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Garmin GAD 42 TSO - User Manual

Garmin GAD 42 TSO
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190-00159-10 May, 2016 Revision B
GAD 42 TSO
Installation Manual
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Summary

1 GENERAL DESCRIPTION

1.1 Introduction

Overview of the manual's purpose and scope for GAD 42 installation.

1.2 Equipment Description

Details the capabilities and functions of the GAD 42 Interface Adapter Unit.

1.2.1 GAD 42 (-00 and -10) Comparison

Compares the -00 and -10 versions of the GAD 42, highlighting form, fit, and function differences.

1.3 Technical Specifications

Outlines critical technical data, including environmental, power, and installation requirements.

1.3.3 General Specifications

Lists general operating parameters such as temperature range, humidity, altitude, software, and testing standards.

1.3.4 Power Requirements

Details the input voltage, power consumption, and AC reference signal specifications for the GAD 42.

1.3.5 Minimum Installation Requirements

Specifies the GPS receiver response time requirement for GAD 42 installations.

1.4 Certification

Covers TSO approval standards and aircraft installation requirements for the GAD 42 article.

1.5 Operating Instructions

Explains how the GAD 42 operates, noting its remote nature and user interface via other devices.

2 INSTALLATION OVERVIEW

2.1 Introduction

Introduces hardware information for installing the GAD 42 and related components, referencing advisory circulars.

2.1.1 Unit Configurations

Lists the available part numbers for the GAD 42 unit, specifying standard and unit-only options.

2.1.2 Required Accessories

Identifies essential connector kits required for GAD 42 installation, noting interchangeability.

2.2 Installation Considerations

Provides general guidance on fabrication, mechanical, and electrical practices for GAD 42 installation.

2.3 Cabling and Wiring

Offers advice on wire gauge, insulation, routing, and avoiding interference for GAD 42 wiring.

2.4 Mounting Requirements

Specifies that the GAD 42 mounting surface must provide structural support and electrical bonding.

3 INSTALLATION PROCEDURE

3.1 Unpacking Unit

Instructs on carefully unpacking the GAD 42, inspecting for damage, and handling claims.

3.2 Wiring Harness Installation

Details the process of installing wiring harnesses, referencing connector types and electrical characteristics.

3.3 Backshell Assembly

Guides on assembling backshell connectors for the GAD 42, referencing specific installation instructions.

3.4 Unit Installation

Outlines the steps for physically mounting the GAD 42 unit, including connector and screw requirements.

3.5 Post Installation Configuration & Checkout

Covers configuration methods and testing procedures after GAD 42 installation.

3.5 Post Installation Configuration & Checkout

Configuration Options

Details various configuration parameters like RMI, Course Select, Airspeed, Heading, and ARINC modes.

Troubleshooting Messages

Guides on interpreting and resolving "GAD 42 NEEDS SERVICE" messages using label definitions.

Ground and Flight Tests

Outlines essential ground and flight tests to verify the proper installation and operation of the GAD 42.

4 SYSTEM INTERCONNECTS

4.1 Pin Function List

Provides a detailed list of pin names, their corresponding connectors (J421, J422), and I/O for the GAD 42.

4.2 Power and GPS Serial Data

Covers aircraft power input and GPS serial data interfaces, including ARINC 429 communication.

4.3 Heading

Describes the GAD 42's heading function, its inputs (Synchro, ARINC 429), and required valid signals.

4.4 Flight Control

Explains how the GAD 42 converts ARINC 429 steering data to analog signals for flight control systems.

4.5 Selected Course

Describes the GAD 42's ability to read remote course panels and drive course arrows via ARINC 429 or analog signals.

4.6 RMI;OBI Drive

Explains how the GAD 42 drives RMI/OBI pointers using GPS or VOR bearing data via 400 Hz analog signals.

4.7 Collins EFIS

Describes the GAD 42's interface with Collins EFIS systems for navigation data display.

4.8 King Serial DME and ARINC 561;568 Serial Data

Details GAD 42 outputs for King Serial DME and ARINC 561/568 data, including required inputs.

4.9 True Airspeed

Explains how the GAD 42 receives analog True Airspeed formats and transmits TAS data via ARINC 429.

4.10 ARINC 565 Conversion Mode (ADC Mode)

Describes GAD 42 reception of Barometric Altitude/Static Air Temp via ARINC 565 and transmission via ARINC 429.

APPENDIX A Outline and Installation Drawings

Figure A-1 GAD 42 w;Edge Connector Outline Drawing

Provides dimensional outlines and mounting information for the GAD 42 with edge connectors.

Figure A-2 GAD 42 w;Jackscrew Connector Outline Drawing

Shows dimensional outlines and mounting details for the GAD 42 unit equipped with jackscrew connectors.

Figure A-3 GAD 42 w;Edge Connector Installation Drawing

Illustrates the assembly process for the GAD 42 with edge connectors, showing component part numbers.

APPENDIX B Interconnect Drawings

Figure B-1 GAD 42 System Interface Diagram

A high-level diagram illustrating the GAD 42's connections to various aircraft systems and components.

Figure B-2 Power and Miscellaneous Interconnect

Details the specific wiring connections for power, GPS serial data, and other miscellaneous functions.

Figure B-3 Heading Interconnect

Illustrates the interconnect wiring for heading signals between the GAD 42 and compass/gyro systems.

Figure B-4 Flight Control Interconnect

Shows the interconnect wiring for flight control signals, connecting the GAD 42 to autopilot systems.

