ADS600-B Installation and User Manualgrants permission to download a single copy of this document onto a hard drive or other ... (ARINC 429) Wiring Diagram. Added wiring ... Uniquely

2011-07-04 P/N: 240-0008-00-14

Copyright 2009-2011 NavWorx ® Page 1 of 76 All rights reserved. Printed in the U.S.A.

ADS600-B™ Installation and User Manual

®

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Business Address: NavWorx Inc.

3906 Industrial St, Suite 100

Rowlett, TX 75088

Telephone:

(888)-NAVWORX (628-9679)

Facsimile: 888- 628-9679

Email: [email protected]

Website: www.NavWorx.com

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.

mailto:[email protected]

2011-07-04 P/N: 240-0008-00-14


Revision History Revision Date Comments

01 04/20/2010 Initial release

02 05/11/2010 Revised FCC statement

03 08/29/2010 Updated Wiring Diagrams. Added content to 3.4.1 GPS Antenna, 3.5.4 Cabling and Wiring, 3.5.5 Air Circulation and Cooling Sections, and 3.8.3 Mounting and Wiring Sections.

04 09/12/2010 Added ADS600-B to GRT Wiring Diagrams. Replaced text of Maintenance PC section with reference to Maintenance Port Tutorial document, 240-0007-00-02.

05 09/18/2010 Added Quick Start Guide and ADS600-B Maintenance Port Tutorial Sections.

06 10/10/2010 Changed download link for TeraTermPro

07 10/17/2010 Added GNS 430(W) (ARINC 429) Wiring Diagram. Added wiring diagrams to table of contents.

08 12/02/2010 Added GMX 200/MX20 RS422 and ARINC 429 Interconnect Diagrams.

09 12/30/2010 Added GTX 330, GTX 327 and SL70 Transponder Interconnect Diagrams.

10 01/28/2011 Added Suppression Input and UAT Indicator to Interconnect Diagrams. Uniquely identify ports of GNS480 743A Interconnect Diagram. Added ADS600-B to AFS (ADS-B) Interconnect Diagram.

11 04/06/2011 Corrected Disclaimer.

12 04/25/2011 Added ground signal to GTX 330 and GTX 327 Interconnect Diagrams.

13 06/18/2011 Changed pin outs for ADS600- B serial numbers 851 and above.

14 07/04/2011 Corrected UAT control panel interface. Corrected pins 33 and 34 of table 3-6. Changed UAT control from pin 7 to pin 33 for SL70, GTX330, and GTX327 diagrams.

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List of Effective Pages

Page Rev Page Rev Page Rev Page Rev Page Rev

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End User License Agreement (EULA)

Terms. By installing or using the ADS600-B (“product”), you agree to be bound by the terms and conditions of the

following license agreement. Please read this agreement carefully. NavWorx Incorporated ("NavWorx") grants you

a limited, non-exclusive license to use the product. Title, ownership rights, and intellectual property rights in and to

the product remain with NavWorx.

Refund. If you do not agree to the terms of this EULA, NavWorx Inc. is unwilling to license the product to you. In

such event, you may not use the licensed product, and you should promptly contact NavWorx for a refund. The

product must not have been used or installed in order to obtain a full refund.

No Warranties. Except as expressly provided in the limited warranty section, the products’ hardware and its

operating system software are provided to you “as is” without warranty of any kind, either expressed or implied,

including, but not limited to, waranties of noninfringement, merchantability, and /or fitness for a particular purpose.

The entire risk of the quality and performance of both the software and hardware is with the user.

Copyright. You acknowledge that the product is the property of NavWorx and is protected under United States of America copyright laws and international copyright treaties. You further acknowledge that the structure,

organization, and source design of the hardware and software are valuable trade secrets of NavWorx. You agree not

to open the product, break the EULA seal, nor decompile, disassemble, modify, reverse assemble, reverse engineer,

or reduce to human readable form the hardware or software or any part thereof or create any derivative works based

on the product.

No Liability for Consequential Damages. NavWorx Inc. and its suppliers shall not be held liable for any damages

suffered or incurred by you (including, but not limited to, general, special, consequential or incidental damages for

loss of business profits, business interruption, personal compensation and the like), arising from or in connection

with the delivery, use, or performance of the product and its software.

Customer Remedies. NavWorx Inc. and its suppliers entire liability and your exclusive remedy shall be, at

NavWorx’ option, either (1) return of the product purchase price, not to exceed list price, or (2) repair or

replacement of the product which is returned to NavWorx with original proof of purchase.

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Disclaimer Symbology seen throughout this documentation highlight important information. The following table defines how to

interpret these symbols:

Symbol Description

Hazardous.

Warning.

Important.

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 an MFD or CDTI to display UAT, TIS-B and FIS-B products. NavWorx is not responsible for how a display device renders these products. Nor

is NavWorx responsible for the failure of the display device to render these products.

The ADS600-B receives TIS-B and FIS-B products from ADS-R ground stations. NavWorx is not responsible for the content, or lack of content, in TIS-B and FIS-B product offerings by the FAA.

NavWorx is not responsible for the failure of ADS-R groundstations 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.

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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 email 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 (628-9679)

Email [email protected]

Step 2. Once you have received an RMA number, securely pack the unit and ship it, insured, to the following address:

NavWorx Incorporated

RMA Number: (insert your RMA number here)

3906 Industrial St, Suite 100

Rowlett, TX 75088

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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). A log file recording the

current configuration of the ADS600-B must be emailed to [email protected] for our

support personnel to be able to answer your questions.

The following MUST be completed before powering up the ADS600-B:

Connect (RG-400) the UAT antenna to the port labeled “UAT ANT”

Connect (RG-400) the GPS antenna to the port labeled “GPS ANT”

Connect ‘fused’ power to the ADS600-B unit via port 1 (DB37

connector)

Ensure that the ADS600-B’s maintenance port (DB9 connector) is

accessible

Verify that a pressure altitude encoder source is connected to the

ADS600-B (via the DB37 connector)

Before your first flight you MUST verify the configuration of the

ADS600-B unit.

Position aircraft and the ADS600-B unit to have a ‘view’ of

the sky and the GPS satellites

Load TERATERM onto your PC

Configure TeraTerm terminal emulator

Connect the (TeraTerm) COM port of your PC to the

maintenance port (DB9 connector) of the ADS600-B unit

Enable TeraTerm logging

Type “READ ALL” on the TeraTerm input

Type “READ GPS ALL” on the TeraTerm input

Email log file (captured by TeraTerm) to

[email protected]

Refer to the ADS600-B Maintenance Port Tutorial section for more detailed configuration

instructions.



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Table of Contents Revision History .........................................................................................................................3

List of Effective Pages ................................................................................................................4

End User License Agreement (EULA) ........................................................................................5

Disclaimer ...................................................................................................................................6

NavWorx Two Year Limited Warranty .......................................................................................7

ADS600-B Installation Quick Start Guide ...................................................................................8

Definitions and Acronyms ......................................................................................................... 13

1 Accessories and Packing List .............................................................................................. 14

1.1 Unpacking Equipment .................................................................................................. 14

1.2 Package Contents ......................................................................................................... 14

2 About this Manual .............................................................................................................. 15

2.1 FCC Grant of Equipment Authorization ....................................................................... 15

3 Equipment Description ....................................................................................................... 15

3.1 Overall Specifications .................................................................................................. 16

3.2 Transmitter Specification ............................................................................................. 18

3.3 System Interfaces ......................................................................................................... 18

3.3.1 Display .................................................................................................................. 19

3.3.2 Maintenance Port ................................................................................................... 19

3.3.3 Annunciator Output ............................................................................................... 19

3.4 Antenna Requirements ................................................................................................. 19

3.4.1 GPS Antenna ......................................................................................................... 19

3.4.2 UAT Antenna ........................................................................................................ 19

3.5 Installation ................................................................................................................... 20

3.5.1 Materials Not Supplied .......................................................................................... 20

3.5.2 Tools Required ...................................................................................................... 21

3.5.3 Equipment Mounting ............................................................................................. 21

3.5.4 Cabling and Wiring ................................................................................................ 22

