ALERT AUDIO OUT HI ALERT AUDIO OUT LO HEADING Z HI (GROUND) HEADING Z LO (GROUND) SIGNAL GROUND 26 VAC HEADING REF HI 26 VAC HEADING REF LO SIGNAL GROUND SPARE SPARE HEADING VALID HEADING VALID* SIGNAL GROUND ANALOG RADAR ALTIMETER HI ANALOG RADAR ALTIMETER LO SIGNAL GROUND SELF TEST INITIALIZE SELECT* TRAFFIC OPERATE/STANDBY* ANALOG RADAR ALTIMETER VALID SPARE SIGNAL GROUND I/O --In ---I/O -Out Out -Out Out ---Out Out In --In In ---In In -In In -In In In --- An asterisk (*) following a signal name denotes that the signal is Active Low. Refer to Section 4.6.4 for signal description. Page 4-4 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.1.3 P8003 (Power Supply) View of J8003 connector from back of unit 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 Pin 10 11 12 13 14 15 16 17 18 19 20 21 22 23 24 25 26 27 28 29 30 31 32 33 34 35 36 37 Pin Name POWER GROUND AIRCRAFT POWER 1 AIRCRAFT POWER 1 AIRCRAFT POWER 2 AIRCRAFT POWER 2 POWER GROUND +6 VDC PA/LNA POWER OUT +6 VDC PA/LNA POWER OUT RESERVED RESERVED POWER GROUND +35 VDC PA/LNA POWER OUT +35 VDC PA/LNA POWER OUT POWER GROUND -5 VDC PA/LNA POWER OUT -5 VDC PA/LNA POWER OUT POWER GROUND TRAFFIC SYSTEM REMOTE POWER ON* POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND POWER GROUND TRAFFIC SYSTEM REMOTE POWER OFF POWER GROUND I/O -In In In In -Out Out ---Out Out -Out Out -In -----------------In -- An asterisk (*) following a signal name denotes that the signal is Active Low. Refer to Section 4.6.4 for signal description. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 4-5 Revision 4TP 4.2 GPA 65 Pin Function List 4.2.1 P651 View of J651 connector from back of unit Pin Pin Name POWER GROUND +35 VDC POWER IN POWER GROUND RESERVED -5 VDC POWER IN PA/LNA DATA RS-422 OUT B PA/LNA DATA RS-422 OUT A PA/LNA DATA RS-422 IN B PA/LNA DATA RS-422 IN A POWER GROUND +6 VDC POWER IN +35 VDC POWER IN RESERVED +6 VDC POWER IN RESERVED -5 VDC POWER IN RESERVED RESERVED RESERVED Page 4-6 Revision 4TP I/O -In --In Out Out In In -In In -In -In ---- GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.3 Power 4.3.1 Aircraft Power Functions This section covers the power input requirements. 4.3.1.1 Aircraft Power Pin Name AIRCRAFT POWER 1 AIRCRAFT POWER 1 AIRCRAFT POWER 2 AIRCRAFT POWER 2 AIRCRAFT GROUND AIRCRAFT GROUND AIRCRAFT GROUND AIRCRAFT GROUND Connector P8003 P8003 P8003 P8003 P8003 P8003 P8003 P8003 Pin 21 22 23 24 I/O In In In In ----- Pins 2 and 3 are internally connected to form AIRCRAFT POWER 1. Pins 4 and 5 are internally connected to form AIRCRAFT POWER 2. AIRCRAFT POWER 1 and AIRCRAFT POWER 2 are “diode ORed” to provide aircraft power redundancy. 4.3.1.2 Remote Power Pin Name Connector TRAFFIC SYSTEM REMOTE POWER ON* P8003 TRAFFIC SYSTEM REMOTE POWER OFF P8003 An asterisk (*) following a signal name denotes that the signal is Active Low. Pin 18 36 I/O In In Used to remotely control power. Remote Power ON* ACTIVE: Vin < 3 VDC or grounded (Unit ON) INACTIVE: Vin > 8 VDC or floating (Unit OFF) Remote Power OFF ACTIVE: Vin > 8 VDC (Unit OFF) INACTIVE: Vin < 3 VDC or floating (Unit ON) Active Low Remote Power On (J8003 Pin 18) State Level Inactive Vin > 8 VDC or Open Active Vin < 3VDC