ADS600-B Installation and User Manual

Transcription

1 ADS600-B Installation and User Manual Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

2 Business Address: NavWorx Incorporated 706 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 of 88 All rights reserved. Printed in the U.S.A.

3 Revision Date Comments 01 0/0/010 Initial release 0 05/11/010 Revised FCC statement Revision History 0 08/9/010 Updated Wiring Diagrams. Added content to..1 GPS Antenna,.5. Cabling and Wiring,.5.5 Air Circulation and Cooling Sections, and.8. Mounting and Wiring Sections. 0 09/1/010 Added ADS600-B to GRT Wiring Diagrams. Replaced text of Maintenance PC section with reference to Maintenance Port Tutorial document, /18/010 Added Quick Start Guide and ADS600-B Maintenance Port Tutorial Sections /10/010 Changed download link for TeraTermPro 07 10/17/010 Added GNS 0(W) (ARINC 9) Wiring Diagram. Added wiring diagrams to table of contents. 08 1/0/010 Added GMX 00/MX0 RS and ARINC 9 Interconnect Diagrams. 09 1/0/010 Added GTX 0, GTX 7 and SL70 Transponder Interconnect Diagrams /8/011 Added Suppression Input and UAT Indicator to Interconnect Diagrams. Uniquely identify ports of GNS80 7A Interconnect Diagram. Added ADS600-B to AFS (ADS-B) Interconnect Diagram. 11 0/06/011 Corrected Disclaimer. 1 0/5/011 Added ground signal to GTX 0 and GTX 7 Interconnect Diagrams. 1 06/18/011 Changed pin outs for ADS600- B serial numbers 851 and above. 1 07/0/011 Corrected UAT control panel interface. Corrected pins and of table -6. Changed UAT control from pin 7 to pin for SL70, GTX0, and GTX7 diagrams /08/011 Added control head input to Figure -, ADS600-B System Block diagram. Updated Section. to include description of control head input. Added WiFi Interconnect Diagram /01/011 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 /1/011 Added RG00 cables to Package Contents Table /0/011 Added callout for GPS NMEA output pin 15 of DB /1/011 Corrected GMX00/MX0 to ADS600-B diagrams (removed redundant grounding shield). Corrected SL70 interconnect diagram (removed incorrect notes). 0 0/0/01 Replaced TeraTermPro with UAT Console as installer interface to the ADS600-B. 1 0/11/01 Corrected Wiring Diagrams for GTX0 (Note #). 0/15/01 Removed table containing DB-7 pin-outs for ADS600-B units with serial numbers below /6/01 Removed Composite TIS. Remove Chelton Composite TIS diagram with Serial ARINC 75B diagram. Updated AFS serial port description. 08/1/01 Issue #166. Updated UAT Console Figures. Added Status Tab to UAT Console. 5 05/09/01 Issue #0. First revision of installation manual withtso-c15c authorization for ADS600-B. 6 06/1/01 Issue #8. Added system block diagrams showing various configurations of ADS600-B. Added descriptions for altitude encoder, ARINC 9 and transponder control panel input formats. 7 06/19/01 Issue #. Reformatted Part Number. 8 07/10/01 Issue #5. Added references to evaluated GPS sources. 9 07/10/01 Issue #11. Revised installation manual with TSO-C15c authorization for ADS600-B part number and /5/01 Issue #77. Add TTX as control panel to ADS600-B. 1 08/9/01 Issue #80. Added Removal/Replacement Section. Updated Troubleshooting Section. Removed AFS TIS-A dwg. 10//01 Issue #507. Add limitations paragraph from TSO-C15c 1//01 Issue #57. Added TransMonSPE as control input to ADS600-B. Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

4 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 () repair or replacement of the product which is returned to NavWorx with original proof of purchase. Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

5 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 5 of 88 All rights reserved. Printed in the U.S.A.

6 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. 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) 706 Big A Road Rowlett, TX Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

7 ADS600-B Installation Quick Start Guide The equipment installer must verify the items of this quick start guide prior to operating the ADS600-B unit in the National Airspace System (NAS). The following MUST be completed before powering up the ADS600-B: Connect (RG-00) the UAT antenna to the port labeled UAT ANT Connect (RG-00) the GPS antenna to the port labeled GPS ANT Connect fused power to the ADS600-B unit via port 1 (DB7 connector) Ensure that the ADS600-B s maintenance port (DB9 connector) is accessible Verify that a pressure altitude encoder source is wired to the ADS600-B (via the DB7 connector) Verify that the control panel (Transponder Control or EFIS) is wired to the ADS600-B (via the DB7 connector) Install the UAT Console onto your PC Before your first flight you MUST configure the ADS600-B. Position aircraft and the ADS600-B unit to have a view of the sky and the GPS satellites Power up avionics (ADS600-B) Connect the (UAT Console) COM port of your PC to the maintenance port (DB9 connector) of the ADS600-B unit Launch the UAT Console on your PC Configure the ADS600-B using the UAT Console Refer to Appendix B for more detailed configuration instructions. Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

8 Table of Contents 1 About this Manual Reference Documents Acronyms Regulatory Compliance TSO TSO Authorization FCC Grant of Equipment Authorization Limitations Installation Certified GPS Receiver (P/N and ) Uncertified GPS Receiver (P/N and ) Surveillance Services Flight Manual Supplement Other Considerations Accessories and Packing List Unpacking Equipment Package Contents Equipment Description Overall Specifications System Interfaces GPS Position Source Display Maintenance Port Annunciator Output Altitude Encoder Input Control Head Antenna Requirements Certified GPS Antenna (P/N and ) Uncertified GPS Antenna (P/N and ) UAT Antenna Installation Materials Not Supplied Tools Required Equipment Mounting Cabling and Wiring... 1 Copyright NavWorx Page 8 of 88 All rights reserved. Printed in the U.S.A.

9 ..5 Air Circulation and Cooling Electrical Connections Connectors Interface Connector Definition I/O Connector (P1)....6 Functional Descriptions Power Discrete Outputs Discrete Inputs PPS Time Mark Input Serial Interfaces ARINC Post Installation Check Configuration of ADS600-B with Maintenance PC Electrical Load Analysis VHF COM Interference GPS Testing Mounting and Wiring Check Weight and Balance....8 ADS600-B Unit Removal and Replacement... 5 Troubleshooting... 6 Maintenance Altitude Source Calibration Tune-Up Cleaning... 5 Appendix A... 6 A.1 Interconnect Diagram: ADS600 to GPSMAP TIS-A... 6 A. Interconnect Diagram: Bluetooth Display Port... 7 A. Interconnect Diagram: WiFi Display Port... 8 A. Interconnect Diagram: Display Port... 9 A.5 Interconnect Diagram: ADS600 Maintenance Port to Computer A.6 Interconnect Diagram: ADS600 to AFS A.7 Interconnect Diagram: ADS600-B to GRT... 5 A.8 Interconnect Diagram: ADS600-B to GRT HX/HS/WS (TIS Traffic)... 5 A.9 Interconnect Diagram: GNS 80 ARINC 7A Position Source... 5 A.10 Interconnect Diagram: ADS600-B to GNS 80 Traffic (ARINC 9) A.11 Interconnect Diagram: ADS600-B to GNS 80 Traffic (RS- TIS) Copyright NavWorx Page 9 of 88 All rights reserved. Printed in the U.S.A.

10 A.1 Interconnect Diagram: ADS600-B to GNS 0 Traffic (ARINC 9) A.1 Interconnect Diagram: ADS600 to Chelton A.1 Interconnect Diagram: ADS600-B to MX0/GMX 00 (RS Traffic/Weather) A.15 Interconnect Diagram: ADS600-B to MX0/GMX 00 (ARINC 9 Traffic) A.16 Interconnect Diagram: ADS600-B to SL70 Transponder Control A.17 Interconnect Diagram: ADS600-B to GTX 0 Transponder Control... 6 A.18 Interconnect Diagram: ADS600-B to GTX 7 Transponder Control... 6 A.19 Interconnect Diagram: ADS600-B to NexNav mini LRU (GPS Source)... 6 A.0 Interconnect Diagram: ADS600-B to TT1/TT Mode S Transponder Control A.1 Interconnect Diagram: ADS600-B to TransMonSPE Control A. Interconnect Diagram: ADS600-B to GNS 80 Remote Transponder Control Appendix B 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 Appendix C... 8 Appendix D Appendix E Copyright NavWorx Page 10 of 88 All rights reserved. Printed in the U.S.A.

11 List of Tables Table -1: Package Contents Table -: ADS600-B Installation Kit Contents (P/N ) Table -1: Acceptable ADS600-B UAT Antennas... 8 Table -: Acceptable ADS600-B GPS Antennas... 9 Table -: Crimp Tools for High Density - AWG Socket Contact... 9 Table -: Connectors... Table -5: I/O Connector Pin-Out (P1) for ADS600-B... 5 Table -6: ARINC 9 (75B) Out Labels... 0 Table -7: ARINC 9 (7A) In Labels... 0 Table -8: Electrical Load Analysis for P/N , Table -9: Electrical Load Analysis for P/N , Table -10: Recommended Circuit Protection Device... 1 Table -11: ADS600-B Weight... Table 5-1: Trouble Shooting Guide... Copyright NavWorx Page 11 of 88 All rights reserved. Printed in the U.S.A.

