NavWorx ADS600-B User Manual

2010-04-20 P/N: 240-0008-00-02

ADS600-B™

Installation and User Manual

®

2010-04-20 P/N: 240-0008-00-02

Business Address: NavWorx Inc. 3906 Industrial St, Suite 100 Rowlett, TX 75088

Telephone: (888)-NAVWORX (628-9679)

Facsimile: 888- 628-9679

Email: support@NavWorx.com

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.

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Revision History

Revision

Date

Comments

01

04/20/2010

Initial release

02

05/11/2010

Revised FCC statement

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List of Effective Pages

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 is not 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

support@NavWorx.com

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

NavWorx Incorporated

RMA Number: (insert your RMA number here)

3906 Industrial St, Suite 100 Rowlett, TX 75088

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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

Definitions and Acronyms ...................................................................................................... 12

1 Accessories and Packing List............................................................................................ 13

1.1 Unpacking Equipment................................................................................................ 13

1.2 Package Contents................................................................................................ ....... 13

2 About this Manual............................................................................................................ 14

2.1 FCC Grant of Equipment Authorization ..................................................................... 14

3 Equipment Description ..................................................................................................... 14

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

3.2 Transmitter Specification ................................................................ ........................... 17

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

3.3 ................................................................................................ ...................................... 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 ................................ ................................................. 22

3.6 Electrical Connections ............................................................................................... 22

3.6.1 Connectors .......................................................................................................... 22

3.6.2 Interface Connector Definition ................................................................ ............. 23

3.6.3 I/O Connector (P1) .............................................................................................. 24

3.7 Functional Descriptions ............................................................................................. 26

3.7.1 Power .................................................................................................................. 26

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3.7.2 Discrete Outputs .................................................................................................. 26

3.7.3 Discrete Inputs .................................................................................................... 26

3.7.4 PPS Time Mark Input ................................ .......................................................... 27

3.7.5 Serial Interfaces ................................................................................................... 27

3.8 Post Installation Check............................................................................................... 28

3.8.1 Maintenance PC ................................................................................................ .. 28

3.8.2 Electrical Load Analysis ...................................................................................... 32

3.8.3 Mounting Check .................................................................................................. 32

3.8.4 Wiring Check ................................................................................................ ...... 32

3.8.5 Functional Test .................................................................................................... 32

3.8.6 Weight and Balance ............................................................................................. 32

4 Limitations ...................................................................................................................... 33

4.1 Traffic Display .......................................................................................................... 33

5 Troubleshooting ............................................................................................................... 33

6 Maintenance .................................................................................................................... 33

6.1 Altitude Source .......................................................................................................... 33

6.2 Calibration................................................................................................................. 33

6.3 Tune-Up ................................................................................................ .................... 33

6.4 Battery Replacement ................................................................ .................................. 33

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

Traffic and Weather Displays ................................................................................................. 34

Product Registration ............................................................................................................... 35

Wiring Diagrams ................................................................ .................................................... 36

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List of Tables

Table 1-1: Package Contents ......................................................................................................................................... 13

Table 1-2: ADS600-B Installation Kit Contents (P/N 210-0004-00-00) ...................................................................... 13

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

Table 3-2: Acceptable ADS600-B GPS Antennas ........................................................................................................ 20

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) ......................................................................................................................... 25

Table 3-6: ADS600-B Maintenance Commands........................................................................................................... 30

Table 3-7: Recommended Circuit Breaker .................................................................................................................... 32

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 23 Figure 3-5: 37 Pin D-Sub Male Connector (P1) 24

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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 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 SDA System Design Assurance SIL System Integrity Level STC Supplemental Type Certificate 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

240-0008-00-01

1

ADS600-B UAT Installation and User Manual

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

201-16384

8

Cable tie

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 GBTs. Data received by the ADS600-B is output to a display device.

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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): 0.7A @ 14VDC, 0.41A @ 24VDC

 UAT Performance

Regulatory: DO-282B Frequency: 978MHz Tolerance: +/- 20ppm Data Rate: 1.04167 Mbps Receiver Sensitivity: Exceeds 90%MSR@-95dBm 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

 Environmental

Operating temperature: -20°C to +55°C Storage temperature: -55°C to +85°C Temperature variation: 5°C per minute

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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

3.2 Transmitter Specification

The ADS600-B is a non-TSO device that complies with RTCA DO-282B. DO-282B compliant messages transmitted by the ADS600-B unit assign the System Integrity Level (SIL) to unknown (0) and the System Design Assurance (SDA) level to unknown (0).

