P/N:

Transcription

1 - Copyright NavWorx Page 1 of 128 All rights reserved. Printed in the U.S.A.

2 Business Address: NavWorx Incorporated 3706 Big A Road Rowlett, TX Telephone: (888)-NAVWORX ( ) Facsimile: support@navworx.com Website: Information in this document is subject to change without notice. NavWorx reserves the right to modify its products and documentation without notice and is under no obligation to notify anyone of such changes or improvements. NavWorx is a registered trademark of NavWorx Incorporated. ADS600-B is a trademark of NavWorx Incorporated. These trademarks may not be used without the express written permission of NavWorx Incorporated. No part of this document may be copied, reproduced, transmitted, disseminated, downloaded or stored on any storage medium without the express written permission of NavWorx. NavWorx grants permission to download a single copy of this document onto a hard drive or other electronic storage medium to be viewed for personal use as long as the downloaded or printed copy contains the complete text of this copyright notice. Unauthorized commercial distribution of any revision of this documentation is strictly prohibited. Copyright NavWorx Page 2 of 128 All rights reserved. Printed in the U.S.A.

3 Revision Date Comments 01 04/20/2010 Initial release 02 05/11/2010 Revised FCC statement Revision History 03 08/29/2010 Updated Wiring Diagrams. Added content to GPS Antenna, Cabling and Wiring, Air Circulation and Cooling Sections, and Mounting and Wiring Sections /12/2010 Added ADS600-B to GRT Wiring Diagrams. Replaced text of Maintenance PC section with reference to Maintenance Port Tutorial document, /18/2010 Added Quick Start Guide and ADS600-B Maintenance Port Tutorial Sections /10/2010 Changed download link for TeraTermPro 07 10/17/2010 Added GNS 430(W) (ARINC 429) Wiring Diagram. Added wiring diagrams to table of contents /02/2010 Added GMX 200/MX20 RS422 and ARINC 429 Interconnect Diagrams /30/2010 Added GTX 330, GTX 327 and SL70 Transponder Interconnect Diagrams /28/2011 Added Suppression Input and UAT Indicator to Interconnect Diagrams. Uniquely identify ports of GNS A Interconnect Diagram. Added ADS600-B to AFS (ADS-B) Interconnect Diagram /06/2011 Corrected Disclaimer /25/2011 Added ground signal to GTX 330 and GTX 327 Interconnect Diagrams /18/2011 Changed pin outs for ADS600- B serial numbers 851 and above /04/2011 Corrected UAT control panel interface. Corrected pins 33 and 34 of table 3-6. Changed UAT control from pin 7 to pin 33 for SL70, GTX330, and GTX327 diagrams /08/2011 Added control head input to Figure 3-2, ADS600-B System Block diagram. Updated Section 3.3 to include description of control head input. Added WiFi Interconnect Diagram /01/2011 Corrected Bluetooth and WiFi diagrams to indicate correct +5VDC pin for adapter when configured with ADS600-B having S/N 851 and greater or with ADS600-B having S/N below /14/2011 Added RG400 cables to Package Contents Table /03/2011 Added callout for GPS NMEA output pin 15 of DB /31/2011 Corrected GMX200/MX20 to ADS600-B diagrams (removed redundant grounding shield). Corrected SL70 interconnect diagram (removed incorrect notes) /04/2012 Replaced TeraTermPro with UAT Console as installer interface to the ADS600-B /11/2012 Corrected Wiring Diagrams for GTX330 (Note #3) /15/2012 Removed table containing DB-37 pin-outs for ADS600-B units with serial numbers below /26/2012 Removed Composite TIS. Remove Chelton Composite TIS diagram with Serial ARINC 735B diagram. Updated AFS serial port description /13/2012 Issue #166. Updated UAT Console Figures. Added Status Tab to UAT Console /09/2013 Issue #330. First revision of installation manual withtso-c154c authorization for ADS600-B /14/2013 Issue #438. Added system block diagrams showing various configurations of ADS600-B. Added descriptions for altitude encoder, ARINC 429 and transponder control panel input formats /19/2013 Issue #443. Reformatted Part Number /10/2013 Issue #454. Added references to evaluated GPS sources /10/2013 Issue #411. Revised installation manual with TSO-C145c authorization for part number and /25/2013 Issue #477. Add TT2X as control panel to ADS600-B /29/2013 Issue #480. Added Removal/Replacement Section. Updated Troubleshooting Section. Removed AFS TIS-A dwg /24/2013 Issue #507. Add limitations paragraph from TSO-C145c 33 12/22/2013 Issue #457. Added TransMonSPE as control input to ADS600-B. Issue #178 Added GNS480 with remote transponder as control input. Copyright NavWorx Page 3 of 128 All rights reserved. Printed in the U.S.A.

4 34 11/06/2014 Issue #513, #514, #583, #633, #644, #683. Updated XPNDR I/F wiring diagrams. Added wiring diagram for STX165R. Updated WiFi diagram. Combined TransMonSPE and ADS600-B IMs /13/2014 Issue #795. Added Receiver part numbers /17/2015 Issue #767. Update TransMonSPE Enclosure /01/2015 Issue #836. Added GPS Aviation Format for ADS600-B receiver part numbers /02/2015 Issue #1018. Output to three displays simultaneously. Issue #908. Updated internal GPS SIL to comply with amended rule. Issue #1101. Updated ADS600-B mounting instructions, revised appendices H & I. Added support for composite aircraft and pressure vessels. Issue #1197. Add Avidyne IFD4xx/5xx wiring diagram (Appendix A.21 & A.22) /12/2016 Issue #1381. Added GPS interface Garmin ADS-B OUT + protocol for all part numbers. Copyright NavWorx Page 4 of 128 All rights reserved. Printed in the U.S.A.

5 End User License Agreement (EULA) Terms. By installing or using the ADS600-B ( product ), you agree to be bound by the terms and conditions of the following license agreement. Please read this agreement carefully. NavWorx Incorporated ("NavWorx") grants you a limited, non-exclusive license to use the product. Title, ownership rights, and intellectual property rights in and to the product remain with NavWorx. Refund. If you do not agree to the terms of this EULA, NavWorx Inc. is unwilling to license the product to you. In such event, you may not use the licensed product, and you should promptly contact NavWorx for a refund. The product must not have been used or installed in order to obtain a full refund. No Warranties. Except as expressly provided in the limited warranty section, the products hardware and its operating system software are provided to you as is without warranty of any kind, either expressed or implied, including, but not limited to, waranties of noninfringement, merchantability, and /or fitness for a particular purpose. The entire risk of the quality and performance of both the software and hardware is with the user. Copyright. You acknowledge that the product is the property of NavWorx and is protected under United States of America copyright laws and international copyright treaties. You further acknowledge that the structure, organization, and source design of the hardware and software are valuable trade secrets of NavWorx. You agree not to open the product, break the EULA seal, nor decompile, disassemble, modify, reverse assemble, reverse engineer, or reduce to human readable form the hardware or software or any part thereof or create any derivative works based on the product. No Liability for Consequential Damages. NavWorx Inc. and its suppliers shall not be held liable for any damages suffered or incurred by you (including, but not limited to, general, special, consequential or incidental damages for loss of business profits, business interruption, personal compensation and the like), arising from or in connection with the delivery, use, or performance of the product and its software. Customer Remedies. NavWorx Inc. and its suppliers entire liability and your exclusive remedy shall be, at NavWorx option, either (1) return of the product purchase price, not to exceed list price, or (2) repair or replacement of the product which is returned to NavWorx with original proof of purchase. Copyright NavWorx Page 5 of 128 All rights reserved. Printed in the U.S.A.

6 Disclaimer NavWorx is not responsible for the failure of ADS-B radio stations to broadcast TIS-B and FIS-B products. NavWorx is not liable for damages as a result of use or misuse of the ADS600-B. NavWorx has tested the product in accordance with FAA guidance material. However, issues may still be present. We ll make a best faith effort to resolve issues as they arise. This product is licensed under an End User License Agreement (EULA). If you don t agree with the EULA, or this Disclaimer, you must return the equipment. Copyright NavWorx Page 6 of 128 All rights reserved. Printed in the U.S.A.

7 NavWorx Two Year Limited Warranty Limited Warranty for FAA Certified Products. Certified NavWorx products are warranted to be free from defects in material and workmanship for two years from the date of original purchase. For the duration of the warranty period, at its option, NavWorx will repair or replace any product which fails during normal use. No charge will be made to the customer for parts and labor for product repair or replacement provided that the customer shall be responsible for all shipping cost. NavWorx, at its sole discretion, retains the exclusive right to either repair or replace the product unit with a new unit or with a newly reconditioned unit. Any replacement product will be warranted for the remainder of the original warranty period or ninety (90) days, whichever is longest. Limited Warranty for Non-Certified Products. Non-certified NavWorx products are warranted to be free from defects in material and workmanship for two years from the date of first flight of the experimental aircraft in which the product is installed. Customer must provide proof of first flight when requesting warranty service. For the duration of the warranty period, at its option, NavWorx will repair or replace any product which fails during normal use. No charge will be made to the customer for parts and labor for product repair or replacement provided that the customer shall be responsible for all shipping cost. NavWorx, at its sole discretion, retains the exclusive right to either repair or replace the product unit with a new unit or with a newly reconditioned unit. Any replacement product will be warranted for the remainder of the original warranty period or ninety (90) days, whichever is longest. Restrictions. This Limited Warranty does not apply if (a) the product has not been installed, operated, or maintained in accordance with instructions supplied by NavWorx, (c) has been altered, except by NavWorx or its authorized representative, or (c) has been subjected to abnormal physical or electrical stress, abnormal environmental conditions, misuse, negligence, or accident, (d) the factory applied original case seals or serial number label has been broken, altered or removed from the product. Disclaimer of Warranty. EXCEPT AS SPECIFIED IN THIS WARRANTY SECTION, ALL EXPRESS OR IMPLIED CONDITIONS, REPRESENTATIONS, AND WARRANTIES INCLUDING, WITHOUT LIMITATION, ANY IMPLIED WARRANTY OR CONDITION OF MERCHANTABILITY, FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE ARE HEREBY EXCLUDED TO THE EXTENT AN IMPLIED WARRANTY CANNOT BE EXCLUDED. SUCH WARRANTY IS LIMITED IN DURATION TO THE EXPRESS WARRANTY PERIOD. BECAUSE SOME STATES OR JURISDICTIONS DO NOT ALLOW LIMITATIONS ON HOW LONG AN IMPLIED WARRANTY LASTS, THE ABOVE LIMITATION MAY NOT APPLY. THIS WARRANTY GIVES THE CUSTOMER SPECIAL LEGAL RIGHTS AND THE CUSTOMER MAY HAVE OTHER LEGAL RIGHTS THAT MAY VARY FROM JURISDICTION TO JURISDICTION. NAVWORX SHALL NOT BE LIABLE, IN ANY EVENT, FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT. BECAUSE SOME STATES OR JURISDICTIONS DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU. Warranty Service. Warranty repair service shall be provided directly by NavWorx. To obtain warranty service, an original copy of the sales receipt for the product from NavWorx or a retailer is required. The following steps describe how to return your unit for warranty service. Step 1. Call or NavWorx and describe the problem that you are having and request a Return Material Authorization (RMA) tracking number. Also, provide the unit s serial number, your shipping address and daytime telephone number. Telephone (888)-NAVWORX ( ) support@navworx.com Step 2. Once you have received an RMA number, securely pack the unit and ship it, insured, to the following address: NavWorx Incorporated RMA Number: (insert your RMA number here) 3706 Big A Road Rowlett, TX Copyright NavWorx Page 7 of 128 All rights reserved. Printed in the U.S.A.

8 Table of Contents 1 About this Manual Reference Documents Acronyms Regulatory Compliance TSO ADS600-B TSO Authorization TransMonSPE TSO Authorization FCC Grant of Equipment Authorization Limitations Installation GPS Receiver (P/N , , and ) GPS Receiver (P/N , , , ) Surveillance Services (P/N , , and ) Accessories and Packing List Unpacking Equipment Package Contents Equipment Description Overall Specifications System Configurations GPS Position Source Display Maintenance Port Annunciator Output Altitude Encoder Input Control Panel Antenna Requirements GPS Antenna (P/N , , and ) GPS Antenna (P/N , , and ) UAT Antenna Installation Pre-Installation Information Installation Overview Tools Required ADS600-B Mounting GPS Antenna Mounting Copyright NavWorx Page 8 of 128 All rights reserved. Printed in the U.S.A.

9 4.4.6 UAT Antenna Mounting TransMonSPE Maintenance Port Circuit Breaker Annunciator Cabling and Wiring Air Circulation and Cooling Electrical Connections Protection Electrical Current DB-37 I/O Connector (P1) Functional Descriptions Power Discrete Outputs Discrete Inputs PPS Time Mark Input Serial Interfaces ARINC ADS600-B Post Installation Check Mounting/Wiring Check Power and Ground Check Antenna Check Configuration of ADS600-B with Maintenance PC Installation Completion VHF COM Interference GPS Testing Weight and Balance TransMonSPE Post Installation Check Mounting and Wiring Check Weight and Balance Appendix A Interconnect Diagrams A.1 Interconnect Diagram: ADS600-B Maintenance Port to Computer A.2 Interconnect Diagram: GNS 480 ARINC 743A Position Source A.3 Interconnect Diagram: ADS600-B to GNS 480 Traffic (ARINC 429) A.4 Interconnect Diagram: ADS600-B to GNS 480 Traffic (RS-232 TIS) A.5 Interconnect Diagram: ADS600-B to GNS 430 Traffic (ARINC 429) A.6 Interconnect Diagram: ADS600-B to MX20/GMX 200 (RS422 Traffic/Weather) A.7 Interconnect Diagram: ADS600-B to MX20/GMX 200 (ARINC 429 Traffic) A.8 Interconnect Diagram: ADS600-B to Control Panel Copyright NavWorx Page 9 of 128 All rights reserved. Printed in the U.S.A.

10 A.9 Interconnect Diagram: ADS600-B to Altitude Encoder A.10 Interconnect Diagram: ADS600-B to NexNav mini LRU (GPS Source) A.11 Interconnect Diagram: ADS600-B to TT21/TT22/TT31 Mode S Transponder Control. 77 A.11.1 UAT Mode (Altitude) Switch used with TC20 Control Panel A.12 Interconnect Diagram: GPS Antenna A.13 Basic Interconnect Diagram: ARINC 743A GPS Source A.14 Basic Interconnect Diagram: RS232 GPS Source A.15 Basic Interconnect Diagram: RS232 Display A.16 Basic Interconnect Diagram: RS422 Display A.17 Basic Interconnect Diagram: ARINC 735A Traffic Display A.18 Interconnect Diagram: UAT Indicator Dialight A.19 Basic Interconnect Diagram: Garmin Aviation Format A.20 Basic Interconnect Diagram: RS232 Display A.21 Interconnect Diagrams IFD 4XX/5XX A.22 Basic Interconnect Diagram: ARINC 429 Pressure Altitude A.23 Interconnect Diagram: Garmin GNS 430W/530W ADS-B Out A.24 Interconnect Diagram: Garmin GTN 650/750 ADS-B Out A.25 Interconnect Diagram: Avidyne IFD 440/540 ADS-B Out Appendix B Uncertified Displays B.1 Interconnect Diagram: RS-232 Display Port B.2 Interconnect Diagram: ADS600-B to GPSMAP TIS-A B.3 Interconnect Diagram: Bluetooth Display Port B.4 Interconnect Diagram: WiFi Display Port B.5 Interconnect Diagram: ADS600-B to AFS B.6 Interconnect Diagram: ADS600-B to GRT B.7 Interconnect Diagram: ADS600-B to MGL B.8 Interconnect Diagram: ADS600-B to Chelton B.9 Interconnect Diagram: RS-232 Display Port Appendix C ADS600-B Maintenance Port Tutorial Starting the UAT Console UAT Console Communication with ADS600-B UAT Console Indicates UAT NOT CONFIGURED Configuring ADS600-B with UAT Console Upgrading ADS600-B View UAT Console Reports Status Tab Copyright NavWorx Page 10 of 128 All rights reserved. Printed in the U.S.A.

11 Appendix D Supported Altitude Encoder Serial Communication Protocols Appendix E ADS600-B Environmental Qualification Form (UAT) Appendix F ADS600-B Amended Environmental Qualification Form (GPS) Appendix G TransMonSPE Environmental Qualification Form Appendix H UAT Antenna Mounting (TSO-C66c, TSO-C74c) Appendix I GPS Antenna Mounting (TSO-C144, TSO-C190) Copyright NavWorx Page 11 of 128 All rights reserved. Printed in the U.S.A.