3.5.5 Air Circulation and Cooling ................................................................................... 23

3.6 Electrical Connections .................................................................................................. 23

3.6.1 Connectors ............................................................................................................. 23

3.6.2 Interface Connector Definition ............................................................................... 24

3.6.3 I/O Connector (P1)................................................................................................. 25

3.7 Functional Descriptions ................................................................................................ 28

3.7.1 Power .................................................................................................................... 28

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3.7.2 Discrete Outputs .................................................................................................... 28

3.7.3 Discrete Inputs ....................................................................................................... 28

3.7.4 PPS Time Mark Input ............................................................................................ 29

3.7.5 Serial Interfaces ..................................................................................................... 29

3.8 Post Installation Check ................................................................................................. 30

3.8.1 Maintenance PC ..................................................................................................... 30

3.8.2 Electrical Load Analysis ........................................................................................ 30

3.8.3 Mounting and Wiring Check .................................................................................. 31

3.8.4 Functional Test ...................................................................................................... 32

3.8.5 Weight and Balance ............................................................................................... 32

4 Limitations ......................................................................................................................... 32

4.1 Traffic Display ............................................................................................................. 32

5 Troubleshooting .................................................................................................................. 32

6 Maintenance ....................................................................................................................... 32

6.1 Altitude Source ............................................................................................................ 32

6.2 Calibration ................................................................................................................... 32

6.3 Tune-Up ....................................................................................................................... 32

6.4 Battery Replacement .................................................................................................... 32

6.5 Cleaning ....................................................................................................................... 33

Product Registration .................................................................................................................. 34

ADS600-B Maintenance Port Tutorial ....................................................................................... 35

ASSUMPTIONS ............................................................................................................................ 35

POWERING UP THE ADS600-B.................................................................................................... 36

ADS600-B COMMAND FORMAT ................................................................................................. 37

CONFIGURING ICAO ADDRESS ................................................................................................... 37

CONFIGURING ADS600-B FOR TRAFFIC/WEATHER DISPLAY DEVICES ........................................ 38

PRESSURE ALTITUDE INPUT ........................................................................................................ 38

DETERMINING GPS RECEPTION .................................................................................................. 39

MONITORING TRAFFIC OUTPUT .................................................................................................. 40

VIEW CURRENT ADS600-B CONFIGURATION & STATUS ............................................................. 41

VERIFYING ADS600-B TO TRAFFIC DISPLAY INTERFACE ............................................................ 41

UPGRADING ADS600-B SOFTWARE ........................................................................................... 42

TERATERM ................................................................................................................................ 49

MAINTENANCE PORT TIPS .......................................................................................................... 52

MAINTENANCE PORT HELP COMMANDS ..................................................................................... 53

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VERIFYING ADS600-B CONFIGURATION .................................................................................... 56

Interconnect Diagram: ADS600 to GPSMAP® TIS-A .............................................................. 57

Interconnect Diagram: Bluetooth Display Port .......................................................................... 58

Interconnect Diagram: Display Port .......................................................................................... 59

Interconnect Diagram: ADS600 Maintenance Port to Computer ................................................ 60

Interconnect Diagram: Composite-TIS™ .................................................................................. 61

Interconnect Diagram: ADS600 to AFS .................................................................................... 62

Interconnect Diagram: ADS600 to AFS (TIS Traffic) ............................................................... 63

Interconnect Diagram: ADS600-B to GRT ................................................................................ 64

Interconnect Diagram: ADS600-B to GRT HX/HS/WS (TIS Traffic) ........................................ 65

Interconnect Diagram: GNS 480 ARINC 743A Position Source ................................................ 66

Interconnect Diagram: ADS600-B to GNS 480 Traffic (ARINC 429) ....................................... 67

Interconnect Diagram: ADS600-B to GNS 480 Traffic (RS-232 TIS)........................................ 68

Interconnect Diagram: ADS600-B to GNS 430 Traffic (ARINC 429) ....................................... 69

Interconnect Diagram: ADS600 to Chelton ............................................................................... 70

Interconnect Diagram: ADS600 to Chelton (Composite TIS™)................................................. 71

Interconnect Diagram: ADS600-B to MX20/GMX 200 (RS422 Traffic/Weather) ..................... 72

Interconnect Diagram: ADS600-B to MX20/GMX 200 (ARINC 429 Traffic) ........................... 73

Interconnect Diagram: ADS600-B to SL70 Transponder Control .............................................. 74

Interconnect Diagram: ADS600-B to GTX 330 Transponder Control ........................................ 75

Interconnect Diagram: ADS600-B to GTX 327 Transponder Control ........................................ 76

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List of Tables

Table 1-1: Package Contents ................................................................................................................................. 14

Table 1-2: ADS600-B Installation Kit Contents (P/N 210-0004-00-00) ................................................................. 14

Table 3-1: Acceptable ADS600-B UAT Antennas ................................................................................................. 20

Table 3-2: Acceptable ADS600-B GPS Antennas ................................................................................................. 21

Table 3-3: Crimp Tools for High Density 22-24 AWG Socket Contact .................................................................. 21

Table 3-4: Connectors .......................................................................................................................................... 23

Table 3-5: I/O Connector Pin-Out (P1) for ADS600-B serial numbers 851 and above ............................................ 26

Table 3-6: I/O Connector Pin-Out (P1) for ADS600-B serial numbers below 851 .................................................. 27

Table 3-7: Recommended Circuit Breaker............................................................................................................. 31

Table 3-8: ADS600-B Weights ............................................................................................................................. 32

List of Figures

Figure 3-1: Top view of ADS600-B UAT Data Link Transceiver 15

Figure 3-2: ADS600-B UAT Data Link Transceiver System Diagram 18

Figure 3-3: ADS600-B Mounting Bracket Pattern 22

Figure 3-4: ADS600-B DB37, UAT and GPS Connectors 24

Figure 3-5: 37 Pin D-Sub Male Connector (P1) 25

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Definitions and 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

CDTI Cockpit Display of Traffic Information

FCC Federal Communications Commission

FAA Federal Aviation Administration

FIS-B Flight Information Services Broadcast

MFD Multifunction Display

GBT Ground Based Transceiver (also known as ADS-R)

PC Personal Computer

STC Supplemental Type Certificate

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

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1 Accessories and Packing List

1.1 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.

1.2 Package Contents

The items included in the ADS600-B package are listed in Tables 1-1and 1-2.

Table 1-1: Package Contents

Part # Quantity Description

210-0004-00-00 1 ADS600 Installation Kit (see Table 1-2 for details)

200-0012-XX-XX 1 ADS600-B UAT Data Link Transceiver

Table 1-2: ADS600-B Installation Kit Contents (P/N 210-0004-00-00)

Part # Quantity Description

201-205167-1 1 Receptacle Female, DSUB 37-pin

201-205161-1 1 Receptacle Female, DSUB 9-pin

201- DC-24660-33 1 DSUB 37-pin back-shell

201-5745407-1 1 Connector DSUB Latch Slide 37 position

201-M39029/63-368 20 Crimp contact, DSUB, 20 to 24 AWG wire

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2 About this Manual This manual describes the installation and checkout procedures for the ADS600-B UAT Data Link Transceiver.

The ADS600-B unit is intended to be installed in aircraft that do not require an STC for

installation.

2.1 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.

3 Equipment Description The ADS600-B UAT Data Link Transceiver contains a GPS/WAAS receiver and a Universal

Access receiver and transmitter. This unit transmits a GPS position and aircraft information

message once per second. Additionally, this unit receives messages from other UAT equipped

aircraft and receives TIS-B/FIS-B messages from ADS-Rs. Data received by the ADS600-B is output to a display device.

Figure 3-1: Top view of ADS600-B UAT Data Link Transceiver

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3.1 Overall Specifications This section includes the physical, electrical, performance and environmental specifications for the ADS600-B UAT Data Link Transceiver.