12 List of Figures Figure -1: Top view of ADS600-B UAT Data Link Transceiver Figure -: ADS600-B UAT uses Internal GPS WAAS Receiver as GPS Position Source.... Figure -: ADS600-B UAT uses External Certified (ADS-B Compliant) GPS Position Source... Figure -: ADS600-B UAT with Pressure Altitude Supplied by Control Head (Transponder) Input... Figure -5: ADS600-B UAT and MFD which includes Control Head Input... 5 Figure -6: ADS600-B Mounting Bracket Pattern... 0 Figure -7: ADS600-B DB7, UAT and GPS Connectors... Figure -8: 7 Pin D-Sub Male Connector (P1)... Figure -9: ADS600-B Center of Gravity... Figure B- 1: UAT Console Launch Screen Figure B- : UAT Console UAT NOT CONNECTED Figure B- : UAT Console UAT NOT CONFIGURED Figure B- : UAT Console Identification sub-tab Figure B- 5: UAT Console Emitter sub-tab... 7 Figure B- 6: UAT Console Inputs sub-tab... 7 Figure B- 7: UAT Console, Control Panel Popup... 7 Figure B- 8: UAT Console Displays sub-tab... 7 Figure B- 9: UAT Console TIS-A and ARINC 9 Displays... 7 Figure B- 10: UAT Console Transmitter sub-tab Figure B- 11: UAT Console Transmitter (TX) indicator illuminates green when UAT Transmitter is enabled Figure B- 1: UAT Console Upgrade Tab Figure B- 1: UAT Console Software Upgrade Start Message Figure B- 1: UAT Console Software Upgrade Complete Figure B- 15: UAT Console Reports Tab Figure B- 16: UAT Console Traffic Messages Figure B- 17: UAT Console ADS600-B Ready for Flight Figure B- 18: UAT Console ADS600-B Not Ready for Flight... 8 Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

13 1 About this Manual This manual describes the installation and checkout procedures for the ADS600-B Universal Access Transceiver (UAT) Data Link Transceiver, part numbers: [HWMOD]-[SWMOD] (978 MHz UAT with Internal uncertified SiRF IV GPS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT with Internal uncertified SiRF IV GPS Receiver and ARINC 9) [HWMOD]-[SWMOD] (978 MHz UAT with TSO-C15c GPS SBAS Class Beta 1 Receiver) [HWMOD]-[SWMOD] (978 MHz UAT with TSO-C15c GPS SBAS Class Beta 1 Receiver and ARINC 9) This document describes the ADS600-B operating with software version.0.1 and later. 1.1 Reference Documents RTCA/DO-8B RTCA/DO-9D RTCA/DO-160F TSO-C15c TSO-C15c AC.1-1B AC 0-165A AC 0-18B RTCA/DO-10 TSO-C190 TSO-C1a 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 The ADS600-B Interface Control Document ( ) defines the message formats of the public messages sent and received by the ADS600-B. The NexNav mini Interface Document for the Receiver Circuit Card Assembly (CCA) GPS/SBAS WAAS Class Beta 1 Receiver, ID-CCA-GPSBL, describes the (TSO-C15c compliant) GPS SBAS Class Beta 1 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 of AC Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

14 1. 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 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 TSO Technical Standard Order UAT Universal Access Transceiver WAAS Wide Area Augmentation System Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

15 1. Regulatory Compliance 1..1 TSO TSO-C15c TSO-C15c 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 Number HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD HWMOD-SWMOD 1.. TSO Authorization Function TSO Minimum Performance Standard UAT Transceiver GPS SBAS Class Beta 1 Receiver TSO-C15c Class A1S TSO-C15c Class Beta 1 Software RTCA/DO-178B Hardware RTCA/DO-5 Environmental RTCA/DO-8B Level C Level C RTCA/DO-160F See Appendix D RTCA/DO-9D Level C Level C RTCA/DO-160F See Appendix E 1.. 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. Limitations.1 Installation 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 1 CFR part or the applicable airworthiness requirements. The article may be installed only according to AC applicable airworthiness requirements. Copyright NavWorx Page 15 of 88 All rights reserved. Printed in the U.S.A.

16 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 7 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-8B.. Certified GPS Receiver (P/N and ) For ADS600-B part numbers and , the internal GPS is FAA TSO-C15c Class Beta 1 approved and it can be operated in Oceanic, En-route, Terminal, LNAV airspace, and Beta 1 applications. The ADS600-B may operate with either a TSO-C190 or TSO-C1 approved antenna for TSO- C15c Class Beta 1 operations. The recommended antenna is a DO-01 compliant antenna meeting the requirements of TSO-C190. Table - provides the recommended antennas for use with ADS600-B part numbers and The performance of the ADS600-B GPS SBAS Class Beta 1 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-9D.. Uncertified GPS Receiver (P/N and ) The ADS600-B has an internal uncertified GPS WAAS receiver which does not meet the 1 CFR 91 FAA rule for certified GPS position source. If the ADS600-B is configured to use the internal uncertified GPS as the position source the ADS-B messages transmitted by the unit reports: A Source Integrity Limit (SIL) of 0 indicating that the GPS position source does not meet the 1 CFR 91 FAA rule. Note: The Notice of Proposed Rule Making (NPRM) for ADS-B Out Performance Requirements to Support ATC Service (1 CFR 91 FAA ) states that the compliance date for this NPRM rule is January 1, 00.. Surveillance Services 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 Copyright NavWorx Page 16 of 88 All rights reserved. Printed in the U.S.A.

17 onboard transponder and ADS600-B UAT. The ADS600-B supports the following control panel interfaces: If the aircraft is not transponder equipped, an Electronic Flight Instrument System (EFIS) display may be configured to provide the squawk code entry. The MX0, GMX 00, GNS80 (standalone and with attached transponder) and other displays may be configured to enter squawk codes to the ADS600-B. Compatible Transponders may be configured to act as a control panel for the ADS600-B. transponders are GTX 0, GTX 7, SL70/70R and TT1/TT. These If the aircraft is equipped with an older-style Mode C transponder, the TransMonSPE may be installed as the control input for the ADS600-B. 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 a Mode C transponder to pick up altitude and reply codes, decode the information and transmit it digitally for use by an ADS600-B..5 Flight Manual Supplement The Aircraft Flight Manual Supplement for installations of the ADS600-B must include the following operational limitations: When the transponder is set to Standby or OFF the ADS600-B stops transmitting ADS-B messages. The ADS-B ground stations only transmit Traffic Information Services Broadcast (TIS-B) and (ADS- Rebroadcast) ADS-R messages to participating aircraft. Participating aircraft are identified as aircraft transmitting ADS-B messages. When the transponder is set to Standby or OFF the UAT no longer receives TIS-B and ADS-R messages from the ADS-B ground stations because the aircraft is not participating in the ADS-B surveillance system. When the transponder is set to Mode-C the ADS600-B transmits the barometric altitude as the primary altitude and the geometric altitude as the secondary altitude in the ADS-B messages. When the transponder is set to Mode-A the ADS600-B transmits geometric altitude as primary altitude and barometric altitude as secondary altitude in the ADS-B messages. For all installations that include a traffic display the following must be included in the Flight Manual Supplement: Caution: Traffic shown on the display may or may not have traffic alerting available..6 Other Considerations The ADS600-B is used as an aid to visual acquisition of traffic and weather and it is to be used only for pilot and crew situational awareness. The ADS600-B does not relieve the flight crew of seeing and avoiding traffic, obstacles and weather. Installation of the ADS600-B does not relieve the pilot of consulting approved data sources prior to and during each flight. The ADS600-B is not a collision-avoidance-device. Any deviation from ATC clearance, given cockpit information derived from the ADS600-B, must be approved by ATC. The ADS600-B is a Universal Access Transceiver (UAT) that interfaces with MFDs, CDTIs and/or EFISs to display ADS-B, ADS-R, TIS-B and FIS-B products. It is the responsibility of the display manufacturer to render or not render these products. The ADS600-B receives ADS-R, TIS-B and FIS-B products from ADS-B radio stations. The content, or lack of content, in the product offerings is the responsibility of the FAA. Copyright NavWorx Page 17 of 88 All rights reserved. Printed in the U.S.A.

18 Accessories and Packing List.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.. Package Contents The items included in the ADS600-B package are listed in Tables -1and -. Table -1: Package Contents Part # Qty Description ADS600 Installation Kit (see Table - for details) One of the following: [HWMOD]-[SWMOD] (978 MHz UAT with Internal uncertified SiRF IV GPS Receiver) [HWMOD]-[SWMOD] (978 MHz UAT with Internal uncertified SiRF IV GPS Receiver and ARINC 9) [HWMOD]-[SWMOD] (978 MHz UAT with TSO-C15c GPS SBAS Class Beta 1 Receiver) [HWMOD]-[SWMOD] (978 MHz UAT with TSO-C15c GPS SBAS Class Beta 1 Receiver and ARINC 9) 1 ADS600-B UAT Data Link Transceiver XX RG00 cable with male TNC connector, 9 feet Table -: ADS600-B Installation Kit Contents (P/N ) Part # Quantity Description Receptacle Female, DSUB 7-pin Receptacle Female, DSUB 9-pin 01- DC DSUB 7-pin back-shell Connector DSUB Latch Slide 7 position 01-M909/ Crimp contact, DSUB, 0 to AWG wire Copyright NavWorx Page 18 of 88 All rights reserved. Printed in the U.S.A.