or Gnd Inactive Vin > 8 VDC or Open Active Vin < 3VDC or Gnd GTS 8XX/GPA 65 Installation Manual 190-00587-00 Active High Remote Power Off (J8003 Pin 36) State Level Inactive Vin < 3VDC or Open Inactive Vin < 3VDC or Open Active Vin > 8 VDC Active Vin > 8 VDC Expected Unit State OFF ON OFF OFF Page 4-7 Revision 4TP 4.3.1.3 PA/LNA Pin Name +6 VDC PA/LNA POWER OUT +6 VDC PA/LNA POWER OUT +35 VDC PA/LNA POWER OUT +35 VDC PA/LNA POWER OUT -5 VDC PA/LNA POWER OUT -5 VDC PA/LNA POWER OUT +6 VDC POWER IN +6 VDC POWER IN +35 VDC POWER IN +35 VDC POWER IN -5 VDC POWER IN -5 VDC POWER IN Connector P8003 P8003 P8003 P8003 P8003 P8003 P651 P651 P651 P651 P651 P651 Pin 12 13 15 16 I/O Out Out Out Out Out Out In In In In In In Used to provide power to the GPA 65. Page 4-8 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.4 Serial Data 4.4.1 RS-232 Pin Name RS-232 OUT 1 RS-232 IN 1 RS-232 OUT 2 RS-232 IN 2 RS-232 OUT 3 RS-232 IN 3 RS-232 OUT 4 RS-232 IN 4 Connector P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 Pin 11 12 I/O Out In Out In Out In Out In The RS-232 outputs conform to EIA Standard RS-232C with an output voltage swing of at least ±5V when driving a standard RS-232 load. 4.4.2 RS-422 Pin Name RS-422 IN A RS-222 IN B RS-422 OUT A RS-422 OUT B TOP PA/LNA DATA RS-422 OUT A TOP PA/LNA DATA RS-422 OUT B TOP PA/LNA DATA RS-422 IN A TOP PA/LNA DATA RS-422 IN B PA/LNA DATA RS-422 OUT B PA/LNA DATA RS-422 OUT A PA/LNA DATA RS-422 IN B PA/LNA DATA RS-422 IN A Connector P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P651 P651 P651 P651 Pin 37 38 57 58 61 62 63 64 I/O Out In Out In Out Out In In Out Out In In The RS-422 channels conform to EIA standard RS-422. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 4-9 Revision 4TP 4.4.3 ARINC 429 Pin Name ARINC 429 OUT 1 A ARINC 429 OUT 1 B ARINC 429 IN 1 A ARINC 429 IN 1 B ARINC 429 OUT 2 A ARINC 429 OUT 2 B ARINC 429 IN 2 A ARINC 429 IN 2 B ARINC 429 OUT 3 A ARINC 429 OUT 3 B ARINC 429 IN 3 A ARINC 429 IN 3 B ARINC 429 OUT 4 A ARINC 429 OUT 4 B ARINC 429 IN 4 A ARINC 429 IN 4 B ARINC 429 OUT 5 A ARINC 429 OUT 5 B ARINC 429 IN 5 A ARINC 429 IN 5 B ARINC 429 OUT 6 A ARINC 429 OUT 6 B ARINC 429 IN 6 A ARINC 429 IN 6 B Connector P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 P8001 Pin 14 15 16 17 23 24 25 26 28 29 30 31 33 34 35 36 42 43 44 45 47 48 49 50 I/O Out Out In In Out Out In In Out Out In In Out Out In In Out Out In In Out Out In In The ARINC 429 outputs conform to ARINC 429 electrical specifications when loaded with up to 5 standard ARINC 429 receivers. 4.4.4 Ethernet Pin Name ETHERNET OUT A ETHERNET OUT B EHTERNET IN A ETHERNET IN B Connector P8001 P8001 P8001 P8001 Pin 52 53 54 55 I/O Out Out In In This Ethernet based HSDB (High Speed Data Bus) meets the hardware aspects of IEEE standard 802.3 for 10 base T Ethernet communications. Page 4-10 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.4.5 USB Pin Name Connector Pin I/O USB VBUS POWER** P8001 75 In USB DATA HI** P8001 76 I/O USB DATA LO** P8001 77 I/O USB GROUND P8001 78 -**Signals have ESD (Electrostatic Discharge) protection, but not lightning protection. USB TYPE B RECEPTACLE pigtail cable must be wired directly to P8001 