190-00906-00
GTX 33 Installation Manual
Rev. F
Page iii
1
GENERAL DESCRIPTION
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1-1
1.1 Introduction
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1-1
1.2 Equipment Description
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1-1
1.3 ADS-B Capabilities
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1-2
1.4 TIS System Capabilities
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1-3
1.5 Mutual Suppression Pulses
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1-3
1.6 Interface Summary
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1-4
1.7 Technical Specifications
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1-5
1.8 License Requirements
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1-7
1.9 Certification
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1-8
1.10 Reference Documents
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1-11
1.11 Limited Warranty
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1-12
2
INSTALLATION OVERVIEW
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2-1
2.1 Introduction
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2-1
2.2 Installation Materials
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2-1
2.3 Installation Considerations
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2-3
2.4 Cabling and Wiring
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2-5
2.5 Installation Approval Considerations for Pressurized Aircraft
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2-6
2.6 Cooling Air
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2-6
2.7 GTX 33 Mounting Requirements
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2-7
3
INSTALLATION PROCEDURE
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3-1
3.1 Unpacking Unit
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3-1
3.2 Wiring Harness Installation
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3-2
3.3 Backshell Assembly
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3-3
3.4 Weight and Balance
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3-5
3.5 Electrical Load Analysis
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3-5
3.6 Final Installation
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3-5
3.7 Post Installation Configuration and Checkout
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3-6
3.8 Continued Airworthiness
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3-8
4
SYSTEM INTERCONNECTS
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4-1
4.1 Pin List
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4-1
4.2 Power Functions
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4-4
4.3 Temperature Inputs
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4-4
4.4 Altitude Functions
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4-5
4.5 Discrete Functions
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4-7
4.6 Serial Data Electrical Characteristics
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4-8
4.7 RS-232 Input/Output, Software Update Connections
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4-11