Physical

Height: 2.1 inches

Width: 5.4 inches (w/o mounting bracket)

7.3 inches (w/ mounting bracket)

Depth: 6.2 inches

Weight: 1.5 lbs (w/o mounting bracket, excluding cables)

1.6 lbs (w/ mounting bracket, excluding cables)

Electrical

Voltage: 9-36VDC

Input Current (10W nominal): Steady State: 0.7A @ 14VDC, 0.41A @ 24VDC

Transmit Peak: 1.1A @ 14VDC, 0.59A @24VDC

UAT Performance

Regulatory: DO-282B

Frequency: 978MHz

Tolerance: +/- 20ppm

Data Rate: 1.04167 Mbps

Receiver Sensitivity: Exceeds 90%MSR@-98dBm

Transmit Power: 40W nominal at antenna

Equipment Class: A1S (single bottom UAT antenna)

GPS/WAAS Receiver Performance

Number of channels: 20

Frequency: 1575.42MHz L1

Sensitivity (Tracking Mode): -159dBm (Tracking mode)

Sensitivity (Acquisition Mode): -142dBm (Acquisition mode)

TTFF Hot (valid almanac, position, time and ephemeris): 1 second

TTFF Warm (valid almanac, position and time): < 35 seconds

TTFF Cold (valid almanac): < 35 seconds

Reacquisition (<10seconds obstruction): 0.1seconds

Position Update Interval: 5Hz

Velocity: 1,000 Kts maximum @ 60,000 ft MSL

Datum: WGS-84

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Environmental

Operating temperature: -20°C to +55°C

Storage temperature: -55°C to +85°C

Temperature variation: 5°C per minute

Humidity: 94% at 65°C

Maximum continuous altitude: 40,000 feet

Decompression: 40,000 feet

External Cooling: Not required

Avionics Interfaces

Annunciator Outputs: Capable of sinking 500mA for turning on annunciator lamp

Altitude Encoder: RS232 asynchronous serial, ARINC429 ADC/AHRS source

Maintenance Port: RS232 asynchronous serial

External Position Input: From ARINC743A source

Display: RS232 asynchronous serial (Pass-through or Traffic interfaces)

RS422 asynchronous serial (Pass-through or Traffic interfaces)

ARINC735 Traffic interface

TIS-A Traffic interface

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3.2 Transmitter Specification The ADS600-B is a non-TSO device that complies with RTCA DO-282B.

3.3 System Interfaces

Figure 3-2: ADS600-B UAT Data Link Transceiver System Diagram

GPS Antenna

Maintenance Port UAT Antenna

Display (MFD, Portable, etc.)

A/C Power

ADS600-B

Annunciator (Lamp)

Altitude

Encoder

DB37 Connector

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3.3.1 Display The ADS600-B outputs traffic and weather information to compatible display. The ability to

display traffic and/or weather depends on the display device.

3.3.2 Maintenance Port The ADS600-B provides an RS232 communication port that is used to configure and monitor the

status of the ADS600-B system via a computer. The maintenance port is required to be installed and connected.

3.3.3 Annunciator Output The ADS600-B can drive an external annunciator lamp.

3.4 Antenna Requirements

3.4.1 GPS Antenna The ADS600-B requires one GPS antenna. GPS antenna performance is critical to the operation

of the ADS600-B GPS/WAAS receiver. Table 3-2 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. Contact the factory to ensure antenna compatibility prior to

installing your ADS600-B.

3.4.2 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 3-1 contains a list of UAT antennas that are recommended for use with the ADS600-B.

Some types (1030 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 3.0:1 or less.

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3.5 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) 43.13-1B, 43-13-2A, or FAA approved revisions to these documents.

Perform an electrical load analysis in accordance with AC 43.13-1B, 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 3.1 describes the power consumption of the ADS600-B.

3.5.1 Materials Not Supplied The following items are required for the ADS600-B installation, but are not supplied:

UAT Antenna (Table 3-1 provides a list of recommended UAT Antennas)

GPS Antenna, if installing an external GPS input for ADS600-B (Table 3-2 provides a

list of recommended GPS Antennas)

Wire (MIL-W-22759/16 or equivalent)

Shielded wire (MIL-C-27500 or equivalent)

Circuit Breakers

Ring Terminals (for grounding)

Table 3-1: Acceptable ADS600-B UAT Antennas

Manufacturer Part Num Connector Hole Template

RAMI AV-74 BNC http://www.rami.com/files/2/AV-74-Footprint.pdf

RAMI AV-741 BNC http://www.rami.com/files/2/AV-741-Footprint.pdf

Comant CI-105 BNC

Comant CI-105-11 TNC

Delta Pop ADSB-UAT BNC http://www.deltapopaviation.com/Delta_Pop_Aviati

on/Mounting_Detail.html

http://www.rami.com/files/2/AV-74-Footprint.pdf

http://www.rami.com/files/2/AV-741-Footprint.pdf

http://www.deltapopaviation.com/Delta_Pop_Aviation/Mounting_Detail.html

http://www.deltapopaviation.com/Delta_Pop_Aviation/Mounting_Detail.html

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Table 3-2: Acceptable ADS600-B GPS Antennas

Manufacturer Part Num Connector Hole Template

RAMI AV-GPS BNC http://www.rami.com/files/2/AV-GPS-Footprint.pdf

Comant CI-2480-400 GPS Uses TNC



3.5.2 Tools Required The D-Sub connector supplied with the ADS600-B uses crimp contacts. Table 3-3 identifies the

crimp tool required to ensure consistent and reliable crimp contact connections for the D-Sub

connector.

Table 3-3: Crimp Tools for High Density 22-24 AWG Socket Contact

Type Hand Crimping Tool Positioner Insertion/Extraction Tool

Military P/N M22520/2-01 M22520/2-09 M81969/1-04

Positronic 9507 9502-3 M81969/1-04

AMP 601966-1 601966-6 91067-1

Daniels AFM8 K42 M81969/1-04

Astro 615717 615725 M81969/1-04

3.5.3 Equipment Mounting The ADS600-B may be mounted in either a portable or remote mount configuration.

3.5.3.1 ADS600-B Portable Mount

The ADS600-B may be mounted in a portable configuration. The unit may be placed on a glare

shield or any hard surface and affixed in place using Velcro®. The unit may also be portably

attached to the aircraft using a RAM® mounting system.

3.5.3.2 ADS600-B Remote Mount

This option is recommended for non-certified, experimental or light sport aircraft to remotely

mount the ADS600-B to the aircraft. The ADS600-B may be ordered with optional mounting

brackets. Figure 3-3 describes the ADS600-B mounting bracket bolt pattern.

http://www.rami.com/files/2/AV-GPS-Footprint.pdf

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Figure 3-3: ADS600-B Mounting Bracket Pattern

3.5.3.3 Antenna Placement

3.5.3.3.1 GPS Antenna

The GPS Antenna placement guidelines can be found in AC 20-138A section 16. Refer to

http://rgl.faa.gov/REGULATORY_AND_GUIDANCE_LIBRARY/RGADVISORYCIRCULAR

.NSF/0/8a2ae2491c85226f86256e35004c638b/$FILE/AC20-138A.pdf

3.5.3.3.2 UAT Antenna

The UAT Antenna MUST be installed no less than 5 feet from any Transponder /TCAS/TAS

or DME antenna. Failure to adhere to this critical installation note will result in failure of the

ADS600-B and void your warranty.

3.5.4 Cabling and Wiring The ADS600-B should be installed in accordance with Refer to AC 43.13-1B Chapter 11. Refer to http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/list/AC%2043.13-

1B/$FILE/Chapter%2011.pdf

The cable harness should not be exposed to wire chafing

The cable harness should not be located near the fuel lines.

The cable harness should not be located near high electrical capacity lines.

The cable harness should not be routed near high energy sources.

The cable harness should not be located near the flight control cables.

Isolate the cable harness from the engine. Install cable harness in a protected area of the aircraft.

