Garmin 0104455 Users Manual

190-00587-50 January, 2012 Revision A

GTS Processor

Installation Manual

DRAFT

Garmin Ltd. or its subsidiaries

Except as expressly provided herein, no part of this manual may be reproduced, copied,

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the express prior written consent of Garmin. Garmin hereby grants permission to download a

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this manual or any revision hereto is strictly prohibited.

Garmin International, Inc.

1200 E. 151st Street

Olathe, KS 66062 USA

Telephone: 913.397.8200

Aviation Panel-Mount Technical Support Line (Toll Free) 1.888.606.5482

www.garmin.com

Garmin (Europe) Ltd.

Liberty House, Bulls Copse Road

Hounsdown Business Park

Southampton, SO40 9RB U.K.

+44/ (0) 870.8501241

Garmin AT, Inc.

2345 Turner Rd., SE

Salem, OR 97302 USA

Telephone: 503.581.8101

RECORD OF REVISIONS

Revision Revision Date Description

A 01/06/2012 Initial Release

Page A GDR 66 Installation Manual Revision A 190-00587-50

INFORMATION SUBJECT TO EXPORT CONTROL LAWS

DRAFT

This document may contain information which is subject to the Export Administration Regulations ("EAR") issued by the United States Department of Commerce (15 CFR, Chapter VII, Subchapter C) and which may not be exported, released, or disclosed to foreign nationals inside or outside of the United States without first obtaining an export license. The preceding statement is required to be included on any and all reproductions in whole or in part of this manual.

WARNING

This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This Notice is being provided in accordance with California's Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/prop65

CURRENT REVISION DESCRIPTION

Revision

A All All Initial release

Page

Number(s)

Section

Number

DOCUMENT PAGINATION

Section Page Range

Table of Contents i – viii

Section 1 1-1 – 1-10 Section 2 2-1 – 2-10 Section 3 3-1 – 3-22

Section 4 4-1 – 4-14 Appendix A A-1 – A-4 Appendix B B-1 – B-10

Description of Change

GTS Processor Installation Manual Page i 190-00587-50 Revision A

TABLE OF CONTENTS

DRAFT

PARAGRAPH PAGE

Section 1 GENERAL DESCRIPTION .............................................................1-1

1.1 Introduction...................................................................................................................... 1-1

1.2 Equipment Description .................................................................................................... 1-1

1.2.1 GTS Processor Configuration Options.................................................................................1-2

1.3 Interface Summary...........................................................................................................1-2

1.4 Technical Specifications .................................................................................................. 1-2

1.4.1 Environmental Qualification Form.......................................................................................1-2

1.4.2 Physical Characteristics........................................................................................................1-3

1.4.3 General Specifications..........................................................................................................1-3

1.4.4 Power Requirements.............................................................................................................1-3

1.5 Certification ..................................................................................................................... 1-4

1.5.1 GTS Processor TSO/ETSO Compliance ..............................................................................1-4

1.5.2 GTS Processor TSO/ETSO Deviations ................................................................................1-5

1.6 Reference Documents ...................................................................................................... 1-8

1.7 Aviation Limited Warranty.............................................................................................. 1-9

Section 2 INSTALLATION OVERVIEW........................................................2-1

2.1 Introduction...................................................................................................................... 2-1

2.1.1 Unit Configurations ..............................................................................................................2-1

2.1.2 Required Accessories ...........................................................................................................2-1

2.2 Installation Considerations .............................................................................................. 2-3

2.2.1 Antenna Considerations........................................................................................................2-3

2.3 Electrical Bonding ........................................................................................................... 2-3

2.4 Cabling and Wiring..........................................................................................................2-4

2.4.1 Coaxial Cable .......................................................................................................................2-4

2.5 Cooling Requirements ..................................................................................................... 2-9

2.6 Mounting Requirements ................................................................................................ 2-10

Section 3 INSTALLATION PROCEDURE.....................................................3-1

3.1 Unpacking Unit................................................................................................................ 3-1

3.2 Wiring Harness Installation ............................................................................................. 3-1

3.3 Backshell and Configuration Module Assemblies........................................................... 3-3

3.4 GA 58 Antenna Installation ............................................................................................. 3-3

3.5 Sensor Systems Incorporated Low-Profile Antenna Installation..................................... 3-3

3.6 Unit Installation ............................................................................................................... 3-3

3.7 Downloading and Installing the GTS Processor Install Tool .......................................... 3-4

3.8 Downloading and Installing the GTS Assert Log Diagnosis Tool .................................. 3-6

3.9 Post Installation Configuration & Checkout.................................................................... 3-9

3.9.1 GTS Processor Configuration/Checkout for Different Installation Types ...........................3-9

3.9.2 Using the GTS Processor Install Tool ................................................................................3-10

3.9.3 Suppression Bus I/O Check................................................................................................3-16

3.9.4 CDTI (Cockpit Display of Traffic Information) Display Setup and Configuration...........3-17

3.9.5 Calibration/Self Test...........................................................................................................3-17

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PARAGRAPH PAGE

DRAFT

3.9.6 Ramp Test and Return To Service Test..............................................................................3-20

3.9.7 Antenna Verification ..........................................................................................................3-22

3.10 Continued Airworthiness ............................................................................................. 3-23

Section 4 SYSTEM INTERCONNECTS..........................................................4-1

4.1 GTS Processor Pin Function List..................................................................................... 4-1

4.1.1 P8001 (Digital) .....................................................................................................................4-1

4.1.2 P8002 (Analog/Discrete) ......................................................................................................4-3

4.1.3 P8003 (Power Supply)..........................................................................................................4-6