to minimize lightning exposure. This interface is used for unit configuration and software uploads. Conforms to the Universal Serial Bus Version 1.1 standard for a “full-speed” device. GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 4-11 Revision 4TP 4.5 Configuration 4.5.1 Configuration Module Pin Name Connector CONFIG MODULE GND P8001 CONFIG MODULE PWR OUT** P8001 CONFIG MODULE DATA** P8001 CONFIG MODULE CLK** P8001 **Signals have ESD (Electrostatic Discharge) protection, but not lightning protection. 4.6 Pin 21 40 60 I/O --I/O I/O Pin 63 64 I/O In In Pin 71 72 I/O In In Analog/Discrete 4.6.1 Heading Input 4.6.1.1 26 Volt AC References Pin Name 26 VAC HEADING REF HI 26 VAC HEADING REF LO Connector P8002 P8002 Used to sample AC inputs. This signal must be the same phase and frequency as the indicator being driven. Frequency: Voltage: Input Impedance: 400 Hz ± 10% 22.6 Vrms to 28.6 Vrms >10 kΩ 4.6.1.2 Radar Altimeter Pin Name ANALOG RADAR ALTIMETER HI ANALOG RADAR ALTIMETER LO Connector P8002 P8002 Provides altitude information during approach. Page 4-12 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 4.6.2 Inputs From Gyros Pin Name HEADING X HEADING LO (GROUND) HEADING Y HEADING LO (GROUND) HEADING Z (GROUND) HEADING LO (GROUND) Connector P8002 P8002 P8002 P8002 P8002 P8002 Pin 41 42 44 45 60 61 I/O In -In -In -- Inputs heading information from a directional gyro. 3-wire synchro magnetic heading input, with HEADING Z grounded. Index reference is 0° as specified by ARINC 407. Frequency: Voltage: Input Impedance: Resolution: Accuracy: 400Hz ± 10% 11.8 Vrms nominal, 13.0 Vrms maximum >10 kΩ ± 0.1° or better ± 2° 4.6.3 Audio Pin Name ALERT AUDIO OUT HI ALERT AUDIO OUT LO Connector P8002 P8002 Pin 58 59 I/O Out Out Pin Name Connector AIR/GROUND* P8002 TRAFFIC DISPLAY 1 STATUS VALID* P8002 TRAFFIC DISPLAY 2 STATUS VALID* P8002 GEAR DOWN AND LOCKED* P8002 TA INHIBIT* 1 P8002 TA INHIBIT* 2 P8002 SELF TEST INHIBIT PROGRAM* P8002 TA INTRUDER DISPLAY LIMIT 16 PROGRAM * P8002 TA INTRUDER DISPLAY LIMIT 8 PROGRAM * P8002 TA INTRUDER DISPLAY LIMIT 4 PROGRAM * P8002 TA INTRUDER DISPLAY LIMIT 2 PROGRAM * P8002 TA INTRUDER DISPLAY LIMIT 1 PROGRAM * P8002 DATA RECORDER ENABLE* P8002 HEADING VALID* P8002 SELF TEST INITIALIZE SELECT* P8002 TRAFFIC OPERATE/STANDBY* P8002 An asterisk (*) following a signal name denotes that the signal is Active Low. Pin 10 11 12 14 15 16 17 18 19 20 69 74 75 I/O In In In In In In In In In In In In In In In In 4.6.4 Active Low Discrete Inputs ACTIVE: 0 V ≤ Vin ≤ 3.5 V, or Rin ≤ 375 ohms INACTIVE: 8 V ≤ Vin ≤ 36 V, or Rin ≥ 100k ohms Source current is internally limited to approximately 1 mA max for a grounded input GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page 4-13 Revision 4TP 4.6.5 Active High Discrete Inputs Pin Name Connector Pin I/O HEADING VALID P8002 68 In ANALOG RADAR ALTIMETER VALID P8002 76 In ACTIVE: 8 V ≤ Vin ≤ 36 V INACTIVE: 0 V ≤ Vin ≤ 3.5 V, or Rin ≥ 100k ohms Sink current is internally limited to approximately 1 mA typical for an input connected to +28VDC. 4.6.6 Annunciator Output Pin Name Connector TA DISPLAY ENABLE* P8002 AURAL TA ALERT* P8002 VISUAL TA ALERT* P8002 TRAFFIC SYSTEM STATUS