19 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 is output to a display device. Figure -1: Top view of ADS600-B UAT Data Link Transceiver Copyright NavWorx Page 19 of 88 All rights reserved. Printed in the U.S.A.

20 .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 , ):.08 inches.5 inches 7.8 inches (includes mounting bracket) 6. inches 1. 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 D and Appendix E. Operating temperature: Storage temperature: -0 C to +55 C -55 C to +85 C Temperature variation: 5 C per minute Humidity: 95% at 50 C Maximum continuous altitude: External Cooling: 5,000 feet Not required Electrical (P/N , ) Voltage: Input Current (8W nominal): 9-VDC Steady State: 1VDC, 8VDC Transmit Peak: 1VDC, Electrical (P/N , ) Voltage: Input Current (11W nominal): 9-VDC Steady State: 1VDC, 8VDC Transmit Peak: 1VDC, UAT Performance TSO Compliance: Regulatory: Frequency: Tolerance: Data Rate: Receiver Sensitivity: Transmit Power: Equipment Class: TSO-C15c RTCA/DO-8B 978MHz +/- 0ppm Mbps Exceeds 90%MSR@-9dBm 0W nominal A1S (single bottom UAT antenna) Copyright NavWorx Page 0 of 88 All rights reserved. Printed in the U.S.A.

21 GPS SBAS Class Beta 1 Receiver (P/N , ) TSO Compliance: TSO-C15c Class Beta 1 Regulatory: General: Number of Channels: Position Update Interval: Sensitivity Tracking: Sensitivity Reacquisition: Position Accuracy RMS Horizontal with WAAS Position Accuracy RMS Vertical with WAAS 1PPS (Pulse Per Second) Altitude Dynamics Speed, Acceleration and Jerk Dynamics Velocity Dynamics Accuracy TTFF (Time to First Fix) Cold Start TTFF (Time to First Fix) Warm Start Integrity Monitoring RAIM Integrity Monitoring FD/FDE Integrity Monitoring Alert Integrity Monitoring BIT SATCOM Compatibility RTCA/DO-9D MHz L1, C/A code receiver with SBAS capability 1 GPS and SBAS/WAAS parallel channels 5 Hz -15 dbm 6 seconds typical at -10 dbm GPS 9 seconds typical at -10 dbm SBAS 5 meters, RMS 7 meters, RMS 0 ns, RMS Uncertified Internal GPS/WAAS Receiver Performance (P/N , ) (see Section.1 for GPS limitations) Number of channels: 0 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: Maximum 18,87 meters Per DO-9D requirements for oceanic, en-route, terminal, LNAV, and non precision approach modes of operation Maximum 51 m/s 0.1 m/s RMS 90 seconds at -10 dbm (typical) 66 seconds at -10 dbm (typical) SBAS Integrity incorporated FD/FDE incorporated Navigation alert as per DO-9D Comprehensive power on and online self tests Compatible on aircraft equipped with SATCOM, when installed with TSO-C1( ) or TSO-C190( ) approved antenna 1575.MHz L1-159dBm (Tracking mode) -1dBm (Acquisition mode) 1 second < 5 seconds < 5 seconds 0.1seconds 5Hz 1,000 knots 60,000 ft MSL WGS-8 Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

22 Avionics Interfaces Annunciator Outputs: Altitude Encoder: Control Port: Maintenance Port: External Position Input: Note: An external position input is not required for ADS600-B P/Ns and Display/Control: Capable of sinking 500mA for turning on annunciator lamp RS asynchronous serial ARINC9 ADC/AHRS source (pressure altitude label 0) RS asynchronous serial RS asynchronous serial RS asynchronous serial (NexNav mini LRU Legacy Protocol). ARINC7A GNSS sensor RS asynchronous serial (Pass-through or Traffic Alert interfaces) RS asynchronous serial (Pass-through or Traffic Alert interfaces) ARINC75 Traffic interface TIS-A Traffic interface Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

23 . System Interfaces The ADS600-B must be configured with a GPS position source, a pressure altitude source, and a control head for pilot input. Optionally, the ADS600-B may be configured with a display to display ADS-B, ADS-R, TIS-B traffic and FIS-B weather. Figures - through -5 depict typical ADS600-B system configurations. Display (MFD, handheld, etc.) GPS Antenna DB 7 Connector Annunciator Lamp Pressure Altitude Encoder Maintenance Port Control Head Input Aircraft Power UAT Antenna Figure -: ADS600-B UAT uses Internal GPS WAAS Receiver as GPS Position Source. The Internal GPS Receiver may be configured as uncertified or certified (TSO-C15c). Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

24 GPS Antenna Display (MFD, handheld, etc.) ADS-B Compliant GPS Receiver (TSO-C15, TSO-C16, TSO-C19, TSO-C196) DB 7 Connector Annunciator Lamp Pressure Altitude Encoder Maintenance Port Control Head Input Aircraft Power UAT Antenna Figure -: ADS600-B UAT uses External Certified (ADS-B Compliant) GPS Position Source GPS Antenna Display (MFD, handheld, etc.) ADS-B Compliant GPS Receiver (TSO-C15, TSO-C16, TSO-C19, TSO-C196) DB 7 Connector Annunciator Lamp Maintenance Port Control Head Input, with Pressure Altitude Aircraft Power UAT Antenna Figure -: ADS600-B UAT with Pressure Altitude Supplied by Control Head (Transponder) Input Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

25 GPS Antenna Display (MFD, handheld, etc.) and Control Head Input ADS-B Compliant GPS Receiver (TSO-C15, TSO-C16, TSO-C19, TSO-C196) DB 7 Connector Annunciator Lamp Pressure Altitude Encoder Maintenance Port Aircraft Power UAT Antenna Figure -5: ADS600-B UAT and MFD which includes Control Head Input Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

26 ..1 GPS Position Source 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- or ARINC 9 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 0-165A: Accord Technology LLC NexNav mini LRU GPS Receiver, P/N 1000 Garmin GNS80 GPS/Comm Navigator.. Display The ADS600-B outputs traffic and weather information to compatible displays. The ability to display traffic and/or weather depends on the display device... Maintenance Port The ADS600-B provides an RS 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... Annunciator Output The ADS600-B can drive an external annunciator lamp...5 Altitude Encoder Input The AD600-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- or ARINC Control Head The ADS600-B may be configured with a control head input. The control head input provides squawk code, IDENT, ALT/STANDBY/ON/OFF functionality for the ADS600-B.. Antenna Requirements..1 Certified GPS Antenna (P/N and ) If the ADS600-B is configured to use the internal certified (NexNav) 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-01 compliant antenna meeting the requirements of TSO-C190. For installations where the aircraft has an existing antenna complying with DO-8 (TSO-C1a), the ADS600-B Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

27 (part numbers and ) may be installed utilizing this antenna, as per DO-9D Note 1, Section The performance of the ADS600-B GPS SBAS Class Beta 1 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-9D. 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 - contains a list of GPS antennas that are recommended for use with the ADS600-B... Uncertified GPS Antenna (P/N and ) If the ADS600-B is configured to use the internal uncertified GPS as its position source, a GPS antenna must be attached to the GPS TNC antenna connector of the ADS600-B. GPS antenna performance is critical to the operation of the ADS600-B GPS/WAAS receiver. Table - 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 -1 contains a list of UAT antennas that are recommended for use with the ADS600-B. Some types (100 and 1090MHz) of transponder antennas use very thin radiator elements. These types of antennas should be closely evaluated to determine their suitability as UAT data link antennas. Operating the ADS600-B without RF terminations on the UAT Antenna port can result in equipment damage. Operate the ADS600-B with the UAT antenna port terminated with a VSWR ratio of.0:1 or less. Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

28 . Installation This section describes the installation of the ADS600-B including mounting, wiring and connections. Read this entire section before proceeding with the installation of the ADS600-B. Follow avionics installation practices per FAA Advisory Circular (AC).1-1B, -1-A, or FAA approved revisions to these documents. Perform an electrical load analysis in accordance with AC.1-1B, Chapter 11, on the aircraft prior to installation to ensure that the aircraft s electrical system is capable of carrying the ADS600-B load. Section.1 describes the power consumption of the ADS600-B...1 Materials Not Supplied The following items are required for the ADS600-B installation, but are not supplied: UAT Antenna (Table -1 provides a list of recommended UAT Antennas) GPS Antenna, if operating with internal GPS (Table - provides a list of recommended GPS Antennas) Wire (MIL-W-759/16 or equivalent) Shielded wire (MIL-C-7500 or equivalent) Circuit Breaker/Fuse, as applicable to aircraft Ring Terminals (for grounding) Bolts, Nuts and Washers for permanently mounting ADS600-B o Four AN-A bolts o Eight AN steel flat washers, washers placed on bolt side and nut side o Four AN65-10A elastic stop nuts Table -1: Acceptable ADS600-B UAT Antennas Manufacturer Part Num Connector RAMI AV-7 BNC RAMI AV-71 BNC Comant CI-105 BNC Comant CI TNC Delta Pop** ADSB-UAT BNC ** Experimental and Light Sport Aircraft use only. Copyright NavWorx Page 8 of 88 All rights reserved. Printed in the U.S.A.