Summary

1 GENERAL DESCRIPTION

1.1 Introduction

Overview of the manual's purpose and scope for GAD 42 installation.

1.2 Equipment Description

Details the capabilities and functions of the GAD 42 Interface Adapter Unit.

1.2.1 GAD 42 (-00 and -10) Comparison

Compares the -00 and -10 versions of the GAD 42, highlighting form, fit, and function differences.

1.3 Technical Specifications

Outlines critical technical data, including environmental, power, and installation requirements.

1.3.3 General Specifications

Lists general operating parameters such as temperature range, humidity, altitude, software, and testing standards.

1.3.4 Power Requirements

Details the input voltage, power consumption, and AC reference signal specifications for the GAD 42.

1.3.5 Minimum Installation Requirements

Specifies the GPS receiver response time requirement for GAD 42 installations.

1.4 Certification

Covers TSO approval standards and aircraft installation requirements for the GAD 42 article.

1.5 Operating Instructions

Explains how the GAD 42 operates, noting its remote nature and user interface via other devices.

2 INSTALLATION OVERVIEW

2.1 Introduction

Introduces hardware information for installing the GAD 42 and related components, referencing advisory circulars.

2.1.1 Unit Configurations

Lists the available part numbers for the GAD 42 unit, specifying standard and unit-only options.

2.1.2 Required Accessories

Identifies essential connector kits required for GAD 42 installation, noting interchangeability.

2.2 Installation Considerations

Provides general guidance on fabrication, mechanical, and electrical practices for GAD 42 installation.

2.3 Cabling and Wiring

Offers advice on wire gauge, insulation, routing, and avoiding interference for GAD 42 wiring.

2.4 Mounting Requirements

Specifies that the GAD 42 mounting surface must provide structural support and electrical bonding.

3 INSTALLATION PROCEDURE

3.1 Unpacking Unit

Instructs on carefully unpacking the GAD 42, inspecting for damage, and handling claims.

3.2 Wiring Harness Installation

Details the process of installing wiring harnesses, referencing connector types and electrical characteristics.

3.3 Backshell Assembly

Guides on assembling backshell connectors for the GAD 42, referencing specific installation instructions.

3.4 Unit Installation

Outlines the steps for physically mounting the GAD 42 unit, including connector and screw requirements.

3.5 Post Installation Configuration & Checkout

Covers configuration methods and testing procedures after GAD 42 installation.

3.5 Post Installation Configuration & Checkout

Configuration Options

Details various configuration parameters like RMI, Course Select, Airspeed, Heading, and ARINC modes.

Troubleshooting Messages

Guides on interpreting and resolving "GAD 42 NEEDS SERVICE" messages using label definitions.

Ground and Flight Tests

Outlines essential ground and flight tests to verify the proper installation and operation of the GAD 42.

4 SYSTEM INTERCONNECTS

4.1 Pin Function List

Provides a detailed list of pin names, their corresponding connectors (J421, J422), and I/O for the GAD 42.

4.2 Power and GPS Serial Data

Covers aircraft power input and GPS serial data interfaces, including ARINC 429 communication.

4.3 Heading

Describes the GAD 42's heading function, its inputs (Synchro, ARINC 429), and required valid signals.

4.4 Flight Control

Explains how the GAD 42 converts ARINC 429 steering data to analog signals for flight control systems.

4.5 Selected Course

Describes the GAD 42's ability to read remote course panels and drive course arrows via ARINC 429 or analog signals.

4.6 RMI;OBI Drive

Explains how the GAD 42 drives RMI/OBI pointers using GPS or VOR bearing data via 400 Hz analog signals.

4.7 Collins EFIS

Describes the GAD 42's interface with Collins EFIS systems for navigation data display.

4.8 King Serial DME and ARINC 561;568 Serial Data

Details GAD 42 outputs for King Serial DME and ARINC 561/568 data, including required inputs.

4.9 True Airspeed

Explains how the GAD 42 receives analog True Airspeed formats and transmits TAS data via ARINC 429.

4.10 ARINC 565 Conversion Mode (ADC Mode)

Describes GAD 42 reception of Barometric Altitude/Static Air Temp via ARINC 565 and transmission via ARINC 429.

APPENDIX A Outline and Installation Drawings

Figure A-1 GAD 42 w;Edge Connector Outline Drawing

Provides dimensional outlines and mounting information for the GAD 42 with edge connectors.

Figure A-2 GAD 42 w;Jackscrew Connector Outline Drawing

Shows dimensional outlines and mounting details for the GAD 42 unit equipped with jackscrew connectors.

Figure A-3 GAD 42 w;Edge Connector Installation Drawing

Illustrates the assembly process for the GAD 42 with edge connectors, showing component part numbers.

APPENDIX B Interconnect Drawings

Figure B-1 GAD 42 System Interface Diagram

A high-level diagram illustrating the GAD 42's connections to various aircraft systems and components.

Figure B-2 Power and Miscellaneous Interconnect

Details the specific wiring connections for power, GPS serial data, and other miscellaneous functions.

Figure B-3 Heading Interconnect

Illustrates the interconnect wiring for heading signals between the GAD 42 and compass/gyro systems.

Figure B-4 Flight Control Interconnect

Shows the interconnect wiring for flight control signals, connecting the GAD 42 to autopilot systems.

Garmin GAD 42 TSO Specifications

General IconGeneral
BrandGarmin
ModelGAD 42 TSO
CategoryAdapter
LanguageEnglish

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