12 List of Tables Table 3-1: Package Contents Table 3-2: ADS600-B Installation Kit Contents (P/N ) Table 4-1: ADS600-B Installation Parts List Table 4-2: TransMonSPE Parts List Table 4-3: Acceptable UAT Antennas Table 4-4: Acceptable GPS Antennas Table 4-5: Crimp Tools for High Density AWG Socket Contact Table 4-6: Connectors Table 4-7: Circuit Breaker Protection Table 4-8: Electrical Load Requirement for P/N , Table 4-9: Electrical Load Requirement for P/N , Table 4-10: Electrical Load Requirement for P/N , Table 4-11: Electrical Load Requirement for P/N , Table 4-12: I/O Connector Pin-Out (P1) for ADS600-B Table 4-13: ARINC 429 (735B) Out Labels Table 4-14: ARINC 429 (743A) In Labels Table 4-15: ADS600-B Weight Copyright NavWorx Page 12 of 128 All rights reserved. Printed in the U.S.A.

13 List of Figures Figure 4-1: ADS600-B Universal Access Transceiver Figure 4-2: TransMonSPE Figure 4-3: ADS600-B UAT Transceiver with External Compliant GPS Figure 4-4: ADS600-B UAT Transceiver with Internal Compliant TSO-C154c GPS Figure 4-5: ADS600-B UAT Transceiver with Internal Compliant TSO-C145c GPS Figure 4-6: ADS600-B UAT Receiver with External Compliant GPS Figure 4-7: UAT Receiver with Internal Compliant TSO-C154c GPS Figure 4-8: ADS600-B UAT Receiver with Internal Compliant TSO-C145c GPS Figure 4-9: ADS600-B Mounting-Hole Pattern Figure 4-10: ADS600-B Exploded View Figure 4-11: Coax in Channel of TransMonSPE Base Figure 4-12: TransMonSPE Bottom Cover over Coax Figure 4-13: TransMonSPE Fully Installed Bottom Cover Figure 4-14: TransMonSPE with Attached USB Connector Figure 4-15: Securing TransMonSPE with Clamp Figure 4-16: Clamp Ground Termination Figure 4-17: 37 Pin D-Sub Male Connector (P1) Figure 4-18: ADS600-B Center of Gravity Copyright NavWorx Page 13 of 128 All rights reserved. Printed in the U.S.A.

14 1 About this Manual This manual describes the installation procedures for the ADS600-B Universal Access Transceiver (UAT) Data Link Transceiver and TransMonSPE (Transponder Monitor Single Point of Entry). The installation of the TransMonSPE is optional and typically is installed in aircraft with older style transponders. This manual also describes installation of the ADS600-B receiver product; note that the TransMonSPE is not part of the receiver installation. This document describes installation for ADS600-B part numbers: [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO-C154c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO-C154c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO-C145c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO-C145c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C154c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C154c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C145c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C145c GPS SBAS Receiver and ARINC 429) This document describes the installation for TransMonSPE part number: [HWMOD]-[SWMOD] Transponder Monitor Single Point of Entry The TransMonSPE part number (or later) operates with the ADS600-B UAT transceiver part numbers: , , and Copyright NavWorx Page 14 of 128 All rights reserved. Printed in the U.S.A.

15 1.1 Reference Documents RTCA/DO-282B RTCA/DO-229D RTCA/DO-160F TSO-C154c TSO-C145c AC B AC B AC D RTCA/DO-310 TSO-C190 TSO-C144a RTCA Document. Minimum Operational Performance Standards for Universal Access Transceiver (UAT) Automatic Dependent Surveillance Broadcast (ADS-B) RTCA Document. Minimum Operational Performance Standards for Global Positioning System/Wide Area Augmentation System Airborne Equipment RTCA Document. Environmental Conditions and Test Procedures for Airborne Equipment. Technical Standard Order Universal Access Transceiver (UAT) Automatic Dependent Surveillance-Broadcast (ADS-B) Equipment Operating on Frequency of 978MHz Technical Standard Order for Airborne Navigation Sensors Using The Global Positioning System (GPS) Augmented By The Satellite Based Augmentation System (SBAS) Acceptable Methods, Techniques, and Practices Aircraft Inspection and Repair Airworthiness Approval of Automatic Dependent Surveillance-Broadcast (ADS-B) Out Systems Airworthiness Approval of Global Navigation Satellite Systems (GNSS) Equipment RTCA Document. Minimum Operational Performance Standards for Global Navigation Satellite System (GNSS) Airborne Active Antenna Equipment for the L1 Frequency Band Technical Standard Order for Active Airborne Global Navigation Satellite System (GNSS) Antenna Technical Standard Order for Passive Airborne Global Navigation Satellite System (GNSS) Antenna Revision 11 The ADS600-B Interface Control Document defines the message formats of the public messages sent and received by the ADS600-B. ID-CCA-GPSBL The NexNav mini Interface Document for the Receiver Circuit Card Assembly (CCA) GPS/SBAS WAAS Class Beta 1 Receiver, describes the (TSO-C145c compliant) GPS SBAS Receiver internally integrated with the ADS600-B (P/Ns , , and ). Appendix D of ID-CCA-GPSBL describes general guidance for installing GPS SBAS receivers with ADS-B systems as per Appendix 2 of AC Revision 9 Instructions for Continued Airworthiness Copyright NavWorx Page 15 of 128 All rights reserved. Printed in the U.S.A.

16 1.2 Acronyms ADC Air Data Computer ADS600-B Automatic Dependent Surveillance universal access transceiver ADS-B Automatic Dependent Surveillance Broadcast ADS-R Automatic Dependent Surveillance Rebroadcast AHRS Attitude Heading Reference System ATC Air Traffic Control CCA Circuit Card Assembly CDTI Cockpit Display of Traffic Information DME Distance Measuring Equipment EFIS Electronic Flight Information System FCC Federal Communications Commission FAA Federal Aviation Administration FIS-B Flight Information Services Broadcast GNSS Global Navigation Satellite System GPS Global Positioning System MFD Multifunction Display PC Personal Computer SBAS Satellite-based Augmentation System SIL Source Integrity Level STC Supplemental Type Certificate TAS Traffic Advisory System TCAS Traffic Collision Alert System TIS-A Traffic Information Services provided by Mode S transponder TIS-B Traffic Information Services Broadcast TransMonSPE Transponder Monitor Single Point of Entry TSO Technical Standard Order UAT Universal Access Transceiver WAAS Wide Area Augmentation System Copyright NavWorx Page 16 of 128 All rights reserved. Printed in the U.S.A.

17 1.3 Regulatory Compliance TSO TSO-C154c TSO-C145c Universal Access Transceiver (UAT) Automatic Dependent Surveillance- Broadcast (ADS-B) Equipment Operating on Frequency of 978MHz Airborne Navigation Sensors Using The Global Positioning System Augmented By The Satellite Based Augmentation System ADS600-B Part Transceiver Number HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD TSO-C154c Universal Access Transceiver (UAT) Automatic Dependent Surveillance- Broadcast (ADS-B) Equipment Operating on Frequency of 978MHz ADS600-B Receiver Part Number HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD TSO-C145c Airborne Navigation Sensors Using The Global Positioning System Augmented By The Satellite Based Augmentation System HWMOD-SWMOD HWMOD-SWMOD TSO-C154c Universal Access Transceiver (UAT) Automatic Dependent Surveillance- Broadcast (ADS-B) Equipment Operating on Frequency of 978MHz TransMonSPE Part Number HWMOD-SWMOD ADS600-B TSO Authorization Function TSO Minimum Performance Standard UAT Transceiver GPS SBAS Receiver TSO-C154c Class A1S Software RTCA/DO-178B Hardware RTCA/DO-254 Environmental RTCA/DO-282B Level C Level C RTCA/DO-160F See Appendix E TSO-C145c RTCA/DO-229D Level C Level C RTCA/DO-160F See Appendix F Copyright NavWorx Page 17 of 128 All rights reserved. Printed in the U.S.A.

18 1.3.3 TransMonSPE TSO Authorization The TransMonSPE is approved under 14 CFR 21.8(d). TSO Minimum Performance Standard Software RTCA/DO-178B Hardware RTCA/DO-254 Environmental TSO-C154c RTCA/DO-282B Level D Level D RTCA/DO-160F See Appendix G FCC Grant of Equipment Authorization This equipment has been issued an FCC Grant of Equipment Authorization. The FCC ID is marked on the equipment nameplate. 2 Limitations 2.1 Installation This manual stipulates the requirements for an airworthy installation under the STC. The conditions and tests required for TSO approval of this article are minimum performance standards. Those installing this article, on or in a specific type or class of aircraft, must 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 according to 14 CFR part 43 or the applicable airworthiness requirements. The UAT Antenna MUST be installed no less than 5 feet from any L-Band (Transponder, TCAS, TAS) antenna. Failure to adhere to this critical installation note will result in failure of the ADS600-B and void your warranty. The UAT Antenna MUST be installed no less than 5 feet from any Distance Measuring Equipment (DME) antenna. Failure to adhere to this critical installation note will result in failure of the ADS600-B and void your warranty. The ADS600-B does not transmit Target State or Trajectory Change messages as defined by RTCA/DO-282B. This manual does not support antenna installations on pressure vessels without additional approved data, or specific approved data is provided in this manual. If additional approved data is required, contact NavWorx for guidance. Copyright NavWorx Page 18 of 128 All rights reserved. Printed in the U.S.A.

19 This manual does not support antenna installations on composite aircraft without additional approved data, or specific approved data is provided in this manual. If additional approved data is required, contact NavWorx for guidance. 2.2 GPS Receiver (P/N , , and ) For ADS600-B part numbers , , and , the internal GPS is FAA TSO-C145c approved, is compliant with AC B, and it can be operated in Oceanic, En-route, Terminal airspace, and Beta 1 applications. The ADS600-B may operate with either a TSO-C190 or TSO-C144 approved antenna for TSO- C145c operations. The recommended antenna is a DO-301 compliant antenna. Table 4-4 provides the recommended antennas for use with ADS600-B part numbers , , and The performance of the ADS600-B GPS SBAS Receiver is unaffected when operating in a satellite communications SATCOM environment. The performance of the ADS600-B GPS Receiver is compliant for SATCOM compatibility per DO-229D. 2.3 GPS Receiver (P/N , , , ) For ADS600-B part numbers , , and , the internal GPS WAAS receiver is compliant with AC B. The ADS600-B may operate with either a TSO-C190 or TSO-C144 approved antenna. Table 4-4 provides the recommended antennas for use with ADS600-B part numbers , , and Copyright NavWorx Page 19 of 128 All rights reserved. Printed in the U.S.A.

20 2.4 Surveillance Services (P/N , , and ) Air Traffic Control (ATC) Surveillance Services are available through the UAT data link technology. To use these services there must be a single point of entry for the ATC assigned squawk code. A single point of entry allows the squawk code to be transmitted by both the onboard transponder and ADS600-B UAT. The following control panel interfaces are eligible to operate with the ADS600-B UAT Transceiver: If the aircraft is not transponder equipped, an Electronic Flight Instrument System (EFIS) display may be configured to provide the squawk code entry. The MX20, GMX 200, GNS480 (standalone and with attached transponder) and other displays may be configured to enter squawk codes to the ADS600-B. Eligible Transponders may be configured to act as a control panel for the ADS600-B. These transponders are GTX-330/33, GTX-327/32, SL70/70R, TT21/TT22/TT31, and STX-165. If the aircraft is equipped with an older-style Mode C or Mode S transponder, the TransMonSPE may be installed as the control input for the ADS600-B. The TransMonSPE (Transponder Monitor Single Point of Entry) is a standalone device that monitors transponder transmissions through a shielded RF coupler connection to an aircraft s transponder antenna coax cable. The TransMonSPE is attached to the existing transponder antenna coax cable of the transponder to pick up altitude and reply codes, decode the information and transmit it digitally for use by the ADS600-B. Copyright NavWorx Page 20 of 128 All rights reserved. Printed in the U.S.A.

21 3 Accessories and Packing List 3.1 Unpacking Equipment Carefully unpack the equipment from the shipping container. Inspect the ADS600-B unit and the package contents for evidence of shipping damage. Retain the shipping container and packaging material for reshipment if necessary. 3.2 Package Contents The items included in the ADS600-B package are listed in Tables 3-1and 3-2. Table 3-1: Package Contents Part # Qty Description ADS600 Installation Kit (see Table 3-2 for details) One of the following: [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO- C154c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO- C154c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO- C145c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Receiver, compliant TSO- C145c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C154c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C154c GPS SBAS Receiver and ARINC 429) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C145c GPS SBAS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT Transceiver, compliant TSO-C145c GPS SBAS Receiver and ARINC 429) 1 ADS600-B UAT Data Link Transceiver or Receiver Table 3-2: ADS600-B Installation Kit Contents (P/N ) Part # Quantity Description Receptacle Female, DSUB 37-pin Receptacle Female, DSUB 9-pin 201- DC DSUB 37-pin back-shell Connector DSUB Latch Slide 37 position 201-M39029/ Crimp contact, DSUB, 20 to 24 AWG wire Copyright NavWorx Page 21 of 128 All rights reserved. Printed in the U.S.A.

22 4 Equipment Description The ADS600-B UAT Data Link Transceiver transmits GPS position and aircraft information in the form of an ADS-B message once per second. Additionally, this unit receives messages from other UAT equipped aircraft and receives TIS-B/ADS-R/FIS-B messages from ADS-B Radio Stations. Data received by the ADS600-B UAT is output to a display device. Figure 4-1: ADS600-B Universal Access Transceiver The ADS600-B UAT Receiver receives messages from other UAT equipped aircraft and receives TIS-B/ADS-R/FIS-B messages from ADS-B Radio Stations. Data received by the ADS600-B UAT Receiver is output to a display device. The TransMonSPE (Transponder Monitor Single Point of Entry patent pending) is a standalone device that monitors transponder transmissions through a shielded RF coupler connection to an aircraft s transponder antenna coax cable. The TransMonSPE is attached to the existing transponder antenna coax cable of an older-style MODE C transponder to pick up the Reply, Mode, and other information, decode it and transmit it digitally for use by an ADS600-B UAT Transceiver. Figure 4-2: TransMonSPE Copyright NavWorx Page 22 of 128 All rights reserved. Printed in the U.S.A.

23 4.1 Overall Specifications This section includes the physical, electrical, performance and environmental specifications for the ADS600-B UAT Data Link Transceiver. Physical Height (PN , ): Height (PN , ): Width: Depth: Weight(PN , ): Weight(PN , ): Weight(PN , ): Weight(PN , ): inches 2.45 inches inches (includes mounting bracket) 6.02 inches 1.0 lbs (excluding cables) 1.2 lbs (excluding cables) 1.6 lbs (excluding cables) 1.8 lbs (excluding cables) Environmental The ADS600-B is designed and tested to meet the categories as shown in the Environmental Qualification Form included in Appendix E and Appendix F. Operating temperature: Storage temperature: Temperature variation: -20 C to +55 C -55 C to +85 C 5 C per minute Humidity: 95% at 50 C Maximum continuous altitude: External Cooling: 25,000 feet Not required Electrical (P/N , ) Voltage: Input Current (6W nominal): 9-33VDC Steady State: 14VDC, 28VDC Electrical (P/N , ) Voltage: Input Current (8W nominal): 9-33VDC Steady State: 14VDC, 28VDC Transmit Peak: 14VDC, Electrical (P/N , ) Voltage: Input Current (8W nominal): 9-33VDC Steady State: 14VDC, 28VDC Electrical (P/N , ) Voltage: Input Current (11W nominal): 9-33VDC Steady State: 14VDC, 28VDC Transmit Peak: 14VDC, Copyright NavWorx Page 23 of 128 All rights reserved. Printed in the U.S.A.

24 UAT Performance TSO Compliance: Regulatory: Frequency: Tolerance: Data Rate: Receiver Sensitivity: Transmit Power: Equipment Class: TSO-C154c RTCA/DO-282B 978MHz +/- 20ppm Mbps Exceeds 40W nominal A1S (single bottom UAT antenna) Compliant TSO-C145c GPS SBAS Receiver Performance (P/N , , , ) TSO Compliance: TSO-C145c Class Beta 1 Regulatory: General: Number of Channels: Position Update Interval: Sensitivity Tracking: Sensitivity Reacquisition: Altitude Velocity TTFF (Time to First Fix) Cold Start TTFF (Time to First Fix) Warm Start RTCA/DO-229D MHz L1, C/A code receiver with SBAS capability 15 channels 5 Hz -145 dbm 6 seconds typical at -130 dbm GPS 9 seconds typical at -130 dbm SBAS Maximum 18,287 meters Maximum 513 m/s 90 seconds at -130 dbm (typical) 66 seconds at -130 dbm (typical) Compliant TSO-C154c GPS SBAS Receiver Performance (P/N , , , ) TSO Compliance: Regulatory: Number of channels: 20 Frequency: Sensitivity (Tracking Mode): Sensitivity (Acquisition Mode): TTFF Hot (valid almanac, position, time and ephemeris): TTFF Warm (valid almanac, position and time): TTFF Cold (valid almanac): Reacquisition (<10seconds obstruction): Position Update Interval: Velocity: Datum: TSO-C154c RTCA/DO-282B MHz L1 with SBAS capability -152 dbm (Tracking mode) -139 dbm (Acquisition mode) 1 second < 35 seconds < 35 seconds 0.1seconds 1 Hz 1,000 knots 60,000 ft MSL WGS-84 Copyright NavWorx Page 24 of 128 All rights reserved. Printed in the U.S.A.

