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General| Type | Transponder |
|---|---|
| Weight | 1.5 lbs (0.68 kg) |
| DSC Capability | No |
| GPS Integration | Yes |
| Waterproof Rating | IPX7 |
| Interface | NMEA 0183 |
| Frequency Range | 156-162 MHz |
| Power Output | 5W |
Overview of the GTX 33 Mode S Transponder and its installation.
Details the GTX 33 rack mounted Mode S Transponder's function and capabilities.
Explains the Automatic Dependent Surveillance-Broadcast (ADS-B) technology capabilities of the GTX 33.
Describes the Traffic Information Service (TIS) graphic display for non-TCAS equipped aircraft.
Discusses mutual suppression pulses relevant to transponder operation.
Lists the interface connections available via the GTX 33's rear connector.
Details the physical and general specifications of the GTX 33 transponder.
Outlines compliance with current transmitter licensing requirements for aircraft.
Discusses TSO approval standards and aircraft installation requirements.
Lists publications for additional information regarding GTX 33 installation.
Details the warranty terms and conditions for Garmin avionics products.
Provides equipment information for installing the GTX 33 Mode S Transponder and related hardware.
Lists the part numbers for the GTX 33 unit and its availability.
Covers general installation considerations for the GTX 33 in various aircraft systems.
Details cabling and wiring requirements for the GTX 33 installation.
Addresses FAA approval requirements for installations on pressurized aircraft.
Provides information for testing load-carrying capabilities of mounting structures.
Details how to determine the structural capability for mounting the GTX 33.
Details the procedure for carefully unpacking and inspecting the GTX 33 unit for shipping damage.
Covers the installation of wiring harnesses, including connector details and caution for wiring errors.
Explains the assembly of the backshell and grounding methods for the GTX 33 connector.
Outlines the requirement for weight and balance computation after GTX 33 installation.
Details the process of completing an electrical load analysis for the aircraft installation.
Refers to outline and installation drawings for final assembly of the GTX 33.
Covers post-installation steps including configuration and operational checkout procedures.
Specifies testing requirements for continued airworthiness and maintenance approach.
Provides a list of pin assignments for the P3301 connector.
Details the aircraft power input and switched power output functions.
Lists the pin assignments for various altimeter inputs used by the GTX 33.
Lists discrete outputs available from the GTX 33, including altitude alert and suppression.
Discusses serial data interfaces supported by the GTX 33, including GPS and ARINC 429.
Covers RS-232 connections for software upgrades and system integration.
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