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RevisionRevision DateSubject
15/8/15Experimental Release.
190-01499-02GTX 3x5 TSO Installation Manual
Rev. 1Page A
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DEFINITIONS OF WARNINGS, CAUTIONS, AND NOTES
Warnin g s indicate that immediate attention must be given to avoid potential equipment
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190-01499-02GTX 3x5 TSO Installation Manual
Rev. 1Page i
TABLE OF CONTENTS
1 SYSTEM OVERVIEW .....................................................................................................................1-1
190-01499-02GTX 3x5 TSO Installation Manual
Rev. 1Page v
1SYSTEM OVERVIEW
NOTE
1.1Scope
Mechanical and electrical information for use in the planning and design of an installation of the GTX 3x5
into an aircraft is provided in this manual. This manual is not a substitute for an approved airframe-specific
maintenance manual, installation design drawing, or complete installation data package. Attempting to
install equipment by reference to this manual alone and without first planning or designing an installation
specific to your aircraft may compromise your safety and it is not recommended. The content of this
manual assumes use by competent and qualified avionics engineering personnel and/or avionics
installation specialist using standard maintenance practices in accordance with Title 14 of the Code of
Federal Regulation and other relevant accepted practices.
Garmin recommends installation of the GTX 3x5 by a Garmin–authorized installer. To the
extent allowable by law, Garmin will not be liable for damages resulting from improper or
negligent installation of the GTX 3x5. For questions, contact Garmin Aviation Product
Support at 1-888-606-5482.
1.2Equipment Description
The GTX 3x5 is a family of ATCRBS and Mode S transponders, with some models including ADS-B in
capabilities and optional internal GPS/WAAS receivers. The following is a summary of the different units.
Table 1-1 GTX 3x5 Units
GTX
335R
w/
GPS
GTX
345
GTX 3
45 w/
GPS
GTX
345R
GTX 3
45R w/
GPS
Feature
ATCRBSX
GTX
325
GTX
335
GTX
335 w/
GPS
GTX
335R
Mode SXXXXXXXX
Panel MountXXXXX
RemoteXXXX
ADS-B out (1090)XXXXXXXX
ADS-B in
(UAT,1090)
Internal GPSXXXX
BluetoothXXXX
XXXX
The GTX 325 is an ATCRBS transponder.
The GTX 335 is a Mode S transponder with ADS-B extended squitter capability.
The GTX 345 is a Mode S transponder with ADS-B extended squitter capability and also includes UAT
and 1090 receivers for ADS-B in capabilities.
The GTX 335 and GTX 345 units can be ordered with an internal GNSS receiver, used for the ADS-B
extended squitter output or as remote-mounted units. Remote mounted units do not have a front panel with
a display or keypad.
Except where specifically noted, references made to GTX 3x5 will equally apply to all GTX 3x5 variants.
Abbreviations
The following abbreviations/acronyms are used within this document:
ACAdvisory Circular
ADFAutomatic Direction Finder
ADS-BAutomatic Dependent Surveillance-Broadcast
ADS-RAutomatic Dependent Surveillance-Rebroadcast
AFMSAircraft Flight Manual Supplement
ATCRBSAir Traffic Control Radar Beacon System
CFRCode of Federal Regulations
CGCenter of Gravity
CSAConflict Situational Awareness
DCDirect Current
DMEDistance Measuring Equipment
EQFEnvironmental Qualification Form
FAAFederal Aviation Administration
FCCFederal Communications Commission
FIS-BFlight Information Services-Broadcast
FMSFlight Manual Supplement
GNSSGlobal Navigation Satellite System
GPSGlobal Positioning System
HSDBHigh Speed Data Bus
LATLatitude
LONLongitude
MFDMultifunction Display
POHPilot Operating Handbook
RFMSRotorcraft Flight Manual Supplement
SATCOMSatellite Communications
SBASSatellite-Based Augmentation System
TASTraffic Advisory System
TCASTraffic Collision Avoidance System
TIS-BTraffic Information Service-Broadcast
TSOTechnical Standing Order
UATUniversal Access Transceiver
UHFUltra-High Frequency
USBUniversal Serial Bus
VHFVery High Frequency
WAASWide Area Augmentation System
ADS-B technology is used to improve situational awareness and flight safety. With ADS-B capabilities,
position, velocity, and heading information are automatically transmitted to other aircraft and ground
stations. ADS-B provides automatic transmission of aircraft information without a request.