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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 to compatible displays both traffic and weather information. 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 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

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

Comant

CI-420-200

TNC

Comant

CI-429-200

TNC

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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.

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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

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

3.5.5 Air Circulation and Cooling

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.

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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

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

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.

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Table 3-5: I/O Connector Pin-Out (P1)

Pin #

I/O

Name

Description

1

--

RESERVED

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

10

--

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 Fail Out

UAT Fail Output (active low)

15 I TCAS RA Active In

TCAS Resolution Advisory Active Discrete In (active low)

16

--

RESERVED

17

--

RESERVED

18

--

Power +

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

19

--

Power +

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

20

--

RESERVED

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

26

--

RESERVED

27 O 429 OUT 1A

ARINC 429 Output Channel 1A

28 I 429 IN 1B

ARINC 429 Input Channel 1B

29

--

RESERVED

30 O RS422 TX +

RS422 display channel data output +

31 I RS422 RX -

RS422 display channel data input -

32

--

RESERVED

33 I TCAS Operational In

TCAS Operational Discrete Input (active low)

34 I Air/Ground In

Air / Ground Discrete Input (active low)

35 O Suppression Output

Suppression Output (active high)

36 I Power Ground

Main Aircraft Power Ground

37 I Power Ground

Main Aircraft Power Ground

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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 Fail Indicator

The UAT Fail Out (P1-14) is used to indicate the status of the ADS600-B receiver. UAT Fail 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 reserved for future use and is intended to suppress other Lband equipment (such as a transponder) when the UAT transmits. It will provide a high signal (Vin – 1.5V) 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

3.7). 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 in the air. Otherwise, a grounded

Air/Ground In indicates that the aircraft is on the ground.

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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 P1-3 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 3.7) 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

3.7) 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 3.7) 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 3.7) 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 (P1-3, 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 38,400 baud, 8 data, no parity, 1 stop.

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

3.8.1.1 Using Maintenance Port with a Windows Terminal Emulator

For configuration and testing of the ADS600-B, a PC running a terminal emulator is required to connect to the maintenance port of the ADS600-B.

With the ADS600-B powered on and the maintenance port connected to the PC terminal emulator software, a test to determine if the emulator program is connected and working is to

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press any key – should you see the key appear on the emulator program then the ADS600-B is echoing the character.

Type “Help” to view the list of all ADS600-B commands. See Table 3-6 for the complete list of ADS600-B maintenance commands.

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3.8.1.2 Maintenance Commands

Table 3-6: ADS600-B 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

RS232

Display configuration of RS232 interface.

READ

RS422

Display configuration of RS422 interface.

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

Command

Option

Description

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

MAXDIST [x.y]

Set maximum distance in 1/10

ths

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.

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TRANSMITTER Commands

Command

Option

Description

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.

SET

CALLSIGN <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

Assign aircraft category.

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

Command

Option

Description

SET

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.

UTILITY Commands

Command

Option

Description

RESET

Reset unit.

ENABLE

SIM

Enable simulation mode.

DISABLE

SIM

Disable simulation mode.

SET

LOADER

Used for updating unit software.

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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.

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 Check

3.8.4 Wiring Check

3.8.5 Functional Test

3.8.6 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

1.5lbs

ADS600-B (optional) Mounting bracket

0.1lbs

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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.

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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Traffic and Weather Displays

Weather

Traffic

Display

Advanced Flight Systems™ Inc., http://www.advanced-flight-systems.com/

Chelton FlightLogic Synthetic Vision EFIS, http://www.cheltonflightsystems.com

GPSMAP® 396/496/495/696/695

Grand Rapids Technologies, Inc., http://www.grtavionics.com/

MountainScope™, http://www.pcavionics.com/index.jsp

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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.

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Wiring Diagrams

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ADS

600

Maintenance Port TX

Maintenance Port RX

Maintenance Port Ground

P

1

3

4

22

DB

9

Female

Connector

3

2

5

NOTES

:

1

.