4.2 Power ............................................................................................................................... 4-7

4.2.1 Aircraft Power Functions......................................................................................................4-7

4.3 Serial Data........................................................................................................................ 4-8

4.3.1 RS-232..................................................................................................................................4-8

4.3.2 RS-422..................................................................................................................................4-8

4.3.3 ARINC 429...........................................................................................................................4-9

4.3.4 Ethernet.................................................................................................................................4-9

4.3.5 USB ....................................................................................................................................4-10

4.4 Configuration ................................................................................................................. 4-10

4.4.1 Configuration Module ........................................................................................................4-10

4.5 Analog/Discrete .............................................................................................................4-10

4.5.1 Heading Input .....................................................................................................................4-10

4.5.2 Inputs From Compass System/Directional Gyros ..............................................................4-11

4.5.3 Audio ..................................................................................................................................4-12

4.5.4 Active Low Discrete Inputs................................................................................................4-12

4.5.5 Active High Discrete Inputs ...............................................................................................4-13

4.5.6 Annunciator Output ............................................................................................................4-14

4.6 Mutual Suppression Bus ................................................................................................ 4-14

Appendix A Outline and Installation Drawings .............................................A-1

Appendix B Interconnect Examples ................................................................B-1

GTS Processor Installation Manual Page iii 190-00587-50 Revision A

LIST OF FIGURES

DRAFT

FIGURE PAGE

Section 1 GENERAL DESCRIPTION .............................................................1-1

Section 2 INSTALLATION OVERVIEW........................................................2-1

Figure 2-1 GTS Processor Installation with Top and Bottom Directional Antennas ........... 2-5

Figure 2-2 GTS Processor Installation with Top Directional and

Bottom Monopole Antennas.................................................................................................. 2-5

Figure 2-3 GTS 855/GTS 825 Installation with Top Directional Antenna and

No Bottom Antenna ...............................................................................................................2-6

Figure 2-4 Heat Shrink Positioning ...................................................................................... 2-8

Figure 2-5 GTS Processor Vertical Installation Rack (Garmin P/N 011-02572-00).......... 2-10

Figure 2-6 GTS Processor Horizontal Installation Rack (Garmin P/N 115-00784-00) ..... 2-10

Section 3 INSTALLATION PROCEDURE.....................................................3-1

Figure 3-1 GTS Processor Install Tool – Installation ........................................................... 3-4

Figure 3-2 GTS Processor Install Tool – Installation ........................................................... 3-5

Figure 3-3 GTS Processor Install Tool – Installation ........................................................... 3-5

Figure 3-4 GTS Processor Install Tool – Installation ........................................................... 3-5

Figure 3-5 GTS Processor Install Tool – Installation ........................................................... 3-6

Figure 3-6 GTS Processor Install Tool – Installation ........................................................... 3-6

Figure 3-7 GTS Assert Log Diagnosis Tool – Installation.................................................. 3-7

Figure 3-8 GTS Assert Log Diagnosis Tool – Installation ................................................... 3-7

Figure 3-9 GTS Assert Log Diagnosis Tool – Installation.................................................. 3-8

Figure 3-10 GTS Assert Log Diagnosis Tool – Installation................................................ 3-8

Figure 3-11 GTS Assert Log Diagnosis Tool – Installation................................................ 3-8

Figure 3-12 GTS Processor Install Tool – Normal Tab...................................................... 3-11

Figure 3-13 GTS Processor Install Tool – Configuration Tab (GTS 825 and GTS 855)... 3-12

Figure 3-14 GTS Processor Install Tool – Upload Tab ...................................................... 3-15

Figure 3-15 GTS Processor Install Tool – Assert Tab........................................................ 3-16

Figure 3-16 Self Test ..........................................................................................................3-19

Figure 3-17 Ground Test Enable, GTS Processor Install Tool........................................... 3-20

Figure 3-18 GND TEST Softkey ........................................................................................ 3-20

Section 4 SYSTEM INTERCONNECTS..........................................................4-1

Figure 4-1 View of J8001 connector from back of unit ....................................................... 4-1

Figure 4-2 View of J8002 connector from back of unit ....................................................... 4-3

Figure 4-3 View of J8003 connector from back of unit ....................................................... 4-6

Appendix A Outline and Installation Drawings .............................................A-1

Figure A-1 GTS Processor Vertical Outline Drawing......................................................... A-1

Figure A-2 GTS Processor Vertical Installation Drawing.................................................. A-2

Figure A-3 GTS Processor Horizontal Outline Drawing..................................................... A-3

Figure A-4 GTS Processor Horizontal Installation Drawing............................................... A-4

Page iv GTS Processor Installation Manual Revision A 190-00587-50

FIGURE PAGE

DRAFT

Appendix B Interconnect Examples ................................................................B-1

Figure B-1 GTS Processor Interconnect Example Notes .....................................................B-1

Figure B-2 GTS Processor Interconnect Example................................................................B-2

Figure B-3 GTS Processor Garmin Integrated Flight Deck Interconnect Example .............B-3

Figure B-4 GTS Processor Field Approved (Retrofit) Garmin Integrated

Flight Deck Interconnect Example ........................................................................................B-4

Figure B-5 GTS Processor GNS 4XX/5XX/GMX 200 Interconnect Example....................B-5

Figure B-6 GTS Processor GMA/HSI/Altimeter Interconnect Example .............................B-6

Figure B-7 GTS Processor Dongle Cable (see Sections 3.7 and 3.8.6)................................B-7

Figure B-8 GTS Processor Discrete Interconnect Example .................................................B-8

Figure B-9 GTS Processor Configuration Module Interconnect Example...........................B-9