29 Table -: Acceptable ADS600-B GPS Antennas Manufacturer Part Num TSO Recommended for ADS600-B Part Number Cobham Antennas (Comant) Sensor Systems Inc. CI 9-00 CI CI 01-0 CI S S S TSO-C190 TSO-C190 TSO-C1 TSO-C1 TSO-C190 TSO-C190 TSO-C Aero Antenna AT575- TSO-C Garmin GA-56 TSO-C19 Class A Tools Required The D-Sub connector supplied with the ADS600-B uses crimp contacts. Table - identifies the crimp tool required to ensure consistent and reliable crimp contact connections for the D-Sub connector. Table -: Crimp Tools for High Density - AWG Socket Contact Type Hand Crimping Tool Positioner Insertion/Extraction Tool Military P/N M50/-01 M50/-09 M81969/1-0 Positronic M81969/1-0 AMP Daniels AFM8 K M81969/1-0 Astro M81969/1-0 Copyright NavWorx Page 9 of 88 All rights reserved. Printed in the U.S.A.

30 .. Equipment Mounting 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 AN-A bolts, AN65-10A 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. Figure -6 describes the ADS600-B mounting bracket bolt pattern. Figure -6: ADS600-B Mounting Bracket Pattern...1 Antenna Placement GPS Antenna 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. The GPS antenna placement guidelines can be found in AC 0-18A section 16. Refer to For best performance, select an antenna location with an unobstructed view of the sky above the aircraft when in level flight UAT Antenna 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. Copyright NavWorx Page 0 of 88 All rights reserved. Printed in the U.S.A.

31 The UAT Antenna MUST be installed no less than 7 feet from any DME antenna. Failure to adhere to this critical installation note will result in failure of the ADS600-B and void your warranty... Cabling and Wiring After the DB7 cable assembly is made and installed on the ADS600-B, route the wire bundle as appropriate. Use cable ties to secure the cable assembly. The ring terminals that are affixed to the cable shields of the cable assembly should be attached to the ADS600-B ground via the one of the two DB7 slide latch studs. The ADS600-B should be installed in accordance with Refer to AC.1-1B Chapter 11. Refer to The cable assembly should not be exposed to wire chafing The cable assembly should not be located near the fuel lines. The cable assembly should not be located near high electrical capacity lines. The cable assembly should not be routed near high energy sources. The cable assembly should not be located near the flight control cables. Isolate the cable assembly from the engine. Install cable assembly in a protected area of the aircraft. Grounding pigtails should not exceed more than inches in length. Use AWG or larger for all wiring except for power. See Wiring Diagrams in Appendix A for recommended power and ground wiring. RG-00 coaxial cable is required for UAT Antenna. UAT Antenna cable loss should not exceed db. The 9 foot cable supplied with the ADS600-B has 1.5 db loss. Limit the RG00 cable length to 15 feet. RG-00 coaxial cable is recommended for the GPS Antenna. The GPS Antenna coaxial cable loss, including connectors, must be less than 10dB. Limit the RG00 cable length to 50 feet...5 Air Circulation and Cooling The ADS600-B meets all DO-8B 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 1 of 88 All rights reserved. Printed in the U.S.A.

32 .5 Electrical Connections.5.1 Connectors Table - describes the connectors supplied with the ADS600-B installation kit. The kit also contains crimp contacts for the D-Sub connector. Table - identifies the crimp tool required to ensure consistent and reliable crimp contact connections. Table -: Connectors Ref Description Connector Type Crimp Contact P1 I/O 7 Pin D-Sub Receptacle 0- AWG socket contact P UAT Antenna TNC jack N/A P GPS Antenna TNC jack N/A Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

33 .5. Interface Connector Definition The following figure shows the top view of the ADS600-B depicting the DSUB and TNC connectors. P1 DB7 Connector P UAT Antenna P GPS Antenna Figure -7: ADS600-B DB7, UAT and GPS Connectors Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

34 .5. I/O Connector (P1) A 7 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 -8: 7 Pin D-Sub Male Connector (P1) The pin-out description for the I/O connector is defined in Table -5. Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

35 Table -5: I/O Connector Pin-Out (P1) for ADS600-B Pin # I/O Name Description 1 -- Audio Out + RESERVED Feature, Not Functional. I Time mark In - ARINC 7A/NexNav Mini LRU Time Mark In VDC PWR Roving Networks Bluetooth &Wifi module power 100mA max. I RS Maintenance RX RS Maintenance Port Serial Data Input 5 O DISPLAY PORT RS TX RS Display Serial Data Output 6 -- Ground, Signal Ground, Signal 7 I Altitude Encoder RX RS Altitude Encoder Input 8 O 9 OUT 1B ARINC 9 Output Channel 1B 9 I 9 IN 1A ARINC 9 Input Channel 1A RESERVED RESERVED 11 I External PPS TTL In External PPS TTL In 1 O RS TX - RS Display Channel Data Output - 1 I RS RX + RS Display Channel Data Input + 1 O UAT Indicator Out UAT Indicator Output (active low) 15 O GPS NMEA RS RESERVED, not functional NEXNAV GPS TX External Accord Technology NexNav Mini LRU GPS TX Ground, Signal Ground, Signal Power + Main Aircraft Power Input (+9 to +VDC) Power + Main Aircraft Power Input (+9 to +VDC) 0 -- Audio Out - RESERVED Feature, not functional 1 I Time mark In + ARINC 7A/NexNav mini LRU Time Mark In + O RS Maintenance TX RS Maintenance Port Serial Data Output -- Ground, Signal Ground, Signal I DISPLAY PORT RS RX RS Display Serial Data Input 5 O TIS TX TIS Serial Data Output 6 -- Ground, Signal Ground, Signal 7 O 9 OUT 1A ARINC 9 Output Channel 1A 8 I 9 IN 1B ARINC 9 Input Channel 1B 9 -- Squat Switch In RESERVED 0 O RS TX + RS display channel data output + 1 I RS RX - RS display channel data input - -- Ground, Signal Ground, Signal I Transponder Control RX RX Data from Transponder configured for Remote Mode I NEXNAV GPS RX External Accord Technology NexNav Mini LRU GPS RX 5 O Suppression Output Suppression Output (active high) 6 I Power Ground Main Aircraft Power Ground 7 I Power Ground Main Aircraft Power Ground Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

36 .6 Functional Descriptions.6.1 Power Aircraft power is provided to the ADS600-B on the P1 I/O connector. The ADS600-B accepts input power from +9 to + VDC. P1-18 Power + P1-19 Power + P1-6 Power Ground P1-7 Power Ground.6. 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 (P1-1) 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..6.. Suppression Output The Suppression Output (P1-5) 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..6. 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 6 of 88 All rights reserved. Printed in the U.S.A.

37 .6. PPS Time Mark Input When used with an external ARINC 7A position source or with external NexNav mini LRU, the time mark signals from the navigation sensor are connected to the ADS600-B time mark input pins (P1- and P1-1)..6.5 Serial Interfaces The ADS600-B provides two bi-directional RS- serial interfaces, three receive only RS interfaces, one transmit only RS interface, one bi-directional RS- interface and one ARINC 9 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: P1-1 RS Display Serial Data Input + P1-1 RS Display Serial Data Input - P1-1 RS Display Serial Data Output - P1-0 RS Display Serial Data Output + P1-9 ARINC 9 Input Channel 1A P1-7 ARINC 9 Output Channel 1A P1-8 ARINC 9 Input Channel 1B P1-8 ARINC 9 Output Channel 1B P1-7 RS Altitude Encoder Serial Data Input P1-5 RS TIS Serial Data Output P1-6 RS Altitude Encoder and TIS Output Ground P1- RS Transponder Control Panel Input P1- RS Transponder Control Panel Ground P1- RS Display Serial Data Input P1-5 RS Display Serial Data Output P1- RS Display Ground Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

38 P1- RS Maintenance Port Serial Data Input P1- RS Maintenance Port Serial Data Output P1-6 RS Maintenance PC Ground P1- NexNav mini LRU GPS Receive (GNSS Position Source) P1- Ground RS Altitude Encoder Input An altitude encoder input may be provided through a RS serial data input (P1-7 and P1-6) 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. The ADS600-B is compatible with equipment with the following formats: Icarus, Shadin Z, Shadin RMS, UPSAT Apollo and EFIS. The format of the EFIS protocol is described in ADS600-B Interface Control Document ( ). The other compatible altitude encoder formats are described in Appendix C RS Control Panel Input A transponder control panel input may be provided through a RS serial data input (P1- and P1-) to the ADS600-B. The UAT Console is used to select the type of transponder control panel input. The ADS600-B is compatible with the following transponder control panel serial outputs: NavWorx TransMonSPE, Garmin GTX 0, Garmin GTX 7, Garmin SL70/70R, Garmin GNS80 (standalone and with attached transponder), and Trig TT1/TT RS TIS Output (Garmin portables GPSMAP x96) The ADS600-B may be configured to output TIS data via a RS serial data output (P1-6 and P1-5) to a portable GPSMAP display device. The UAT Console describes how to select the serial data port for the TIS Output. The baud rate for this port is defaulted to RS In/Out Display The ADS600-B may be configured to output to a display device using the RS serial interface (P1-1, P-1, P1-0, and P1-1). 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 RS serial interface RS In/Out Display The ADS600-B may be configured to output to a display device using the RS serial interface (P1-5, P1-, and P1-). 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 RS serial interface RS Maintenance PC The ADS600-B communicates with the maintenance PC using a RS serial interface (P1-6, P1-, and P1-). 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 115,00 baud, 8 data, no parity, 1 stop Copyright NavWorx Page 8 of 88 All rights reserved. Printed in the U.S.A.