25 Avionics Interfaces Annunciator Outputs: Altitude Encoder: Control Port: Maintenance Port: External Position Input: Display/Control: Capable of sinking 500mA for grounding an annunciator lamp RS232 asynchronous serial ARINC429 ADC/AHRS source (pressure altitude label 203) RS232 asynchronous serial RS232 asynchronous serial RS232 asynchronous serial (NexNav mini LRU Legacy Protocol, Aviation Format, and Garmin ADS-B Out +) ARINC743A GNSS sensor RS232 asynchronous serial (Pass-through or Traffic Alert interfaces) RS232 asynchronous serial (Pass-through, Traffic Alert or TIS-A interfaces) RS422 asynchronous serial (Pass-through or Traffic Alert interfaces) ARINC735 Traffic interface Copyright NavWorx Page 25 of 128 All rights reserved. Printed in the U.S.A.

26 4.2 System Configurations The ADS600-B UAT Transceiver must be configured with a GPS position source, a pressure altitude source, and a control panel for pilot input. Optionally, the ADS600-B UAT Transceiver may be configured with a display to display ADS-B, ADS-R, TIS-B traffic and FIS-B weather. Figures 4-3 through 4-5 depict typical ADS600-B UAT Transceiver system configurations. The ADS600-B UAT Receiver may be configured with a GPS position source. Optionally, the ADS600-B UAT Receiver may be configured with a display to display ADS-B, ADS-R, TIS-B traffic and FIS-B weather. Figures 4-6 through 4-8 depict typical ADS600-B UAT Receiver system configurations. Appendix A Interconnect Diagrams includes ADS600-B interconnection wiring diagrams. Copyright NavWorx Page 26 of 128 All rights reserved. Printed in the U.S.A.

27 GPS Antenna External GPS Source [8] Display (Traffic and/or Weather) [5][7] Compliant TSO-C154c GPS SBAS Receiver 9 33 VDC Avionics Bus Altitude Encoder [1] Control Panel [1] Annuciator Lamp [4] Maintenance Port (PC System using UAT Console Application) [1] Squat Switch [3] ADS600-B UAT Transceiver (TSO-C154c) P/N: , Notes: [1] Required for ADS-B Out [2] N/A [3] Optional for ADS-B Out [4] Required for ADS600-B Installations without a display [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously [8] Required when not using internal GPS Source L-band Equipment [1] Suppression Out UAT Antenna [1][6] Figure 4-3: ADS600-B UAT Transceiver with External Compliant GPS Copyright NavWorx Page 27 of 128 All rights reserved. Printed in the U.S.A.

28 GPS Antenna [2] Display (Traffic and/or Weather) [5][7] Compliant TSO-C154c GPS SBAS Receiver 9 33 VDC Avionics Bus Altitude Encoder [1] Control Panel [1] Annuciator Lamp [4] Maintenance Port (PC System using UAT Console Application) [1] ADS600-B UAT Transceiver (TSO-C154c) P/N: , Notes: [1] Required for ADS-B Out [2] Required for Internal GPS Source [3] Optional for ADS-B Out [4] Required for ADS600-B Installations without a display [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously Squat Switch [3] L-band Equipment [1] Suppression Out UAT Antenna [1][6] Figure 4-4: ADS600-B UAT Transceiver with Internal Compliant TSO-C154c GPS Copyright NavWorx Page 28 of 128 All rights reserved. Printed in the U.S.A.

29 GPS Antenna [2] Display (Traffic and/or Weather) [5][7] Compliant TSO-C145c GPS SBAS Receiver 9 33 VDC Avionics Bus Altitude Encoder [1] Control Panel [1] Annuciator Lamp [4] Maintenance Port (PC System using UAT Console Application) [1] ADS600-B UAT Transceiver (TSO-C154c) P/N: , Notes: [1] Required for ADS-B Out [2] Required for Internal GPS Source [3] Optional for ADS-B Out [4] Required for ADS600-B Installations without a display [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously Squat Switch [3] L-band Equipment [1] Suppression Out UAT Antenna [1][6] Figure 4-5: ADS600-B UAT Transceiver with Internal Compliant TSO-C145c GPS Copyright NavWorx Page 29 of 128 All rights reserved. Printed in the U.S.A.

30 GPS Antenna External GPS Source [8] Display (Traffic and/or Weather) [5][7] Compliant TSO-C154c GPS SBAS Receiver 9 33 VDC Avionics Bus Maintenance Port (PC System using UAT Console Application) ADS600-B UAT Receiver (TSO-C154c) P/N: , Notes: [1] N/A [2] N/A [3] N/A [4] N/A [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously [8] Required when not using internal GPS Source UAT Antenna [6] Figure 4-6: ADS600-B UAT Receiver with External Compliant GPS Copyright NavWorx Page 30 of 128 All rights reserved. Printed in the U.S.A.

31 GPS Antenna [2] Display (Traffic and/or Weather) [5][7] Compliant TSO-C154c GPS SBAS Receiver 9 33 VDC Avionics Bus Maintenance Port (PC System using UAT Console Application) ADS600-B UAT Receiver (TSO-C154c) P/N: , Notes: [1] N/A [2] Required for Internal GPS Source [3] N/A [4] N/A [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously UAT Antenna [6] Figure 4-7: UAT Receiver with Internal Compliant TSO-C154c GPS Copyright NavWorx Page 31 of 128 All rights reserved. Printed in the U.S.A.

32 GPS Antenna [2] Display (Traffic and/or Weather) [5][7] Compliant TSO-C145c GPS SBAS Receiver 9 33 VDC Avionics Bus Maintenance Port (PC System using UAT Console Application) ADS600-B UAT Receiver (TSO-C154c) P/N: , Notes: [1] N/A [2] Required for Internal GPS Source [3] N/A [4] N/A [5] Optional for ADS-B In [6] Required for ADS-B In [7] Traffic and Weather may be displayed on up to 3 displays simultaneously UAT Antenna [6] Figure 4-8: ADS600-B UAT Receiver with Internal Compliant TSO-C145c GPS Copyright NavWorx Page 32 of 128 All rights reserved. Printed in the U.S.A.

33 4.2.1 GPS Position Source Transceiver (P/N , , and ) The AD600-B must be configured with a GPS position source input. The GPS position source provides geometric position information to the ADS600-B to be transmitted in the ADS-B (out) messages. The GPS position source input may be obtained externally via RS-232 or ARINC 429, or internally. If the internal GPS is selected an external GPS antenna must be connected to the ADS600-B. The following external GPS position sources have been evaluated to show compliance with AC B: Accord Technology LLC NexNav mini LRU GPS Receiver, P/N FreeFlight 1201 WAAS GPS Garmin GNS480 GPS/Comm Navigator Garmin ADS-B Out Receiver (P/N , , and ) The ADS600-B must be configured with a GPS position source input. The GPS position source input may be obtained externally via RS-232 or ARINC 429, or internally. If the internal GPS is selected, an external GPS antenna must be connected to the ADS600-B. The following external GPS position sources are eligible to interface with the above part numbers: Accord Technology LLC NexNav mini LRU GPS Receiver, P/N FreeFlight 1201 WAAS GPS Garmin GNS480 GPS/Comm Navigator Garmin Aviation Format Garmin ADS-B Out Display The ADS600-B outputs traffic and weather information to up to three compatible displays simultaneously. The ability to display traffic and/or weather depends on the display device Maintenance Port The ADS600-B provides an RS232 communication port that is used to configure and monitor the status of the ADS600-B system via a computer. The maintenance port is required to be installed and connected. Copyright NavWorx Page 33 of 128 All rights reserved. Printed in the U.S.A.

34 4.2.4 Annunciator Output The ADS600-B can drive an external annunciator lamp. The annunciator is capable of sinking 500ma of current Altitude Encoder Input The ADS600-B must be configured with an altitude encoder input. This altitude encoder input provides pressure altitude to the ADS600-B to be transmitted in the ADS-B (out) messages. The pressure altitude encoder input may be obtained via RS-232 or ARINC 429. Section describes the RS-232 altitude encoder equipment that is eligible for operation with the ADS600-B. Section describes the ARINC 429 Pressure Altitude format that is eligible for operation with the ADS600-B Control Panel The transponder serves as a single-point of entry for squawk code (including emergency codes), ALT/STANDBY/ ON/OFF functionality and IDENT, as required by AC B. The control panel input may be obtained via RS-232 or RS-422. Section describes the RS-232 control panel equipment that is eligible for operation with the ADS600-B. Section describes the RS-422 control panel equipment that is eligible for operation with the ADS600-B. 4.3 Antenna Requirements GPS Antenna (P/N , , and ) If the ADS600-B is configured to use the internal compliant GPS as its position source, a GPS antenna must be attached to the GPS TNC antenna connector of the ADS600-B. The antenna performance is critical to the operation of the GPS/SBAS receiver. The recommended antenna is a DO-301 compliant antenna meeting the requirements of TSO-C190. For installations where the aircraft has an existing antenna complying with DO-228 (TSO-C144a), the ADS600-B (part numbers , , and ) may be installed utilizing this antenna, as per DO-229D Note 1, Section The performance of the ADS600-B GPS SBAS Receiver is affected by the gain, noise figure, impedance, and frequency selectivity characteristics of the antenna. The ADS600-B should be used only with the recommended antenna and cable. Use of other antennas and cables may not meet all of the performance characteristics specified in DO-229D. Copyright NavWorx Page 34 of 128 All rights reserved. Printed in the U.S.A.

35 The ADS600-B utilizes an active GPS antenna which means that the antenna includes a low noise amplifier. The power for the low noise amplifier is provided from the GPS receiver via the antenna coax cable. Table 4-4 contains a list of GPS antennas that are recommended for use with the ADS600-B GPS Antenna (P/N , , and ) If the ADS600-B is configured to use the internal compliant GPS as its position source, a GPS antenna must be attached to the GPS TNC antenna connector of the ADS600-B. Table 4-4 contains a list of GPS antennas that are recommended for use with the ADS600-B. Other GPS antennas may meet the installation requirements of the ADS600-B UAT Antenna The ADS600-B requires one UAT antenna meeting the following specification: standard 50Ω vertically polarized antenna with a VSWR < 1.7:1 at 978MHz. Table 4-3 contains a list of UAT antennas that are recommended for use with the ADS600-B. Antennas that meet TSO C66c and TSO-C74c are eligible for installation with the ADS600-B. Copyright NavWorx Page 35 of 128 All rights reserved. Printed in the U.S.A.

36 4.4 Installation This section describes the installation of the UAT, UAT Antenna, GPS Antenna and optionally the TransMonSPE for the ADS600-B article including mounting, wiring, and connections. A post installation checkout procedure is included at the end of this section. Obtain Appendix A from the Instructions for Continued Airworthiness, document To provide information for future maintenance activities, permanently draw into the diagrams in Section A.2 the following: - Specific locations of all equipment and antennas installed - Wire routing diagram sketches for all system wiring and cables installed Pre-Installation Information Read this entire section before proceeding with the installation of the ADS600-B. Perform the post installation checkout described in Section 4.7 prior to closing the work area to resolve wiring, mounting and configuration issues should they occur. Follow avionics installation practices per FAA Advisory Circular (AC) B, A, or FAA approved revisions to these documents. Perform an electrical load analysis on the aircraft prior to installation to ensure that the aircraft s electrical system is capable of carrying the ADS600-B load. Section describes the power consumption of the ADS600-B Installation Overview Installation of the ADS600-B UAT, the UAT antenna, and the GPS antenna requires determination of the location of the UAT, UAT indicator, UAT circuit breaker, UAT/GPS antennas, UAT maintenance port, and cable/wire routing to interfacing equipment. Installation of the optional TransMonSPE requires determination of the location of the TransMonSPE and cable/wire routing to the ADS600-B. Installation of the traffic/weather display, external GPS (if required), control panel (if required) and altitude encoder (if required) are not covered in this manual and should be installed in a manner approved by the FAA. Table 4-1 identifies the parts list for the installation of the ADS600-B. Table 4-2 identifies the parts list for the installation of the TransMonSPE. Copyright NavWorx Page 36 of 128 All rights reserved. Printed in the U.S.A.

37 Table 4-1: ADS600-B Installation Parts List Description Qty. Part Number Model Number 978MHz UAT Receiver (including items listed in Table 3-1and Table 3-2) 978MHz UAT Transceiver (including items listed in Table 3-1and Table 3-2) [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] [HWMOD]-[SWMOD] UAT Indicator 1 MS , (FAA TSO-C190, TSO-C144) GPS Antenna (including Gasket) (FAA TSO-C66c, TSO-C74c) UAT Antenna (including Gasket) Circuit Protection 3A Circuit Breaker (14VDC) OR 2A Circuit Breaker (28VDC) UAT Attachment Hardware: Ring Terminal Bolts Steel Flat Washers Elastic Stop Nuts GPS Antenna Attachment Hardware: Locking Hex Nuts Mounting Screws Doubling Plate UAT Antenna Attachment Hardware: Locking Hex Nuts Wire Shielded Wire Doubling Plate x or equivalent Installer Provided ADS600-B 1 See Table See Table or equivalent Installer Provided Installer Provided AN3-3A AN AN A 6-32UNC MS Installer Provided 8-32UNC Installer Provided MIL-W-22759/16 or equivalent Installer Provided MIL-C or equivalent Installer Provided Manufacturer NavWorx ITT Cannon Dialight Klixon Klixon Copyright NavWorx Page 37 of 128 All rights reserved. Printed in the U.S.A.

38 Table 4-2: TransMonSPE Parts List Description Qty. Part Number Model Number Manufacturer Transponder Monitor (Single Point of Entry) [HWMOD]-[SWMOD] TransMonSPE NavWorx USB Cable 10 feet TransMonSPE USB Cable - - Tie wraps As Installer Provided - - needed Cushion Clamp 1 Installer Provided MS21919-DG Screw (10-32) Steel Flat Washer Elastic Stop Nut Installer Provided MS Installer Provided AN Installer Provided AN A - - Copyright NavWorx Page 38 of 128 All rights reserved. Printed in the U.S.A.

39 Table 4-3: Acceptable UAT Antennas Manufacturer Part Num Connector RAMI AV-74 BNC RAMI AV-741 BNC Comant CI-105 BNC Comant CI TNC RAMI AV-22 BNC Table 4-4: Acceptable GPS Antennas Manufacturer Part Num TSO Recommended for ADS600-B Part Number Cobham Antennas (Comant) Sensor Systems Inc. CI CI CI CI S S S TSO-C190 TSO-C190 TSO-C144 TSO-C144 TSO-C190 TSO-C190 TSO-C Aero Antenna AT TSO-C Garmin GA-56 TSO-C129 Class A Copyright NavWorx Page 39 of 128 All rights reserved. Printed in the U.S.A.

40 4.4.3 Tools Required The D-Sub connector supplied with the ADS600-B uses crimp contacts. Table 4-5 identifies the crimp tool required to ensure consistent and reliable crimp contact connections for the D-Sub connector. Table 4-5: Crimp Tools for High Density AWG Socket Contact Type Hand Crimping Tool Positioner Insertion/Extraction Tool Military P/N M22520/2-01 M22520/2-09 M81969/1-04 Positronic M81969/1-04 AMP Daniels AFM8 K13-1 M81969/1-04 Astro M81969/ ADS600-B Mounting Select a mounting location on a sufficiently flat surface that has (or is made to have with structural enhancements) the ability to withstand the inertial forces imposed by the 1.6 pound unit (3g up, 18g forward and 4.5g lateral). Allow for three inches of clearance on the antenna connector side of the UAT and four inches of clearance on the D-Sub side of the UAT. Mount the UAT with 4 each AN3-3A bolts, 4 each AN nuts and 8 each washers where the washers are placed on both the bolt and nut side. Refer to Figure 4-9 for the ADS600-B mounting hole pattern. Installation of the ADS600-B must be in accordance with AC B, Chapter 1. The installer must verify by FAA approved data that the mounting surface can support the following loads: Shear: 36 lbs Tension: 36 lbs Bearing: lbs/mounting hole The ADS600-B should be mounted to a surface known to have sufficient structural integrity to withstand inertial forces imposed by the 1.6 pound unit. The ADS600-B may be mounted using 4 AN3-3A bolts, 4 AN A nuts and 8 washers where the washers are placed on both the bolt side and nut side. Refer to the bolt/nut fastener manufacturer for torque guidelines. The ADS600-B should be connected to the airframe ground via the mounting bolts or braided strap. Copyright NavWorx Page 40 of 128 All rights reserved. Printed in the U.S.A.