Grounding pigtails should not exceed more than 4 inches in length.

http://rgl.faa.gov/REGULATORY_AND_GUIDANCE_LIBRARY/RGADVISORYCIRCULAR.NSF/0/8a2ae2491c85226f86256e35004c638b/$FILE/AC20-138A.pdf

http://rgl.faa.gov/REGULATORY_AND_GUIDANCE_LIBRARY/RGADVISORYCIRCULAR.NSF/0/8a2ae2491c85226f86256e35004c638b/$FILE/AC20-138A.pdf

http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/list/AC%2043.13-1B/$FILE/Chapter%2011.pdf

http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/list/AC%2043.13-1B/$FILE/Chapter%2011.pdf

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RG-400 coaxial cable is required for UAT Antenna. UAT Antenna cable loss should not exceed

3 dB. The 11 foot cable supplied with the ADS600-B has 1.5 dB loss. Limit the RG400 cable length to 15 feet.

RG-400 coaxial cable is recommended for the GPS Antenna. The GPS Antenna coaxial cable loss, including connectors, must be less than 10dB.

Use 24 AWG or larger for all wiring except for power. See Wiring Diagrams section at the end of this document for recommended power and ground wiring.

3.5.5 Air Circulation and Cooling The ADS600-B meets all DO-282B requirements without external cooling. However, as with all

electronic equipment, lower operating temperatures will extend equipment life. It is not recommended to use outside forced air to cool the unit. Instead it is recommended that an electric forced air fan be installed

to cool the equipment. If forced air cooling is installed, ensure that rainwater cannot enter or be sprayed

on the ADS600-B.

3.6 Electrical Connections

3.6.1 Connectors Table 3-4 describes the connectors supplied with the ADS600-B installation kit. The kit also

contains crimp contacts for the D-Sub connector. Table 3-3 identifies the crimp tool required to ensure consistent and reliable crimp contact connections.

Table 3-4: Connectors

Ref Description Connector Type Crimp Contact

P1 I/O 37 Pin D-Sub Receptacle 20-24 AWG socket contact

P2 UAT Antenna TNC connector. N/A

P3 GPS Antenna TNC connector. N/A

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3.6.2 Interface Connector Definition The following figure shows the side view of the ADS600-B depicting the DSUB and TNC connectors.

Figure 3-4: ADS600-B DB37, UAT and GPS Connectors

P3 GPS Antenna P2 UAT

Antenna

P1 DB37 Connector

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3.6.3 I/O Connector (P1) A 37 pin D-Sub connector interfaces to external equipment and aircraft power. This connector

can be found at the rear of the ADS600-B unit.

View looking at ADS600-B.

Figure 3-5: 37 Pin D-Sub Male Connector (P1)

The pin-out description for the I/O connector is defined in Table 3-5 and Table 3-6. Table 3-5

pertains to ADS600-B serial numbers 851 and above. Table 3-6 pertains to ADS600-B serial

numbers below 851.

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Table 3-5: I/O Connector Pin-Out (P1) for ADS600-B serial numbers 851 and above

Pin # I/O Name Description

1 -- Audio Out + Traffic Alert Audio +

2 I Time mark In - ARINC 743A Time Mark In -

3 -- +5VDC PWR Roving Networks Bluetooth &Wifi module power – 100mA max

4 I RS232 Maintenance RX RS232 Maintenance Port Serial Data Input

5 O DISPLAY PORT RS232 TX RS232 Display Serial Data Output

6 -- Ground, Signal Ground, Signal

7 I Altitude Encoder RX RS232 Altitude Encoder Input

8 O 429 OUT 1B ARINC 429 Output Channel 1B

9 I 429 IN 1A ARINC 429 Input Channel 1A

10 -- RESERVED RESERVED

11 I External PPS TTL In External PPS TTL In

12 O RS422 TX - RS422 Display Channel Data Output -

13 I RS422 RX + RS422 Display Channel Data Input +

14 O UAT Indicator Out UAT Indicator Output (active low)

15 O RESERVED RX RS232 TX Data to NexNav GPS

16 -- NEXNAV GPS TX External Accord Technology NexNav Mini GPS TX


18 -- Power + Main Aircraft Power Input (+9 to +36VDC)


20 -- Audio Out - Traffic Alert Audio -

21 I Time mark In + ARINC 743A Time Mark In +

22 O RS232 Maintenance TX RS232 Maintenance Port Serial Data Output


24 I DISPLAY PORT RS232 RX RS232 Display Serial Data Input

25 O TIS TX TIS Serial Data Output


27 O 429 OUT 1A ARINC 429 Output Channel 1A

28 I 429 IN 1B ARINC 429 Input Channel 1B

29 -- Squat Switch In Discrete Input (Active Low)

30 O RS422 TX + RS422 display channel data output +

31 I RS422 RX - RS422 display channel data input -


33 I Transponder Control RX RX Data from Transponder configured for Remote Mode

34 I NEXNAV GPS RX External Accord Technology NexNav Mini GPS RX

35 O Suppression Output Suppression Output (active high)

36 I Power Ground Main Aircraft Power Ground


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Table 3-6: I/O Connector Pin-Out (P1) for ADS600-B serial numbers below 851

Pin # I/O Name Description

1 -- BLUETOOTH +5VDC PWR Roving Networks Bluetooth &Wifi module power

2 I Time mark In - ARINC 743A Time Mark In -

3 -- Ground RS232 Maintenance Port Ground

4 I RS232 Maintenance RX RS232 Maintenance Port Serial Data Input

5 O RS232 TX RS232 Display Serial Data Output

6 -- Ground RS232 Altitude Encoder and TIS Output Ground

7 I Altitude Encoder RX RS232 Altitude Encoder Input

8 O 429 OUT 1B ARINC 429 Output Channel 1B

9 I 429 IN 1A ARINC 429 Input Channel 1A


11 I External PPS TTL In External PPS TTL In

12 O RS422 TX - RS422 Display Channel Data Output -

13 I RS422 RX + RS422 Display Channel Data Input +

14 O UAT Indicator Out UAT Indicator Output (active low)

15 O NexNav GPS TX TX Data to NexNav GPS


17 -- Ground Ground




21 I Time mark In + ARINC 743A Time Mark In +

22 O RS232 Maintenance TX RS232 Maintenance Port Serial Data Output

23 -- Ground RS232 Display Ground

24 I RS232 RX RS232 Display Serial Data Input

25 O TIS TX TIS Serial Data Output


27 O 429 OUT 1A ARINC 429 Output Channel 1A

28 I 429 IN 1B ARINC 429 Input Channel 1B

29 -- Squat Switch In Discrete Input (Active Low)

30 O RS422 TX + RS422 display channel data output +

31 I RS422 RX - RS422 display channel data input -

32 -- Ground Ground

33 I UAT Control Panel IN UAT Control Panel IN

34 I NexNav GPS RX RX Data from NexNav GPS

35 O Suppression Output Suppression Output (active high)



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3.7 Functional Descriptions

3.7.1 Power Aircraft power is provided to the ADS600-B on the P1 I/O connector. The ADS600-B accepts

input power from +9 to +36 VDC.

P1-18 Power +

P1-19 Power +

P1-36 Power Ground

P1-37 Power Ground

3.7.2 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.

3.7.2.1 UAT Indicator

The UAT Indicator Out (P1-14) is used to indicate the status of the ADS600-B receiver. UAT

Indicator Out will be grounded when the ADS600-B has detected a system failure. Otherwise,

this output will be open.

3.7.2.2 Suppression Output

The Suppression Output (P1-35) is intended to suppress other L-band equipment (such as a

transponder) when the UAT transmits. It will provide a high signal (Vin – 1.0V) whenever the

UAT is transmitting and ground otherwise.

3.7.3 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.

3.7.3.1 Air/Ground Discrete Input

The Air/Ground In (P1-34) is reserved for future use. It provides air/ground status input to the

ADS600-B. The function of this input is configurable via the Maintenance PC (refer to section 3.8.1). The Air/Ground Input must be configured for one of the following options:

A grounded Air/Ground In indicates that the aircraft is on the ground. Otherwise, an open indicates that the aircraft is in the air.

An open Air/Ground In indicates that the aircraft is on the ground. Otherwise, a

grounded Air/Ground In indicates that the aircraft is in the air.

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An air/ground switch is not installed. The air/ground state is set automatically based on the GPS ground speed. The air/ground speed threshold is configurable.