39 bit. The UAT Console, a Windows PC application, communicates to the ADS600-B using this port RS GNSS Position Source The ADS600-B may be configured to use the Accord Technology NexNav mini LRU (P/N 1000) as its external GNSS Position Source input (P1- and P1-). The UAT Console allows the installer to select the GNSS Position Source to use with the ADS600-B. Copyright NavWorx Page 9 of 88 All rights reserved. Printed in the U.S.A.

40 .6.6 ARINC9 The ADS600-B provides one ARINC 9 input and output (P1-8, P1-9, P1-7, and P1-8) interface. The ARINC 9 baud rate can be set to either High or Low to match the baud rate of the connected equipment. This interface supports: ARINC 75B Traffic Computer (TCAS and ADS-B) output. The output labels are listed in Table -6. ARINC Label 0 (Pressure Altitude) input. ARINC 7A- GNSS Sensor input. The input labels are listed in Table -7. The ARINC input/output is configured using the UAT Console. Table -6: ARINC 9 (75B) Out Labels Label Number Parameter Name 10 Intruder Range 11 Intruder Altitude (relative) 1 Intruder Bearing Estimate 70 Vertical RA Data Output 7 Selected Sensitivity Level 50 Fault Summary 57 Request to Send (RTS) or End of Transmission (ETX) 71 General Aviation Equipment ID 77 Equipment ID Table -7: ARINC 9 (7A) In Labels Label Number Parameter Name 110 GNSS Latitude 111 GNSS Longitude 10 GNSS Latitude Fine 11 GNSS Longitude Fine 10 AUT Horizontal Integrity Limit 16 Vertical Figure of Merit 150 UTC 165 Vertical Velocity 166 North/South Velocity 17 East/West Velocity 7 Horizontal Figure of Merit 70 GNSS Height 77 Equipment ID Copyright NavWorx Page 0 of 88 All rights reserved. Printed in the U.S.A.

41 .7 Post Installation Check.7.1 Configuration of ADS600-B with Maintenance PC The UAT Console is a Windows PC application required to configure the ADS600-B. Refer to Appendix B for a description of how to configure the ADS600-B unit via the Maintenance Personal Computer (PC)..7. Electrical Load Analysis The ADS600-B is powered via a separate circuit protection device. For aircraft with multiple power buses, this protection device is sourced from the non-essential bus. Circuits should be protected in accordance with guidelines in AC.1-1B, Chapter 11. An electrical load analysis should be completed on each aircraft prior to installation in accordance with AC.1-1B, Chapter 11. Use Tables -8 and -9 to aid in load analysis computations. Table -8: Electrical Load Analysis for P/N , Input Voltage 1 VDC 8 VDC Current Consumption Typical Maximum Table -9: Electrical Load Analysis for P/N , Input Voltage 1 VDC 8 VDC Current Consumption Typical Maximum 1..7 Table -10: Recommended Circuit Protection Device ADS600-B/ADS600-B-B 1 VDC 8 VDC **Circuit Protection AMP AMP ** If using a fuse, it must be a slow blow fuse type. The circuit protection device placard should be labeled UAT. Copyright NavWorx Page 1 of 88 All rights reserved. Printed in the U.S.A.

42 .7. VHF COM Interference GPS Testing This section applies to all ADS600-B part numbers. Susceptibility to harmonics of VHF COM transceivers shall be evaluated. If harmonic interference is identified, then more isolation or greater distance may be required between the GPS and COM antennas to reduce or eliminate harmonic interference. 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.7..1 describes how to verify the GPS Position. VHF COM Frequency MHz MHz MHz MHz MHz MHz.7..1 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 B- 15: 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..7. Mounting and 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 depicted in Section.5.. Verify that the display port, maintenance port and power/ground are securely cabled to the DB7 connector of the ADS600-B. Ensure that the slide lock of the DB7 is in the locked position. If any ADS600-B cabling is routed near the aircraft controls, verify free movement of the aircraft controls. Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

43 .7.5 Weight and Balance An aircraft weight and balance is required after installation of the ADS600-B. Follow the guidelines in AC.1-1B, Chapter 10, Section. Update the aircraft equipment list indicating the items relocated, added or removed. Table -11 identifies the weight of the ADS600-B equipment. Figure -9 depicts the ADS600-B center of gravity. Table -11: ADS600-B Weight Item ADS600-B (P/N , ) ADS600-B (P/N , ) Weight 1. lbs 1.8 lbs Figure -9: ADS600-B Center of Gravity Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

44 .8 ADS600-B Unit Removal and Replacement Whenever the ADS600-B unit is removed and reinstalled, verify that the unit is mounted and wired as described in section.7. and verify that the unit is properly configured as described in section Troubleshooting Table 5-1: Trouble Shooting Guide Problem Possible Cause Remedial Action Traffic Targets are not shown on Display Ghost Traffic Target shown on Display Simulation Traffic Targets are not shown on Display ADS600-B does not communicate with UAT Console (PC) via Maintenance Port Transponder is set to Standby or OFF ADS600-B Transmitter is disabled ADS600-B does not have a valid GPS solution Mode-S Transponder installed: ICAO address of transponder is different from that of ADS600-B UAT Transponder: Squawk code of ADS600-B is different than Transponder ADS600-B does not have a valid GPS solution USB to RS Cable is not detected by Windows PC Maintenance Port incorrectly wired Set Transponder to On or ALT Enable Transponder Turn on GPS position source. Secure GPS antenna connection to ADS600-B. Set ICAO address of Transponder and ADS600-B with the same address. Configure ADS600-B control panel input to specify type of transponder. Verify transponder wiring to ADS600-B Control Panel Input (DB 7 pin ). Turn on GPS position source. Secure GPS antenna connection to ADS600-B. Copyright NavWorx Page of 88 All rights reserved. Printed in the U.S.A.

45 6 Maintenance 6.1 Altitude Source The altitude source provide to the ADS600-B must be tested and inspected every months as referenced in FAR Calibration There are no user-serviceable adjustments. There are no periodic maintenance functions to be performed on the ADS600-B product. 6. Tune-Up The ADS600-B is tuned at the factory. No tune-up procedure or servicing is required by the user. 6. Cleaning The ADS600-B does not require regular cleaning. Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

46 GPSMAP P1 5 6 ADS600 Maintenance Port RX Maintenance Port TX Maintenance Port Ground P/N: Appendix A A.1 Interconnect Diagram: ADS600 to GPSMAP TIS-A 5 6 TIS Ground NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC 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 db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 NavWorx, Inc. 706 Big A Road Rowlett, TX Data In Ground ADS600 to GPSMAP TIS-A Interconnect Diagram TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME GROUND PIN, P CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 10 Yellow Black MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder TX Ground Maintenance Port DB9 Female Connector 5 TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 7 6 TIS TX 8 Altitude Encoder RX Altitude Encoder Ground 8 10 TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND P1 Power + 18 Power + 19 Power Ground 6 Power Ground 7 Suppression Output 5 UAT Indicator 1 GPS UAT P P 0AWG 0AWG 0AWG 0AWG Rev Date Description RG00 RG00 / AMP UAT AIRCRAFT GROUND P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) - A 6 7 0/1/09 Initial Release 08/9/10 B 01/8/11 C 06/18/11 Transponder Suppression Input 9 Added power and ground wiring recommendations Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number D 06//1 Removed Composite TIS AVIONICS BUS (1/8 VDC) Top GPS Antenna Bottom UAT Antenna Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

47 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC 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 db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX Bluetooth Display Port Interconnect Diagram (Requires Hardware MOD A) TO ROVING NETWORKS BLUETOOTH ADAPTOR (RN-0M) RECOMMENDED BAUD RATE: DB9 Female Connector TX RX Ground 5 +5VDC 9 ADS600 SUPPLIES FUSED AND FILTERED +5VDC TO BLUETOOTH ADAPTOR ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder Maintenance Port DB9 Female Connector RX TX Ground TX Ground CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. MAINTENANCE PORT GROUND: USE P1-6 for ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW BLUETOOTH +5VDC: USE P1- FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1-1 FOR ADS600-B SERIAL NUMBERS BELOW REFER TO COMPOSITE-TIS DIAGRAM FOR WIRING REQUIRED FOR COMPOSITE-TIS. 5 8 P1 5 6 Display RX Display TX Display Ground ADS600 Maintenance Port RX Maintenance Port TX Maintenance Port Ground P1 5 / AMP VDC TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Altitude Encoder RX Altitude Encoder Ground Power + 18 Power + 19 Power Ground 6 Power Ground 7 Suppression Output 5 UAT Indicator 1 GPS UAT P P TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 0AWG 0AWG 0AWG 0AWG RG00 RG00 UAT AIRCRAFT GROUND P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) 6 7 Rev Date Description - A Transponder Suppression Input 9 0/1/09 Initial Release 08/9/10 B 01/8/11 C 06/18/11 D 09/01/11 AVIONICS BUS (1/8 VDC) Top GPS Antenna Bottom UAT Antenna TWISTED SHIELDED FOUR CONDUCTOR SHIELD TERMINATED TO GROUND 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 P/N: A. Interconnect Diagram: Bluetooth Display Port Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

