Garmin GTX 330 User Manual

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190-00207-02 December, 2013 Revision U

GTX 330/330D

Transponder

Installation Manual

Table of Contents

Default Chapter7
- Table of Contents7
Paragraph Page8
Section 1 GENERAL DESCRIPTION13
- Introduction13
- Equipment Description13
Section 1 GENERAL DESCRIPTION14
- ADS-B Capabilities14
- Table 1-1 ADS-B Versions14
- TIS System Capabilities16
- Mutual Suppression Pulses16
- Interface Summary17
- Technical Specifications18
- Table 1-2 General Specifications18
- Table 1-3 Physical Characteristics19
- Table 1-4 Power Requirements19
- Certification20
- Table 1-5 TSO/ETSO/RTCA/ICAO Compliance20
- Operating Instructions22
- Aircraft Station Licensing Requirements22
- Table 1-6 TSO/ETSO Deviations22
- Section 1 1-1 –22
Section 2 INSTALLATION OVERVIEW23
Section 2 INSTALLATION OVERVIEW23
- Introduction23
- Installation Materials23
- Table 2-1 Available Configurations23
- Installation Considerations24
- Table 2-2 Equipment Available24
Section 2 INSTALLATION OVERVIEW25
- Antenna Installation25
- Figure 2-1 Antenna Installation Considerations25
- Cabling and Wiring Considerations26
- Table 2-3 Cable Specifications26
- Installation Approval Considerations for Pressurized Aircraft27
- Cooling Air27
- GTX 330 Installation27
- Table 2-4 Viewing Angles27
- Figure 2-2 GTX 330 Unit Rack (115-00294-00)28
- Section 2 2-1 –28
Section 3 INSTALLATION PROCEDURE29
Section 3 INSTALLATION PROCEDURE29
- Unpacking Unit29
- Wiring Harness Installation29
- Table 3-1 Pin Contact Part Numbers (High Density)29
- Circuit Breaker Placard30
- Post Installation Checkout30
- Table 3-2 Recommended Crimp Tools (High Density)30
- Section 3 3-1 –30
Section 4 SYSTEM INTERCONNECTS31
Section 4 SYSTEM INTERCONNECTS31
Section 4 SYSTEM INTERCONNECTS31
- Pin Function List31
- Figure 4-1. Rear Connector, J330131
- Table 4-1 J3301 Pin Assignments31
- Power and Lighting Function33
- Temperature Inputs33
- Table 4-2 Aircraft Power Pin Assignments33
- Table 4-3 Aircraft Lighting Pin Assignments33
- Table 4-4 Temperature Probe Pin Assignments33
- Altitude Functions34
- Table 4-5 Encoded Altitude Pin Assignments34
- Figure 4-2. Dual GTX 330, Single Encoder, Serial Input Connections35
- Discrete Functions36
- Table 4-6 Discrete Outputs Pin Assignments36
- Serial Data Electrical Characteristics37
- Table 4-7 Discrete Inputs Pin Assignments37
- Table 4-8 RS-232 Pin Assignments38
- Figure 4-3. GTX 330 Software Update Connections39
- Table 4-9 Affected Serial Numbers39
- Table 4-10 ARINC 429 Pin Assignments40
- Section 4 4-1 –40
Procedure 5-141
Section 5 POST INSTALLATION CONFIGURATION and CHECKOUT41
Section 5 POST INSTALLATION CONFIGURATION and CHECKOUT PROCEDURE41
- Operation41
- Figure 5-1. GTX 330 Front Panel41
- Code Selection43
- Configuration44
Section 5 POST INSTALLATION CONFIGURATION and CHECKOUT46
- Table 5-1 Configuration Menu Selections46
- Table 5-2 Audio Mode Selections46
- Table 5-3 Display Mode Selections47
- Table 5-4 Display Backlight Selections47
- Table 5-5 Backlight Source Selections48
- Table 5-6 Key Lighting Selections49
- Table 5-7 Key Source Selections49
Table50
- Table 5-8 Contrast Mode Selections50
- Table 5-9 VFR Key Selections50
- Table 5-10 Speed Selections51
- Table 5-11 Data Selections51
- Table 5-12 ARINC Channel Selections52
- Table 5-13 ARINC Output Labels, Data, and Rates53
- Table 5-14 ARINC Output Labels, High Speed Data53
- Table 5-15 RS-232 Input Selections54
- Table 5-16 RS-232 Output Selections55
- Table 5-17 Altitude Format Selections55
- Table 5-18 Auto Flight Timer Selections56
- Table 5-19 Mode S Address Selections57
- Table 5-20 Flight ID Selections58
- Table 5-21 GPS Configuration Page59
- Table 5-22 Mode S Aircraft Type Selections60
- Table 5-23 Received Labels and Data from AHRS63
- Table 5-24 Received Labels and Data from ADC64
- Table 5-25 Received Labels and Data from EFIS Display64
- Table 5-26 Received Labels and Data from GPS/FMS65
- Table 5-27 Received Labels and Data from Garmin Display65
Paragraph66
- Enhanced Surveillance (EHS)66
- Table 5-28 Received Labels and Data from ARINC 743A66
- Table 5-29 Received Labels and Data from AFCS66
- Table 5-30 Required EHS Equipment Connections67
- Section 5 5-1 –68
Appendix A CERTIFICATION DOCUMENTS69
- STC Permission69
- Continued Airworthiness71
Appendix A CERTIFICATION DOCUMENTS73
- Matrix73
Appendix B VERSION 1 ADS-B FIELD APPROVAL COMPLIANCE MATRIX73
- Table B-1 Compliance Matrix74
Appendix B VERSION 1 ADS-B FIELD APPROVAL COMPLIANCE74
Appendix C ASSEMBLY and INSTALLATION DRAWINGS85
- Figure C-1 GTX 330 Outline Drawing85
- Figure C-2 GTX 330 Connector/Rack Assembly Drawing86
- Figure C-3 GTX 330 Recommended Panel Cutout Dimensions87
Appendix C ASSEMBLY and INSTALLATION DRAWINGS88
Appendix D INTERCONNECT DRAWINGS88
- Figure D-1 GTX 330 to 400/500 Series Units, Typical Interconnect Wiring Diagram88
Appendix D INTERCONNECT DRAWINGS88
- Figure D-2 GTX 330 to GNS 480(CNX80), Typical Interconnect Wiring Diagram89
- Figure D-3 GTX 330 to GNS 480 (CNX80) and MFD, Simplified Interconnect Wiring Diagram90
- Figure D-4 GTX 330 Interconnect Wiring Diagram, Discrete and Audio Connections91
- Figure D-5 GTX 330 Interconnect Wiring Diagram, Serial Devices Connections92
- Figure D-6 GTX 330 Interconnect Wiring Diagram, Altitude and Temperature Connections93
- Figure D-7 Dual Transponder Interconnect Wiring Diagram, Dual Display Connections94
- Figure D-7 Dual Transponder Interconnect Wiring Diagram, Dual Display Connections95
- Figure D-8 GTX 330 Interconnect Wiring Diagram, Aircraft with TIS and TCAD/TCAS96
- Figure D-9 Dual TXP Interconnect Wiring Diagram, Encoding Altitude Connections (Sheet 197
- Figure D-9 Dual TXP Interconnect Wiring Diagram, Encoding Altitude Connections (Sheet 298
- Figure D-9 Dual TXP Interconnect Wiring Diagram, Encoding Altitude Connections (Sheet 399
- Figure D-10 Dual TXP to GTN 6XX/7XX Interconect Wiring Diagram, Encoding Altitude Connections (Sheet 1100
- Figure D-10 Dual TXP to GTN 6XX/7XX Interconect Wiring Diagram, Encoding Altitude Connections (Sheet 2101
- Figure D-11 GTX 330 W/Es to GDL 90 Connections102
- Figure D-12 GTX 330 to 400/500 Series Units ADS-B Interconnect103
- Figure D-13 GTX 330 to 400W/500W Series Units ADS-B TX Only Interconnect104
- Figure D-14 GTX 330 to GTN 6XX/7XX Simplified Interconnect Wiring Diagram105