VALID* P8002 An asterisk (*) following a signal name denotes that the signal is Active Low. Pin 50 51 53 54 I/O Out Out Out Out Pin 48 I/O I/O ACTIVE: 0 V ≤ Vout ≤ 0.5 V or Rout ≤ 10 ohms, sinking up to 500 mA INACTIVE: Rout ≥ 100k ohms to ground, withstanding up to +36 VDC. 4.7 Mutual Suppression Bus Pin Name EXTERNAL SUPPRESSION I/O Connector P8002 Mutual Suppression Input/Output bus compliant with ARINC 735A Attachment 8, with the exception that the maximum applied DC steady state voltage is +30.3V. Suppression I/O signal is pulsed under normal operation. Page 4-14 Revision 4TP GTS 8XX/GPA 65 Installation Manual 190-00587-00 APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-1. GTS 8XX Vertical Outline Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-1 (Page A-2 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-2. GTS 8XX Vertical Installation Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-3 (Page A-4 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-3. GTS 8XX Horizontal Outline Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-5 (Page A-6 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-4. GTS 8XX Horizontal Installation Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-7 (Page A-8 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-5. GPA 65 Outline Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-9 (Page A-10 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-6. GPA 65 Installation Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-11 (Page A-12 blank) Revision 4TP APPENDIX A OUTLINE & INSTALLATION DRAWINGS Figure A-7. GA 58 Antenna Outline Drawing GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page A-13 (Page A-14 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-1. Notes GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-1 (Page B-2 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-2. GTS 820/850/GPA 65 Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-3 (Page B-4 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-3. GTS 800 Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-5 (Page B-6 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-4. GTS 8XX G1000 Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-7 (Page B-8 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-5. GTS 8XX GNS 4XX/GNS 5XX/GMX 200 Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-9 (Page B-10 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-6. GTS 8XX/GMA/HSI/Altimeter Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-11 (Page B-12 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-7. GTS 8XX Dongle Cable (Non-G1000 Installations Only) GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-13 (Page B-14 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE Figure B-8. GTS 8XX Discrete Interconnects GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-15 (Page B-16 blank) Revision 4TP APPENDIX B INTERCONNECT EXAMPLE The Configuration Module is only applicable for retrofit installtions Figure B-9. GTS 8XX Config Module Example Interconnect GTS 8XX/GPA 65 Installation Manual 190-00587-00 Page B-17 (Page B-18 blank) Revision 4TP
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