48 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 7 NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX WiFi Display Port Interconnect Diagram (Requires Hardware MOD A) TO ROVING NETWORKS WIFLY SERIAL ADAPTOR WITH RECHARGEABLE BATTERIES (RN-70M) RECOMMENDED BAUD RATE: THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 DB9 Female Connector TX RX Ground 5 +5VDC 9 ADS600 SUPPLIES FUSED AND FILTERED +5VDC TO WIFI ADAPTOR ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder Maintenance Port DB9 Female Connector RX TX Ground TX Ground CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. MAINTENANCE PORT GROUND: USE P1-6 for ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW WIFI +5VDC: USE P1- FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1-1 FOR ADS600-B SERIAL NUMBERS BELOW REFER TO COMPOSITE-TIS DIAGRAM FOR WIRING REQUIRED FOR COMPOSITE-TIS. 5 8 P1 5 6 Display RX Display TX Display Ground ADS600 Maintenance Port RX Maintenance Port TX Maintenance Port Ground P1 5 / AMP VDC Altitude Encoder RX TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Altitude Encoder Ground Power + 18 Power + 19 Power Ground 6 Power Ground 7 Suppression Output 5 UAT Indicator 1 GPS UAT P P 0AWG 0AWG 0AWG 0AWG RG00 RG00 UAT AIRCRAFT GROUND P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Rev Date Description A 08/08/11 Initial Release Transponder Suppression Input 9 B 09/01/ Clarify WiFi power relative to ADS600-B S/N AVIONICS BUS (1/8 VDC) Top GPS Antenna Bottom UAT Antenna TWISTED SHIELDED FOUR CONDUCTOR SHIELD TERMINATED TO GROUND P/N: A. Interconnect Diagram: WiFi Display Port Copyright NavWorx Page 8 of 88 All rights reserved. Printed in the U.S.A.

49 Display NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED NavWorx, Inc. 706 Big A Road Rowlett, TX Display Port Interconnect Diagram TX RX Ground POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. TX Ground Maintenance Port 8 DB9 Female Connector 5 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 9 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. P Display RX Display TX Display Ground ADS600 Altitude Encoder RX Altitude Encoder Ground Maintenance Port RX Maintenance Port TX Maintenance Port Ground 9 P1 Power + 18 Power + 19 Power Ground 6 Power Ground 7 Suppression Output 5 UAT Indicator 1 GPS UAT TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND P P 0AWG 0AWG 0AWG 0AWG RG00 RG00 / AMP UAT AIRCRAFT GROUND P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) Rev Date Description A TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 0/1/09 Initial Release 08/9/10 B 01/8/11 Transponder Suppression Input 8 C 06/18/11 Added power and ground wiring recommendations Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number D 06//1 Removed Composite TIS 5 AVIONICS BUS (1/8 VDC) Top GPS Antenna Bottom UAT Antenna P/N: A. Interconnect Diagram: Display Port Copyright NavWorx Page 9 of 88 All rights reserved. Printed in the U.S.A.

50 A.5 Interconnect Diagram: ADS600 Maintenance Port to Computer ADS600 Maintenance Port RX Maintenance Port TX Maintenance Port Ground P1 6 NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600 Maintenance (Serial) Port to Computer Interconnect Diagram Rev Date Description 0/09/09 Initial Release A B 06/18/11 08/9/10 Added Diagram Headers Changed Maintenance Port Ground Pin number - Maintenance Port Computer DB9 Male Connector DB9 Female Connector 5 5 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 50 of 88 All rights reserved. Printed in the U.S.A.

51 AFS Serial Port NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 6 10 NavWorx, Inc. 706 Big A Road Rowlett, TX ADS600-B to AFS Interconnect Diagram 11 Ground 1 RX 5 TX ***ALTITUDE ENCODER INPUT REQUIRED*** AFS Serial Port Altitude Encoder THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. TX Ground 1 Maintenance Port DB9 Female Connector 7 5 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME GROUND PIN, P CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 10 AFS ADS-B FUNCTIONALITY REQUIRES S SERIES CPU. 11 THE ADS600-B MAY CONNECT TO ANY AVAILABLE AFS SERIAL PORT. THE ADS600-B ALTITUDE ENCODER PORT SHOULD CONNECT TO AFS SERIAL PORT. USE THE AFS ADMIN SETTINGS WINDOW TO CONFIGURE THE DISPLAY SERIAL PORT TO ADSB 57K AND THE ALTITUDE ENCODER SERIAL PORT TO TFC/ ICARUS. 1 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW P1 ADS600-B Altitude Encoder RX Altitude Encoder Ground 8 Maintenance Port RX Maintenance Port TX Maintenance Port Ground P1 5 / AMP Display Ground 5 Display TX Display RX 1 Suppression Output 5 Power + Power Power Ground 6 Power Ground 7 UAT Indicator 1 GPS UAT P P 0AWG 0AWG 0AWG 0AWG RG00 RG00 UAT AIRCRAFT GROUND P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Transponder Suppression Input Rev Date Description A 01/8/11 Initial Release B 06/18/11 C 06//1 Changed Maintenance Port Ground Pin number Add text describing AFS serial port configuration AVIONICS BUS (1/8 VDC) Top GPS Antenna Bottom UAT Antenna TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND P/N: A.6 Interconnect Diagram: ADS600 to AFS Copyright NavWorx Page 51 of 88 All rights reserved. Printed in the U.S.A.

52 A.7 Interconnect Diagram: ADS600-B to GRT NavWorx, Inc. 706 Big A Road Rowlett, TX ADS600-B to GRT Interconnect Diagram Rev Date Description A 09/11/10 Initial Release B 01/8/11 C 06/18/11 Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number D 06//1 Removed Composite TIS ADS600 GRT Connector B ***ALTITUDE ENCODER INPUT REQUIRED*** GRT Connector A Altitude Encoder Serial Output 6 1 Altitude Encoder RX Ground P1 Altitude Encoder Ground 8 Display Ground Power + Power + P AWG 0AWG / AMP UAT 5 AVIONICS BUS (1/8 VDC) 9 10 Serial Input 7 Serial Output 7 Maintenance Port DB9 Female Connector 5 Display TX Display RX Maintenance Port RX Power Ground 6 Power Ground 7 Suppression Output 5 UAT Indicator 1 0AWG 0AWG Transponder Suppression Input 11 AIRCRAFT GROUND Top GPS Antenna Maintenance Port TX 5 6 Maintenance Port Ground P 6 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. 1 GPS RG00 POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC 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 db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 TISA AND ALTITUDE ENCODER INPUT SHARE SAME GROUND PIN (P1-6). 9 GRT SOFTWARE VERSION REQUIRED TO DISPLAY ADS-B TRAFFIC AND WEATHER: * HORIZON HX VERSION * HORIZON HS/WS VERSION * SPORT WS/HS/SX VERSION 7 10 IN A DUAL DISPLAY CONFIGURATION, CONNECT ONLY SERIAL OUT 7 (PIN ) OF THE MFD (HX) TO THE ADS600-B (PIN P1-). 11 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 1 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. UAT P RG00 P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND 7 Bottom UAT Antenna TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

53 A.8 Interconnect Diagram: ADS600-B to GRT HX/HS/WS (TIS Traffic) NavWorx, Inc. 706 Big A Road Rowlett, TX ADS600-B to GRT HX/HS/WS Interconnect Diagram TIS Traffic Interface GRT Connector A Serial Output 6 1 ***ALTITUDE ENCODER INPUT REQUIRED*** Serial Input 6 Ground 17 Maintenance Port DB9 Female Connector 5 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 7 TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME GROUND PIN, P1-6. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 10 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. Rev Date Description A 09/11/10 Initial Release B 01/8/11 C 06/18/11 Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number D 06//1 Removed Composite TIS ADS600 P1 7 Altitude Encoder RX 5 TISA TX Altitude Encoder/TISA Ground Power + Power + P AWG 0AWG / AMP UAT 5 AVIONICS BUS (1/8 VDC) Power Ground 6 Power Ground 7 0AWG 0AWG AIRCRAFT GROUND Top GPS Antenna Suppression Output 5 Transponder Suppression Input UAT Indicator 1 Maintenance Port RX 9 Maintenance Port TX 6 Maintenance Port Ground P 6 10 GPS RG00 P UAT RG00 7 P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) Bottom UAT Antenna TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

54 A.9 Interconnect Diagram: GNS 80 ARINC 7A Position Source NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX GNS 80 ARINC 7A Position Source Rev Date Description TWISTED SHIELDED TWO - 0/1/09 CONDUCTOR Initial Release SHIELD TERMINATED TO GROUND A 08/9/10 Added Diagram Headers B 01/8/11 Identified GNS 80 connectors ADS600 GNS 80 P1: 7-PIN D-SUB, MALE CONNECTOR ARINC 9 Out A P In 1A ARINC 9 Out B P In 1B Time Mark Out + P A Time Mark In + Time Mark Out - P1-17 7A Time Mark In - NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. GNS 80 ARINC 9 #1 OUT (P5-/) MAY BE USED INSTEAD OF 9 # (P5-5/5) OUT. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 5 of 88 All rights reserved. Printed in the U.S.A.