3.7.4 PPS Time Mark Input When used with an external ARINC 743A position source, the time mark signals from the navigation sensor are connected to the ADS600-B time mark input pins (P1-2 and P1-21).

3.7.5 Serial Interfaces The ADS600-B provides two bi-directional RS-232 serial interfaces, one receive only RS232

interface, one transmit only RS232 interface, one bi-directional RS-422 interface and one

ARINC 429 input/output. These serial interfaces can be connected to:

Display(s)

Maintenance PC

Altitude Encoder

The serial port pin-outs are:

P1-13 RS422 Display Serial Data Input +

P1-31 RS422 Display Serial Data Input -

P1-12 RS422 Display Serial Data Output -

P1-30 RS422 Display Serial Data Output +

P1-9 ARINC 429 Input Channel 1A

P1-27 ARINC 429 Output Channel 1A

P1-28 ARINC 429 Input Channel 1B

P1-8 ARINC 429 Output Channel 1B

P1-7 RS232 Altitude Encoder Serial Data Input

P1-25 RS232 TIS Serial Data Output

P1-6 RS232 Altitude Encoder and TIS Output Ground

P1-24 RS232 Display Serial Data Input

P1-5 RS232 Display Serial Data Output

P1-23 RS232 Display Ground

P1-4 RS232 Maintenance Port Serial Data Input

P1-22 RS232 Maintenance Port Serial Data Output

P1-26 RS232 Maintenance PC Ground

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3.7.5.1 RS232 Altitude Encoder Input

An altitude encoder input may be provided through a RS232 serial data input (P1-7 and P1-6) to

the ADS600-B. The maintenance PC commands (see section 3.8.1) describe how to enable the

serial port for the Altitude Encoder Input. The baud rate for this port is also configurable via a maintenance command.

3.7.5.2 RS232 TIS Output (Garmin portables GPSMAP® x96)

The ADS600-B may be configured to output TIS data via a RS232 serial data output (P1-6 and

P1-25) to a portable GPSMAP® display device. The maintenance PC commands (see section

3.8.1) describe how to enable the serial data port for the TIS Output. The baud rate for this port

is also configurable via a maintenance command.

3.7.5.3 RS422 In/Out Display

The ADS600-B may be configured to output to a display device using the RS422 serial interface

(P1-12, P-13, P1-30, and P1-31). The type of display device is configurable. The maintenance

PC commands (see section 3.8.1) allow the installer to select a display device, as well as, a baud rate for the RS422 serial interface.

3.7.5.4 RS232 In/Out Display

The ADS600-B may be configured to output to a display device using the RS232 serial interface

(P1-5, P1-23, and P1-24). The type of display device is configurable. The maintenance PC

commands (see section 3.8.1) allow the installer to select a display device, as well as, a baud rate

for the RS232 serial interface.

3.7.5.5 RS232 Maintenance PC

The ADS600-B communicates with the maintenance PC using a RS232 serial interface (P1-26,

P1-4, and P1-22). This interface is used to view system status and to set the configuration of the

ADS600-B. The maintenance PC serial channel is fixed at 115,200 baud, 8 data, no parity, 1 stop bit.

3.7.5.6 ARINC429

The ADS600-B provides one ARINC 429 input and output (P1-8, P1-9, P1-27, and P1-28)

interface.

3.8 Post Installation Check

3.8.1 Maintenance PC Refer to the ADS600-B Maintenance Port Tutorial section for a description of how to configure the ADS600-B unit via the Maintenance Personal Computer (PC).

3.8.2 Electrical Load Analysis The ADS600-B is powered via a separate circuit breaker. For aircraft with multiple power

buses, this circuit breaker is sourced from the non-essential bus. Circuits should be protected in

accordance with guidelines in AC 43.13-1B, Chapter 11.

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An electrical load analysis should be completed on each aircraft prior to installation in accordance with AC 43.13-1B, Chapter 11.

Table 3-7: Recommended Circuit Breaker

ADS600-B/ADS600-B-B 14 VDC 28 VDC

Circuit Breaker 3 AMP 2 AMP

The circuit breaker placard should be labeled “UAT.”

3.8.3 Mounting and Wiring Check Verify that the ADS600-B is secured to the aircraft as described in section 3.5.3. Verify that both

the UAT and GPS antennas are securely cabled to the appropriate connectors as depicted in

Section 3.6.2. Verify that the display port, maintenance port and power/ground are securely

cabled to the DB37 connector of the ADS600-B. Ensure that the slide lock of the DB37 is in the

locked position. If any ADS600-B cabling is routed near the aircraft controls, verify free movement of the aircraft controls.

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3.8.4 Functional Test

3.8.5 Weight and Balance An aircraft weight and balance is required after installation of the ADS600-B. Follow the

guidelines in AC 43.13-1B, Chapter 10, Section 2. Update the aircraft equipment list indicating

the items relocated, added or removed. Table 3-8 identifies the weight of the ADS600-B equipment.

Table 3-8: ADS600-B Weights

Item Weight

ADS600-B Only 1.5 lbs

ADS600-B with Mounting brackets 1.6 lbs

4 Limitations

4.1 Traffic Display

5 Troubleshooting

6 Maintenance

6.1 Altitude Source The altitude source provide to the ADS600-B must be tested and inspected every 24 months as

referenced in FAR 91.411

6.2 Calibration There are no user-serviceable adjustments. There are no periodic maintenance functions to be

performed on the ADS600-B product.

6.3 Tune-Up The ADS600-B is tuned at the factory. No tune-up procedure or servicing is required by the user.

6.4 Battery Replacement The internal GPS/WAAS receiver utilizes a lithium cell battery to store the GPS Almanac when

the unit is not in operation. The lithium battery has an approximate service life of 7 years. The

unit should be sent back to the factory for battery replacement every 7 years.

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If the battery is not replaced per this interval, and becomes discharged, the ADS600-B will still

remain fully functional and accurate; however the GPS acquisition time (during initial turn-on)

will be increased.

6.5 Cleaning The ADS600-B does not require regular cleaning.

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Product Registration

Record the serial number of your unit here: ____________________________________

Please help us better support you by connecting to the NavWorx website (www.navworx.com)

and completing the online product registration. Select the Product Registration link on the home

page. You’ll need to provide your product serial number when registering your unit.

http://www.navworx.com/

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ADS600-B Maintenance Port Tutorial

ASSUMPTIONS

This tutorial assumes that the ADS600-B is connected to a Personal Computer (PC) which is running a terminal emulator such as TeraTerm . The TeraTerm terminal emulator can be downloaded from:

http://sourceforge.jp/projects/ttssh2/downloads/50074/teraterm-4.68.exe/

The baud rate of the terminal emulator must match that of the ADS600 maintenance port. The terminal emulator is configured for: baud rate 115200 bps, 8 bits, 1 stop bit, no parity and no flow control. Refer to the Interconnect Diagram: ADS600 Maintenance Port to Computer section for a diagram of the ADS600 maintenance port to PC serial port connection. Refer to the TERATERM section for a description on how configure the terminal emulator.

The aircraft should be located outside so as to allow the ADS600-B to receive the best GPS reception.

Unless otherwise noted, the commands described in this manual apply to both the ADS600 Receiver and ADS600-B Transceiver units.

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POWERING UP THE ADS600-B

When the ADS600-B powers up, it will send a power up message to the terminal emulator display. See Figure A below for an example of the power up message.

Figure A: ADS600-B Power Up Message

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ADS600-B COMMAND FORMAT ADS600-B maintenance port commands fall into 4 categories:

1) SET commands that allow the user to configure the ADS600-B

2) READ commands that display the status or configuration of the ADS600-B,

3) MAP commands that map a display protocol to a display port, and

4) ENABLE|DISABLE commands that enable or disable ADS600-B features.

Some commands are repeatable, as opposed to one-time commands. One-time commands elicit a

single response from the ADS600-B. Repeatable commands are those whose repetition rate can be

selected by the user and will display information at the repetition rate provided until the user interacts

to stop the display. An example of a repeatable command is READ GPS 2. This command displays the

reception status of the GPS receiver every 2 seconds. An example of a one-time command is READ GPS

ALL. This displays the reception status of the GPS receiver one time.

