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Garmin GTX 3X5 Series Installation Manual Download Page 9

190-01499-02

GTX 3X5 Transponder TSO Installation Manual

Rev. 4

Page v

LIST OF FIGURES

Figure 3-1 

Air Data Discrete Priority Order........................................................................................3-11

Figure 3-2 

Pressure Altitude Priority Order ........................................................................................3-12

Figure 3-3 

GPS Locations of Antennas...............................................................................................3-23

Figure 4-1 

Shielded Cable Preparation..................................................................................................4-4

Figure 4-2 

Shield Termination on Backshell Assembly........................................................................4-6

Figure 4-3 

Connector and Backshell Assembly ....................................................................................4-7

Figure 4-4 

Configuration Module Installation ......................................................................................4-9

Figure 6-1 

Audio Group ........................................................................................................................6-3

Figure 6-2 

Audio Page...........................................................................................................................6-4

Figure 6-3 

Audio Page 2........................................................................................................................6-4

Figure 6-4 

Audio Page 3........................................................................................................................6-4

Figure 6-5 

Interface Group....................................................................................................................6-5

Figure 6-6 

RS-232 Interface Page .........................................................................................................6-7

Figure 6-7 

RS-422 Output Page ............................................................................................................6-8

Figure 6-8 

A429 In Page .......................................................................................................................6-9

Figure 6-9 

A429 Output Page..............................................................................................................6-10

Figure 6-10  HSDB Interface Page.........................................................................................................6-11
Figure 6-11  Discrete In Page.................................................................................................................6-12
Figure 6-12  Discrete Out Page ..............................................................................................................6-13
Figure 6-13  Unit Group .........................................................................................................................6-14
Figure 6-14  FIS-B Processing Page ......................................................................................................6-14
Figure 6-15  Altitude and Temperature Units Page................................................................................6-15
Figure 6-16  Installation and VFR ID Page............................................................................................6-15
Figure 6-17  Altitude Alert Deviation and Restore Page .......................................................................6-16
Figure 6-18  Bluetooth Page...................................................................................................................6-16
Figure 6-19  Display Group....................................................................................................................6-17
Figure 6-20  Display Pages.....................................................................................................................6-18
Figure 6-21  Sensor Group .....................................................................................................................6-20
Figure 6-22  Sensor Page........................................................................................................................6-21
Figure 6-23  Altitude Source Page .........................................................................................................6-21
Figure 6-24  Source, Integrity, and Offset Page.....................................................................................6-23
Figure 6-25  Internal Alt Encoder Page..................................................................................................6-23
Figure 6-26  Internal Alt Encoder Adjustment Page ..............................................................................6-23
Figure 6-27  Setting the Yaw Angle.......................................................................................................6-24
Figure 6-28  Internal AHRS Orientation Page .......................................................................................6-24
Figure 6-29  ADS-B Group ....................................................................................................................6-25
Figure 6-30  Aircraft Category and Max Airspeed Page........................................................................6-26
Figure 6-31  Aircraft Length and Width Page........................................................................................6-27
Figure 6-32  1090ES Out Control and UAT Out Remote Control Page ................................................6-27
Figure 6-33  1090ES In Capable and UAT In Capable Page .................................................................6-27
Figure 6-34  ADS-B In Processing Page................................................................................................6-28
Figure 6-35  Aircraft Tail Number and Address Page ...........................................................................6-28
Figure 6-36  Allow Pilot to Edit Flight ID Page ....................................................................................6-28
Figure 6-37  Default Flight ID and Flight ID Prefix Page .....................................................................6-29
Figure 6-38  Diagnostics Group .............................................................................................................6-30
Figure 6-39  Diagnostics Page................................................................................................................6-31
Figure 6-40  USB-A and USB-B Connectors.........................................................................................6-32
Figure 6-41   Aircraft Configuration Page .............................................................................................6-33

Summary of Contents for GTX 3X5 Series

Page 1: ...190 01499 02 February 2016 Revision 4 GTX 3X5 Transponder TSO Installation Manual ...

Page 2: ...ational or its subsidiaries Connext GDU and GTN are trademarks of Garmin International or its subsidiaries These trademarks may not be used without the express permission of Garmin 2016 SiriusXM Radio Inc Sirius XM and all related marks and logos are trademarks of SiriusXM Radio Inc All other marks and logos are property of their respective owners All rights Reserved Skywatch is a registered trade...

Page 3: ...e B RECORD OF REVISIONS Revision Revision Date Subject 2 12 14 15 Reorganized manual 3 2 11 16 Rewrote for clarity Refer to current revision description 4 2 26 2016 Added information for vertical remote mount and other minor edits Refer to current revision description ...