41 Figure 4-9: ADS600-B Mounting-Hole Pattern Copyright NavWorx Page 41 of 128 All rights reserved. Printed in the U.S.A.

42 Figure 4-10: ADS600-B Exploded View Copyright NavWorx Page 42 of 128 All rights reserved. Printed in the U.S.A.

43 4.4.5 GPS Antenna Mounting The GPS antenna should not be mounted close to VHF COM transmitter antenna, and other antennas emitting high power. Special care should be taken to ensure that the GPS antenna is not mounted in close proximity to antennas that may emit harmonic interference at the L1 frequency of MHz. Select a mounting location on the top of the aircraft that is at least 18 from VHF COM transmitter antennas and within +/-4 degrees of the longitudinal axis of the aircraft. For best performance, select an antenna location with an unobstructed view of the sky above the aircraft when in level flight. See Appendix I for mounting instructions for TSO-C144 and TSO-C190 GPS Antennas UAT Antenna Mounting Select a mounting location on the underside of the aircraft that is at least 5 feet from any L-Band (Transponder, TCAS, TAS) antenna and at least 7 feet from any DME antenna and within +/-4 degrees of the longitudinal axis of the aircraft. See Appendix for mounting instructions for TSO-C66c and TSO-C74c UAT Antennas. Copyright NavWorx Page 43 of 128 All rights reserved. Printed in the U.S.A.

44 4.4.7 TransMonSPE The following sections describe how to attach the TransMonSPE to the transponder coax cable, connect the TransMonSPE to the ADS600-B and secure the TransMonSPE in the aircraft. The TransMonSPE dimensions are: 3.0 x x (includes USB plug) Attaching TransMonSPE to Transponder Coax 1. Place the transponder antenna coax cable into the channel of the TransMonSPE base. See Figure Slide the bottom cover into the TransMonSPE base and over the coax cable. See Figure Screw in flat head screw to keep bottom cover in place. See Figure Attach two tie wraps, one around the USB cable and the other adjacent to the end of the TransMonSPE. Remove the excess tie wrap using diagonal cutters. See Figure Figure 4-11: Coax in Channel of TransMonSPE Base Figure 4-12: TransMonSPE Bottom Cover over Coax Counter sink hole faces up Copyright NavWorx Page 44 of 128 All rights reserved. Printed in the U.S.A.

45 Figure 4-13: TransMonSPE Fully Installed Bottom Cover Figure 4-14: TransMonSPE with Attached USB Connector Connecting TransMonSPE to ADS600-B The TransMonSPE is shipped with a 10 foot cable terminated on one end with a USB style connector. This connector is attached to the USB plug of the TransMonSPE. The other end of the cable is attached to the ADS600-B as described in A.8 Interconnect Diagram: ADS600-B to Control Panel Securing TransMonSPE in Aircraft Using a MS21919-DG21 clamp, secure the TransMonSPE to the aircraft structure. See Figure Follow installation practices per FAA Advisory Circular (AC) B Chapter 11 Section 11. Figure 4-15: Securing TransMonSPE with Clamp Copyright NavWorx Page 45 of 128 All rights reserved. Printed in the U.S.A.

46 4.4.8 Maintenance Port Select a mounting location that allows for easy access to the DB-9 connector. The maintenance port is used to configure and perform software upgrades of the ADS600-B Circuit Breaker The circuit breaker is placarded as UAT, and the placard font size should be equivalent to the font size of the adjacent circuit breaker labels to ensure legibility. Select a mounting location that is co-located with the circuit breaker or fuse panel of the aircraft Annunciator The annunciator is placarded as UAT Fail, and the placard font size should be equivalent to the font size of the existing placards that are within the normal field of view of the pilot s control wheel. If placards do not exist for this view, then the placard font size should be equivalent to the placard font size of the circuit breaker. Copyright NavWorx Page 46 of 128 All rights reserved. Printed in the U.S.A.

47 Cabling and Wiring Refer to the interconnect diagrams of Appendix A Interconnect Diagrams for appropriate wiring connections to assemble the DB37 harness. After the DB37 harness assembly is built and installed on the ADS600-B, route the wire bundle as appropriate. Use cable ties to secure the harness assembly. The ring terminals that are affixed to the cable shields of the harness assembly should be attached to ground via the DB-37 back shell cable clamp. See Figure 4-16 for ground attachment. The equipment wiring should be performed in accordance with AC B Chapter 11. Ensure that the harness assembly is not routed near high energy sources. Isolate the harness assembly from the engine. Install harness assembly in a protected area of the aircraft. Use 24 AWG or larger for all wiring expect for power. RG-400 coaxial cable is required for the UAT Antenna. UAT Antenna cable loss should not exceed 3 db. Figure 4-16: Clamp Ground Termination Air Circulation and Cooling The ADS600-B meets all DO-282B requirements without external cooling. However, as with all electronic equipment, lower operating temperatures will extend equipment life. It is not recommended to use outside forced air to cool the unit. Instead it is recommended that an electric forced air fan be installed to cool the equipment. If forced air cooling is installed, ensure that rainwater cannot enter or be sprayed on the ADS600-B. Copyright NavWorx Page 47 of 128 All rights reserved. Printed in the U.S.A.

48 4.5 Electrical Connections The installation kit includes a D-Sub 37 pin connector and crimp contacts for the UAT. The crimp contacts are specified for 20 to 24 AWG wire. Route the harness to the ADS600-B. Cut to length, ensuring a small service loop exists for strain relief. For shielded cables, where the cable shield will not be grounded on the ADS600-B side, strip and trim the braided shield then cover the exposed area with heat shrink material to prevent the braid from contacting other wires in the bundle. Crimp and insert pins into the D-Sub 37 pin connector. After installing the pins, assemble the back shell for strain relief. Make the crimp connections with a crimp tool as specified in the Table 4-5. Table 4-6 describes the connectors supplied with the ADS600-B installation kit. The kit also contains crimp contacts for the D-Sub connector. Table 4-5 identifies the crimp tools required to ensure consistent and reliable crimp contact connections. Table 4-6: Connectors Ref Description Connector Type Crimp Contact P1 I/O 37 Pin D-Sub Receptacle AWG socket contact P2 UAT Antenna TNC jack N/A P3 GPS Antenna TNC jack N/A Protection The ADS600-B is protected via a dedicated circuit breaker. Refer to guidelines in AC B, Chapter 11 Section 4. The circuit breaker is placarded with the description UAT. Table 4-7: Circuit Breaker Protection ADS600-B 14 VDC 28 VDC **Circuit Protection 3 AMP 2 AMP ** If using a fuse, it must be a slow blow fuse type. Copyright NavWorx Page 48 of 128 All rights reserved. Printed in the U.S.A.

49 4.5.2 Electrical Current Use Table 4-9 and Table 4-11 to aid in electrical load analysis computations. Table 4-8: Electrical Load Requirement for P/N , Input Voltage 14 VDC 28 VDC Current Consumption Typical Table 4-9: Electrical Load Requirement for P/N , Input Voltage 14 VDC 28 VDC Current Consumption Typical Maximum Table 4-10: Electrical Load Requirement for P/N , Input Voltage 14 VDC 28 VDC Current Consumption Typical Table 4-11: Electrical Load Requirement for P/N , Input Voltage 14 VDC 28 VDC Current Consumption Typical Maximum Copyright NavWorx Page 49 of 128 All rights reserved. Printed in the U.S.A.

50 4.5.3 DB-37 I/O Connector (P1) A 37 pin D-Sub connector interfaces to external equipment and aircraft power. This connector can be found at the rear of the ADS600-B unit. View looking at ADS600-B. Figure 4-17: 37 Pin D-Sub Male Connector (P1) The pin-out description for the I/O connector is defined in Table Equipment interconnect diagrams are shown in Appendices A and B. Copyright NavWorx Page 50 of 128 All rights reserved. Printed in the U.S.A.

51 Table 4-12: I/O Connector Pin-Out (P1) for ADS600-B Pin # I/O Name Description 1 -- Audio Out + RESERVED Feature, Not Functional. 2 I Time mark In - ARINC 743A Time Mark In VDC PWR Roving Networks Bluetooth &WiFi module power 100mA max. 4 I RS232 Maintenance RX RS232 Maintenance Port Serial Data Input 5 O DISPLAY PORT 1 RS232 TX RS232 Display 1 Serial Data Output 6 -- Ground, Signal Ground, Signal 7 I Altitude Encoder RX RS232 Altitude Encoder Input 8 O 429 OUT 1B ARINC 429 Output Channel 1B 9 I 429 IN 1A ARINC 429 Input Channel 1A RESERVED RESERVED 11 I External PPS TTL In External PPS TTL In 12 O RS422 TX - RS422 Display 1 Channel Data Output - 13 I RS422 RX + RS422 Display 1 Channel Data Input + 14 O UAT Indicator Out UAT Indicator Output (active low) 15 O ADS-B Compliant GPS Functional on part numbers XX only 16 O GPS TX GPS Position Source TX Ground, Signal Ground, Signal Power + Main Aircraft Power Input (+9 to +33VDC) Power + Main Aircraft Power Input (+9 to +33VDC) Audio Out - RESERVED Feature, not functional 21 I Time mark In + ARINC 743A Time Mark In + 22 O RS232 Maintenance TX RS232 Maintenance Port Serial Data Output Ground, Signal Ground, Signal 24 I DISPLAY PORT 1 RS232 RX RS232 Display 1 Serial Data Input 25 O DISPLAY PORT 2 RS232 TX RS232 Display 2 Serial Data Output Ground, Signal Ground, Signal 27 O 429 OUT 1A ARINC 429 Output Channel 1A 28 I 429 IN 1B ARINC 429 Input Channel 1B Squat Switch In RESERVED 30 O RS422 TX + RS422 Display 1 channel data output + 31 I RS422 RX - RS422 Display 1 channel data input Ground, Signal Ground, Signal 33 I Transponder Control RX RX Data from Transponder configured for Remote Mode 34 I GPS RX GPS Position Source Input 35 O Suppression Output Suppression Output (active high) 36 I Power Ground Main Aircraft Power Ground 37 I Power Ground Main Aircraft Power Ground Copyright NavWorx Page 51 of 128 All rights reserved. Printed in the U.S.A.

52 4.6 Functional Descriptions Power Aircraft power is provided to the ADS600-B on the P1 I/O connector. The ADS600-B accepts input power from +9 to +33 VDC. P1-18 Power + P1-19 Power + P1-36 Power Ground P1-37 Power Ground Discrete Outputs The ADS600-B provides discrete outputs to provide status and drive annunciator lamps or other equipment. All discrete outputs are active low (i.e. grounded when active) and are of open collector design, capable of sinking up to 500 ma UAT Indicator The UAT Indicator Out (P1-14) is used to indicate the status of the ADS600-B receiver. UAT Indicator Out will be grounded when the ADS600-B has detected a system failure. Otherwise, this output will be open Suppression Output The Suppression Output (P1-35) is intended to suppress other L-band equipment (such as a transponder) when the UAT transmits. It will provide a high signal (Vin 1.0V) whenever the UAT is transmitting and ground otherwise Discrete Inputs The ADS600-B accepts discrete inputs to provide additional status information from the aircraft systems or equipment. All inputs are active low (i.e. grounded when active) and each input presents a load of greater than 100 kω. Copyright NavWorx Page 52 of 128 All rights reserved. Printed in the U.S.A.

53 4.6.4 PPS Time Mark Input When used with an external ARINC 743A position source, external NexNav mini LRU, or GTN 650/750 (ADS-B Out +), the time mark signals from the navigation sensor are connected to the ADS600-B time mark input pins (P1-2 and P1-21). When used with a GNS 430W/530W (ADS-B Out+) or Avidyne IFD 440/540 (ADS-B Out +), the time mark signal from the navigation sensor is connected to ADS600-B External PPS TTL In (pin p1-11). PPS Time Mark Input is not required for ADS600-B (UAT Receiver) part numbers , , and Serial Interfaces The ADS600-B provides two bi-directional RS-232 serial interfaces, three receive only RS232 interfaces, one transmit only RS232 interface, one bi-directional RS-422 interface and one ARINC 429 input/output. The serial interfaces can be connected to: Display(s) Maintenance PC Altitude Encoder Control Panel Global Navigation Satellite System (GNSS) Position Source The serial port pin-outs are: P1-13 RS422 Display 1 Serial Data Input + P1-31 RS422 Display 1 Serial Data Input - P1-12 RS422 Display 1 Serial Data Output - P1-30 RS422 Display 1 Serial Data Output + P1-9 ARINC 429 Input Channel 1A P1-27 ARINC 429 Output Channel 1A P1-28 ARINC 429 Input Channel 1B P1-8 ARINC 429 Output Channel 1B P1-7 RS232 Altitude Encoder Serial Data Input P1-25 RS232 Display 2 Serial Data Output P1-6 RS232 Altitude Encoder and Display 2 Ground P1-33 RS232 Transponder Control Panel Input Copyright NavWorx Page 53 of 128 All rights reserved. Printed in the U.S.A.

54 P1-32 RS232 Transponder Control Panel Ground P1-24 RS232 Display 1 Serial Data Input P1-5 RS232 Display 1 Serial Data Output P1-23 RS232 Display 1 Ground P1-4 RS232 Maintenance Port Serial Data Input P1-22 RS232 Maintenance Port Serial Data Output P1-26 RS232 Maintenance PC Ground P1-34 GPS Receive (external GNSS Position Source) P1-32 Ground RS232 Altitude Encoder Input An altitude encoder input may be provided through a RS232 serial data input (P1-7) to the ADS600-B. The UAT Console is used to select the format of altitude encoder input, as well as, the serial baud rate of the altitude encoder input port. Any altitude encoder that supports the following formats is eligible for operation with the ADS600-B: Icarus, Shadin Z, Shadin RMS, UPSAT Apollo and EFIS. The details of the altitude encoder formats are described in Appendix D. The format of the EFIS protocol is described in ADS600-B Interface Control Document ( Rev 10 or later). Refer to section A.17 of Appendix A Interconnect Diagrams for Altitude Encoder Equipment wiring RS232 Control Panel Input A transponder control panel input may be provided through a RS232 serial data input (P1-33) to the ADS600-B. The UAT Console is used to select the type of transponder control panel input. The following transponder control panels are eligible for operation with the ADS600-B: NavWorx TransMonSPE, Garmin GTX-330, GTX-327, SL70/70R, GNS480, Trig TT21/TT22/TT31, and Sandia STX-165. Refer to section A.16 of Appendix A Interconnect Diagrams for Control Panel Equipment wiring RS232 Out Display 2 The ADS600-B may be configured to output to a display device using the RS232 serial interface (P1-6 and P1-25). The type of display device is configurable. The UAT Console allows the installer to select a display device, as well as, a baud rate for the RS232 serial interface. Equipment that supports the Capstone Traffic Report, Capstone Pass-through and TIS-A protocols are eligible for operation with the ADS600-B. The ADS600-B Interface Control Document, Rev 12 (or later) describes these protocols. Copyright NavWorx Page 54 of 128 All rights reserved. Printed in the U.S.A.

55 RS422 In/Out Display The ADS600-B may be configured to output to a display device using the RS422 serial interface (P1-12, P-13, P1-30, and P1-31). The type of display device is configurable. The UAT Console allows the installer to select a display device, as well as, a baud rate for the RS422 serial interface. Equipment that supports the Capstone Traffic Report and Pass-through display protocols are eligible for operation with the ADS600-B. The ADS600-B Interface Control Document, Rev 12 (or later) describes these protocols. In addition to serving as a display device, the Garmin MX20 and GMX 200 are eligible to operate as a control panel input to the ADS600-B. Refer to section A.14 of Appendix A Interconnect Diagrams for Control Panel wiring RS232 In/Out Display 1 The ADS600-B may be configured to output to a display device using the RS232 serial interface (P1-5, P1-23, and P1-24). The type of display device is configurable. The UAT Console allows the installer to select a display device, as well as, a baud rate for the RS232 serial interface. Equipment that supports the Capstone Traffic Report and Capstone Pass-through protocols are eligible for operation with the ADS600-B. The ADS600-B Interface Control Document, Rev 12 (or later) describes these protocols RS232 Maintenance PC The ADS600-B communicates with the maintenance PC using a RS232 serial interface (P1-26, P1-4, and P1-22). This interface is used to view system status and to set the configuration of the ADS600-B. The maintenance PC serial channel is fixed at 115,200 baud, 8 data, no parity, 1 stop bit. The UAT Console, a Windows PC application, communicates to the ADS600-B using this port RS232 GNSS Position Source The ADS600-B may be configured to use the Accord Technology NexNav mini LRU (P/N 21000) as its external GNSS Position Source input (P1-34 and P1-32). The ADS600-B may be configured to use the Garmin ADS-B Out+ Format as its external GNSS Position Source input (P1-34 and P1-32). ADS600-B part numbers and may be configured with the Garmin Aviation Format as its external GNSS Position Source input (P1-34 and P1-32). The UAT Console allows the installer to select the GNSS Position Source to use with the ADS600-B. Copyright NavWorx Page 55 of 128 All rights reserved. Printed in the U.S.A.