MAINTENANCE PORT HELP COMMANDS contains a list of the ADS600-B commands. Also, entering the HELP command will list all of the available commands. The following sections describe some of the more commonly used ADS600-B commands.

MAINTENANCE PORT TIPS contains tips on entering maintenance port commands.

CONFIGURING ICAO ADDRESS It is required to set the ICAO address for your aircraft. Go to the www.faa.gov website and find your aircrafts Mode-S code. This number is in octal format. Use an appropriate calculator to convert this octal number to a hex number. Use the SET ICAO 0x<hex_number> command to set your ICAO address. Use either READ ICAO or READ ALL command to verify that your ICAO is correctly set.

http://www.faa.gov/

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CONFIGURING ADS600-B FOR TRAFFIC/WEATHER DISPLAY DEVICES To configure the ADS600-B traffic and weather display port, the port type and speed, and the type of protocol to be mapped to the display port must be specified. For example, to configure the ADS600-B traffic and weather output for the SkyVision Extreme, the following commands would be entered:

SET PROTOCOL SKY MAP SKY RS232 SET BAUD RS232 115200

Since the TIS-A protocol has a dedicated port on the ADS600-B it is possible to output traffic to the TIS-A port, as well as, the serial display port. For example, to configure the ADS600-B traffic and weather output for the SkyVision Extreme and a TIS-A display (such as the Garmin® GPSMAP 496), the following commands would be entered (note the baud rate is only applicable to the SkyVision display as the TISA is always 9600):

SET PROTOCOL SKY TISA MAP SKY RS232 SET BAUD RS232 115200 The READ ALL command can be used to verify the correct display port configuration.

The ADS600-B supports several display protocols and display port types. MAINTENANCE PORT HELP

COMMANDS lists the protocols specified by the SET PROTOCOL type, the baud rates for the SET BAUD RS232|RS422 baud-rate command, and the display-protocol to port-mapping options of the MAP protocol port-type command.

ENABLING COMPOSITE TIS (OPTIONAL) If the ADS600-B is wired to accept TIS-A traffic sent from a Mode S transponder, then Composite TIS must be enabled. Enabling Composite TIS will allow the ADS600-B to forward both TIS-A traffic and UAT traffic to the configured traffic display devices. Enter the ENABLE COMPTIS command to enable Composite TIS. Enter DISABLE COMPTIS to disable the Composite TIS command.

PRESSURE ALTITUDE INPUT Provide the ADS600-B with a pressure altitude input. This can be accomplished with either the dedicated serial input, or if the unit has the optional ARINC-429 interface, it will take Arinc label 203.

If the ADS600-B is not configured to use a pressure altitude encoder input, it uses the geometric altitude (GPS altitude) for all altitude references. The geometric and pressure altitudes may differ by many hundreds of feet. This becomes critical when determining how close a traffic target is to your ownship. Today, all traffic targets report pressure altitude to ATC (via the aircrafts altitude encoder). If the ADS600-B is using the geometric altitude for its ownship altitude reference, the accuracy of the altitude distance measure of a traffic target to the ownship altitude may be inaccurate by many hundreds of feet. To confirm that the pressure altitude encoder input is configured and indicates the correct pressure altitude, enter the READ ALL command and verify that the PRIMARY altitude indicates the pressure altitude source.

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DETERMINING GPS RECEPTION

To determine if the ADS600-B is receiving signals from the GPS constellation the user may enter either a repeatable or one-time GPS command. The repeatable command format is READ GPS num_of_seconds, where num_of_seconds can be specified from 1 to 30 seconds. For example if READ GPS 5 is entered, the GPS constellation status will be displayed every 5 seconds. The one-time command format is READ GPS ALL. This command will display the GPS constellation status one time.

Figure B shows the display output of the READ GPS 5 command. To determine whether you have good GPS satellite reception verify that the #SVs (Space Vehicle) is greater than or equal 7. When “DGPS Corrections” is displayed WAAS is enabled.

#SVs reporting less 7 may indicate that your GPS antenna and/or cable may need maintenance.

Figure B: READ GPS 5 Command Output

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MONITORING TRAFFIC OUTPUT

To verify that the ADS600-B is receiving traffic messages from other UAT equipped aircraft and/or ADS-R ground stations enter the READ TM number_of_seconds command. A one second repetition rate is recommended since the traffic list is updated once per second.

Figure C shows an output of the READ TM 1 command. Referring to the figure, the number following the AL: indicates the number of traffic targets in the traffic list that have been sent to the traffic display device. Likewise, the number following the UL: indicates the number of weather uplink messages that have been sent to the display device.

Figure C: READ TM 1 Command Output

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VIEW CURRENT ADS600-B CONFIGURATION & STATUS

The READ ALL command displays the current status and configuration of the ADS600-B. Figure D shows the output of the READ ALL command.

Figure D: READ ALL Command Output

VERIFYING ADS600-B TO TRAFFIC DISPLAY INTERFACE

To verify that the ADS600-B is correctly connected to your traffic display device(s) enable the ADS600-B simulation mode. To do this, enter ENABLE SIM at the terminal emulator input. Your display device should display 1 traffic target. If your ownship’s heading is north then the traffic targets should be displayed at 0⁰, 45⁰ and 90⁰. Note, while in simulation mode the ADS600-B is still receiving UAT signals from other UAT equipped aircraft and the ADS-B ground stations so you may see more than 3 traffic targets on your traffic display device.

The simulation mode is disabled either by cycling power on the ADS600-B or entering the DISABLE SIM command. Remember to disable the simulation mode prior to flying.

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UPGRADING ADS600-B SOFTWARE

Power up the ADS600-B, connect the maintenance port and run the terminal program (TeraTerm).

Verify that the ADS600-B powered up correctly by viewing the startup info on the terminal program. It should look something like this:

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Save the ADS600-B release to your PC. The following example shows where the ADS600-B releases are saved:

Figure E: ESTABLISH ADS600-B SOFTWARE RELEASE DIRECTORY ON PC

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Now type in the “SET LOADER” command. The terminal should look something like this:

Figure F: SET LOADER COMMAND

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After the “READY FOR FILE TRANSFER” message appears, send the attached “flash” file (file with the extension of .flash). Using the TeraTerm program, browse to the flash file that will be loaded. TeraTerm should look something like this:

Figure G: TeraTerm SELECT FILE TO TRANSFER TO ADS600-B

From the terminal program, send this file to the ADS600-B just once. To send the file, select “Open”.

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The file takes about 3 minutes to load. During this time, the terminal program will display an increasing number of “.” characters:

Figure H: ADS600-B FILE TRANSFER STATUS

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When the entire file is downloaded to the ADS600-B, it will then erase and reprogram its internal memory. This is indicated on the terminal program by:

Figure I: ADS600-B PROGRAMMING STATUS

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The ADS600-B now instructs that the power should be cycled (turned off, then on). When powered up, the ADS600-B will show its startup screen, and you should verify that the new software release number is displayed (see Figure A). That’s it! Your ADS600-B is now ready for flight!

Figure J: POWER CYCLE ADS600-B

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TERATERM

DOWNLOAD:

http://sourceforge.jp/projects/ttssh2/downl

oads/50074/teraterm-4.68.exe

ABOUT TeraTerm:

TeraTerm 4.6.8 is the latest version as of this document release.

After launching TeraTerm go to the Setup/Terminal page and set both the Transmit and Receive New Line to CR+TX. Also, set the Terminal ID to VT320. Verify that Local Echo is selected.

Figure K: TeraTerm TERMINAL SETUP

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The baud rate of the terminal emulator must match that of the ADS600-B maintenance port so go to Setup/Serial Port and use the COM port of your choice configured for: baud rate 115200 bps, 8 bits, 1 stop bit, no parity and no flow control.

Figure L: TeraTerm PORT SETUP

These properties assume COM 1 port. If your computer is using another port, you should modify the “Port: COM1” selection above.