55 A.10 Interconnect Diagram: ADS600-B to GNS 80 Traffic (ARINC 9) NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX GNS 80 ARINC 9 In A ADS600-B togns 80 Traffic (ARINC 9) P P1 9 Out 1A ADS600 Power + Power + P AWG 0AWG Rev Date Description A 0/1/09 Initial Release 08/9/10 B 01/8/11 C 06/18/11 / AMP UAT Added power and ground wiring recommendations Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number 5 AVIONICS BUS (1/8 VDC) ARINC 9 In B P5-9 Maintenance Port 8 9 Out 1B Power Ground 6 Power Ground 7 0AWG 0AWG AIRCRAFT GROUND Top GPS Antenna DB9 Female Connector Suppression Output 5 Transponder Suppression Input UAT Indicator 1 9 Maintenance Port RX Maintenance Port TX 5 6 Maintenance Port Ground P 6 10 GPS RG00 ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder TX Ground 7 6 Altitude Encoder RX Altitude Encoder Ground UAT P RG00 7 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC 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 db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 IF THE ARINC 9 TRAFFIC OPTION IS CONFIGURED FOR THE GNS 80, THE GNS 80 SERIAL TIS OPTION IS NOT AVAILABLE. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 10 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND - Copyright NavWorx Page 55 of 88 All rights reserved. Printed in the U.S.A.

56 A.11 Interconnect Diagram: ADS600-B to GNS 80 Traffic (RS- TIS) NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to GNS 80 Traffic (RS- TIS) Rev Date Description A 0/06/09 Initial Release 08/9/10 B 01/8/11 C 06/18/11 Added power and ground wiring recommendations Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number GNS 80 RS RxD6 Serial Ground 6 P5- P5-8 Maintenance Port DB9 Female Connector P1 5 6 TIS TX TIS Ground 9 ADS600 Power + Power + P Power Ground 6 Power Ground 7 Suppression Output 5 0AWG 0AWG 0AWG 0AWG Transponder Suppression Input / AMP UAT AIRCRAFT GROUND 5 AVIONICS BUS (1/8 VDC) Top GPS Antenna UAT Indicator 1 10 Maintenance Port RX Maintenance Port TX 5 6 Maintenance Port Ground P 6 11 GPS RG00 P UAT RG00 ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder TX Ground 7 6 Altitude Encoder RX Altitude Encoder Ground 7 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 IF THE SERIAL TIS OPTION IS CONFIGURED FOR THE GNS 80, THE GNS 80 ARINC 9 TRAFFIC OPTION IS NOT AVAILABLE. 9 TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME GROUND PIN, P CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 9 P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 5 THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 11 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 1. REFER TO COMPOSITE-TIS DIAGRAM FOR WIRING REQUIRED FOR COMPOSITE-TIS. - Copyright NavWorx Page 56 of 88 All rights reserved. Printed in the U.S.A.

57 A.1 Interconnect Diagram: ADS600-B to GNS 0 Traffic (ARINC 9) NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to GNS 0 Traffic (ARINC 9) Rev Date Description A 10/17/09 Initial Release B 01/8/11 C 06/18/11 Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number GNS 0 ARINC 9 In 1A P P1 7 9 Out 1A ADS600 Power + Power + P AWG 0AWG / AMP UAT 5 AVIONICS BUS (1/8 VDC) ARINC 9 In 1B P001-9 Maintenance Port DB9 Female Connector 8 9 Out 1B Power Ground 6 Power Ground 7 Suppression Output 5 0AWG 0AWG Transponder Suppression Input AIRCRAFT GROUND Top GPS Antenna UAT Indicator 1 Maintenance Port RX 9 Maintenance Port TX 5 6 Maintenance Port Ground P 6 10 GPS RG00 ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder TX Ground 7 6 Altitude Encoder RX Altitude Encoder Ground UAT P RG00 7 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND USE 0 AWG WIRE. P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) 5 WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 IF GNS 0 ARINC 9 IN PORT 1 (P001-8/9) IS USED FOR ANOTHER PURPOSE, USE ARINC 9 IN PORT (p001-50/51). CONFIGURE THE ARINC 9 IN PORT FOR THE GTX 0 TRAFFIC INTERFACE. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. 10 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. Copyright NavWorx Page 57 of 88 All rights reserved. Printed in the U.S.A.

58 A.1 Interconnect Diagram: ADS600 to Chelton NavWorx, Inc. 706 Big A Road Rowlett, TX ADS600 to Chelton ADS-B ADS600 Rev Date Description A 0/1/09 Initial Release 08/9/10 B 01/8/11 C 06/18/11 Added power and ground wiring recommendations Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number D 06//1 Removed Composite TIS Chelton Serial Port 8 J1 RS Datalink RX ***ALTITUDE ENCODER INPUT REQUIRED*** Altitude Encoder TX Ground 7 6 P1 Altitude Encoder RX Altitude Encoder Ground 5 Display TX Power + Power + P1 Suppression Output AWG 0AWG Transponder Suppression Input / AMP UAT 5 AVIONICS BUS (1/8 VDC) Ground Maintenance Port Ground RS Datalink TX 5 Display RX Power Ground 6 Power Ground 7 0AWG 0AWG AIRCRAFT GROUND Top GPS Antenna DB9 Female Connector UAT Indicator 1 9 CHELTON CONFIGURATON Maintenance Port RX On the Factory Programmed Settings page in the Chelton Limits Setup: Datalink Receiver = ADS-B NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 7 5 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 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. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 6 Maintenance Port TX Maintenance Port Ground 10 GPS UAT P P RG00 RG00 P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 10 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Bottom UAT Antenna 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. - Copyright NavWorx Page 58 of 88 All rights reserved. Printed in the U.S.A.

59 A.1 Interconnect Diagram: ADS600-B to MX0/GMX 00 (RS Traffic/Weather) NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to MX0 or GMX 00 ADS-B Traffic and Weather RS Interconnect Diagram Rev Date Description A 1/0/010 Initial Release B 01/8/11 C 06/18/11 D 10/1/011 Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number Removed redundant ground shield for MX0 to ADS600-B connection. ***ALTITUDE ENCODER INPUT REQUIRED*** P1 ADS600 Altitude Encoder 7 Altitude Encoder RX 6 MX0 or GMX 00 Altitude Encoder Ground P1 8 RS TX + 8 RS TX - 10 PORT CONFIG (GMX 00 ONLY) P001 9 RS RX + 11 RS RX Maintenance Port 1 RX RX + 1 RX RX - 0 RX TX + 1 RX TX - Suppression Output 5 Power + Power Power Ground 6 Power Ground 7 0AWG 0AWG 0AWG 0AWG Transponder Suppression Input / AMP UAT AIRCRAFT GROUND 5 AVIONICS BUS (1/8 VDC) Top GPS Antenna DB9 Female Connector UAT Indicator 1 9 Maintenance Port RX Maintenance Port TX 5 6 Maintenance Port Ground P 6 10 GPS RG00 P NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 7 THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. 8 REQUIRED FOR GMX 00 ONLY. JUMPER MUST BE INSTALLED BETWEEN PIN 9 AND PIN 9 OF P001 TO CONFIGURE PORT FOR RS OPERATION. WHEN PORT IS USED AS AN RS PORT, RS PORT CAN NOT BE USED. 9 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. UAT RG00 P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) 7 Bottom UAT Antenna 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 10 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBER 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND 6 THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING CONNECTORS, MUST BE LESS THAN 10dB. Copyright NavWorx Page 59 of 88 All rights reserved. Printed in the U.S.A.