56 4.6.6 ARINC429 The ADS600-B provides one ARINC 429 input and output (P1-8, P1-9, P1-27, and P1-28) interface. The ARINC 429 baud rate can be set to either High or Low to match the baud rate of the connected equipment. Equipment that supports the following ARINC format/labels is eligible to operate with the ADS600-B: ARINC 735B Traffic Computer (TCAS and ADS-B) output. The output labels are listed in Table ARINC Label 203 (Pressure Altitude) input. ARINC 743A-4 GNSS Sensor input. The input labels are listed in Table The ARINC input/output is configured using the UAT Console. Table 4-13: ARINC 429 (735B) Out Labels Label Number Parameter Name 130 Intruder Range 131 Intruder Altitude (relative) 132 Intruder Bearing Estimate 203 Pressure Altitude 270 Vertical RA Data Output 274 Selected Sensitivity Level 350 Fault Summary 357 Request to Send (RTS) or End of Transmission (ETX) 371 General Aviation Equipment ID 377 Equipment ID Table 4-14: ARINC 429 (743A) In Labels Label Number Parameter Name 110 GNSS Latitude 111 GNSS Longitude 120 GNSS Latitude Fine 121 GNSS Longitude Fine 130 AUT Horizontal Integrity Limit 136 Vertical Figure of Merit 150 UTC 165 Vertical Velocity 166 North/South Velocity 174 East/West Velocity 247 Horizontal Figure of Merit 370 GNSS Height 377 Equipment ID Copyright NavWorx Page 56 of 128 All rights reserved. Printed in the U.S.A.

57 4.7 ADS600-B Post Installation Check Mounting/Wiring Check Verify that the ADS600-B is secured to the aircraft as described in section Verify that both the UAT and GPS antennas are securely cabled to the appropriate connectors as described in sections and Verify that the maintenance port and power/ground are securely cabled to the DB37 connector of the ADS600-B. Ensure that the slide lock of the DB37 is in the locked position. If any ADS600-B cabling is routed near the aircraft controls, verify free movement of the aircraft controls Power and Ground Check After the harness is installed and terminated, check for power and ground with a DVM (Digital voltmeter) at the following locations: Ground: P1-pin 36, P1-pin 37 Power: P1-pin 18, P1-pin Antenna Check Check antenna wiring with a DVM that has a diode check function mode. When testing, the return lead of the DVM must be connected to the coax shield conductor. Using the aircraft ground may result in invalid reading because of too much resistance UAT Antenna Using the ohms mode of a DVM, check the resistance of the UAT antenna. Apply one test lead to the coax connector center conductor and the other lead to the coax shield. The impedance should show greater than 10 ohms GPS Antenna Using the diode test mode of the DVM, check the GPS antenna. Place the black ( ) lead to the center conductor and the red (+) lead to the coax shield. The DVM should read between 0.3 V and 0.9 V Configuration of ADS600-B with Maintenance PC The UAT Console is a Windows PC application required to configure the ADS600-B. Refer to Appendix C for a description of how to configure the ADS600-B unit via the Maintenance Personal Computer (PC). The maintenance port of the ADS600-B is connected to a Windows serial port. Older computers have physical DB-9 serial connectors attached to the computer, while newer computers have only USB ports in this case an off-the-shelf serial-to-usb adapter cable needs to be installed to create the serial port. The computer s serial port is then connected to the ADS600-B maintenance port using a straight-through DB9 extension cable. Copyright NavWorx Page 57 of 128 All rights reserved. Printed in the U.S.A.

58 The UAT Console communicates with the ADS600-B via the Windows serial port. There is no need for the installer to configure the serial port as it is automatically done by the UAT Console. The UAT Console is launched by either clicking the desktop icon, or selecting the UAT Console from the Windows Start Menu. The UAT Console will display a list of available COM ports: the installer must select the COM port that is connected to the ADS600-B GPS Position Source Check With the ADS600-B powered up and the aircraft in full view of the sky, use the UAT Console to verify that the GPS Position Source has been successfully configured. View the Status tab of the UAT Console and observe that the GPS position source is correctly configured and indicates: GPS Position Source Passed. Note: the displayed GPS position (latitude, longitude and altitude) should be within 169 feet of the GPS Position Source. Copyright NavWorx Page 58 of 128 All rights reserved. Printed in the U.S.A.

59 Serial Altitude Encoder Check With the ADS600-B powered up, as well as the aircraft s Altitude Encoder, use the UAT Console to verify that the Altitude Encoder has been successfully configured. View the Status tab of the UAT Console and observe that the altitude format is correctly configured and indicates: Altitude Encoder Input Passed. Verify that the pressure altitude is correct and matches that of the encoder. Copyright NavWorx Page 59 of 128 All rights reserved. Printed in the U.S.A.

60 Control Panel Check With the ADS600-B powered up, use the UAT Console to verify that the Control Input has been successfully configured. View the Status tab of the UAT Console and observe that the Control Panel Type is correctly configured and indicates: Transponder Control Input Passed. Verify that the Flight ID of the Transponder and ADS600-B are identical. Copyright NavWorx Page 60 of 128 All rights reserved. Printed in the U.S.A.

61 Display Check With the ADS600-B and connected Display powered up, select the Enable Traffic Simulation button of the UAT Console. Observe traffic target circling (above and below) the own ship position. To disable the traffic simulation, select the Disable Traffic Simulation button or cycle power to the ADS600-B. Select Enable Traffic Simulation Installation Completion After ensuring that all portions of the installation are successfully completed, visually inspect all installed items and cover all open areas. Copyright NavWorx Page 61 of 128 All rights reserved. Printed in the U.S.A.

62 4.7.6 VHF COM Interference GPS Testing This section applies to all ADS600-B part numbers. Susceptibility to harmonics of VHF COM transceivers shall be evaluated in compliance with AC D. Confirm compatibility by tuning the VHF COM transceiver(s) to the following frequencies and then and confirm the GPS position (latitude/longitude) transmitted by ADS600-B. Section describes how to verify the GPS Position. VHF COM Frequency MHz MHz MHz MHz MHz MHz Confirm GPS Position The GPS latitude/longitude position may be verified by either: a. Using the UAT Console. The GPS Antenna must have a view of the sky and the ADS600-B must be powered up and a PC (with the UAT Console application) must be connected to the maintenance port of the ADS600-B. Using the UAT Console select the Reports Tab, then select the View Status Messages check box. Verify that the latitude and longitude displayed on the Reports Tab is within 169 feet of position of the GPS antenna. See Figure C- 14: UAT Console Reports Tab. b. Using a display that receives ownship messages from the ADS600-B. The GPS Antenna must have a view of the sky and the ADS600-B and avionics display must be powered up. Verify that the latitude and longitude displayed on the avionics display is within 169 feet of position of the GPS antenna. Copyright NavWorx Page 62 of 128 All rights reserved. Printed in the U.S.A.

63 4.7.7 Weight and Balance An aircraft weight and balance is required after installation of the ADS600-B. Follow the guidelines in AC B, Chapter 10, Section 2. Update the aircraft equipment list indicating the items relocated, added or removed. Table 4-15 identifies the weight of the ADS600-B equipment. Figure 4-18 depicts the ADS600-B center of gravity. Table 4-15: ADS600-B Weight Item ADS600-B (P/N , ) ADS600-B (P/N , ) ADS600-B (P/N , ) ADS600-B (P/N , ) Weight 1.0 lbs 1.4 lbs 1.2 lbs 1.8 lbs Figure 4-18: ADS600-B Center of Gravity Copyright NavWorx Page 63 of 128 All rights reserved. Printed in the U.S.A.

64 4.8 TransMonSPE Post Installation Check Mounting and Wiring Check 1. Apply power to the ADS600-B and the aircraft s transponder. 2. Utilizing a transponder test set (IFR ATC-600 or equivalent) to interrogate the aircraft s transponder. 3. Using the UAT Console, verify (on the Status page) that the Transponder Control input indicates the Mode 3/A code, IDENT, and emergency status as configured on the transponder. Refer to section Weight and Balance The TransMonSPE weighs 2.4 ounces. The guidelines of AC B CHG 1, Chapter 10-1 and 10-2.c. categorizes the weight of the TransMonSPE as negligible and thus the installation of the TransMonSPE does not require a weight and balance check. Copyright NavWorx Page 64 of 128 All rights reserved. Printed in the U.S.A.

65 Appendix A Interconnect Diagrams The following matrix illustrates which GPS Position Sources, Control Panels, Altitude Encoders, and Displays connect to the various part numbers of the ADS600-B. The cells of the matrix identify the Appendix A reference and page of the relevant Interconnect Wiring diagram. ADS600-B Part Number ARINC 743A GPS Source RS232 GPS Source A.14, Page A.13, Page A.14, Page A.13, Page Basic Interconnect System with RS232 Display A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 A15, Page 82 A20, Page 87 System with RS422 Display A16, Page 83 - System with ARINC 735B Traffic A16, Page 83 A17, Page 84 A16, Page 83 - A16, Page 83 A17, Page 84 A16, Page 83 - A16, Page 83 A17, Page 84 A16, Page 83 - A16, Page 83 A17, Page 84 ADS600-B Part Number Internal GPS Compliant TSO-C145c A.12, Page A.12, Page A.12, Page A.12, Page 79 GPS Position Source Internal GPS Compliant TSO-C154c A.12, Page A.12, Page A.12, Page A.12, Page External GPS A.10, Page 76, A.19, Page 86, A.23, Page 90, A.24, Page 91, A.25, Page 92 A.2, Page 68, A.10, Page 76, A.19, Page 86, A.23, Page 90, A.24, Page 91, A.25, Page 92 A.10, Page 76, A.23, Page 90, A.24, Page 91, A.25, Page 92 A.2, Page 68, A.10, Page 76, A.23, Page 90, A.24, Page 91, A.25, Page 92 Copyright NavWorx Page 65 of 128 All rights reserved. Printed in the U.S.A.

66 Control Panel / Altitude Encoder * ADS600-B Part Number TransMonSPE GTX 33/330 GTX 32/327 TT21/TT22/TT31 STX-165(R) SL70(R) A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 A.8, Page 74 * Some devices output encoder data with control data Altitude Encoder ADS600-B SSD120-30/35N- A U SAE T TC20 ARINC 429 Part Number RS A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.9, Page 75 A.11, Page 77 A.22, Page 89 Display (Certified) ADS600-B Part Number GNS480 (ARINC 429) GNS480 (RS-232 TIS) GNS 430 (ARINC 429) MX20/GMX200 (RS-422) MX20/GMX200 (ARINC 429) IFD 4XX/5XX A.4, Page 70 - A.6, Page 72 - A.21, Page A.3, Page 69 - A.5, Page 71 A.7, Page 73 A.21, Page A.4, Page 70 - A.6, Page A.3, Page 69 - A.5, Page 71 A.7, Page A.4, Page 70 - A.6, Page 72 - A.21, Page A.3, Page 69 - A.5, Page 71 A.7, Page 73 A.21, Page A.4, Page 70 - A.6, Page A.3, Page 69 - A.5, Page 71 A.7, Page 73 Copyright NavWorx Page 66 of 128 All rights reserved. Printed in the U.S.A.

67 A.1 Interconnect Diagram: ADS600-B Maintenance Port to Computer NavWorx, Inc Big A Road Rowlett, TX ADS600-B Maintenance (Serial) Port to Computer Interconnect Diagram Rev Date Description - A B 06/18/11 04/09/09 Initial Release 08/29/10 Added Diagram Headers Changed Maintenance Port Ground Pin number C 06/22/14 Updated type of wire used DB9 Male Connector 2 Maintenance Port DB9 Female Connector P1 ADS600-B Computer Maintenance Port RX Maintenance Port TX Maintenance Port Ground NOTES: 1. ALL WIRES 24 AWG or LARGER UNLESS OTHERWISE SPECIFIED. 2 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT, NO FLOW CONTROL. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. Copyright NavWorx Page 67 of 128 All rights reserved. Printed in the U.S.A.

68 A.2 Interconnect Diagram: GNS 480 ARINC 743A Position Source NavWorx, Inc Big A Road Rowlett, TX GNS 480 ARINC 743A Position Source Attention: Use the UAT Console to configure the GNS 480 as the GPS Source for the ADS600-B. On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the GNS480 item. Rev Date Description TWISTED SHIELDED TWO - 04/14/09 CONDUCTOR Initial Release SHIELD TERMINATED TO GROUND A 08/29/10 Added Diagram Headers B 01/28/11 Identified GNS 480 connectors C 06/22/14 Added UAT Console Note ADS600-B GNS 480 P1 P3 2 1 GPS 3 ARINC 429 Out 2A P In 1A ARINC 429 Out 2B P In 1B Time Mark Out + P A Time Mark In + Time Mark Out - P A Time Mark In - NOTES: 1 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2 GNS 480 ARINC 429 #1 OUT (P5-4/24) MAY BE USED INSTEAD OF 429 #2 (P5-5/25) OUT. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P1: 37-PIN D-SUB, MALE CONNECTOR P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 3 DO NOT CONNECT GPS ANTENNA. Copyright NavWorx Page 68 of 128 All rights reserved. Printed in the U.S.A.

69 A.3 Interconnect Diagram: ADS600-B to GNS 480 Traffic (ARINC 429) NavWorx, Inc Big A Road Rowlett, TX ADS600-B to GNS 480 Traffic (ARINC 429) P1 ADS600-B Rev Date Description - 04/14/09 Initial Release A 08/29/10 Added power and ground wiring recommendations B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/22/14 Updated Wire Type GNS 480 ARINC 429 In 3A P5-9 8 Control Panel 11 Suppression In +5VDC RS232 Out Serial Ground 4 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground Out 1A Power + Power + P Attention: Use the UAT Console to configure GNS 480 as a display. On the UAT Console select the Initialization tab, then select the Displays tab. To enable ARINC select ARINC 429 Installed. Then from the ARINC 429 Port Display Type pull-down menu select the ARINC 429 Traffic Advisories item. From the ARINC 429 Port Rate pull-down menu select High. 3/2 AMP UAT 5 AVIONICS BUS (14/28 VDC) ARINC 429 In 3B P Out 1B Power Ground 36 Power Ground 37 1 AIRCRAFT GROUND Maintenance Port Top GPS Antenna 3 DB9 Female Connector 3 4 UAT Indicator 14 Maintenance Port RX Maintenance Port TX 5 26 Maintenance Port Ground P3 6 GPS RG400 P2 NOTES: Altitude Encoder 10 TX Ground 7 6 Altitude Encoder RX Altitude Encoder Ground UAT RG POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 IF THE ARINC 429 TRAFFIC OPTION IS CONFIGURED FOR THE GNS 480, THE GNS 480 SERIAL TIS OPTION IS NOT AVAILABLE. P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. Copyright NavWorx Page 69 of 128 All rights reserved. Printed in the U.S.A.

70 A.4 Interconnect Diagram: ADS600-B to GNS 480 Traffic (RS-232 TIS) NavWorx, Inc Big A Road Rowlett, TX GNS 480 RS232 RxD6 ADS600-B to GNS 480 Traffic (RS-232 TIS) P5-2 8 Control Panel 12 Suppression In +5VDC RS232 Out Serial Ground 4 P1 ADS600-B 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground Power + 25 TIS TX Power + P Rev Date Description - 04/06/09 Initial Release A 08/29/10 Added power and ground wiring recommendations B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/22/14 Updated Wire Type Attention: Use the UAT Console to configure TIS-A as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the TIS-A Display Type pull-down menu select the GPSMAP (396,496,696,etc) item. 3/2 AMP UAT 5 AVIONICS BUS (14/28 VDC) Serial Ground 6 P TIS Ground 9 Power Ground 36 Power Ground 37 1 AIRCRAFT GROUND Maintenance Port Top GPS Antenna 3 DB9 Female Connector 3 4 UAT Indicator 14 Maintenance Port RX Maintenance Port TX 5 26 Maintenance Port Ground P3 6 GPS RG400 4 P2 Altitude Encoder 11 TX Ground 7 6 Altitude Encoder RX Altitude Encoder Ground UAT RG400 7 NOTES: 9 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 IF THE SERIAL TIS OPTION IS CONFIGURED FOR THE GNS 480, THE GNS 480 ARINC 429 TRAFFIC OPTION IS NOT AVAILABLE. P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) Bottom UAT Antenna 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 9 TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME GROUND PIN, P CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 11 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 12 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. Copyright NavWorx Page 70 of 128 All rights reserved. Printed in the U.S.A.

