Manuels d'utilisation pour Garmin International Inc 01443

Table des matières

• Section 1 GENERAL DESCRIPTION

  1
• Introduction

  1
• Equipment Description

  1
• Interface Summary

  1
• Technical Specifications

  1
• General Specifications

  1
• Transponder Capabilities

  1
• ADS-B Capabilities

  1
• Physical Characteristics

  1
• Power Requirements

  1
• 1.5 License Requirements

  1
• 1.6 Certification

  1
• 1.6.1 TSO/ETSO/RTCA/ICAO Compliance

  1
• 1.6.2 TSO/ETSO Deviations

  1
• 1.7 Reference Documents

  1
• 1.8 Aviation Limited Warranty

  1
• Section 2 INSTALLATION OVERVIEW

  2
• 2.1 Introduction

  2
• 2.2 Installation Materials

  2
• 2.2.1 Equipment Available

  2
• 2.2.2 Additional Equipment Required

  2
• 2.3 Installation Considerations

  2
• 2.3.1 Preservation of Previous Systems

  2
• 2.3.2 Antenna Location Considerations

  2
• 2.4 Cabling and Wiring

  2
• 2.4.1 Cable Routing Considerations

  2
• 2.5 Installation Approval Considerations for Pressurized Aircraft

  2
• 2.6 Cooling Air

  2
• 2.7 GTX 3000 Mounting Requirements

  2
• 2.7.1 Remote Mounted Stand-Alone Rack Considerations

  2
• Section 3 INSTALLATION PROCEDURE

  3
• Unpacking Unit

  3
• Wiring Harness Installation

  3
• Backshell Assembly

  3
• Weight and Balance

  3
• Electrical Load Analysis

  3
• 3.5.1 Circuit Breaker Placard

  3
• 3.6 Final Installation

  3
• 3.7 Post Installation Configuration and Checkout

  3
• 3.7.1 Configuration

  3
• 3.7.2 Interference Check

  3
• 3.7.3 Operation/Performance Checkout

  3
• 3.7.4 Performance (Ramp) Test

  3
• 3.8 Continued Airworthiness

  3
• Section 4 SYSTEM INTERCONNECTS

  4
• 4.1 Pin Function List

  4
• 4.1.1 P3301

  4
• 4.1.2 P3302

  4
• 4.2 Power Function

  4
• 4.2.1 Aircraft Power

  4
• 4.3 Altitude Functions

  4
• 4.3.1 Altimeter Inputs

  4
• 4.3.2 Altimeter Interconnect, Dual GTX 3000 Installation

  4
• 4.3.3 Altimeter Selection Priority

  4
• AF4.4 Discrete Functions

  4
• 4.4.1 Discrete Outputs

  4
• 4.4.2 Discrete Inputs

  4
• 4.5 Serial Data Electrical Characteristics

  4
• RS-232 Input/Output

  4
• RS-422 Input/Output

  4
• Configuration Module Connections

  4
• ARINC 429 Input/Output

  4
• 4.6 RS-232 Input/Output, Software Update Connections

  4
• Section 1 GENERAL DESCRIPTION

  1
• Section 2 INSTALLATION OVERVIEW

  2
• Figure 2-1 Antenna Installation Considerations

  2
• Figure 2-2 GTX 3000 Stand Rack (011-02515-00)

  2
• Figure 2-3 GTX 3000 Rack, Suggested Mounting Locations

  2
• Section 3 INSTALLATION PROCEDURE

  3
• Section 4 SYSTEM INTERCONNECTS

  4
• Figure 4-1 View of J3301 connector, looking at unit

  4
• Figure 4-2 View of J3302 connector, looking at unit

  4
• AFFigure 4-3 GTX 3000 Software Update Connections

  4
• Section 1 GENERAL DESCRIPTION

  1
• General Specifications

  1
• Transponder Capabilities

  1
• GTX 3000 with 011-02515-00 Rack

  1
• Power Requirements

  1
• TSO/ETSO/RTCA/ICAO Compliance

  1
• TSO/ETSO Deviations

  1
• Reference Documents

  1
• Section 2 INSTALLATION OVERVIEW

  2
• Installation Materials

  2
• Available Equipment

  2
• Connector Kit (011-02019-00)

  2
• Connector Kit, 90 Degree (011-02019-01)

  2
• Cable Specifications

  2
• Maximum Difference in Cable Lengths

  2
• Section 3 INSTALLATION PROCEDURE

  3
• Table 3-1: Pin Contact Part Numbers

  3
• Table 3-2 Recommended Crimp Tools

  3
• Table 3-3 Unit Power Loads

  3
• Section 4 SYSTEM INTERCONNECTS

  4
• Table 4-1 P3301 Pin List

  4
• Table 4-2 P3302 Pin List

  4
• Table 4-3 Aircraft Power

  4
• Table 4-4 Altimeter Inputs

  4
• Table 4-5 Discrete Outputs

  4
• Table 4-6 Discrete Inputs

  4
• Table 4-7 RS-232 Input/Output

  4
• Table 4-8 RS-422 Input/Output

  4
• Table 4-9 Configuration Module Connections

  4
• Table 4-10 ARINC 429 Input/Output

  4
• Table 4-11 Transmit Data Labels

  4