2011-07-04 P/N: 240-0008-00-14


To log the output of the ADS600-B unit go to the TeraTerm Log page and select the file to save the output:

Figure M: LOG ADS600-B OUTPUT TO A FILE

2011-07-04 P/N: 240-0008-00-14


MAINTENANCE PORT TIPS

This section lists ADS600-B maintenance port tips.

To stop the display of a repeating command press any key “A through Z” and then press enter.

The ADS600-B maintenance port has no editing functionality (such as backspace, etc.). When a

command doesn’t appear to work, press enter several times and then reenter the command.

2011-07-04 P/N: 240-0008-00-14


MAINTENANCE PORT HELP COMMANDS

Type HELP command to get list of available maintenance commands.

READ Commands

Command Option Description

HELP List maintenance commands.

READ ALL Display all pertinent status and configuration for unit.

READ PORTS Display mapping of protocol to RS232/RS422 ports.

READ GPS ALL Display GPS configuration and status.

READ GPS SV Display GPS service vehicle status.

READ GPS <seconds> Display GPS statistics at an interval as specified by seconds.

READ ICAO Display aircraft 24-bit ICAO address.

READ OWNSHIP Display ownship message.

READ TM <seconds> Display traffic manager information at an interval as specified by

<seconds>.

READ UM <seconds> Display uplink manager (FIS-B) information at an interval as specified

by <seconds>.

DISPLAY Commands


DISABLE COMPTIS Disable Composite-TIS mode.

ENABLE COMPTIS Enable Composite-TIS mode.

MAP <SKY|PASS|TA|A429S> <RS232|RS422> Map protocols to physical port.

SET BAUD ARINC429 <LOW|HIGH> Set ARINC429 clock speed.

SET BAUD RS232 <9600|19200|38400|57600|115200> Set baud rate for RS232 display port.

SET BAUD RS422 <9600|19200|38400|57600|115200> Set baud rate for RS422 display port.

SET FIS [number] Set maximum number of FIS-B messages sent to the display.

SET FIS NRST <ALL|NRST> Display FIS-B messages received from nearest ground station or

display FIS-B messages received from all ground stations.

SET MAXDIST [x.y] Set maximum distance in 1/10ths

of a nautical mile for traffic targets.

Traffic targets that are greater than this distance from the ownship

location will not be passed on to the display(s).

SET MAXALT [feet] Set maximum vertical distance in feet for traffic targets. Traffic targets

that are greater than this distance from the ownship location will not

be passed on to the display(s).

SET PROTOCOL <PASS|TA|A429|SKY|NONE> |

<TISA|A429|A429S>

Enter 1 or 2 protocols.

2011-07-04 P/N: 240-0008-00-14


TRANSMITTER Commands


ENABLE CSID Enable call sign identification flag logic.

DISABLE CSID Disable call sign identification flag logic.

ENABLE PALT Enable pressure altitude input.

DISABLE PALT Disable pressure altitude input.

ENABLE TX Enable UAT transmitter.

DISABLE TX Disable UAT transmitter.

SET CALLSIGN <1-8 character callsign> Assign aircraft call-sign. The call-sign may not exceed 8 characters.

Must be Alpha-Numeric characters only. No other characters

allowed.

SET CAT <NOTYPE | LIGHT | SMALL | LARGE |

VERYLARGE | HEAVY | MANEUVERABLE |

ROTORCRAFT | GLIDER |LIGHTERTHANAIR |

PARACHUTIST | ULTRALIGHT | UAV |

SPACEVEHICLE | EMERGENCY | SERVICE |

POINTOBSTACLE |CLUSTEROBSTACLE |

LINEOBSTACLE>

Assign aircraft category to one of the following categories.

SET GPSANT <left|right> <x.y> Set GPS antenna lateral axis [left or right of centerline] position in

meters.

SET GPSANT nose <x.y> Set GPS antenna longitudinal axis [from nose] position in meters.

SET GS <knots> Assign speed in knots which determines when aircraft is airborne.

SET ICAO <hexadecimal> Assign the aircraft’s ICAO address in a hexadecimal format.

http://www.smalluas.com/download/ICAO_Annex_10_Volume_III.p

df

SET LENGTH <x.y> Set length of aircraft in meters.

SET WIDTH <x.y> Set width of aircraft in meters.

TRANSMITTER (Pilot Input) Commands


SET EMERGENCY <NONE | GENERAL | MEDICAL |

MINFUEL | NOCOMM | HIJACK | ACFTDOWN>

Set emergency code.

SET FLIGHTID O:<octal-number> Set flight ID as an octal 4 to 6 digit number. E.g.

SET FLIGHTID O:1200

IDENT Start IDENT. Mode status message is transmitted for 20 +/- 4

seconds.

ENABLE SAA Enable transmission of the temporary self-assigned address. The

self-assigned address will be transmitted instead of the ICAO

address.

DISABLE SAA Disable transmission of the temporary self-assigned address. The

ICAO address will be transmitted instead of the self-assigned

address.

2011-07-04 P/N: 240-0008-00-14


UTILITY Commands


RESET Reset unit.

ENABLE SIM Enable simulation mode.

DISABLE SIM Disable simulation mode.

SET GPSSRC <INT|A743> Set source of GPS: internal or external (ARINC 743A).

SET LOADER Used for updating unit software.

2011-07-04 P/N: 240-0008-00-14


VERIFYING ADS600-B CONFIGURATION

Power up the ADS600-B.

Type “READ ALL” on TeraTerm input.

Observe the output on the TeraTerm monitor. This output is saved to a log file that you

specified above when logging was enabled.

Verify the ICAO address. If the ICAO address is not correct, set the address using the SET

ICAO <hexadecimal number> as described in the CONFIGURING ICAO ADDRESS section.

Verify the aircraft category. If the aircraft category is incorrect, set the category using

the SET CAT <category> command as described in the MAINTENANCE PORT HELP

COMMANDS.

Verify the aircraft callsign. If the aircraft callsign is incorrect, set the callsign using the

SET CALLSIGN <8 characters> command as described in the MAINTENANCE PORT HELP

COMMANDS.

Verify that the flight ID is set to 1200. If the flight ID is not set to 1200, use SET FLIGHTID

O:<octal number> command as described in the MAINTENANCE PORT HELP COMMANDS.

Verify that the transmitter is enabled. WARNING: If the transmitter is enabled, the UAT

antenna must be connected to the ADS600-B; otherwise damage to the ADS600-B will

occur and your warranty will not be honored. If the transmitter is not enabled, use the

ENABLE TX command as described in the MAINTENANCE PORT HELP COMMANDS.

If a pressure altitude encoder is connected to the ADS600-B, the output of READ ALL

command will indicate the PRIMARY SOURCE is PRESSURE and the SECONDARY SOURCE

is GEOMETRIC.

Type READ GPS ALL command. The DETERMINING GPS RECEPTION section describes how to

interpret the GPS reception status. Verify that the ADS600-B reports good GPS reception.

2011-07-04 P/N: 240-0008-00-14


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2011-07-04 P/N: 240-0008-00-14


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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: Display Port

AD

S6

00

Main

ten

an

ce P

ort

TX

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tena

nce

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rt R

X

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inte

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ce P

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24

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pla

y G

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d

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pla

y T

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ING

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0 A

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600 Maintenance Port to Computer

AD

S6

00

Ma

inte

na

nce

Po

rt T

X

Ma

inte

na

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Po

rt R

X

Ma

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24

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/09

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4

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: Composite-TIS™

ADS600

NOTES:

1. ALL WIRES 24 AWG OR LARGER UNLESS OTHERWISE SPECIFIED.

2. P1: 37-PIN D-SUB, MALE CONNECTOR.

GTX330

429 In 1B

429 In 1A

ARINC 429 Out 2B

ARINC 429 Out 2A

28

9

28

30

TWISTED SHIELDED TWO

CONDUCTOR SHIELD

TERMINATED TO GROUND

P1

In addition to receiving and processing ADS-B

FIS-B and TIS-B messages, the ADS600 may be

configured for Composite-TIS™. In this

configuration, the ADS600 outputs both TIS-A

and TIS-B traffic to a compatible display: traffic is

the combination of TIS-A targets (from a Mode-S

transponder) when in Mode-S coverage, as well

as TIS-B targets when in ADS-B coverage.

