Manuais de utilizador para Garmin International Inc 0104455

índice analítico

• Section 1 GENERAL DESCRIPTION

  1
• 1.1 Introduction

  1
• 1.2 Equipment Description

  1
• 1.2.1 GTS Processor Configuration Options

  1
• 1.3 Interface Summary

  1
• 1.4 Technical Specifications

  1
• 1.4.1 Environmental Qualification Form

  1
• 1.4.2 Physical Characteristics

  1
• 1.4.3 General Specifications

  1
• 1.4.4 Power Requirements

  1
• 1.5 Certification

  1
• 1.5.1 GTS Processor TSO/ETSO Compliance

  1
• 1.5.2 GTS Processor TSO/ETSO Deviations

  1
• 1.6 Reference Documents

  1
• AF 1.7 Aviation Limited Warranty

  1
• Section 2 INSTALLATION OVERVIEW

  2
• 2.1 Introduction

  2
• 2.1.1 Unit Configurations

  2
• 2.1.2 Required Accessories

  2
• 2.2 Installation Considerations

  2
• 2.2.1 Antenna Considerations

  2
• 2.3 Electrical Bonding

  2
• 2.4 Cabling and Wiring

  2
• 2.4.1 Coaxial Cable

  2
• 2.5 Cooling Requirements

  2
• 2.6 Mounting Requirements

  2
• Section 3 INSTALLATION PROCEDURE

  3
• 3.1 Unpacking Unit

  3
• 3.2 Wiring Harness Installation

  3
• 3.3 Backshell and Configuration Module Assemblies

  3
• 3.4 GA 58 Antenna Installation

  3
• 3.5 Sensor Systems Incorporated Low-Profile Antenna Installation

  3
• 3.6 Unit Installation

  3
• 3.7 Downloading and Installing the GTS Processor Install Tool

  3
• 3.8 Downloading and Installing the GTS Assert Log Diagnosis Tool

  3
• 3.9 Post Installation Configuration & Checkout

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• 3.9.1 GTS Processor Configuration/Checkout for Different Installation Types

  3
• 3.9.2 Using the GTS Processor Install Tool

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• 3.9.3 Suppression Bus I/O Check

  3
• 3.9.4 CDTI (Cockpit Display of Traffic Information) Display Setup and Configuration

  3
• 3.9.5 Calibration/Self Test

  3
• 3.9.6 Ramp Test and Return To Service Test

  3
• 3.9.7 Antenna Verification

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• 3.10 Continued Airworthiness

  3
• Section 4 SYSTEM INTERCONNECTS

  4
• 4.1 GTS Processor Pin Function List

  4
• 4.1.1 P8001 (Digital)

  4
• 4.1.2 P8002 (Analog/Discrete)

  4
• 4.1.3 P8003 (Power Supply)

  4
• 4.2 Power

  4
• 4.2.1 Aircraft Power Functions

  4
• 4.3 Serial Data

  4
• 4.3.1 RS-232

  4
• 4.3.2 RS-422

  4
• 4.3.3 ARINC 429

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• 4.3.4 Ethernet

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• 4.3.5 USB

  4
• 4.4 Configuration

  4
• 4.4.1 Configuration Module

  4
• 4.5 Analog/Discrete

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• 4.5.1 Heading Input

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• 4.5.2 Inputs From Compass System/Directional Gyros

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• 4.5.3 Audio

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• 4.5.4 Active Low Discrete Inputs

  4
• 4.5.5 Active High Discrete Inputs

  4
• 4.5.6 Annunciator Output

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• 4.6 Mutual Suppression Bus

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• Section 1 GENERAL DESCRIPTION

  1
• Section 2 INSTALLATION OVERVIEW

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

  2
• Bottom Monopole Antennas

  2
• No Bottom Antenna

  2
• Figure 2-4 Heat Shrink Positioning

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

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

  2
• Section 3 INSTALLATION PROCEDURE

  3
• Figure 3-1 GTS Processor Install Tool – Installation

  3
• Figure 3-2 GTS Processor Install Tool – Installation

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• Figure 3-3 GTS Processor Install Tool – Installation

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• Figure 3-4 GTS Processor Install Tool – Installation

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• Figure 3-5 GTS Processor Install Tool – Installation

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• Figure 3-6 GTS Processor Install Tool – Installation

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

  3
• Figure 3-8 GTS Assert Log Diagnosis Tool – Installation

  3
• Figure 3-9 GTS Assert Log Diagnosis Tool – Installation

  3
• Figure 3-10 GTS Assert Log Diagnosis Tool – Installation

  3
• Figure 3-11 GTS Assert Log Diagnosis Tool – Installation

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• Figure 3-12 GTS Processor Install Tool – Normal Tab

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• Figure 3-14 GTS Processor Install Tool – Upload Tab

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• Figure 3-15 GTS Processor Install Tool – Assert Tab

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• Figure 3-16 Self Test

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

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• Figure 3-18 GND TEST Softkey

  3
• Section 4 SYSTEM INTERCONNECTS

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

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• Figure 4-2 View of J8002 connector from back of unit

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• Figure 4-3 View of J8003 connector from back of unit

  4
• Section 1 GENERAL DESCRIPTION

  1
• Compatible Transponders

  1
• Configuration Options

  1
• Physical Characteristics

  1
• General Specifications

  1
• Maximum Operation Current Draw

  1
• Maximum Boot-Up Current Draw

  1
• TSO/ETSO Compliance

  1
• TSO/ETSO Deviations

  1
• Reference Documents

  1
• Section 2 INSTALLATION OVERVIEW

  2
• Unit Configuration

  2
• Required Accessories

  2
• Connector Kits

  2
• Optional Accessories

  2
• Antennas

  2
• Configuration Module

  2
• Recommended Coaxial Length

  2
• Coaxial Cable Set Length Tolerance

  2
• Section 3 INSTALLATION PROCEDURE

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

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

  3
• GPN 336-00023-00 Crimp Tooling

  3
• Table 3-5 Self Test

  3
• Section 4 SYSTEM INTERCONNECTS

  4
• Table 4-1 P8001 Connector

  4
• Table 4-2 P8002 Connector

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• Table 4-3 P8002 Connector

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• Table 4-4 Aircraft Power

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• Table 4-5 Remote Power

  4
• Table 4-6 Power On/Off Matrix

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• Table 4-7 RS-232

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• Table 4-8 RS-422

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• Table 4-9 ARINC 429

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• Table 4-10 Ethernet

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• Table 4-11 USB

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• Table 4-12 Configuration Module

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• Table 4-13 26 Volt AC References

  4
• Radar Altimeter

  4
• Inputs From Compass System/Directional Gyros

  4
• Audio

  4
• Active Low Discrete Inputs

  4
• Active High Discrete Inputs

  4
• Annunciator Output

  4
• Mutual Suppression Bus

  4