Figure B-10 GTS Processor Dual Transponder Interconnect Example..............................B-10

GTS Processor Installation Manual Page v 190-00587-50 Revision A

LIST OF TABLES

DRAFT

TABLE PAGE

Section 1 GENERAL DESCRIPTION .............................................................1-1

Table 1-1 Compatible Transponders..................................................................................... 1-2

Table 1-2 Configuration Options.......................................................................................... 1-2

Table 1-3 Physical Characteristics........................................................................................ 1-3

Table 1-4 General Specifications.......................................................................................... 1-3

Table 1-5 Maximum Operation Current Draw ..................................................................... 1-3

Table 1-6 Maximum Boot-Up Current Draw ....................................................................... 1-3

Table 1-7 TSO/ETSO Compliance ....................................................................................... 1-4

Table 1-8 TSO/ETSO Deviations ......................................................................................... 1-5

Table 1-9 Reference Documents........................................................................................... 1-8

Section 2 INSTALLATION OVERVIEW........................................................2-1

Table 2-1 Unit Configuration ............................................................................................... 2-1

Table 2-2 Required Accessories ........................................................................................... 2-1

Table 2-3 Connector Kits...................................................................................................... 2-2

Table 2-4 Optional Accessories............................................................................................ 2-2

Table 2-5 Antennas............................................................................................................... 2-2

Table 2-6 Configuration Module .......................................................................................... 2-2

Table 2-7 Recommended Coaxial Length ............................................................................ 2-7

Table 2-8 Coaxial Cable Set Length Tolerance.................................................................... 2-8

Section 3 INSTALLATION PROCEDURE.....................................................3-1

Table 3-1 Socket and Pin Contact Part Numbers ................................................................. 3-1

Table 3-2 Socket Contact MIL SPEC M39029/5-115 Crimp Tooling................................. 3-1

Table 3-3 Pin Contact GPN 336-00021-00 MIL SPEC M39029/58-360 Crimp Tooling.... 3-2

Table 3-4 Pin Socket Contacts GPN 336-00022-00 MIL SPEC M39029/63-368 and

GPN 336-00023-00 Crimp Tooling....................................................................................... 3-2

Table 3-5 Self Test.............................................................................................................. 3-19

Section 4 SYSTEM INTERCONNECTS..........................................................4-1

Table 4-1 P8001 Connector .................................................................................................. 4-1

Table 4-2 P8002 Connector .................................................................................................. 4-3

Table 4-3 P8002 Connector .................................................................................................. 4-6

Table 4-4 Aircraft Power ...................................................................................................... 4-7

Table 4-5 Remote Power ...................................................................................................... 4-7

Table 4-6 Power On/Off Matrix ........................................................................................... 4-7

Table 4-7 RS-232.................................................................................................................. 4-8

Table 4-8 RS-422.................................................................................................................. 4-8

Table 4-9 ARINC 429........................................................................................................... 4-9

Table 4-10 Ethernet .............................................................................................................. 4-9

Table 4-11 USB .................................................................................................................. 4-10

Table 4-12 Configuration Module ...................................................................................... 4-10

Table 4-13 26 Volt AC References..................................................................................... 4-10

Page vi GTS Processor Installation Manual Revision A 190-00587-50

TABLE PAGE

DRAFT

Table 4-14 Radar Altimeter ................................................................................................ 4-11

Table 4-15 Inputs From Compass System/Directional Gyros ............................................ 4-11

Table 4-16 Audio ................................................................................................................ 4-12

Table 4-17 Active Low Discrete Inputs.............................................................................. 4-12

Table 4-18 Active High Discrete Inputs ............................................................................. 4-13

Table 4-19 Annunciator Output.......................................................................................... 4-14

Table 4-20 Mutual Suppression Bus................................................................................... 4-14

GTS Processor Installation Manual Page vii 190-00587-50 Revision A

Page viii GTS Processor Installation Manual

DRAFT

Revision A 190-00587-50

1 GENERAL DESCRIPTION

DRAFT

1.1 Introduction

This manual presents mechanical and electrical installation requirements for installing the GTS Processor as a Traffic Advisory System (TAS) (GTS 825), Traffic Collision Avoidance System (TCAS I) (GTS 855), and Traffic Collision Avoidance System (TCAS II) (GTS 8000).

1.2 Equipment Description

The GTS Processor is a microprocessor-based Line Replaceable Unit (LRU) that uses active interrogations of Mode S and Mode A/C transponders to provide Traffic Advisories and Resolution Advisories (GTS 8000 only) to the pilot. When installed in a system the GTS Processor can be configured as a TAS (GTS

825) or can be upgraded to a TCAS I (GTS 855) or TCAS II (GTS 8000) by purchasing an enablement card from Garmin. The GTS Processor meets the TSO/ETSO requirements for the configured traffic system function (TAS, TCAS I, or TCAS II). When installed with a 1090 MHz ADS-B transmit class of equipment the GTS Processor also utilizes passive surveillance. Traffic is displayed on an external MFD via ARINC 429 and/or Ethernet High Speed Data Bus (HSDB). An aural alert is also provided to inform the crew a traffic advisory (TA) or resolution advisory (RA) (GTS 8000 only) will be displayed.

A top-mounted directional antenna is used to derive bearing of the intruder aircraft, which is displayed with relative altitude to own aircraft. Top antenna transmitted interrogations are directional, reducing the number of transponders that receive the interrogation, and thus reducing potential garble on the 1090 MHz band. For GTS 825 and GTS 855 installations, a bottom monopole or directional (highly recommended) antenna is optional. For GTS 8000 installations, a bottom monopole or directional (highly recommended) antenna is required. Bottom antenna transmit interrogations and broadcasts (GTS 8000 only) are omni directional, using a monopole antenna or a directional antenna. A bottom directional antenna installation gives the benefit of intruder bearing visibility for targets that are shaded from the top directional antenna. The target bearing accuracy may be degraded for bottom directional antenna installations on aircraft with fixed gear.