71 A.5 Interconnect Diagram: ADS600-B to GNS 430 Traffic (ARINC 429) Copyright NavWorx Page 71 of 128 All rights reserved. Printed in the U.S.A.

72 A.6 Interconnect Diagram: ADS600-B to MX20/GMX 200 (RS422 Traffic/Weather) MX20 or GMX NavWorx, Inc Big A Road Rowlett, TX ADS600-B to MX20 or GMX 200 ADS-B Traffic and Weather RS422 Interconnect Diagram RS422 TX4 + 8 RS422 TX4-10 PORT 4 CONFIG (GMX 200 ONLY) P RS422 RX RS422 RX Control Panel Altitude Encoder TX Ground Suppression In +5VDC RS232 Out Serial Ground 4 P1 ADS600-B 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground 7 6 Altitude Encoder RX Altitude Encoder Ground 13 RX422 RX + P1 31 RX422 RX - Power + 18 Power RX422 TX + Power Ground RX422 TX - Power Ground 37 1 Rev Date Description A 12/02/10 Initial Release B 01/28/11 C 06/18/11 D 10/31/11 E 06/22/14 Update Wire Type 3/2 AMP UAT AIRCRAFT GROUND Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number Removed redundant ground shield for MX20 to ADS600-B connection. MX20 Attention: Use the UAT Console to configure MX20 as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port (Serial) Display Type pull-down menu select the MX20 item. From the Display Port (Serial) Serial Baud Rate pull-down menu select as baud rate. GMX200 Attention: Use the UAT Console to configure GMX200 as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port (Serial) Display Type pull-down menu select the GMX200 item. From the Display Port (Serial) Serial Baud Rate pull-down menu select as baud rate. 5 AVIONICS BUS (14/28 VDC) 3 Maintenance Port Top GPS Antenna DB9 Female Connector UAT Indicator Maintenance Port RX 2 22 Maintenance Port TX 5 26 Maintenance Port Ground P3 6 GPS RG400 NOTES: P2 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 REQUIRED FOR GMX 200 ONLY. JUMPER MUST BE INSTALLED BETWEEN PIN 29 AND PIN 9 OF P2001 TO CONFIGURE PORT 4 FOR RS422 OPERATION. WHEN PORT 4 IS USED AS AN RS422 PORT, RS232 PORT 4 CAN NOT BE USED. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 10 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 11 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. UAT P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND RG400 TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 7 Bottom UAT Antenna Copyright NavWorx Page 72 of 128 All rights reserved. Printed in the U.S.A.

73 A.7 Interconnect Diagram: ADS600-B to MX20/GMX 200 (ARINC 429 Traffic) Copyright NavWorx Page 73 of 128 All rights reserved. Printed in the U.S.A.

74 A.8 Interconnect Diagram: ADS600-B to Control Panel NavWorx, Inc Big A Road, Rowlett, TX ADS600-B to Transponder Control Panel Rev Date Description - 09/13/14 Initial Release A 09/13/14 Added TransMonSPE Transponder Control Panel GTX 33/330 J3301 Garmin GTX 32/327 J3271 SL70(R) - Sandia Aerospace STX 165(R) J3 Trig Avionics TT21/22/31 - NavWorx TransMonSPE USB P1 ADS600-B 4. ADS600-B CONFIGURATION. USE THE UAT CONSOLE TO CONFIGURE THE CONTROL INPUT FOR THE ADS600-B. ON THE UAT CONSOLE SELECT THE INITIALIZATION TAB, THEN SELECT THE INPUTS TAB, THEN FROM THE CONTROL PANEL TYPE PULL-DOWN MENU SELECT THE CONTROL PANEL TYPE: 4.a GTX330 [DB37-33] Suppression In +5VDC RS232 Out Serial Ground Red Green Black 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground 4.b GTX327 [DB37-33] 4.c SL70R, STX165 [DB37-33] FOR SL70 REMOTE CONFIGURATION. FOR SL70 PANEL MOUNT CONFIGURATION SELECT EITHER SL70 (Panel Mount 1200bps) [DB37-33] OR SL70 (Panel Mount 9600bps) [DB37-33] DEPENDING ON THE BAUD RATE SELECTED ON THE SL70. [WIRING] [ALTITUDE ENCODER] 1.a 1.a 1.a 1.a 1.a 1.b 2.a 2.b 2.c 4.d SL70R, STX165 [DB37-33] [XPNDR CONFIGURATION] 3.a 3.b 4.e TRIG TT22, TT30 [DB37-33] [ADS600-B CONFIGURATION] 4.a 4.b 4.c 4.d 4.e 4.f 4.f ADS600-B TRANS-MON [DB37-33] 2. ALTITUDE ENCODER. 2.a CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6, TO THE GTX 330 POWER GROUND (EITHER J3301-PIN 27 OR J3301-PIN 43). NOTES: 1. CONTROL PANEL TO ADS600-B WIRING. 1.a WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 1.b THE TRANSMONSPE IS SHIPPED WITH 3-CONDUCTOR DOUBLE SHIELDED 24AWG CABLE WHICH IS TERMINATED WITH A USB CONNECTOR ON ONE END. THE SHIELD OF THE OTHER END OF THE CABLE MUST BE TERMINATED TO GROUND. FOR EXAMPLE, A RING TERMINAL MAY BE AFFIXED TO THE CABLE SHIELD WHEREBY THE RING TERMINAL IS ATTACHED TO GROUND VIA THE DB-37 BACK SHELL CABLE CLAMP. 2.b CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6, TO THE GTX 327 POWER GROUND (EITHER J3271-PIN 13 OR J3271-PIN 25). 2.c THE TTXX ALSO CONNECTS TO THE TRIG TC20 ALTITUDE ENCODER. SEE APPENDIX A.11 FOR WIRING. 3. XPNDR CONFIGURATION. 3.a THE GTX 330 RS-232 OUTPUT MUST BE CONFIGURED FOR REMOTE (ONLY). THE GTX 330 HAS TWO RS-232 OUTPUT CHANNELS: RS-232 Out 1 (PIN 23) AND, RS- 232 Out 2 (PIN 25). EITHER OF THESE OUTPUTS MAY BE CONNECTED TO P1-33 OF THE ADS600-B. 3.b TTXX CONFIGURATION, TIS OUTPUT GRMN REMOTE + TIS (19200 BAUD), UAT RCVR INSTALLED YES. TTXX XPNDR MUST BE CONFIGURED WITH NEXNAV GPS INPUT. Copyright NavWorx Page 74 of 128 All rights reserved. Printed in the U.S.A.

75 A.9 Interconnect Diagram: ADS600-B to Altitude Encoder NavWorx, Inc Big A Road, Rowlett, TX ADS600-B to Altitude Encoder Rev Date Description - 08/27/14 Initial Release Altitude Encoder ALL ALTITUDE ENCODERS LISTED ON THIS PAGE SUPPORT ICARUS 9600BPS PROTOCOL ACK A30.9 J1 Icarus Serializer 3000U P3 Sandia Aerospace SAE5-35 J5 Shadin 8800-T DB15 TransCal SSD120-30/ 35N-RS232 DB9 P1 ADS600-B Altitude Out 7 or Altitude Encoder RX Serial Ground Altitude Encoder Ground [WIRING] 1.a 1.a 1.a 1.a 1.a [ALTITUDE ENCODER CONFIGURATION] 2.a 2.b 2.c 2.d 2.e [ADS600-B CONFIGURATION] 3.a 3.a 3.a 3.a 3.a NOTES: 1. CONTROL PANEL TO ADS600-B WIRING. 1.a WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2. ALTITUDE ENCODER CONFIGURATION. 2.a NO JUMPER INSTALLED. 2.b ICARUS 9600BPS DEFAULT = NO JUMPERS ON P3-3 OR P3-9 2.c ICARUS 9600BPS DEFAULT = J5-4 IS OPEN 3. ADS600-B CONFIGURATION. 3.a USE THE UAT CONSOLE TO CONFIGURE THE ALTITUDE ENCODER INPUT FOR THE ADS600-B. ON THE UAT CONSOLE SELECT THE INITIALIZATION TAB, THEN SELECT THE INPUTS TAB, THEN FROM THE PRESSURE ALTITUDE ENCODER PULL-DOWN MENU SELECT THE Icarus ITEM. FROM THE ALTITUDE ENCODER SERIAL BAUD RATE PULL- DOWN MENU SELECT 9600 AS BAUD RATE. 2.d ICARUS 9600BPS 2.e ICARUS 9600BPS = DB9-7 GROUNDED, DB9-2,6 DON'T CARE Copyright NavWorx Page 75 of 128 All rights reserved. Printed in the U.S.A.

76 A.10 Interconnect Diagram: ADS600-B to NexNav mini LRU (GPS Source) NavWorx, Inc Big A Road Rowlett, TX NexNav mini LRU GPS SBAS Class Beta-1 Receiver P/N Rev Date Description A- 06/04/13 Initial Release B- 06/22/14 Update Wire Type Attention: Use the UAT Console to configure the NexNav mini LRU as the GPS source for the ADS600-B. On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the Internal Certified (ADS600-BG), NexNav LRU (ADS600-B) item. ADS600-B P1: 37-PIN D-SUB, MALE CONNECTOR NexNav mini LRU P/N RS-232 Receive Port NEXNAV GPS TX P3 GPS 3 RS-232 Transmit Port RS-232 Signal Ground Port NEXNAV GPS RX GND 1 PPS Y 2 21 NEXNAV LRU Time Mark In + 1 PPS Z 15 2 NEXNAV LRU Time Mark In - NOTES: 1 2 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. USING NEXNAV LEGACY PROTOCOL. RS-232 BAUD RATE 19200bps. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P1: 37-PIN D-SUB, MALE CONNECTOR P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 3 DO NOT CONNECT GPS ANTENNA. Copyright NavWorx Page 76 of 128 All rights reserved. Printed in the U.S.A.

77 A.11 Interconnect Diagram: ADS600-B to TT21/TT22/TT31 Mode S Transponder Control Copyright NavWorx Page 77 of 128 All rights reserved. Printed in the U.S.A.

78 A.11.1 UAT Mode (Altitude) Switch used with TC20 Control Panel The following instructions pertain to installations with Trig transponder TC20 software version 1.5 or earlier. The UAT Mode switch should be positioned within the normal field of view of the pilot s control wheel, and grouped with the UAT Annunciator. The switch s open position is marked ON. The switch s closed position is marked ALT. The switch is placarded as UAT Mode, and the placard font size sufficient to be viewed from the pilot s control wheel. The UAT Mode Switch is used in conjunction with the Trig TC20 control panel function Mode A vs. Mode C. When Mode C is selected on the Trig transponder the UAT Mode Switch shall be moved to the placarded ALT (switch UP) position. When Mode A is selected on the Trig transponder the UAT Mode Switch shall be moved to the placarded ON (DOWN) position. The following depicts the UAT MODE Switch and TC20 Control Panel: Copyright NavWorx Page 78 of 128 All rights reserved. Printed in the U.S.A.

79 A.12 Interconnect Diagram: GPS Antenna NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 08/30/14 Initial Release GPS Antenna ADS600-B 3 2 Top GPS Antenna P3 1 GPS RG400 P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) NOTES: 1 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 2 FOR ADS600-B PART NUMBERS AND THE GPS ANTENNA MUST BE COMPLIANT WITH EITHER TSO-C190 OR TSO-C FOR ADS600-B PART NUMBERS AND THE GPS ANTENNA MUST BE COMPLIANT WITH EITHER TSO-C190, TSO-C144 OR TSO-C129. Copyright NavWorx Page 79 of 128 All rights reserved. Printed in the U.S.A.

80 A.13 Basic Interconnect Diagram: ARINC 743A GPS Source Copyright NavWorx Page 80 of 128 All rights reserved. Printed in the U.S.A.

81 A.14 Basic Interconnect Diagram: RS232 GPS Source NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 09/27/14 Initial Release GPS Position Source (RS232) ADS600-B P1: 37-PIN D-SUB, MALE CONNECTOR GPS Position Source GPS RS232 RX 1 16 GPS TX GPS P3 2 GPS RS232 TX GPS RS232 Common GPS RX GND Time Mark Out + Time Mark Out Time Mark In + Time Mark In - NOTES: 1 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P1: 37-PIN D-SUB, MALE CONNECTOR P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 2 DO NOT CONNECT GPS ANTENNA. Copyright NavWorx Page 81 of 128 All rights reserved. Printed in the U.S.A.

82 A.15 Basic Interconnect Diagram: RS232 Display 1 NavWorx, Inc Big A Road Rowlett, TX Basic Interconnect: RS232 Display 1 Rev Date Description - 09/27/14 Initial Release A 08/18/15 Changed TIS-A port to Display 2 serial port. Serial RS232 Display 2 P1 ADS600-B Ground Capstone RS232 RX Capstone RS232 TX 23 Display 1 Ground 5 Display 1 TX 24 Display 1 RX NOTES: 1. WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2 EQUIPMENT THAT SUPPORTS THE CAPSTONE TRAFFIC REPORT AND PASS-THROUGH DISPLAY PROTOCOLS ARE ELIGIBLE FOR OPERATION WITH THE ADS600-B. P1: 37-PIN D-SUB, MALE CONNECTOR TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 82 of 128 All rights reserved. Printed in the U.S.A.

83 A.16 Basic Interconnect Diagram: RS422 Display NavWorx, Inc Big A Road Rowlett, TX Basic Interconnect: RS422 Display Rev Date Description - 09/27/14 Initial Release ADS600-B Serial RS422 Display Capstone RS422 TX + Capstone RS422 TX - P1 13 RX422 RX + 31 RX422 RX - 2 Capstone RS422 RX + Capstone RS422 RX - 30 RX422 TX + 12 RX422 TX - NOTES: 1. WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2 EQUIPMENT THAT SUPPORTS THE CAPSTONE TRAFFIC REPORT AND PASS-THROUGH DISPLAY PROTOCOLS ARE ELIGIBLE FOR OPERATION WITH THE ADS600-B. P1: 37-PIN D-SUB, MALE CONNECTOR TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 83 of 128 All rights reserved. Printed in the U.S.A.

84 A.17 Basic Interconnect Diagram: ARINC 735A Traffic Display Copyright NavWorx Page 84 of 128 All rights reserved. Printed in the U.S.A.

85 A.18 Interconnect Diagram: UAT Indicator Dialight NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 10/05/14 Initial Release UAT Indicator - Dialight 14VDC or 28VDC A + DIALIGHT LAMP HOLDER B - ADS600-B (PIN 14) WARNING: REVERSING POLARITY OF +/- TERMINALS WILL DAMAGE LAMP. DIALIGHT LAMP P/N: 14VDC: VDC: Copyright NavWorx Page 85 of 128 All rights reserved. Printed in the U.S.A.

86 A.19 Basic Interconnect Diagram: Garmin Aviation Format NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 06/01/15 Initial Release Garmin Aviation Format GPS Position Attention: Use the UAT Console to configure the Aviation Format as the GPS source for the ADS600-B. On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the Aviation Format item. ADS600-B P1: 37-PIN D-SUB, MALE CONNECTOR Aviation Format 1 GPS P3 2 Aviation Format TX 34 GPS RX Aviation Format GND 32 GND NOTES: 1 WIRING TO BE MULTICONDUCTOR SHIELDED: P1: 37-PIN D-SUB, MALE CONNECTOR 22TG2T14 2 CONDUCTOR 22 AWG TWISTED SHIELDED TWO 22TG3T14 3 CONDUCTOR 22 AWG CONDUCTOR SHIELD P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. TERMINATED TO GROUND 2 DO NOT CONNECT GPS ANTENNA. Copyright NavWorx Page 86 of 128 All rights reserved. Printed in the U.S.A.