1.4.1ADS-B Out
When properly installed with a GPS position source, meeting the guidance of AC 20-165 the GTX 335 and
GTX 345 include ADS-B Out capabilities. See section __ for additional information. The GTX 335 and
GTX 345 will broadcast the position, velocity, and heading information using the mode S transponder
transmitter.
1.4.2ADS-B In
The GTX 345 includes 978 MHz UAT and 1090 MHz receivers for ADS-B In capabilities. The GTX 345
can receive airborne position from other aircraft with either the UAT or 1090 MHz receivers. The
GTX 345 can receive FIS-B information from ground stations.
1.4.3Installation Approval for ADS-B Systems
Need information
1.5TIS System Capabilities
The GTX 3x5 provides uplink information of nearby traffic from the TIS. TIS is a ground-based service
providing relative location of all transponder equipped aircraft within a specified service area. The TIS
ground sensor uses real time track reports to generate traffic notifications. TIS provides a graphical display
of traffic advisory information in the cockpit for non-TCAS equipped aircraft.
Advisory traffic information is available to aircraft equipped with a Mode S data link such as the Garmin
GTX 335 or GTX 345. Advisory traffic information may be displayed on a Garmin 400W/500W Series
unit.
The GTX 3x5 unit can be incorporated into installations with other compatible control/display units such
as the Garmin GNS 480 (CNX80), GTN 6XX/7XX, GMX 200, and MX20 MFD.
Surveillance data is provided for transponder equipped aircraft within the coverage volume. Aircraft
without an operating transponder are invisible to TIS. TIS displays traffic within seven nautical miles from
3000 feet below to 3500 feet above the requesting aircraft. The pilot sees the location, relative direction
and altitude of other aircraft.
It is the responsibility of the installing agency to obtain the latest revision of the GTX 3x5 EQF. To obtain
a copy of the EQF, see Garmin’s Dealer Resource Center
Table 1-3 Physical Characteristics - Panel Mount Units
CharacteristicSpecification
Bezel height1.65 inches (42 mm)
Bezel width6.25 inches (159 mm)
Rack height (dimple to dimple)1.68 inches (43 mm)
Rack width6.30 inches (160 mm)
Depth behind panel with connectors (measured from face of aircraft
panel to rear of connector backshells)
GTX 325 weight (unit only)2.01 lb (0.91 kg)
GTX 335 weight (unit only)2.01 lb (0.91 kg)
GTX 335 with GPS weight (unit only)2.12 lb (0.96 kg)
GTX 345 weight (unit only)2.27 lb (1.01 kg)
GTX 345 with GPS weight (unit only)2.38 lb (1.08 kg)
GTX 325 installed with rack and connectors2.83 lb (1.28 kg)
GTX 335 installed with rack and connectors2.83 lb (1.28 kg)
GTX 335 with GPS installed with rack and connectors2.94 lb (1.33 kg)
GTX 345 installed with rack and connectors3.09 lb (1.40 kg)
GTX 345 with GPS installed with rack and connectors3.20 lb (1.45 kg)
Operating temperature range
Altitude range55,000 feet
Humidity95% non-condensing
CoolingExternal cooling not required
Audio output100 mW into 500 Ω
.
10.07 inches (256 mm)
-4°F to 131°F (-20°C to + 55°C)
For more details refer to the
environmental qualification forms at
Garmin’s Dealer Resource Center
See appendix A for form part
numbers.
Antenna performance is critical to GNSS receiver operation. Antennas listed in table 1-10 meet
specifications outlined in Antenna Minimum Performance Specification for Garmin’s GPS/WAAS Receiver System. To achieve acceptable performance with the GTX 335 or GTX 345 with internal GNSS receiver,
antennas listed table 1-10 must be used.