NOTE

GTS Processor installations, configured as a GTS 855 TCAS I or GTS 825 TAS, require a Garmin-approved transponder capable of receiving TCAS II broadcast data.

NOTE

GTS Processor installations, configured as a GTS 8000 TCAS II, require a GTX 3000 or other Garmin-approved RTCA DO-185A/B compatible transponder.

NOTE

The GTS Processor is not to be installed in an aircraft with a TSO-C119a-only compatible transponder.

NOTE

A co-installed mode S transponder should be connected to the mutual suppression bus, and meet the mutual suppression requirements of DO-181A or later

GTS Processor Installation Manual Page 1-1 190-00587-50 Revision A

Refer to Table 1-1 for a list of compatible transponders.

DRAFT

Table 1-1 Compatible Transponders

Capable of

GTX Transponder

Model

GTX 330/330D

GTX 330 ES/330D ES

GTX 33/33D

GTX 33 ES/33D ES

GTX 328

GTX 3000 Yes Yes Yes

1. Remote mounted transponders require a compatible controller. Contact Garmin for details.

2. Factory update is required to allow ADS-B functionality.

3. GTX Software version 6.11 or higher.

4. GTX Software version 6.10 or higher.

1.2.1 GTS Processor Configuration Options

Table 1-2 lists the GTS Processor surveillance configuration options, enabled at the time of installation.

(1)

Receiving TCAS II

Broadcast Data

(Required for GTS

Processor)

(3)

Yes

(3)

Yes

(3)

Yes

(3)

Yes

(4)

Yes

Table 1-2 Configuration Options

ADS-B Capable

RTCA DO-185A/B

Compatible

(2)

Yes

Yes No

(2)

Yes

Yes No

No No

Traffic

Model

Number

GTS 825 011-02571-00 TSO-C147 X X 400

GTS 855* 011-02571-00 TSO-C118 X X 400

GTS 8000* 011-02571-00 TSO-C119c X X 400

*Requires upgrade using GTX Processor TCAS I/TCAS II Enablement Process. See Section XXX for instructions.

1.3 Interface Summary

The GTS Processor is designed as an open architecture system that uses typical ARINC 429, RS-232, and Ethernet communications interfaces.

1.4 Technical Specifications

1.4.1 Environmental Qualification Form

It is the responsibility of the installing agency to obtain the latest revision of the GTS Processor Environmental Qualification Form. To obtain a copy of this form, see the dealer/OEM portion of the Garmin web site (www.garmin.com number:

Garmin Part

Number

GTS Processor Environmental Qualification Form, Garmin part number 005-00630-02

Applicable

TSO

). This form is available directly from Garmin under the following part

Advisory

System

(TAS)

Traffic Alert and Collision

Avoidance

System

(TCAS I)

Traffic Alert and Collision

Avoidance

System

(TCAS II)

1090 ES

ADS-B

Receiver

Transmit

Power

(Watts)

Page 1-2 GTS Processor Installation Manual Revision A 190-00587-50

1.4.2 Physical Characteristics

DRAFT

Table 1-3 Physical Characteristics

Characteristics Specifications

GTS Processor Width w/out rack 3.42 inches (86.9 mm)

GTS Processor Height w/out rack 6.25 inches (158.8 mm)

GTS Processor Width with vertical rack 3.67 inches (93.1 mm)

GTS Processor Height with vertical rack 6.74 inches (171.1 mm)

GTS Processor Depth with vertical rack 15.48 inches (396.7 mm)

GTS Processor Width with horizontal rack 6.42 inches (163.1 mm)

GTS Processor Height with horizontal rack 4.10 inches (104.1 mm)

GTS Processor Depth with horizontal rack 14.79 inches (375.7 mm)

GTS Processor Depth w/Connector Kit 14.78 inches (375.4 mm)

GTS Processor Unit Weight w/out Connector Kit 11.30 lbs (5.13 kg)

GTS Processor Unit Weight with Connector Kit w/Vertical Rack 12.65 lbs (5.74 kg)

GTS Processor Unit Weight with Connector Kit w/Horizontal Rack 13.25 lbs (6.01 kg)

1.4.3 General Specifications

Table 1-4 contains general specifications. For detailed environmental specifications, see the Environmental Qualification Form.

Table 1-4 General Specifications

Characteristics Specifications

Operating Temperature Range -55°C to +70°C.

Humidity 95% non-condensing

Altitude Range -1,500 ft to 55,000 ft

Software Compliance RTCA/DO-178B level B

Hardware Compliance RTCA/DO-254 Level B

Environmental Compliance RTCA/DO-160F

1.4.4 Power Requirements

Tables list the power requirements for the GTS Processor

Table 1-5 Maximum Operation Current Draw

Characteristics Specifications

GTS Processor Power Consumption

Table 1-6 Maximum Boot-Up Current Draw

Characteristics Specifications

GTS Processor Boot-Up Current Draw

2.5 A max operating at 28.0 Vdc

5.0 A max operating at 14.0 Vdc

2.5 A at 28.0 Vdc for 700 ms

5.0 A at 14.0 Vdc for 700 ms

GTS Processor Installation Manual Page 1-3 190-00587-50 Revision A

1.5 Certification

DRAFT

The conditions and tests required for TSO/ETSO approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or within a specific type or class of aircraft to determine that the aircraft installation conditions are within the TSO/ETSO standards. TSO/ ETSO articles must have separate approval for installation in an aircraft. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements.