NavWorx®, Inc.3906 Industrial Street, Suite 100 Rowlett, TX 75088

www.navworx.com

Composite-TIS™ Interconnect Diagram

Rev Date Description

-

A

04/14/09 Initial Release

08/29/10 Added Diagram Headers

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600 to AFS

AD

S60

0-B

Main

ten

ance P

ort

TX

Ma

inte

na

nce

Port

RX

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inte

nan

ce P

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S S

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al

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DB

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em

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Conn

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TE

S:

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R L

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5

D

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4

9 10

11

11

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600 to AFS (TIS Traffic)

AD

S6

00

Main

ten

ance P

ort

TX

Ma

inte

na

nce

Port

RX

Ma

inte

nan

ce P

ort

Gro

und

P1

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AF

S S

eri

al

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rt 2

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GRT

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GRT HX/HS/WS (TIS Traffic)

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: T

NC

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IAL

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R (

GP

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P2

P3

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ten

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6

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et,

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ite

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0 R

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50

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o G

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HX

/HS

/WS

Inte

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nn

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Tra

ffic

In

terf

ac

e

Re

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ate

De

sc

rip

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n

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1/1

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itia

l R

ele

ase

Se

ria

l O

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ut 6

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8

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ato

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Su

pp

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n O

ut

Su

pp

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sp

on

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r

Su

pp

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pu

t

UA

T In

dic

ato

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9

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nce

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rt

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be

r

10

10

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: GNS 480 ARINC 743A Position Source

-

ADS600

NOTES:


GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH.

GNS 480 ARINC 429 #1 OUT (P5-4/24) MAY BE USED INSTEAD OF

429 #2 (P5-5/25) OUT.

2

3

P1: 37-PIN D-SUB, MALE CONNECTOR

GNS 480

429 In 1B

429 In 1A

ARINC 429 Out 2B

ARINC 429 Out 2A

28

9

P5-25

P5-5


CONDUCTOR SHIELD


2

743A Time Mark In +

743A Time Mark In -

21P1-19

P1-17

Time Mark Out +

Time Mark Out -

32


www.navworx.com

GNS 480 ARINC 743A Position Source


CONDUCTOR SHIELD



A

04/14/09 Initial Release

08/29/10 Added Diagram Headers

-

B 01/28/11 Identified GNS 480 connectors

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GNS 480 Traffic (ARINC 429)

AD

S6

00

Ma

inte

na

nce

Po

rt T

X

Ma

inte

na

nce

Po

rt R

X

Ma

inte

na

nce

Po

rt G

rou

nd

P1

264 22

DB

9 F

em

ale

Co

nn

ecto

r 3 2 5

NO

TE

S:

1. A

LL

WIR

ES

24

AW

G O

R L

AR

GE

R U

NL

ES

S O

TH

ER

WIS

E S

PE

CIF

IED

.

P

OW

ER

AN

D G

RO

UN

D W

IRIN

G:

WIR

E L

EN

GT

H G

RE

AT

ER

TH

AN

12

FE

ET

2 E

AC

H 2

0 A

WG

WIR

E,

or

1 E

AC

H 1

6 A

WG

WIR

E

WIR

E L

EN

GT

H L

ES

S T

HA

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2 F

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T

1 E

AC

H 1

8 A

WG

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W

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EN

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CE

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RT

IS

RE

QU

IRE

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RS

23

2 P

OR

T

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S: 1

15

20

0 B

AU

D, 8

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O P

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ITY

, 1

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OU

NT

TH

E

MA

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EN

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CE

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RT

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AN

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ION

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CO

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GR

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OF

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RO

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US

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BR

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3

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Po

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T A

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P3

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NC

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CO

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S A

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P2

P3

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ten

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ten

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ial S

tre

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10

0 R

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X 7

50

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00

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0 T

raff

ic

(AR

INC

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9)

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ate

De

sc

rip

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n

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04/1

4/0

9In

itia

l R

ele

ase

08/2

9/1

0A

dd

ed

po

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r a

nd

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un

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g r

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en

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1/2

8/1

1A

dd

ed

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T In

dic

ato

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nd

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pp

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n O

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pp

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ran

sp

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pp

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pu

t

UA

T In

dic

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49

9

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rt

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un

d P

in n

um

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r

10

10

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GNS 480 Traffic (RS-232 TIS)

AD

S6

00

Ma

inte

na

nce

Po

rt T

X

Ma

inte

na

nce

Po

rt R

X

Ma

inte

na

nce

Po

rt G

rou

nd

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264 22

DB

9 F

em

ale

Co

nn

ecto

r 3 2 5

NO

TE

S:

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LL

WIR

ES

24

AW

G O

R L

AR

GE

R U

NL

ES

S O

TH

ER

WIS

E S

PE

CIF

IED

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P

OW

ER

AN

D G

RO

UN

D W

IRIN

G:

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E L

EN

GT

H G

RE

AT

ER

TH

AN

12

FE

ET

2 E

AC

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0 A

WG

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r

1 E

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6 A

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E

WIR

E L

EN

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S T

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N 1

2 F

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1 E

AC

H 1

8 A

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W

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QU

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2 P

OR

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20

0 B

AU

D,

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O P

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, 1

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OU

NT

TH

E

MA

INT

EN

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AN

AC

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SS

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OC

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WIL

L B

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NN

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D T

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MIN

G A

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MA

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TH

OF

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ET

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G

RO

UN

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ST

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2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to SL70 Transponder Control

ADS600-B

P1

NOTES:



THE SL70 MODE A/C TRANSPONDER HAS TWO RS-232 OUTPUT

CHANNELS: RS-232 TXD1 (PIN 5) AND, RS-232 TXD2 (PIN 22). EITHER OF

THESE OUTPUTS MAY BE CONNECTED TO P1-7 OF THE ADS600-B.

IF ALTITUDE RECEIVED OVER ARINC 429, THEN PIN 7 MAY BE USED

AS AN ALTERNATE INPUT FOR UAT CONTROL INTERFACE.

2

3

SL70

RS-232 TXD1 5 33 Transponder Control RX

2


www.navworx.com

ADS600-B to SL70 Transponder Control


A 12/30/10 Initial Release

3

RS-232 Ground 3 32 Ground


CONDUCTOR SHIELD


B 07/04/11Corrected pin number for

Transponder Control RX

4

4

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GTX 330 Transponder Control

ADS600-B

P1

NOTES:



THE GTX 330 RS-232 OUTPUT MUST BE CONFIGURED FOR „REMOTE

+ TIS.‟ THE GTX 330 HAS TWO RS-232 OUTPUT CHANNELS: RS-232 Out 1

(PIN 23) AND, RS-232 Out 2 (PIN 25). EITHER OF THESE OUTPUTS MAY BE

CONNECTED TO P1-7 OF THE ADS600-B.

CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6, TO

THE GTX 330 POWER GROUND (EITHER J3301-PIN 27 OR J3301-PIN 43).



2

3

GTX 330

RS-232 Out 2 25 33 Transponder Control RX

2


www.navworx.com

ADS600-B to GTX 330 Transponder Control



3 J3301

B 04/25/11 Added Ground Signal

32 GroundPower Ground 27

4

4

C 07/04/11Corrected pin number for


5

5

2011-07-04 P/N: 240-0008-00-14


Interconnect Diagram: ADS600-B to GTX 327 Transponder Control

ADS600-B

P1

NOTES:



CONNECT ALTITUDE ENCODER GROUND OF THE ADS600-B, P1-6,

TO THE GTX 327 POWER GROUND (EITHER J3271-PIN 13 OR J3271-PIN

25).



2

GTX 327

RS-232 Out 1 20 33 Transponder Control RX

2


www.navworx.com

ADS600-B to GTX 327 Transponder Control



3

J3271

32 GroundPower Ground 13

B 04/25/11 Added Ground Signal

3

C 07/04/11Corrected pin number for


4

4

Documents

ADS600-B Installation and User Manualgrants permission to download a single copy of this document onto a hard drive or other ... (ARINC 429) Wiring Diagram. Added wiring ... Uniquely