Page 4: ... vertical remote mount to table 3 2 3 4 3 Added GTX 3X5 Vertical Remote Mount section 4 7 2 Added Standard to heading 4 7 3 Added Vertical Remote Mount Units section 4 9 Added Vertical Remote Mount Unit Installation and Removal section Appendix B Added GTX 3X5 Vertical Remote Mount as figure B 5 Added GTX 3X5 Vertical Remote Mount Dimensions and CG as figure B 6 Appendix D Updated figure D 3 Updat...

Page 5: ...S OF WARNINGS CAUTIONS AND NOTES WARNING This product s packaging and components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to Garmin s website www garmin com prop65 WARNING Perchlorate Material...

Page 6: ... Data Concentrator Function 2 1 3 INSTALLATION OVERVIEW 3 1 3 1 Introduction 3 2 3 2 Unit Configurations 3 2 3 3 Accessories Supplied 3 3 3 4 Optional Accessories 3 5 3 5 Necessary Installation Materials and Accessories Not Supplied 3 7 3 6 Necessary Special Tools 3 7 3 7 Transponder Antenna 3 8 3 8 GPS Antenna Requirements 3 9 3 9 Minimum Systems Configuration 3 10 3 10 GTX Input Source Priority ...

Page 7: ...GURATION AND CHECKOUT 6 1 6 1 System Configuration Overview 6 1 6 2 Mounting Wiring and Power Checks 6 1 6 3 Configuration Mode and Settings 6 2 6 4 Audio Settings 6 3 6 5 Interfaces 6 5 6 6 Unit Settings 6 14 6 7 Display Pages 6 17 6 8 Sensors 6 20 6 9 ADSB 6 25 6 10 Diagnostics 6 30 6 11 Remote Unit Configuration 6 32 6 12 Ground Check GPS Reception Check 6 40 6 13 Software Installation Procedur...

Page 8: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page iv TABLE OF CONTENTS CONTINUED C 10 TIS A Display C 10 APPENDIX D INTERCONNECT DRAWINGS D 1 ...

Page 9: ...ation and VFR ID Page 6 15 Figure 6 17 Altitude Alert Deviation and Restore Page 6 16 Figure 6 18 Bluetooth Page 6 16 Figure 6 19 Display Group 6 17 Figure 6 20 Display Pages 6 18 Figure 6 21 Sensor Group 6 20 Figure 6 22 Sensor Page 6 21 Figure 6 23 Altitude Source Page 6 21 Figure 6 24 Source Integrity and Offset Page 6 23 Figure 6 25 Internal Alt Encoder Page 6 23 Figure 6 26 Internal Alt Encod...

Page 10: ...ck Assembly with GTX 345R GPS Shown B 8 Figure B 8 G1000 Mounting Rack Dimensions and CG with GTX 345R GPS Shown B 9 Figure B 9 GTX 3X5 Panel Cutout Detail B 10 Figure B 10 GTX 3X5 Connector and Vent Locations B 11 Figure B 11 Optional Garmin Altitude Encoder B 11 Figure D 1 GTX 3X5 Power Configuration Typical Interconnect D 3 Figure D 2 GTX 345 Legacy G1000 Interconnect D 5 Figure D 3 GTX 335 Leg...

Page 11: ...p Tools 3 7 Table 3 7 Acceptable UAT 1090 Antennas 3 8 Table 3 8 GNSS Receiver Antennas 3 9 Table 3 9 Minimum System Configuration 3 10 Table 3 10 Compatible ADS B Traffic FIS B Displays 3 10 Table 3 11 Air Data Select Source Priority 3 12 Table 3 12 Barometric Vertical Rate Source Priority 3 13 Table 3 13 Indicated Airspeed Source Priority 3 13 Table 3 14 True Airspeed Source Priority 3 13 Table ...

Page 12: ... 5 10 ARINC 429 Inputs and Outputs 5 9 Table 5 11 Ethernet Inputs and Outputs 5 10 Table 5 12 RS 422 Outputs 5 10 Table 5 13 External Suppression Bus Pin 5 10 Table 5 14 OAT Input and Output 5 10 Table 5 15 Audio Inputs and Outputs 5 11 Table 5 16 Time Mark Outputs 5 11 Table 5 17 Configuration Module Inputs and Outputs 5 11 Table 5 18 USB Inputs and Outputs 5 12 Table 6 1 RS 232 Channel 1 through...

Page 13: ... 1 6 TIS System Capabilities 1 7 1 7 Interface Summary 1 7 1 8 General Specifications 1 8 1 9 Transponder Specifications 1 10 1 10 UAT Receiver Specifications GTX 345 Only 1 10 1 11 1090 MHz Receiver Specifications 1 11 1 12 GPS Specifications Units with Internal GPS Only 1 11 1 13 Power Specifications 1 12 1 14 Certification 1 13 1 14 1 Non TSO Functions 1 15 1 14 2 Design Assurance Levels 1 15 1...