The following tables provide a list of applicable TSO/ETSOs for the GTS Processor.

1.5.1 GTS Processor TSO/ETSO Compliance

When installed as a system, the GTS Processor, which includes a GA 58 (or other Garmin approved antenna), and a CDTI (Cockpit Display of Traffic Information) comprise what Garmin considers to be a minimum generic GTS Processor system installation. The GTS Processor lacks a display and by itself is an incomplete system and cannot completely meet the requirements of TSO-C119c/ETSO-C119c, TSO-C118/ETSO-C118 or TSO-C147/ETSO-C147.

Table 1-7 TSO/ETSO Compliance

GTS

Processor

Configuration

Traffic Alert and Collision

GTS 8000

GTS 855

GTS 825

GTS 8000,

GTS 855, and

GTX 825

*Equipment is capable of TSO-C166b/ETSO-C166a Class A1S/Type 1 Receiving Only per

RTCA/DO-260B when installed with a single antenna.

*Equipment is capable of TSO-C166b/ETSO-C166a Class A1/Type 1 Receiving Only when installed with

diversity antennas.

*The Class level is dependent upon the installation.

Avoidance System (TCAS II) Airborne Equipment

Traffic Alert and Collision Avoidance System (TCAS I) Airborne Equipment

Traffic Advisory System (TAS) Airborne Equipment

Extended Squitter Automatic Dependent Surveillance – Broadcast (ADS-B) and Traffic Information Service – Broadcast (TIS-B) Equipment Operating on the Radio Frequency of 1090 Megahertz (MHz)

Function TSO/ETSO Category

TSO-C119c

ETSO-C119c

TSO-C118

ETSO-C118

TSO-C147

ETSO-C147

TSO-C166b†

ETSO-C166a†

Class A

Class A1S/

Type 1

Receiving

Only*

Class A1/

Type 1

Receiving

Only*

Applicable

LRU SW Part

Numbers

All

006-B1244-0( )

through

006-B1244-2( )

except

006-B1244-00

through

006-B1244-03

All

006-B1224-0( )

through

006- B1224-2( )

except

006- B1224-00

through

006-B1224-03

All

006-B1224-0( )

through

006- B1224-2( )

except

006- B1224-00

through

006- B1224-03

All

006- B1224-0( )

through

006- B1224-2( )

except

006-B1224-00

through

006-B1224-03

Applicable

CLD Part Numbers

006-C0081-2( )

Page 1-4 GTS Processor Installation Manual Revision A 190-00587-50

NOTE

DRAFT

A statement identifying whether the installation is TSO-C166b/ETSO-C166a Class A1S/Type 1 Receiving Only or TSO-C166b/ETSO-C166a Class A1/Type 1 Receiving Only, per RTCA/DO-260B, should be included in the ship's log during Installation.

† Installation of this Receiving Only class of equipment is intended only for those aircraft in which a 1090 MHz ADS-B transmit class of equipment, or other complementary ADS-B link transmit class of equipment (such as UAT), is already installed. When no such ADS-B link transmit class of equipment is installed, the ADS-B receive functionality is disabled by disabling the 'ADSB TX Capable' configuration option (see section 3.9.2).

1.5.2 GTS Processor TSO/ETSO Deviations

Table 1-8 TSO/ETSO Deviations

TSO/ETSO Deviation

1. Garmin was granted a deviation from TSO-C118 section a.(1) to use RTCA DO-197A, instead of RTCA DO-197 as the Minimum Performance Standard

2. Garmin was granted a deviation from TSO-C118 section a.(2) to use RTCA DO-160F, instead of RTCA DO-160B as the standard for Environmental Conditions and Test Procedures for Airborne Equipment.

3. Garmin was granted a deviation from TSO-C118 section a.(3)(i) to use RTCA DO-178B instead of RTCA DO-178A.

4. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185B section 2.2.3.3 instead of the requirement of RTCA DO-197A section 2.2.3.2.1.

TSO-C118

5. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.5 to use the “Mode C Only All-Call” format specified by RTCA DO-185B section 2.2.3.8.1 instead of the “Mode C” format for ATCRBS interrogations.

6. Garmin was granted a deviation from RTCA DO-197A section 2.2.6 to use selective Mode S interrogations following all the applicable protocols for Mode-S surveillance interrogations in the NAS as stated in DO-185B and DO-181D.

7. Garmin was granted a deviation from RTCA DO-197A section 2.2.9.1 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity.

8. Garmin was granted a deviation from RTCA DO-197A section 2.2.11 to use the suppression pulse on the aircraft suppression bus specified by RTCA DO-185B section 2.2.3.12 (70 +/-1 µs from top antenna and 90 +/-1 µs from bottom antenna) instead of 100 +/-5 µs.

GTS Processor Installation Manual Page 1-5 190-00587-50 Revision A

ETSO-C118

DRAFT

TSO-C119c

ETSO-C119c

Table 1-8 TSO/ETSO Deviations, Continued

1. Garmin was granted a deviation from ETSO-C118 section 3.1.1 to use RTCA DO-197A, instead of RTCA DO-197 as the Minimum Performance Standard.

2. Garmin was granted a deviation from ETSO-C118 section 3.1.2 to use EUROCAE ED-14F, instead of EUROCAE ED-14D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment.

3. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.2.1 to use the Interrogations Spectrum requirement of RTCA DO-185B section 2.2.3.3 instead of the requirement of RTCA DO- 197A section 2.2.3.2.1.