Other manuals for Garmin GTX 330

System Maintenance Manual56 pages

Pilot's Guide12 pages

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Garmin GTX 330 Specifications

General

Reply Frequencies	1090 MHz
Frequency Range	1090 MHz (reply)
Power Output	200 Watts peak
Dimensions	5.7 x 1.6 x 7.5 inches (145 x 41 x 191 mm)
Temperature Range	-20°C to +55°C
Operating Voltage	11-33 VDC

Summary

GTX 330 Hardware Mod Level History

1 General Description

1.3 ADS-B Capabilities

Information on the Automatic Dependent Surveillance-Broadcast capabilities.

1.6 Interface Summary

1.7 Technical Specifications

Provides detailed technical data and specifications for the unit.

2 Installation Overview

2.3 Installation Considerations

Important factors to consider before and during installation.

2.4 Antenna Installation

2.5 Cabling and Wiring Considerations

Recommendations for wire gauge, routing, and cable specifications.

2.8 GTX 330 Installation

Detailed steps for physically installing the unit in the aircraft.

3 Installation Procedure

3.2 Wiring Harness Installation

Steps for connecting the unit via the main wiring harness.

3.4 Post Installation Checkout

Procedures to verify proper installation and functionality.

4 System Interconnects

4.1 Pin Function List

4.2 Power and Lighting Function

4.4 Altitude Functions

5 Post Installation Configuration and Checkout Procedure

5.2 Configuration Pages

Comprehensive guide to configuring the unit's various settings.

5.3 Enhanced Surveillance (EHS)

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