ALL WIRES

24

AWG OR LARGER UNLESS OTHERWISE SPECIFIED

.

WIRING FOR MAINTENANCE PORT IS REQUIRED

.

RS

232

PORT

SETTINGS

:

115200

BAUD

,

8

-

BIT

,

NO PARITY

,

1

-

STOP BIT

,

NO FLOW

CONTROL

.

MOUNT THE MAINTENANCE PORT IN AN ACCESSIBLE

LOCATION

.

IT WILL BE CONNECTED TO A PC DURING PROGRAMMING

AND SYSTEM TESTING

.

THE MAXIMUM LENGTH OF THIS CABLE IS

25

FEET

.

GROUNDING PIGTAILS MUST NOT EXCEED

4

INCHES IN LENGTH

.

2

Maintenance Port

3

ADS

600

Maintenance

(

Serial

)

Port to

Computer Interconnect Diagram

TWISTED SHIELDED THREE

CONDUCTOR SHIELD

TERMINATED TO GROUND

DB

9

Male

Connector

3

2

5

Computer

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ADS600

NOTES:

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

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

Composite-TIS™

Interconnect Diagram

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.

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ADS600

NOTES:

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

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 ARINC 743A Position Source

GNS 480

429 In 1B

429 In 1A

ARINC 429 Out 2B

ARINC 429 Out 2A

28

9

P5-25

P5-5

TWISTED SHIELDED TWO CONDUCTOR SHIELD TERMINATED TO GROUND

2

743A Time Mark In + 743A Time Mark In -

21P1-19

P1-17

Time Mark Out + Time Mark Out -

3

2

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ADS600

Maintenance Port TX

Maintenance Port RX

Maintenance Port Ground

P1

3

4

22

DB9 Female

Connector

3

2

5

NOTES:

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

POWER AND GROUND USE 20 AWG WIRE.

WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT

SETTINGS: 115200 BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE

MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE

CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM

TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET.

GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH.

THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR

14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT

BREAKER SHOULD BE LABELED “UAT”

233

Maintenance Port

4

P1

5

3/2 AMP

AVIONICS BUS

(14/28 VDC)

AIRCRAFT

GROUND

18

19

Power +

2

UAT

P1: 37-PIN D-SUB, MALE CONNECTOR

P2: TNC COAXIAL CONNECTOR (UAT ANTENNA)

P3: TNC COAXIAL CONNECTOR (GPS ANTENNA)

P2

P3

GPS

UAT

Top GPS Antenna

Bottom UAT Antenna

RG400

6

7

20AWG

GNS 480 Traffic (ARINC 429)

GNS 480

ARINC 429 In 3B

ARINC 429 In 3A

8

27

P5-29

P5-9

THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING

CONNECTORS, MUST BE LESS THAN 10dB.

THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING

CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE

LENGTH TO 15 FEET.

IF THE ARINC 429 TRAFFIC OPTION IS CONFIGURED FOR THE

GNS 480, THE GNS 480 SERIAL TIS OPTION IS NOT AVAILABLE.

5

6

7

8

TWISTED SHIELDED TWO

CONDUCTOR SHIELD

TERMINATED TO GROUND

TWISTED SHIELDED THREE

CONDUCTOR SHIELD

TERMINATED TO GROUND

Power Ground 37

Power Ground 36

429 Out 1A

429 Out 1B

8

Altitude

Encoder

TX

Ground

Altitude Encoder RX

Altitude Encoder Ground

7

6

4

***ALTITUDE ENCODER INPUT REQUIRED***

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ADS600

Maintenance Port TX

Maintenance Port RX

Maintenance Port Ground

P1

3

4

22

DB9 Female

Connector

325

NOTES:

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

POWER AND GROUND USE 20 AWG WIRE.

WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT

SETTINGS: 115200 BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE

MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE

CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM

TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET.

GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH.

THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR

14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT

BREAKER SHOULD BE LABELED “UAT”

233

Maintenance Port

4

P1

5

3/2 AMP

AVIONICS BUS

(14/28 VDC)

AIRCRAFT

GROUND

18

19

Power +

2

UAT

P1: 37-PIN D-SUB, MALE CONNECTOR

P2: TNC COAXIAL CONNECTOR (UAT ANTENNA)

P3: TNC COAXIAL CONNECTOR (GPS ANTENNA)

P2

P3

GPS

UAT

Top GPS Antenna

Bottom UAT Antenna

RG400

6

7

20AWG

GNS 480 Traffic (RS-232 TIS)

GNS 480

RS232 RxD6

6

25

P5-42

P5-2

THE GPS ANTENNA COAXIAL CABLE LOSS, INCLUDING

CONNECTORS, MUST BE LESS THAN 10dB.

THE UAT ANTENNA COAXIAL CABLE LOSS, INCLUDING

CONNECTORS, MUST BE LESS THAN 3dB. LIMIT THE RG400 CABLE

LENGTH TO 15 FEET.

IF THE SERIAL TIS OPTION IS CONFIGURED FOR THE GNS 480,

THE GNS 480 ARINC 429 TRAFFIC OPTION IS NOT AVAILABLE. TISA AND ALTITUDE ENCODER INPUT SHARE THE SAME

GROUND PIN, P1-6.

10. REFER TO COMPOSITE-TIS™ DIAGRAM FOR WIRING REQUIRED

FOR COMPOSITE-TIS.

5

6

7

8

TWISTED SHIELDED TWO

CONDUCTOR SHIELD

TERMINATED TO GROUND

TWISTED SHIELDED THREE

CONDUCTOR SHIELD

TERMINATED TO GROUND

Power Ground 37

Power Ground 36

TIS TX

TIS Ground

Serial Ground 6

8

Altitude

Encoder

TX

Ground

Altitude Encoder RX

Altitude Encoder Ground

7

6

4

9

***ALTITUDE ENCODER INPUT REQUIRED***

9

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ADS600

Maintenance Port TX

Maintenance Port RX

Maintenance Port Ground

P1

3

4

22

Chelton Serial

Port 3

DB9 Female

Connector

3

2

5

NOTES:

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

POWER AND GROUND USE 20 AWG WIRE.

WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT

SETTINGS: 115200 BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE

MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE

CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM

TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET.

GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH.

THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR

14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT

BREAKER SHOULD BE LABELED “UAT”

233

Maintenance Port

4

P1

4

5

3/2 AMP

AVIONICS BUS

(14/28 VDC)

AIRCRAFT

GROUND

18

19

Power +

2

UAT

P1: 37-PIN D-SUB, MALE CONNECTOR

P2: TNC COAXIAL CONNECTOR (UAT ANTENNA)

P3: TNC COAXIAL CONNECTOR (GPS ANTENNA)

P2

P3

GPS

UAT

Top GPS Antenna

Bottom UAT Antenna

RG400

6

7

20AWG

ADS600 to Chelton

ADS-B

8

THE GPS ANTENNA COAXIAL CABLE LOSS,

INCLUDING CONNECTORS, MUST BE LESS THAN

10dB.

THE UAT ANTENNA COAXIAL CABLE LOSS,

INCLUDING CONNECTORS, MUST BE LESS THAN

3dB. LIMIT THE RG400 CABLE LENGTH TO 15 FEET.

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. THIS RESTRICTS THE

CHELTON UNIT TO ONLY ADS-B CAPABILITIES.

REFER TO THE “ADS600 TO CHELTON COMPOSITE-

TIS™” DIAGRAM FOR A CONFIGURATION THAT

ALLOWS THE CHELTON TO BE CONFIGURED TO

USE WSI WX WITH COMPOSITE-TIS™.

5

6

7

8

TWISTED SHIELDED TWO

CONDUCTOR SHIELD

TERMINATED TO GROUND

TWISTED SHIELDED THREE

CONDUCTOR SHIELD

TERMINATED TO GROUND

Power Ground 37

Power Ground 36

5 Display TX

23 Ground

RS232 Datalink RX 3

Ground 24

Altitude

Encoder

TX

Ground

Altitude Encoder RX

Altitude Encoder Ground

7

6

4

***ALTITUDE ENCODER INPUT REQUIRED***

RS232 Datalink TX 45

24 Display RX

J1

CHELTON CONFIGURATON

On the “Factory Programmed Settings” page in the Chelton Limits Setup:

Datalink Receiver = ADS-B

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ADS600

Maintenance Port TX

Maintenance Port RX

Maintenance Port Ground

P1

3

4

22

Chelton Serial

Port 5

DB9 Female

Connector

325

NOTES:

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

POWER AND GROUND USE 20 AWG WIRE.