60 A.15 Interconnect Diagram: ADS600-B to MX0/GMX 00 (ARINC 9 Traffic) NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to MX0 or GMX 00 Traffic Only ARINC9 Interconnect Diagram Rev Date Description A 1/0/10 Initial Release B 01/8/11 C 06/18/11 D 10/1/011 Added UAT Indicator And Suppression Out Changed Maintenance Port Ground Pin number Removed redundant ground shield for MX0 to ADS600-B connection. ***ALTITUDE ENCODER INPUT REQUIRED*** P1 ADS600 Altitude Encoder 7 Altitude Encoder RX 6 Altitude Encoder Ground P1 MX0 or GMX 00 P00 ARINC 9 1A In 59 ARINC 9 1B In Out 1A 8 9 Out 1B Suppression Output 5 Power + Power AWG 0AWG Transponder Suppression Input / AMP UAT 5 AVIONICS BUS (1/8 VDC) Maintenance Port Power Ground 6 Power Ground 7 0AWG 0AWG AIRCRAFT GROUND Top GPS Antenna DB9 Female Connector UAT Indicator 1 8 Maintenance Port RX Maintenance Port TX 5 6 Maintenance Port Ground P 6 9 GPS RG00 P UAT RG00 7 NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. POWER AND GROUND WIRING: WIRE LENGTH GREATER THAN 1 FEET EACH 0 AWG WIRE, or 1 EACH 16 AWG WIRE WIRE LENGTH LESS THAN 1 FEET 1 EACH 18 AWG WIRE. 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 db. LIMIT THE RG00 CABLE LENGTH TO 15 FEET. P1: 7-PIN D-SUB, MALE CONNECTOR P: TNC COAXIAL CONNECTOR (UAT ANTENNA) P: TNC COAXIAL CONNECTOR (GPS ANTENNA) Bottom UAT Antenna WIRING FOR MAINTENANCE PORT IS REQUIRED. RS 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 5 FEET. 5 GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE RECOMMENDED CIRCUIT BREAKER RATING IS A FOR 1VDC INSTALLATIONS AND, A FOR 8VDC INSTALLATIONS. CIRCUIT BREAKER SHOULD BE LABELED UAT 8 CONNECTING UAT INDICATOR IS RECOMMENDED BUT OPTIONAL. NO GUIDANCE FROM FAA AT THIS TIME. ACTIVE LOW INDICATOR. 00mA MAXIMUM. 9 MAINTENANCE PORT GROUND: USE P1-6 FOR ADS600-B SERIAL NUMBERS 851 AND ABOVE. USE P1- FOR ADS600-B SERIAL NUMBERS BELOW 851. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND TWISTED SHIELDED THREE CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 60 of 88 All rights reserved. Printed in the U.S.A.

61 A.16 Interconnect Diagram: ADS600-B to SL70 Transponder Control NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to SL70 Transponder Control Rev Date Description A 1/0/10 Initial Release B 07/0/11 Corrected pin number for Transponder Control RX C 10/1/011 Removed notes and. SL70 RS- TXD1 5 RS- Ground ADS600-B P1 Transponder Control RX Ground NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 61 of 88 All rights reserved. Printed in the U.S.A.

62 A.17 Interconnect Diagram: ADS600-B to GTX 0 Transponder Control NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to GTX 0 Transponder Control Rev Date Description A 1/0/10 Initial Release B 0/5/11 Added Ground Signal C 07/0/11 Corrected pin number for Transponder Control RX D 0/11/011 Corrected Note # GTX 0 J01 RS- Out 5 Power Ground 7 ADS600-B P1 5 Transponder Control RX Ground NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. THE GTX 0 RS- OUTPUT MUST BE CONFIGURED FOR REMOTE + TIS. THE GTX 0 HAS TWO RS- OUTPUT CHANNELS: RS- Out 1 (PIN ) AND, RS- Out (PIN 5). EITHER OF THESE OUTPUTS MAY BE CONNECTED TO P1- OF THE ADS600-B. CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6, TO THE GTX 0 POWER GROUND (EITHER J01-PIN 7 OR J01-PIN ). 5 IF ALTITUDE RECEIVED OVER ARINC 9, THEN PIN 7 MAY BE USED AS AN ALTERNATE INPUT FOR UAT CONTROL INTERFACE. Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

63 A.18 Interconnect Diagram: ADS600-B to GTX 7 Transponder Control NavWorx, Inc. 906 Industrial Street, Suite 100 Rowlett, TX ADS600-B to GTX 7 Transponder Control Rev Date Description A 1/0/10 Initial Release B 0/5/11 Added Ground Signal C 07/0/11 Corrected pin number for Transponder Control RX GTX 7 J71 RS- Out 1 0 Power Ground 1 ADS600-B P1 Transponder Control RX Ground NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6, TO THE GTX 7 POWER GROUND (EITHER J71-PIN 1 OR J71-PIN 5). IF ALTITUDE RECEIVED OVER ARINC 9, THEN PIN 7 MAY BE USED AS AN ALTERNATE INPUT FOR UAT CONTROL INTERFACE. Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

64 A.19 Interconnect Diagram: ADS600-B to NexNav mini LRU (GPS Source) NavWorx, Inc. 706 Big A Road Rowlett, TX NexNav mini LRU GPS SBAS Class Beta-1 Receiver P/N 1000 Rev Date Description - 06/0/1 Initial Release ADS600 P1: 7-PIN D-SUB, MALE CONNECTOR NexNav mini LRU P/N 1000 RS- Receive Port NEXNAV GPS TX RS- Transmit Port 1 7 RS- Signal Ground Port 1 10 NEXNAV GPS RX GND 1 PPS Y 1 NEXNAV LRU Time Mark In + 1 PPS Z 15 NEXNAV LRU Time Mark In - NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. USING NEXNAV LEGACY PROTOCOL. RS- BAUD RATE 1900bps. TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND Copyright NavWorx Page 6 of 88 All rights reserved. Printed in the U.S.A.

65 A.0 Interconnect Diagram: ADS600-B to TT1/TT Mode S Transponder Control NavWorx, Inc. 706 Big A Road Rowlett, TX Rev Date Description - 08/5/1 Initial Release ADS600-B to TT1/TT Mode S Transponder Control TTX Mode S Xpndr Mutual Suppression 18 P1 ADS600-B Code Out 7 Transponder Control RX Ground 6 Ground 5 Suppression Output NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. Copyright NavWorx Page 65 of 88 All rights reserved. Printed in the U.S.A.

66 A.1 Interconnect Diagram: ADS600-B to TransMonSPE Control NavWorx, Inc. 706 Big A Road Rowlett, TX Rev Date Description - 1//1 Initial Release TransMonSPE Control Input for ADS600-B ADS600-B P1 Green Transponder Control RX TransMonSPE USB Black Ground Red +5VDC PWR Copyright NavWorx Page 66 of 88 All rights reserved. Printed in the U.S.A.

67 A. Interconnect Diagram: ADS600-B to GNS 80 Remote Transponder Control NavWorx, Inc. 706 Big A Road, Rowlett TX Rev Date Description A 1//1 Initial Release ADS600-B to GNS 80 Remote Transponder Control NOTES: 1. ALL WIRES AWG OR LARGER UNLESS OTHERWISE SPECIFIED. GROUNDING PIGTAILS MUST NOT EXCEED INCHES IN LENGTH. REFER TO THE APPROPRIATE TRANSPONDER INSTALLATION MANUAL FOR GNS 80 TO REMOTE SERIAL TRANSPONDER INTERCONNECT DIAGRAM. ADS600-B P1 Transponder Control RX Ground GTX 0 GTX GTX SL70/70R GNS 80 P5 RS- TXD 6 Signal Ground Copyright NavWorx Page 67 of 88 All rights reserved. Printed in the U.S.A.

68 Appendix B 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.9.0 and above. The UAT Console communicates with the ADS600-B via a serial (RS) communication channel configured to 115,00 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 B- 1: UAT Console Launch Screen Copyright NavWorx Page 68 of 88 All rights reserved. Printed in the U.S.A.

69 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 B- : UAT Console UAT NOT CONNECTED Copyright NavWorx Page 69 of 88 All rights reserved. Printed in the U.S.A.

70 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 B- : UAT Console UAT NOT CONFIGURED Copyright NavWorx Page 70 of 88 All rights reserved. Printed in the U.S.A.

71 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 B-. 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 B- : UAT Console Identification sub-tab Copyright NavWorx Page 71 of 88 All rights reserved. Printed in the U.S.A.

72 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 B- 5: UAT Console Emitter sub-tab Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

73 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 B- 6: UAT Console Inputs sub-tab Figure B- 7: UAT Console, Control Panel Popup Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

74 Displays sub-tab The ADS600-B may be configured with up to displays. Figure B- 8: UAT Console Displays sub-tab Figure B- 9: UAT Console TIS-A and ARINC 9 Displays Copyright NavWorx Page 7 of 88 All rights reserved. Printed in the U.S.A.

75 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. Figure B- 10: UAT Console Transmitter sub-tab Copyright NavWorx Page 75 of 88 All rights reserved. Printed in the U.S.A.

76 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). UAT Transmitter is enabled Figure B- 11: UAT Console Transmitter (TX) indicator illuminates green when UAT Transmitter is enabled Copyright NavWorx Page 76 of 88 All rights reserved. Printed in the U.S.A.

77 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 B- 1. Text will appear in the message window indicating that the software upgrade may take up to minutes. See Figure B- 1. 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 B- 1. 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 B- 1: UAT Console Upgrade Tab Copyright NavWorx Page 77 of 88 All rights reserved. Printed in the U.S.A.

78 Figure B- 1: UAT Console Software Upgrade Start Message Figure B- 1: UAT Console Software Upgrade Complete Copyright NavWorx Page 78 of 88 All rights reserved. Printed in the U.S.A.

79 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 B- 15. Traffic Messages are displayed only when traffic messages are received. See Figure B- 16. 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 -105 Feet will be displayed for altitude. Figure B- 15: UAT Console Reports Tab Copyright NavWorx Page 79 of 88 All rights reserved. Printed in the U.S.A.

80 Figure B- 16: UAT Console Traffic Messages Copyright NavWorx Page 80 of 88 All rights reserved. Printed in the U.S.A.