Page 14: ...upport at 888 606 5482 for questions This manual gives mechanical and electrical information to install the GTX 3X5 into an aircraft It is not equivalent to an approved airframe specific maintenance manual installation design drawing or installation data package The content of this manual assumes use by competent and qualified avionics engineering personnel and or avionics installation specialist ...

Page 15: ...TX 345R GTX 345R w GPS Mode S ES X X X X X X X X X External ADS B control X X X X X ARINC 429 data concentrator X X X X X X X X X ADS B In with alerting UAT and 1090 MHz X X X X Connext via Bluetooth X X X X FIS B X X X X TIS traffic X X X X X ADS B In and TAS TCAS traffic integration X X X X HSDB forwarding X X X X Pressure sensor module optional X X X X X X X X X Flight timers X X X X X Audio ou...

Page 16: ...S Aircraft Flight Manual Supplement AIRMET Airmen Meteorological Information API Appliance Project Identifier CDTI Cockpit Display of Traffic Information ATCRBS Air Traffic Control Radar Beacon System CFR Code of Federal Regulations CG Center of Gravity CONUS Continental United States CSA Conflict Situational Awareness DC Direct Current DME Distance Measuring Equipment EQF Environmental Qualificat...

Page 17: ...ed Augmentation System SIGMET Significant Meteorological Information SIL Source Integrity Level SPI Special Position Indicator SUA Special Use Airspace TAF Terminal Area Forecast TAS Traffic Advisory System TCAS Traffic Collision Avoidance System TIS Traffic Information Service TIS B Traffic Information Service Broadcast TSO Technical Standard Order UAT Universal Access Transceiver UHF Ultra High ...

Page 18: ... the applicable airworthiness requirements All GTX 3X5 unit functions are design approved under the TSO Changes or modifications to any unit that are not approved can void the compliance to necessary regulations and authorization for continued equipment usage It is the installer s responsibility to make sure the ADS B Out system installation is compliant with 14 CFR 91 227 and to make sure compati...

Page 19: ...1 Can be configured to be either input or output on a per discrete basis 2 Use for either the configuration module or combination configuration module GAE 3 The Gray code altitude input pins can be used for other functions when not used for Gray code Interface Description Input Output GTX 335 Qty GTX 345 Qty RS 232 I O 3 4 ARINC 429 O 1 1 I 2 2 HSDB I O N A 2 RS 422 I or O N A 1 Discrete I O I 3 1...

Page 20: ...ircraft panel to rear of connector backshells 10 07 inches 256 mm GTX 335 weight unit only 2 0 lbs 0 91 kg GTX 335 with GPS weight unit only 2 1 lbs 0 95 kg GTX 345 weight unit only 2 3 lbs 1 04 kg GTX 345 with GPS weight unit only 2 4 lbs 1 10 kg GTX 335 with rack backplate and connectors 2 8 lbs 1 27 kg GTX 335 with GPS with rack backplate and connectors 2 9 lbs 1 32 kg GTX 345 with rack backpla...

Page 21: ...d mounting tray backplate and connectors 2 5 lb 1 13 kg GTX 335R with GPS weight withstandard mounting tray backplate and connectors 2 7 lb 1 22 kg GTX 345R weight with standard mounting tray backplate and connectors 2 9 lb 1 32 kg GTX 345R with GPS with standard mounting tray backplate and connectors 3 0 lb 1 36 kg GTX 335R weight with vertical remote mount backplate and connectors 3 0 lb 1 35 kg...

Page 22: ... Height 0 486 inches 12 36 mm Resolution 200 x 33 pixels Viewing angle Left 45 Right 45 From top 30 From bottom 10 Characteristic Specification Transmitter frequency 1090 MHz 1 MHz Transmitter power 125 W min at antenna with max 2dB cable loss 250 W nominal at unit Receiver frequency 1030 MHz 0 01 MHz Receiver sensitivity 74 dBm nominal for 90 replies External suppression input 10 VDC to suppress ...

Page 23: ...GPS and 3 GPS SBAS Frequency 1575 42 MHz L1 C A code Sensitivity acquisition no interference 134 5 dBm GPS 135 5 dBm SBAS Sensitivity drop lock 144 dBm Dynamic range 20 dB LAT LON position accuracy 1 25 meter RMS horizontal 2 meter vertical with SBAS Velocity 1000 knots maximum above 60 000 ft TTFF Time To First Fix 1 45 min typical with current almanac position and time Reacquisition 10 seconds t...

Page 24: ...cteristic Specification 14 VDC 28 VDC GTX 335 Power input 8 W typical 15 W maximum Input current typical 0 57 A 0 29 A Input current maximum 0 86 A 0 43 A GTX 335 GPS Power input 10 W typical 17 W maximum Input current typical 0 72 A 0 36 A Input current maximum 1 22 A 0 61 A GTX 345 Power input 10 W typical 18 W maximum Input current typical 0 72 A 0 36 A Input current maximum 1 30 A 0 65 A GTX 3...