4. Garmin was granted a deviation from RTCA DO-197A section 2.2.3.5 to use the “Mode C Only All-Call” format specified by RTCA DO-185B section 2.2.3.8.1 instead of the “Mode C” format for ATCRBS interrogations.

5. Garmin was granted a deviation from RTCA DO-197A section 2.2.9.1 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity.

6. Garmin was granted a deviation from RTCA DO-197A section 2.2.11 to use the suppression pulse on the aircraft suppression bus specified by RTCA DO-185B section 2.2.3.12 (70 +/-1 μs from top antenna and 90 +/-1 μs from bottom antenna) instead of 100 +/-5 μs.

1. Garmin was granted a deviation from RTCA DO-185B section 2.2.3.13.2.1.1 to not have the ability to interface with FAA TSO-C119a compatible transponder units.

2. Garmin was granted a deviation from RTCA DO-185B section 2.2.4.4.2.2.b to use the Enhanced Preamble Detection method of RTCA DO-260B Appendix I section I.4.1

3. Garmin was granted a deviation from RTCA DO-185B section 2.2.4.4.2.2.c to use the Baseline Multi-sample bit and confidence declaration technique of RTCA DO-260B Appendix I section I.4.2.3.1.

4. Garmin was granted a deviation from RTCA DO-185B section 2.2.6.7.2 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity.

1. Garmin was granted a deviation from ETSO-C119c to use EUROCAE ED-14F instead of EUROCAE ED-14D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment.

2. Garmin was granted a deviation from RTCA DO-185B section 2.2.3.13.2.1.1 to not have the ability to interface with FAA TSO-C119a compatible transponder units.

3. Garmin was granted a deviation from RTCA DO-185B section 2.2.4.4.2.2.b to use the Enhanced Preamble Detection method of RTCA DO-260B Appendix I section I.4.1.

4. Garmin was granted a deviation from RTCA DO-185B section 2.2.4.4.2.2.c to use the Baseline Multi-sample bit and confidence declaration technique of RTCA DO-260B Appendix I section I.4.2.3.1.

5. Garmin was granted a deviation from RTCA DO-185B section 2.2.6.7.2 to realize the bearing estimation function using a direction finding antenna augmented by tracked correlated ADS-B data when such data is available and of sufficient integrity.

Page 1-6 GTS Processor Installation Manual Revision A 190-00587-50

TSO-C147

DRAFT

ETSO-C147

ETSO-C166a

Table 1-8 TSO/ETSO Deviations, Continued

1. Garmin was granted a deviation from TSO-C147 section 1.c to use RTCA DO-160F, instead of RTCA DO-160D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment.

2. Garmin was granted a deviation from TSO-C147 Appendix 1 section 1.6 to use selective Mode S interrogations as specified by RTCA DO-185A section 2.2.3.9 and 2.2.4.5.4.2 following all the applicable protocols for Mode-S surveillance interrogations in the NAS as stated in RTCA DO-185B and RTCA DO-181D.

1. Garmin was granted a deviation from ETSO-C147 section 3.1.2 to use EUROCAE ED-14F, instead of EUROCAE ED-14D as the standard for Environmental Conditions and Test Procedures for Airborne Equipment.

2. Garmin was granted a deviation from ETSO-C147 Appendix 1 section 1.6 to use selective Mode S interrogations as specified by RTCA DO-185B section 2.2.3.9 and 2.2.4.5.4.2 following all the applicable protocols for Mode-S surveillance interrogations in the NAS as stated in RTCA DO185B and RTCA DO-181D.

1. Garmin was granted a deviation from ETSO-C166a, section 4.2 to allow not marking the unit with the class information, which is instead provided in the installation and operation manual.

2. Garmin was granted a deviation from ETSO-C166a to use RTCA DO-260B instead of RTCA DO-260A as the Minimum Performance Standard.

3. Garmin was granted a deviation from ETSO-C166a to use RTCA DO-160F instead of RTCA DO-160E as the Environmental Standard.

4. Garmin was granted a deviation from RTCA DO-260B section 2.2.4.3.4.7.3.b to use the Conservative and Brute Force error correction techniques specified by RTCA DO-260B section

2.2.4.4.3.1 instead of 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185B.

5. Garmin was granted a deviation from RTCA DO-260 and Brute Force error correction techniques specified by RTCA DO-260B section 2.2.4.4.3.1 instead of section 2.2.4.4.2.2.d and Appendix A, Section 3 of RTCA DO-185B.

B section

2.2.4.5.b to use the Conservative

GTS Processor Installation Manual Page 1-7 190-00587-50 Revision A

1.6 Reference Documents

DRAFT

The following publications are sources of additional information for installing the GTS Processor. Before installing the GTS Processor, the installer should read all referenced materials along with the manual.

Table 1-9 Reference Documents

Part Number Document

190-00313-11 Jackscrew Backshell Installation Instructions

190-00303-00 G1000 System Installation Manual

190-00587-51 GTS Processor System Maintenance Manual

190-00903-00 G1000 System Maintenace Manual LJ/VLJ

190-00907-00 G1000 System Maintenance Manual Standard Piston/Turboprop Aircraft

Page 1-8 GTS Processor Installation Manual Revision A 190-00587-50

1.7 Aviation Limited Warranty

DRAFT

All Garmin avionics products are warranted to be free from defects in materials or workmanship for: one years from the date of purchase for new Remote-Mount and Panel-Mount products; one year from the date of purchase for new portable products and any purchased newly-overhauled products; six months for newly-overhauled products exchanged through a Garmin Authorized Service Center; and 90 days for factory repaired or newly-overhauled products exchanged at Garmin in lieu of repair. Within the applicable period, Garmin will, at its sole option, repair or replace any components that fail in normal use. Such repairs or replacement will be made at no charge to the customer for parts or labor, provided that the customer shall be responsible for any transportation cost. This warranty does not apply to: (i) cosmetic damage, such as scratches, nicks and dents; (ii) consumable parts, such as batteries, unless product damage has occurred due to a defect in materials or workmanship; (iii) damage caused by accident, abuse, misuse, water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any country.

THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE.

IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU.

Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or software or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY.

Online Auction Purchases: Products purchased through online auctions are not eligible for warranty coverage. Online auction confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace missing components from any package purchased through an online auction.

International Purchases: A separate warranty may be provided by international distributors for devices purchased outside the United States depending on the country. If applicable, this warranty is provided by the local in-country distributor and this distributor provides local service for your device. Distributor warranties are only valid in the area of intended distribution. Devices purchased in the United States or Canada must be returned to the Garmin service center in the United Kingdom, the United States, Canada, or Taiwan for service.

Garmin International, Inc. Garmin (Europe) Ltd. 1200 East 151st Street Liberty House, Bulls Copse Road Olathe, Kansas 66062, U.S.A. Hounsdown Business Park Phone:913/397.8200 Romsey, SO40 9RB, U.K. FAX:913/397.0836 Phone:44/ (0) 870.8501241 FAX:44/ (0) 870.850125

GTS Processor Installation Manual Page 1-9 190-00587-50 Revision A

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DRAFT

Page 1-10 GTS Processor Installation Manual Revision A 190-00587-50

2 INSTALLATION OVERVIEW

DRAFT

2.1 Introduction

This section provides hardware equipment information for installing the GTS Processor and related hardware. Installation of the GTS Processor should follow the aircraft TC or STC requirements. Cabling is fabricated by the installing agency to fit each particular aircraft. The guidance of FAA advisory circulars AC 43.13-1B and AC 43.13-2B, where applicable, may be found useful for making retro-fit installations that comply with FAA regulations.

2.1.1 Unit Configurations

The GTS Processor is available under the following part numbers:

Table 2-1 Unit Configuration

Item

GTS Processor, (011-02571-00)

Applicable

LRU Software

Part Numbers

All

006-B1244-0( )

through

006-B1244-2( )

except

006-B1244-00

through

006-B1244-03

Applicable Custom

Logic Device

Part Numbers

006-C0081-2( ) 010-00962-00

Garmin P/N

2.1.2 Required Accessories

NOTE

Refer to the Dealer’s Only portion of www.garmin.com for instructions on determining what accessories are needed.

Each of the following accessories are provided separately from the GTS Processor and is required to install the unit. Only one is required.

Table 2-2 Required Accessories

Installation Racks Garmin P/N

GTS Processor Vertical Installation Rack 011-02572-00*

GTS Processor Horizontal Installation Rack 115-00784-00*

*Approved for use in RTCA DO-160F, Section 8, Category S, Curve C, Y, and L installations, as well as RTCA DO-160F, Section 8, Category U, Curve G installations.

For a GTS Processor installation with a single GA 58 directional antenna (GTS 855/GTS 825 only), 8 TNC connectors (not supplied), either straight or right angle, are required.

For a GTS Processor installation with dual GA 58 directional antennas (GTS 8000/GTS 855/GTS 825), 16 TNC connectors (not supplied), either straight or right angle, are required.

For a GTS Processor installation with a single GA 58 directional antenna and a monopole antenna (GTS 8000/GTS 855/GTS 825), 9 TNC connectors and 1 BNC connector (not supplied), either straight or right angle, are required.

TNC 50 Ohm terminations (not supplied) are required for all unused antenna ports.

GTS Processor Installation Manual Page 2-1 190-00587-50 Revision A

Table 2-3 Connector Kits

DRAFT

Connector Kits Garmin P/N

GTS Processor Connector Kit 011-01360-00

GTS Connector Kit w/Config Module and USB Pigtail 011-01360-01

USB-B Pigtail (see GTS Configuration Options) 011-01782-00

Table 2-4 Optional Accessories

Optional Accessories Garmin P/N

Color Coded Heat Shrink Kit 011-02817-00

NOTE

The GTS Processor is to be installed with a four-beam directional interrogation antenna mounted to the top of the aircraft as described in the antenna installation manual.

Table 2-5 Antennas

Antennas Garmin P/N

GA 58 Directional Antenna, QMA (011-01346-00) NOTE: Refer to 190-00587-00 GTS 8XX Installation Manual for installation instructions

GA 58 Directional Antenna, TNC, (011-01346-02) NOTE: Refer to 190-000587-20 GA 58 Installation Manual for installation instructions.

Low Profile Directional Antenna

Monopole Antenna

*010-10720-00 and 010-10720-02 include mounting screws and o-ring, unless specifically requested to exclude.

**Or Sensor Systems Incorporated part number S72-1735-24 (long TNC connectors) or S72-1735-26 (short TNC connectors) that meet the requirements of Garmin part number 013-00276-0X or 013-00276-5X, respectively. Refer to the manufacturer’s installation manual for installation instructions..

010-10160-00 or L-Band Monopole Antenna that meets TSO-C74c

010-10720-00

010-10720-02

013-00276-XX

Table 2-6 Configuration Module

Configuration Module Garmin P/N

Configuration Module* 011-00979-20

*Required for GTS Processor installations that do not have other means (such as a GDU XXXX Configuration Module) to store GTS Processor configuration data. Contact Garmin for additional guidance in determining applicability.