87 A.20 Basic Interconnect Diagram: RS232 Display 2 NavWorx, Inc Big A Road Rowlett, TX Basic Interconnect: RS232 Display 2 Rev Date Description - 08/18/15 Changed TIS-A port to Display 2 serial port. Serial RS232 Display 2 P1 ADS600-B Ground Capstone, TIS-A RS232 RX 6 Display 2 Ground 25 Display 2 TX NOTES: 1. WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2 EQUIPMENT THAT SUPPORTS THE CAPSTONE TRAFFIC REPORT AND PASS-THROUGH DISPLAY PROTOCOLS ARE ELIGIBLE FOR OPERATION WITH THE ADS600-B. EQUIPMENT THAT SUPPORTS THE GPSMAP TIS-A PROTOCOL IS ELIGIBLE FOR OPERATION WITH THE ADS600-B. P1: 37-PIN D-SUB, MALE CONNECTOR TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 87 of 128 All rights reserved. Printed in the U.S.A.

88 A.21 Interconnect Diagrams IFD 4XX/5XX NavWorx, Inc Big A Road Rowlett, TX Rev Date Description A 9/2/15 Initial Release ADS600-B to IFD 4XX/5XX IFD 4XX/5XX 13 P1001 RS232 IN Port 4 55 RS232 OUT Port 4 54 P1 ADS600-B (P/N: , ) 5 Display 1 TX 24 Display 1 RX 23 Ground RS232 GPS OUT Port GPS RX 32 Ground Power + Power + P /2 AMP UAT 5 AVIONICS BUS (14/28 VDC) ARINC 429 Traffic IN 1A Out 1A 1 ARINC 429 Traffic IN 1B Out 1B Power Ground 36 Power Ground 37 AIRCRAFT GROUND 14 Top GPS Antenna ARINC 429 OUT 1A In 1A ARINC 429 OUT 1B In 1B 12 P1 RS232 RTN Port 4 71 UAT Indicator 14 9 NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. USE THE AVIDYNE UAT CONSOLE TO PROGRAM AND CONFIGURE THE ADS600-B. 4 RS232 RX Port Display 2 TX ARINC 429 Traffic IN 2A 45 ARINC 429 Traffic IN 2B 65 EX600/EX500/ EX5000/C MFD GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. Maintenance Port DB9 Female Connector Altitude Encoder 10 3 TX Ground THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 5 8 RS232 GPS CONNECTION TO ADS600-B ONLY REQUIRED WHEN DISPLAYING ADS-B TRAFFIC AND IS NOT REQUIRED IF TRAFFIC IS BEING DISPLAYED FROM ANOTHER SENSOR SUCH AS TAS600 OR SKYWATCH. USE ANY AVAILABLE IFDX40 PORT (CONNECTION TO PORT 2 SHOWN HERE). 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD PLACARDED UAT FAIL. 4 Maintenance Port RX 22 Maintenance Port TX 26 Ground 7 Altitude Encoder RX 6 Ground GPS UAT P3 P2 RG400 RG400 P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 6 7 TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 12 GPS ANTENNA IS NOT REQUIRED IF ADS600-B RECEIVES GPS POSITION FROM AN EXTERNAL SOURCE SUCH AS WHEN PIN P1-34, P1-32 ARE WIRED TO IFD 4XX/5XX. Bottom UAT Antenna 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 10 SEE APPENDIX A.9 FOR RS232 SERIAL ALTITUDE ENCODER WIRING. 11 ARINC 429 CONNECTION ONLY REQUIRED WHEN DISPLAYING ADS-B TRAFFIC AND IT IS NOT REQUIRED IF TRAFFIC IS BEING DISPLAYED FROM ANOTHER SENSOR SUCH AS TAS600 OR SKYWATCH. 13 IN A DUAL IFDX40 INSTALLATION, RS232 FIS-B WEATHER DATA FROM THE ADS600-B MAY BE CONNECTED TO ONE IFD, AND THE WX WILL BE SHARED TO THE OTHER IFD, VIA THE BYTEFLIGHT/ CROSSTALK DATA BUS (TYPICALLY RS232 PORT 3). 14 OPTIONALLY, PRESSURE ALTITUDE MAY BE SOURCED FROM ARINC 429 LABEL 203. Copyright NavWorx Page 88 of 128 All rights reserved. Printed in the U.S.A.

89 A.22 Basic Interconnect Diagram: ARINC 429 Pressure Altitude NavWorx, Inc Big A Road Rowlett, TX Rev Date Description 1 09/02/15 Initial Release ADS600-B to (ARINC 429) Pressure Altitude Label 203 ADS600-B Altitude Encoder P1 ARINC 429 Out A In 1A ARINC 429 Out B In 1B NOTES: 1. WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Attention: Use the UAT Console to configure ARINC 429 as the altitude encoder input for the ADS600-B. On the UAT Console select the Initialization tab, then select the Inputs tab, then from the Pressure Altitude Encoder pulldown menu select the ARINC 429 item. Copyright NavWorx Page 89 of 128 All rights reserved. Printed in the U.S.A.

90 A.23 Interconnect Diagram: Garmin GNS 430W/530W ADS-B Out+ NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 01/23/2016 Initial Release Garmin GNS 430W/530W ADS-B Out+ Attention: On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the Compliant ADS-B Out+ GNS 400W/500W GTN650/750 IFD 440/540 item. ADS600-B GNS 430W/530W 3 P4001(GNS 430W) P5001(GNS 530W) GPS RS-232 OUT P1: 37-PIN D-SUB, MALE CONNECTOR GPS 34 GPS RX P3 2 Time Mark Out Time Mark In TTL 4 NOTES: 1 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. P1: 37-PIN D-SUB, MALE CONNECTOR P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 2 DO NOT CONNECT GPS ANTENNA. 3 ANY OF THE FOUR GPS RS-232 OUT PORTS ON PINS 41, 54, 56 AND 58 MAY BE CONFIGURED FOR ADS-B OUT+ AND MAY SERVE AS THE GPS INPUT TO THE ADS600-B. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 4 GNS 430W/530W MUST BE OPERATING WITH SOFTWARE VERSION 5.0 OR LATER. Copyright NavWorx Page 90 of 128 All rights reserved. Printed in the U.S.A.

91 A.24 Interconnect Diagram: Garmin GTN 650/750 ADS-B Out+ NavWorx, Inc Big A Road Rowlett, TX Rev Date Description - 01/23/2016 Initial Release Garmin GTN 650/750 ADS-B Out+ Attention: On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the Compliant ADS-B Out+ GNS 400W/500W GTN650/750 IFD 440/540 item. ADS600-B GTN 650/750 P1: 37-PIN D-SUB, MALE CONNECTOR 3 P1001 RS-232 OUT GPS RX GPS P3 2 TIME MARK OUT A 3 21 Time Mark In + TIME MARK OUT B 22 2 Time Mark In - NOTES: P1: 37-PIN D-SUB, MALE CONNECTOR 1 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 2 DO NOT CONNECT GPS ANTENNA. 3 ANY OF THE FOUR RS-232 OUT PORTS ON PINS 5, 6, 7 AND 8 MAY BE CONFIGURED FOR ADS-B OUT+ AND MAY SERVE AS THE GPS INPUT TO THE ADS600-B. TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 91 of 128 All rights reserved. Printed in the U.S.A.

92 A.25 Interconnect Diagram: Avidyne IFD 440/540 ADS-B Out+ NavWorx, Inc Big A Road Rowlett, TX Avidyne IFD 440/540 GPS Attention: On the UAT Console select the Initialization tab, then select the Inputs tab, then from the GPS Source pull-down menu select the Compliant ADS-B Out+ GNS 400W/500W GTN650/750 IFD 440/540. Rev Date Description - 01/23/2016 Initial Release Avidyne IFD 440/540 ADS600-B / Avidyne MLX200 P1: 37-PIN D-SUB, MALE CONNECTOR P3 3 P1001 GPS RS-232 OUT GPS RX GPS 2 Time Mark Out Time Mark In TTL 4 NOTES: 1 2 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. DO NOT CONNECT GPS ANTENNA. P1: 37-PIN D-SUB, MALE CONNECTOR P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 3 ANY OF THE SIX GPS RS-232 OUT PORTS MAY BE CONFIGURED FOR ADS-B OUT+ AND MAY SERVE AS THE GPS INPUT TO THE ADS600-B. PINS 56, 58, 41 AND 54 OF P1001 CORRESPOND TO PORTS 1, 2, 3 AND 4, RESPECTIVELY. PINS 60 AND 62 OF P1050 CORRESPOND TO PORTS 5 AND 6, RESPECTIVELY. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 4 IFD 440/540 MUST BE OPERATING WITH SOFTWARE VERSION 10.2 OR LATER. Copyright NavWorx Page 92 of 128 All rights reserved. Printed in the U.S.A.

93 Appendix B Uncertified Displays The following matrix illustrates which Displays connect to the various part numbers of the ADS600-B. The cells of the matrix identify the Appendix B reference and page of the relevant Interconnect Wiring diagram. ADS600-B Part Number Display (Portable) WiFi Bluetooth GPSMAP TIS-A B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.4, Page 97, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 B.1, Page 94, B.3 Page 96 B.2 Page 95, B.9, Page 102 ADS600-B Part Number Display (Uncertified) AFS GRT MGL Chelton B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.5, Page 98, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.6 Page 99, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.7 Page 100, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 B.1, Page 94, B.8, Page 101, B.9, Page 102 Copyright NavWorx Page 93 of 128 All rights reserved. Printed in the U.S.A.

94 B.1 Interconnect Diagram: RS-232 Display Port 1 NavWorx, Inc Big A Road Rowlett, TX RS-232 Display Port 1 Interconnect Diagram Control Panel 10 Suppression In +5VDC RS232 Out Serial Ground ADS600-B P1 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground Rev Date Description - 04/14/09 Initial Release A 08/29/10 Added power and ground wiring recommendations B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/24/12 Removed Composite TIS E 06/22/14 Updated Wire Type F 08/18/15 Changed TIS-A port to Display 2 serial port. RS-232 Display 1 TX RX Ground Bluetooth See Appendix B.3 Altitude Encoder 9 TX Ground WiFi AFS GRT MGL Chelton See Appendix B.4 See Appendix B.5 See Appendix B.6 See Appendix B.7 See Appendix B Altitude Encoder RX Altitude Encoder Ground 24 Display 1 RX 5 Display 1 TX 23 Display 1 Ground +5VDC 3 +5VDC 11 P1 Power + 18 Power + 19 Power Ground 36 Power Ground 37 1 Attention: Use the UAT Console to select the display type that is connected to the ADS600-B. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 1 (Serial) Display Type pull-down menu select the display type. From the Display Port 2 (Serial) Baud Rate pull-down menu select baud rate of the display s serial port. 3/2 AMP UAT AIRCRAFT GROUND 5 AVIONICS BUS (14/28 VDC) Top GPS Antenna Maintenance Port UAT Indicator DB9 Female Connector P3 GPS 6 RG400 NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG Maintenance Port RX Maintenance Port TX Maintenance Port Ground UAT P2 RG WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 9 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 10 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING VDC USED TO POWER WiFI AND BLUETOOTH. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED FOUR CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna Copyright NavWorx Page 94 of 128 All rights reserved. Printed in the U.S.A.

95 B.2 Interconnect Diagram: ADS600-B to GPSMAP TIS-A NavWorx, Inc Big A Road Rowlett, TX ADS600-B to GPSMAP TIS-A Interconnect Diagram GPSMAP Data In Ground Yellow Black Altitude Encoder Control Panel TX Ground Suppression In +5VDC RS232 Out Serial Ground 4 P1 ADS600-B 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground 7 Altitude Encoder RX 6 Altitude Encoder Ground 8 P1 Power Display 2 TX Power Display 2 Ground 8 Power Ground 36 Power Ground 37 1 Rev Date Description - 04/14/09 Initial Release A 08/29/10 Added power and ground wiring recommendations B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/24/12 Removed Composite TIS E 06/22/14 Updated Wire Type F 08/18/15 Attention: Use the UAT Console to configure TIS-A as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display 2 (Serial) pull-down menu select the TIS-A item. 3/2 AMP UAT AIRCRAFT GROUND Changed TIS-A port to Display 2 serial port. 5 AVIONICS BUS (14/28 VDC) Top GPS Antenna Maintenance Port NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ DB9 Female Connector UAT Indicator ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG Maintenance Port RX Maintenance Port TX P3 6 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 5 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 DISPLAY 2, ALTITUDE ENCODER INPUT AND MAINTENANCE PORT SHARE THE SAME GROUND PIN, P GPS UAT P2 P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) RG400 RG THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna 10 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 11 SEE APPENDIX A.8 FOR CONTROL WIRING. Copyright NavWorx Page 95 of 128 All rights reserved. Printed in the U.S.A.

96 B.3 Interconnect Diagram: Bluetooth Display Port NavWorx, Inc Big A Road Rowlett, TX Bluetooth Display Port Interconnect Diagram Rev Date Description - A 04/14/09 Initial Release 08/29/10 B 01/28/11 C 06/18/11 D 09/01/11 Added power and ground wiring recommendations Added UAT Indicator and Suppression Output Changed Maintenance Port Ground Pin number Clarify Bluetooth power relative to ADS600-B S/N E 06/28/14 Updated Wire Type F 08/18/15 Call out Display Port 1 TO ROVING NETWORKS BLUETOOTH ADAPTOR (RN-240M) RECOMMENDED BAUD RATE: DB9 Female Connector TX 3 1 P1 ADS Display 1 RX RX 2 5 Display 1 TX Ground 5 +5VDC 9 23 Display 1 Ground 3 +5VDC 2 3 NOTES: 1 WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 2 ADS600-B SUPPLIES FUSED AND FILTERED +5VDC TO BLUETOOTH ADAPTOR. Attention: Use the UAT Console to configure the Bluetooth as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port (Serial) Display Type pull-down menu select the Traffic Alerts item. From the Display Port (Serial) Serial Baud Rate pull-down menu select " as baud rate. 3 IF THE ADS600-B IS CONFIGURED WITH TRANSMONSPE THEN BLUETOOTH AND TRANSMONSPE SHARE +5VDC. Copyright NavWorx Page 96 of 128 All rights reserved. Printed in the U.S.A.

97 B.4 Interconnect Diagram: WiFi Display Port NavWorx, Inc Big A Road Rowlett, TX ADS600-B Serial Display Port to WiFi Module Interconnect Diagram WingX Attention: Use the UAT Console to configure the WiFi as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port (Serial) Display Type pull-down menu select the Traffic Alerts item. From the Display Port (Serial) Serial Baud Rate pull-down menu select " as baud rate. Rev Date Description - 09/28/13 Initial Release A 06/22/14 Added UAT Console Note B 12./20/14 Removed Green Wire and config note. C 08/18/15 Call out Display Port 1 ekneeboard Attention: Use the UAT Console to configure the WiFi as a display. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port (Serial) Display Type pull-down menu select the ekneeboard item. From the Display Port (Serial) Serial Baud Rate pull-down menu select " as baud rate. ADS600-B Green 1 P1 WiFi USB White Black 5 DISPLAY 1 TX 23 Display Ground Red 3 +5VDC PWR 2 1 THE GREEN WIRE IS NOT USED. 2 IF THE ADS600-B IS CONFIGURED WITH TRANSMONSPE THEN WiFi AND TRANSMONSPE SHARE +5VDC. Copyright NavWorx Page 97 of 128 All rights reserved. Printed in the U.S.A.

98 B.5 Interconnect Diagram: ADS600-B to AFS AFS Serial Port 3 9 NavWorx, Inc Big A Road Rowlett, TX ADS600-B to AFS Interconnect Diagram 10 Ground 21 RX 5 TX 4 Control Panel AFS Serial Port 2 TX Altitude Encoder Ground Suppression In Maintenance Port +5VDC RS232 Out Serial Ground P1 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground Altitude Encoder RX Altitude Encoder Ground ADS600-B P1 3/2 AMP Display 1 Ground 5 Display 1 TX 24 Display 1 RX Power + Power Power Ground 36 Power Ground 37 1 Rev Date Description A 01/28/11 Initial Release B 06/18/11 Changed Maintenance Port Ground Pin number C 06/23/12 Add text describing AFS serial port configuration D 06/22/14 Update Wire Type E 08/18/15 UAT AIRCRAFT GROUND Changed TIS-A port to Display 2 serial port. Attention: Use the UAT Console to configure AFS as a display. DISPLAY PORT 1: On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 1 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 1 (Serial) Baud Rate pull-down menu select the baud rate recommended by AFS. DISPLAY PORT 2:On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 2 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 2 (Serial) Baud Rate pull-down menu select the baud rate recommended by AFS. AVIONICS BUS (14/28 VDC) Top GPS Antenna 3 DB9 Female Connector UAT Indicator Maintenance Port RX 2 22 Maintenance Port TX NOTES: 5 26 Maintenance Port Ground P3 6 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/16-20 GPS RG ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 8 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 9 AFS ADS-B FUNCTIONALITY REQUIRES S SERIES CPU. 10 THE ADS600-B MAY CONNECT TO ANY AVAILABLE AFS SERIAL PORT. THE ADS600-B ALTITUDE ENCODER PORT SHOULD CONNECT TO AFS SERIAL PORT 2. USE THE AFS ADMIN SETTINGS WINDOW TO CONFIGURE THE DISPLAY SERIAL PORT TO THE BAUD RATE RECOMMENDED BY AFS. SET THE ALTITUDE ENCODER SERIAL PORT 2 TO TFC/ICARUS. UAT P2 P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) RG400 7 Bottom UAT Antenna 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 11 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. 12 AFS DISPLAY MAY OPTIONALLY BE WIRED TO P1-6 (GND) AND P1-25 (DISPLAY PORT 2 TX) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 98 of 128 All rights reserved. Printed in the U.S.A.