WIRING FOR MAINTENANCE PORT IS REQUIRED. RS232 PORT

SETTINGS: 115200 BAUD, 8-BIT, NO PARITY, 1-STOP BIT. MOUNT THE

MAINTENANCE PORT IN AN ACCESSIBLE LOCATION. IT WILL BE

CONNECTED TO A PC DURING PROGRAMMING AND SYSTEM

TESTING. THE MAXIMUM LENGTH OF THIS CABLE IS 25 FEET.

GROUNDING PIGTAILS MUST NOT EXCEED 4 INCHES IN LENGTH.

THE RECOMMENDED CIRCUIT BREAKER RATING IS 3A FOR

14VDC INSTALLATIONS AND, 2A FOR 28VDC INSTALLATIONS. CIRCUIT

BREAKER SHOULD BE LABELED “UAT”

233

Maintenance Port

4

P1

4

5

3/2 AMP

AVIONICS BUS

(14/28 VDC)

AIRCRAFT

GROUND

18

19

Power +

2

UAT

P1: 37-PIN D-SUB, MALE CONNECTOR

P2: TNC COAXIAL CONNECTOR (UAT ANTENNA)

P3: TNC COAXIAL CONNECTOR (GPS ANTENNA)

P2

P3

GPS

UAT

Top GPS Antenna

Bottom UAT Antenna

RG400

6

7

20AWG

ADS600 to Chelton

Composite-TIS™

8

THE GPS ANTENNA COAXIAL CABLE LOSS,

INCLUDING CONNECTORS, MUST BE LESS THAN

10dB.

THE UAT ANTENNA COAXIAL CABLE LOSS,

INCLUDING CONNECTORS, MUST BE LESS THAN

3dB. LIMIT THE RG400 CABLE LENGTH TO 15

FEET.

IN THIS CONFIGURATION, THE ADS600

OUTPUTS BOTH TIS-A AND TIS-B (COMPOSITE-

TIS™) TRAFFIC TO THE CHELTON DISPLAY:

TRAFFIC IS THE COMBINATION OF TIS-A

TARGETS (FROM THE GTX330 TRANSPONDER)

WHEN IN MODE-S COVERAGE, AS WELL AS TIS-B

TARGETS WHEN IN ADS-B COVERAGE. WITH

THIS CONFIGURATION THE CHELTON DISPLAY

DOES NOT RECEIVE FIS-B (WEATHER) FROM

THE ADS600. TO CONFIGURE THE CHELTON TO

RECEIVE FIS-B, REFER TO THE “ADS600 TO

CHELTON ADS-B” DIAGRAM.

5

6

7

8

TWISTED SHIELDED TWO

CONDUCTOR SHIELD

TERMINATED TO GROUND

TWISTED SHIELDED THREE

CONDUCTOR SHIELD

TERMINATED TO GROUND

Power Ground 37

Power Ground 36

25 TISA TX

23 Ground

RS232 TAS RX 5

Ground 26

Altitude

Encoder

TX

Ground

Altitude Encoder RX

Altitude Encoder Ground

7

6

4

***ALTITUDE ENCODER INPUT REQUIRED***

RS232 TAS TX 47

24 Display RX

J1

GTX330

429 In 1B

429 In 1A

ARINC 429 Out 2B

ARINC 429 Out 2A

28

9

28

30

CHELTON CONFIGURATON

On the “Factory Programmed Settings” page in the Chelton Limits Setup:

Datalink Receiver = WSI (if equipped)

Traffic Sensor = TCAS-I(ARINC429)

On the “ARINC429 Receive Port Settings” page in the Chelton Limits Setup:

COM23 should be set to HI speed and all columns turned OFF except for TCAS which is ON.

Note that the GTX330 provides ARINC labels for TCAS-I type function to the Chelton using 38,400 baud RS-232 connection.

NavWorx ADS600-B User Manual

Specifications and Main Features

Frequently Asked Questions

User Manual