Table 1-10 GNSS Receiver Antennas
Model/Description
GA 35, GPS/WAAS TNC
GA 36, GPS/WAASTNC
GA 37, GPS/WAAS/
XM
A33W, WAAS
Antenna
GPS/VHF AntennaTNC/BNC ComantCI-2580-200N/A
GPS/VHF AntennaTNC/BNC ComantCI-2728-200N/A
GPS/XM/VHF
Antenna
GPS/XM/VHF
Antenna
GPS/WAAS AntennaTNCComantCI-428-200N/A
GPS/XM AntennaTNC/TNCComantCI-428-410N/A
Connector
Type
TNC
TNC
TNC/TNC/BNC ComantCI-2580-410N/A
TNC/TNC/BNC ComantCI-2728-410N/A
ManufacturerP/N
Garmin013-00235-( )013-00235-( )
Aero Antenna
Garmin013-00244-( )013-00244-( )
Aero Antenna
Garmin013-00245-( )013-00245-( )
Aero Antenna
Garmin013-00261-( )013-00261-( )
Aero Antenna
AT575-93G( )-TNCF-000-RG-27NM
AT575-126G( )-TNCF-000-RG-27NM
AT2300-126G( )-TNCF-000-RG-27NM
AT575-332G( )-TNCF-000-RG-27NM
Garmin
Order
Number
[1] Same mounting hole pattern as GA 56, except GA 35 has a physically larger footprint.
[2] The GPS antenna connector is a TNC and the VHF connector is BNC.
[3] The GPS antenna connector is a TNC connector, the XM connector is TNC, and the VHF
The GTX 3x5 meets compliance with the claimed TSO(s) when interfaced with the equipment defined in
this manual, and installed in accordance with the requirements and limitations as defined.
The Appliance Project Identifier (API) for the GTX 3x5 is GMN-01216. The API is used for project
identification with the FAA and EASA. In addition, the alpha character appended to the end of the API in
the ETSO certificate is added to supplement project identification by EASA. This alpha character does not
represent a version number. To identify appliance approvals, see applicable hardware and software
numbers.
It is the installer’s responsibility to ensure the ADS-B Out system is compliant with AC 20-165 and to
ensure compatibility between the GTX 335 or GTX 345 and the ADS-B Out position source equipment.
For compatible equipment shown to be eligible for 14 CFR 91.227 compliant installations in accordance
with AC 20-165, see 14 CFR 91.227 ADS-B Out Compatible Equipment.
Air Traffic Control Radar Beacon System / Mode Select (ATCRBS/Mode S)
Airborne Equipment
Airborne Navigation Sensors Using the Global Positioning System
Augmented by the Satellite Based Augmentation System
Universal Access Transceiver (UAT) Automatic Dependent Surveillance –
Broadcast (ADS-B) Equipment Operating on Frequency of 978 MHz
Aircraft Flight Information Services – Broadcast (FIS-B) Data Link System
and Equipment
Extended Squitter Automatic Dependent Surveillance – Broadcast (ADS-B)
and Traffic Information Service – Broadcast (TIS-B) Equipment Operating on
the Radio Frequency of 1090 Megahertz (MHz)
1. Garmin requests a deviation from the mentioned TSOs to use RTCA DO-160G instead
TSO-C74d
TSO-C88b
TSO-C112e
of earlier versions of RTCA/DO-160 as the standard for Environmental Conditions and
Test Procedures for Airborne Equipment. ELOS is provided by use of later revision
requirement document. Refer to AC 21-16G for supporting guidance.
1. Garmin requests a deviation from the mentioned TSOs for marking the TSO number,
Type/Class and Date of Manufacture, Deviation and Software Part Number on the
exterior of the unit. Instead, Garmin requests to include product name, part number,
serial number, and this statement on the unit’s nameplate label “TSO-C112e See IM for
Add’l Appliance Apprvls.” The installation manual will contain all equipment approvals,
classes/types/ranges and TSO deviations as required by the TSOs, and the software
part numbers for the unit will be available through electronic query within the unit. ELOS
is provided because the installation manual will list all applicable information and the
article will permanently and legibly list the Primary TSO and state “See IM for Add’l
Appliance Apprvls.” All software part numbers can be verified through electronic query.
See Order 8150.1C Section 7-4e-4 and 8110.49 for further supporting statement of
policy.
1. Garmin requests a deviation from the mentioned TSOs for marking the TSO number,
Type/Class and Date of Manufacture, Deviation and Software Part Number on the
exterior of the unit. Instead, Garmin requests to include product name, part number,
serial number, and this statement on the unit’s nameplate label “TSO-C112e See IM for
Add’l Appliance Apprvls.” The installation manual will contain all equipment approvals,
classes/types/ranges and TSO deviations as required by the TSOs, and the software
part numbers for the unit will be available through electronic query within the unit. ELOS
is provided because the installation manual will list all applicable information and the
article will permanently and legibly list the Primary TSO and state “See IM for Add’l
Appliance Apprvls.” All Software part numbers can be verified through electronic query.
See Order 8150.1C Section 7-4e-4 and 8110.49 for further supporting statement of
policy.