99 B.6 Interconnect Diagram: ADS600-B to GRT NavWorx, Inc Big A Road Rowlett, TX ADS600-B to GRT Interconnect Diagram GRT Connector B GRT Connector A Altitude Encoder Control Panel 11 Serial Output Altitude Encoder RX Ground 17 Suppression In +5VDC RS232 Out Serial Ground P1 35 Suppression Output 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground Altitude Encoder Ground Display 1 Ground ADS600 Power + Power + P Rev Date Description A 09/11/10 Initial Release B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/24/12 Removed Composite TIS E 06/22/14 Update Wire Type F 08/18/15 3/2 AMP UAT Changed TIS-A port to Display 2 serial port. Attention: Use the UAT Console to configure GRT as a display. DISPLAY PORT 1: On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 1 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 1 (Serial) Baud Rate pull-down menu select as baud rate. DISPLAY PORT 2:On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 2 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 2 (Serial) Baud Rate pull-down menu select as baud rate. 5 AVIONICS BUS (14/28 VDC) 8 Serial Input 7 23 Serial Output Display 1 TX 24 Display 1 RX Power Ground 36 Power Ground 37 1 AIRCRAFT GROUND 9 Maintenance Port Top GPS Antenna 3 DB9 Female Connector 3 4 UAT Indicator 14 Maintenance Port RX Maintenance Port TX 5 26 Maintenance Port Ground P3 6 NOTES: GPS RG400 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/16-20 P2 2. ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 8 GRT SOFTWARE VERSION REQUIRED TO DISPLAY ADS-B TRAFFIC AND WEATHER: * HORIZON HX VERSION 3 * HORIZON HS/WS VERSION 34 * SPORT WS/HS/SX VERSION 7 9 IN A DUAL DISPLAY CONFIGURATION, CONNECT ONLY SERIAL OUT 7 (PIN 22) OF THE MFD (HX2) TO THE ADS600-B (PIN P1-24). UAT P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) RG THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 10 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 11 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 12 GRT DISPLAY MAY OPTIONALLY BE WIRED TO P1-6 (GND) AND P1-25 (DISPLAY PORT 2 TX) Copyright NavWorx Page 99 of 128 All rights reserved. Printed in the U.S.A.

100 B.7 Interconnect Diagram: ADS600-B to MGL NavWorx, Inc Big A Road Rowlett, TX ADS600-B to MGL Interconnect Diagram Suppression In P1 35 Suppression Output ADS600-B Rev Date Description - 09/05/14 Initial Release A 08/18/15 Changed TIS-A port to Display 2 serial port. Altitude Encoder Control Panel TX 10 +5VDC RS232 Out Serial Ground 3 +5VDC PWR 33 Transponder Control RX 32 Serial Ground 7 Altitude Encoder RX Attention: Use the UAT Console to configure MGL as a display. DISPLAY PORT 1: On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 1 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 1 (Serial) Baud Rate pull-down menu select as baud rate. DISPLAY PORT 2:On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 2 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 2 (Serial) Baud Rate pull-down menu select as baud rate. MGL Ground MGL G2 EFIS Port 1 5 Ground 9 MGL ibox RS Altitude Encoder Ground Display 1 Ground Power + Power + P /2 AMP UAT 5 AVIONICS BUS (14/28 VDC) RX TX Display 1 TX 24 Display 1 RX Power Ground 36 Power Ground 37 1 AIRCRAFT GROUND Maintenance Port DB9 Female Connector 3 UAT Indicator 14 8 Top GPS Antenna NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ Maintenance Port RX Maintenance Port TX 2. ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 5 26 Maintenance Port Ground GPS P3 6 RG400 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 8 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 9 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 10 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. UAT P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) P2 RG THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 11 COMPATIBLE WITH MGL G2 ODYSSEY/ VOYAGER A2.000 AND LATER RELEASES. 12 COMPATIBLE WITH MGL G2 & G3 iefis (ibox) A1037 AND LATER RELEASES. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna 13 MGL DISPLAY MAY OPTIONALLY BE WIRED TO P1-6 (GND) AND P1-25 (DISPLAY PORT 2 TX) Copyright NavWorx Page 100 of 128 All rights reserved. Printed in the U.S.A.

101 B.8 Interconnect Diagram: ADS600-B to Chelton NavWorx, Inc Big A Road Rowlett, TX ADS600-B to Chelton ADS-B Chelton Serial Port 3 8 J1 RS232 Datalink RX 3 Ground 24 Altitude Encoder 10 Control Panel 3 TX Ground 11 Maintenance Port DB9 Female Connector Suppression In 4 P1 Altitude Encoder RX Altitude Encoder Ground 5 Display 1 TX 23 Ground RS232 Datalink TX Display 1 RX +5VDC RS232 Out Serial Ground 35 Suppression Output VDC PWR 33 Transponder Control RX 32 Serial Ground 12 ADS600-B Power + Power + P Power Ground 36 Power Ground 37 UAT Indicator Rev Date Description - 04/14/09 Initial Release A 08/29/10 Added power and ground wiring recommendations B 01/28/11 Added UAT Indicator And Suppression Out C 06/18/11 Changed Maintenance Port Ground Pin number D 06/24/12 Removed Composite TIS E 06/22/14 Update Wire Type F 08/18/15 3/2 AMP UAT AIRCRAFT GROUND Changed TIS-A port to Display 2 serial port. Attention: Use the UAT Console to configure Chelton as a display. DISPLAY PORT 1: On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 1 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 1 (Serial) Baud Rate pull-down menu select as baud rate. DISPLAY PORT 2:On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 2 (Serial) Display Type pulldown menu select the Traffic Alerts item. From the Display Port 2 (Serial) Baud Rate pull-down menu select as baud rate. 5 AVIONICS BUS (14/28 VDC) Top GPS Antenna NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG 3 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 CHELTON CONFIGURATON On the Factory Programmed Settings page in the Chelton Limits Setup: Datalink Receiver = ADS-B GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 IN THIS CONFIGURATION, THE CHELTON DISPLAY IS SET TO RECEIVE ADS-B SO THAT BOTH TIS-B AND FIS- B DATA ARE PROVIDED THROUGH CHELTON S ADS-B/WSI INPUT. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 10 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 11 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING. 12 CHELTON DISPLAY MAY OPTIONALLY BE WIRED TO P1-6 (GND) AND P1-25 (DISPLAY PORT 2 TX) Maintenance Port RX Maintenance Port TX Maintenance Port Ground GPS UAT P3 P2 TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND RG400 RG400 P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) 6 7 TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna Copyright NavWorx Page 101 of 128 All rights reserved. Printed in the U.S.A.

102 B.9 Interconnect Diagram: RS-232 Display Port 2 NavWorx, Inc Big A Road Rowlett, TX RS-232 Display Port 2 Interconnect Diagram P1 ADS600-B Rev Date Description - 08/18/15 Changed TIS-A port to Display 2 serial port. Suppression In 35 Suppression Output Control Panel 10 +5VDC RS232 Out 3 +5VDC PWR 33 Transponder Control RX Serial Ground 32 Serial Ground Altitude Encoder 9 TX Ground Altitude Encoder RX Altitude Encoder Ground P1 Attention: Use the UAT Console to select the display type that is connected to the ADS600-B. On the UAT Console select the Initialization tab, then select the Displays tab, then from the Display Port 2 (Serial) Display Type pull-down menu select the display type. From the Display Port 2 (Serial) Baud Rate pull-down menu select baud rate of the display s serial port. RS-232 Display 2 RX Ground +5VDC 11 GPSMAP TIS-A See Appendix B.2 WiFi See Appendix B.4 AFS GRT MGL Chelton See Appendix B.5 See Appendix B.6 See Appendix B.7 See Appendix B Display 2 TX 6 Display 2 Ground 3 +5VDC PWR Power + 18 Power + 19 Power Ground 36 Power Ground /2 AMP UAT AIRCRAFT GROUND 5 AVIONICS BUS (14/28 VDC) Top GPS Antenna UAT Indicator 14 8 Maintenance Port 3 DB9 Female Connector P3 GPS 6 RG400 NOTES: 1 POWER AND GROUND WIRE TO BE NON-SHIELDED M22759/ ALL OTHER WIRING TO BE MULTICONDUCTOR SHIELDED: 22TG2T14 2 CONDUCTOR 22 AWG 22TG3T14 3 CONDUCTOR 22 AWG Maintenance Port RX Maintenance Port TX Maintenance Port Ground UAT P2 RG WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT SETTINGS: BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET. 4 GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR 14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET. 8 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. ACTIVE LOW INDICATOR. 400mA MAXIMUM. THE INDICATOR SHOULD BE LABELED UAT FAIL. 9 SEE APPENDIX A.9 FOR ALTITUDE ENCODER WIRING. 10 SEE APPENDIX A.8 FOR CONTROL PANEL WIRING VDC USED TO POWER WiFi. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P1: 37-PIN D-SUB, MALE CONNECTOR P2: TNC COAXIAL CONNECTOR (UAT ANTENNA) P3: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED FOUR CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna Copyright NavWorx Page 102 of 128 All rights reserved. Printed in the U.S.A.

103 Appendix C ADS600-B Maintenance Port Tutorial Starting the UAT Console The UAT Console is a Windows PC application that is required for configuring the ADS600-B, versions and above. The UAT Console communicates with the ADS600-B via a serial (RS232) communication channel configured to 115,200 baud, 8 data, no parity, and 1 stop bit. The UAT Console is launched by either clicking the desktop icon from the Start Menu., or selecting UAT Console The UAT Console will request that the COM port that is connected to the ADS600-B be selected from a list of available COM ports. Figure C- 1: UAT Console Launch Screen Copyright NavWorx Page 103 of 128 All rights reserved. Printed in the U.S.A.

104 UAT Console Communication with ADS600-B If the UAT Console is not communicating with the ADS600-B, an indicator will illuminate in yellow stating UAT NOT CONNECTED. This is an indication that the ADS600-B may not be powered up or that the serial line from the PC to the ADS600-B is not connected. Figure C- 2: UAT Console UAT NOT CONNECTED Copyright NavWorx Page 104 of 128 All rights reserved. Printed in the U.S.A.

105 UAT Console Indicates UAT NOT CONFIGURED When the UAT Console indicates UAT NOT CONFIGURED, the UAT Console is communicating with the ADS600-B, but that the ADS600-B configuration is invalid. The ADS600-B is shipped from the factory with the UAT transmitter disabled and not configured. The UAT Console detects and reports this not configured state. To remedy this, the installer must configure the ADS600-B using the UAT Console. The ADS600-B is configured when the indicator turns green and indicates UAT CONFIGURED. The following sections describe how to configure the ADS600-B. Figure C- 3: UAT Console UAT NOT CONFIGURED Copyright NavWorx Page 105 of 128 All rights reserved. Printed in the U.S.A.

106 Configuring ADS600-B with UAT Console The sub-tabs under the Initialization Tab are used to configure the ADS600-B. The ADS600-B is not configured until the console indicator is illuminated in green indicating UAT CONFIGURED. At a minimum the installer must enter a setting for those fields that are highlighted in red. See Figure C- 3. Note: the UAT Console will not permit the ADS600-B transmitter to be enabled until the ADS600-B is fully configured and UAT CONFIGURED is indicated. Identification sub-tab The installer enters the Call Sign of the aircraft that has the installed ADS600-B. The UAT Console contains a database of the FAA aircraft registry. The Call Sign is used to retrieve the ICAO address of the aircraft from the registry. In the event, that the Call Sign is not found in the registry, the installer may override the ICAO address database search by selecting the Override ICAO Autofill check box and manually enter the ICAO address. Figure C- 4: UAT Console Identification sub-tab Copyright NavWorx Page 106 of 128 All rights reserved. Printed in the U.S.A.

107 Emitter sub-tab The Emitter sub-tab contains fields that describe the configuration of the aircraft (with the installed ADS600-B). The installer must specify the type of aircraft, the position of the GPS antenna used by the ADS600-B, and the length/width dimension of the aircraft. This information is transmitted by the ADS600-B in the ADS-B OUT message. Figure C- 5: UAT Console Emitter sub-tab Copyright NavWorx Page 107 of 128 All rights reserved. Printed in the U.S.A.

108 Inputs sub-tab The GPS source, pressure altitude source and type of control panel that are wired to the ADS600-B are selected from the Inputs sub-tab. Figure C- 6: UAT Console Inputs sub-tab Figure C- 7: UAT Console, Control Panel Popup Copyright NavWorx Page 108 of 128 All rights reserved. Printed in the U.S.A.

109 Displays sub-tab The ADS600-B may be configured with up to 3 displays. Figure C- 8: UAT Console Serial and ARINC 429 Displays Transmitter sub-tab To receive ADS-B IN (traffic) from the ADS-B ground stations the ADS600-B transmitter must be enabled. The UAT Console desensitizes the Transmitter radio buttons if the ADS600-B is not fully configured. Only when the indicator is illuminated in green and states UAT CONFIGURED will the UAT Console allow the installer to enable the transmitter. Copyright NavWorx Page 109 of 128 All rights reserved. Printed in the U.S.A.

110 Figure C- 9: UAT Console Transmitter sub-tab When the UAT Transmitter is enabled the TX indicator located on the blue bar will illuminate in green. Note: when configured, the transmitter control panel mode controls the UAT transmitter state. When in Mode A or Mode C the UAT transmitter is enabled. When in Standby/Off mode the UAT transmitter is disabled. Only when in Mode C will the UAT transmitter transmit a flight ID (squawk code). Copyright NavWorx Page 110 of 128 All rights reserved. Printed in the U.S.A.

111 UAT Transmitter is enabled Figure C- 10: UAT Console Transmitter (TX) indicator illuminates green when UAT Transmitter is enabled Copyright NavWorx Page 111 of 128 All rights reserved. Printed in the U.S.A.

112 Upgrading ADS600-B To upgrade the software on the ADS600-B select the Upgrade Tab and then click the Upgrade ADS600-B To Version x.x.x button. See Figure C- 11. Text will appear in the message window indicating that the software upgrade may take up to 4 minutes. See Figure C- 12. During this period the UAT Console prevents the installer from changing the configuration of the ADS600-B. The screen of the UAT Console will print several rows of periods. When the upgrade is complete the UAT Console will indicate PLEASE CYCLE POWER. Power must be cycled on the ADS600-B for the new software to operate. See Figure C- 13. To verify that the ADS600-B is operating with the new software load view the blue bar that is underneath the menu bar. The software version is shown near the middle of the blue bar as SW Ver x.x.x. Figure C- 11: UAT Console Upgrade Tab Copyright NavWorx Page 112 of 128 All rights reserved. Printed in the U.S.A.

113 Figure C- 12: UAT Console Software Upgrade Start Message Figure C- 13: UAT Console Software Upgrade Complete Copyright NavWorx Page 113 of 128 All rights reserved. Printed in the U.S.A.

114 View UAT Console Reports Select the Reports Tab to view ADS600-B reports. Status Messages are output every second. These messages report the state of the GPS, the state of the ADS600-B, the ADS600-B Software Version Number and the number of ADS-B and Uplink messages received. See Figure C- 14. Traffic Messages are displayed only when traffic messages are received. See Figure C- 15. Uplink Messages are displayed only when uplink messages are received from an ADS-B ground station. When the ADS600-B successfully receives from the GPS constellation, the geometric altitude is displayed in either the Primary or Secondary Altitude panels. Likewise, when the ADS600-B is wired to an operating pressure altitude source, pressure altitude is displayed in the Primary Altitude Panel. Note: when altitude is unavailable the Feet will be displayed for altitude. Figure C- 14: UAT Console Reports Tab Copyright NavWorx Page 114 of 128 All rights reserved. Printed in the U.S.A.

115 Figure C- 15: UAT Console Traffic Messages Copyright NavWorx Page 115 of 128 All rights reserved. Printed in the U.S.A.