Page 2-2 GTS Processor Installation Manual Revision A 190-00587-50

2.2 Installation Considerations

DRAFT

Fabrication of a wiring harness is required. Sound mechanical and electrical methods and practices are required for installation of the GTS Processor.

2.2.1 Antenna Considerations

Refer to GA 58 Installation Manual 190-00587-20 for antenna installation information.

NOTE

For GTS 855/GTS 825 installations, either a monopole antenna or directional antenna may be used if installing an optional bottom mounted antenna. For GTS 8000 installations, a bottom monopole or directional antenna is required. A bottom directional antenna installation (recommended) gives the benefit of intruder bearing visibility for targets that are shaded from the top directional antenna. The target bearing accuracy may be degraded for bottom directional antenna installations on aircraft with fixed gear.

2.2.1.1 TAS/TCAS Antenna Location

Refer to GA 58 Installation Manual 190-00587-20 for antenna installation information

2.3 Electrical Bonding

Electrical equipment, supporting brackets, and racks should be electrically bonded to the aircraft’s main structure. Refer to SAE ARP 1870 section 5 when surface preparation is required to achieve electrical bond. The electrical bond should achieve direct current (DC) resistance less than or equal to 2.5 milliohms to local structure to where the equipment is mounted. Compliance should be verified by inspection using a calibrated milliohm meter. An equivalent OEM procedure may also be substituted. There may be OEMspecific reasons for electrically isolating equipment or having a higher bond resistance. These reasons should be rationalized upon installation approval. In general, Garmin recommends that all GTS Processor equipment be electrically bonded.

Refer to GA 58 Installation Manual 190-00587-20 for antenna installation information.

For composite aircraft, the antenna baseplate must be electrically bonded to the common ground of other installed equipment for lightning purposes. This can be achieved through the antenna mounting screws.

GTS Processor Installation Manual Page 2-3 190-00587-50 Revision A

2.4 Cabling and Wiring

DRAFT

The contacts used to facilitate the use of #18 AWG wire, if used for Aircraft Power and Aircraft Ground, have expanded-diameter barrels that extend out from the back of the standard D-sub connector body to accommodate the larger diameter wire. Appropriate heat shrink tubing should be utilized to provide sufficient insulation from surrounding contacts.

NOTE

When removing an expanded-diameter barrel contact, always cut off the expanded-diameter barrel before using an extraction tool to remove the contact.

Ensure that routing of the wiring does not come in contact with sources of heat, RF or EMI interference. Check that there is ample space for the cabling and mating connectors. Avoid sharp bends in cabling and routing near aircraft control cables.

NOTE

All appliance to antenna coaxial cabling shall bundle top four channels as a group and bottom four channels as a group to prevent incorrect wiring between top and bottom channels.

A visual inspection shall be performed to verify that all coaxial cables are connected properly, before attempting to operate the equipment.

2.4.1 Coaxial Cable

The GTS Processor requires two sets of coaxial cable assemblies when a directional GA 58 antenna (or other Garmin approved antenna) is used for both top and bottom. Each set consists of four coaxial cable assemblies.

Each set of four cables must be assembled using the same type of coaxial cable in order to meet phase and attenuation matching requirements. In order for the system to operate in compliance with manufacturer specifications, the coaxial cable assemblies must not exceed the attenuation specifications as stated in this document. This section explains in further detail the coaxial cable and termination requirements.

NOTE

TNC connectors and BNC connectors, required for building the coaxial cable assemblies for some antenna options, are not provided.

2.4.1.1 GTS Processor Installations

NOTE

For all GTS Processor installations, either a monopole antenna or directional antenna (recommended) may be used if installing a bottom mounted antenna. GTS 8000 installations require either a bottom-mounted directional (recommended) or monopole antenna. A bottom antenna is optional for GTS 855/ GTS 825 installations, but a bottom directional antenna is recommended for best performance. A bottom directional antenna installation gives the benefit of intruder bearing visibility for targets that are shaded from the top directional antenna. The target bearing accuracy may be degraded for bottom directional antenna installations on aircraft with fixed gear.

A GTS Processor installation with both top and bottom mounted directional antennas uses one set of coaxial cables for the four GTS Processor TOP jacks (J1 TOP, J2 TOP, J3 TOP, J4 TOP) that are connected to the corresponding top antenna jacks J1, J2, J3 and J4. A second set of coaxial cables are used for the four GTS Processor BTM jacks (J1 BTM, J2 BTM, J3 BTM, J4 BTM) that are connected to the corresponding bottom antenna jacks J1, J2, J3 and J4. Each cable assembly shall not exceed the maximum

Page 2-4 GTS Processor Installation Manual Revision A 190-00587-50

attenuation of 3.0dB at 1090MHz for a GA 58 directional antenna installations, and 2.5 dB for low-profile

DRAFT

directional antenna installations as shown in Figure 2-1.

Figure 2-1 GTS Processor Installation with Top and Bottom Directional Antennas

If a bottom mount monopole antenna is installed, a single coaxial cable must be used to connect the GTS Processor bottom jack J1 BTM to the monopole antenna jack. The coaxial cable assembly shall not exceed the maximum attenuation of 3.0dB at 1090MHz for a GA 58 directional antenna and 2.5 dB for a low profile directional antenna as shown in Figure 2-2 and stated in Table 2-2. Each of the remaining GTS Processor bottom jacks (J2 BTM, J3 BTM, J4 BTM) are to be terminated using a 50Ω TNC termination.

Figure 2-2 GTS Processor Installation with Top Directional and Bottom Monopole

Antennas

GTS Processor Installation Manual Page 2-5 190-00587-50 Revision A

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