Page 25: ...nal GAE module GTX 335 GTX 345 TSO Class and Level Function X 2 X 2 TSO C88b Automatic Pressure Altitude Reporting Code Generating Equipment X X TSO C112e Class 1 Level 2els Air Traffic Control Radar Beacon System Mode Select ATCRBS Mode S Airborne Equipment X 1 X 1 TSO C145d Class B2 Airborne Navigation Sensors Using the Global Positioning System Augmented by the Satellite Based Augmentation Syst...

Page 26: ...29D Change 1 section 2 1 1 10 to use GPS antennas that meet Garmin Minimum Performance Specifications Document No 004 00287 00 TSO C154c 1 Garmin is granted a deviation from the TSO for marking the TSO number Type Class and Date of Manufacture Deviation and Software Part Number on the exterior of the unit TSO C157a 1 Garmin is granted a deviation from the TSO for marking the TSO number Type Class ...

Page 27: ...uetooth interface GTX 345 1 14 2 Design Assurance Levels Table 1 14 Software Design Assurance Levels System Function DO 178B Level Mode S transponder functionality C Display of TIS A traffic data C Flight information data FIS B including weather information processing and output to display D Display of outside air temperature static C Flight timers C 1090 ADS B transmission C 1090 UAT ADS B recept...

Page 28: ... Telecommunications Act of 1996 effective February 8 1996 provides the FCC discretion to eliminate radio station license requirements for aircraft and ships The GTX 3X5 installation must obey current transmitter licensing requirements In the US to find out the specific details on whether a particular installation is exempt from licensing visit the FCC website http wireless fcc gov aviation If an a...

Page 29: ...0 01533 00 Antenna Minimum Performance Specification for Garmin s GPS WAAS Receiver System 004 00287 00 G1000 System Installation Manual 190 00303 00 GTX 3X5 Pilot s Guide 190 01499 00 GTX 3X5 Series Transponder G1000 Pilot s Guide 190 01499 01 GTX 3X5 Environmental Qualification Form 005 00752 02 Document P N Aerospace Systems Electrical Bonding and Grounding for Electromagnetic Compatibility and...

Page 30: ...stallation of the GTX 3X5 requires separate approval 2 1 HSDB Packet Forwarding The GTX 345 HSDB interface is not approved for forwarding data whose failure condition for loss or malfunction is classified as hazardous or catastrophic 2 2 ARINC 429 Data Concentrator Function ARINC 429 data from the GTX 3X5 must not be used for any function whose associated failure is classified as hazardous or cata...

Page 31: ...3 5 Necessary Installation Materials and Accessories Not Supplied 3 7 3 6 Necessary Special Tools 3 7 3 7 Transponder Antenna 3 8 3 8 GPS Antenna Requirements 3 9 3 9 Minimum Systems Configuration 3 10 3 10 GTX Input Source Priority 3 11 3 11 GPS SBAS Parameters 3 20 3 12 Antenna Considerations 3 21 3 12 1 Transponder Antenna 3 21 3 12 2 GPS Antenna 3 22 3 13 Electrical Bonding 3 24 3 14 Cabling a...

Page 32: ... 01214 00 010 01214 01 GTX 335 NV Panel 011 03300 20 010 01214 20 010 01214 21 GTX 335 GPS Panel X 011 03300 40 010 01214 40 010 01214 41 GTX 335R Remote 011 03301 00 010 01215 00 010 01215 01 Standard GTX 335R Remote 011 03301 00 010 01215 00 010 01215 02 Vertical GTX 335R GPS Remote X 011 03301 40 010 01215 40 010 01215 41 Standard GTX 335R GPS Remote X 011 03301 40 010 01215 40 010 01215 42 Ver...

Page 33: ... rack 115 01771 00 Backplate assembly 011 02976 01 Connector kit 011 02977 00 Configuration module 011 00979 03 Product information kit K00 00598 01 GTX 335R standard mount 010 01215 01 Install rack 115 01771 00 Backplate assembly 011 02976 00 Connector kit 011 02977 00 Configuration module 011 00979 03 Product information kit K00 00598 02 GTX 335R vertical mount 010 01215 02 Install rack vertical...

Page 34: ...y 011 02976 01 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 03 GTX 345R standard mount 010 01217 01 Install rack 115 01771 00 Backplate assembly 011 02976 00 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 04 GTX 345R vertical mount 010 01217 02 Install rack vertical 011 03762 00 Backplate assembly 010...

Page 35: ... 4 GX000 System Rack 3 4 3 GTX 3X5 Vertical Remote Mount The GTX 3X5 vertical remote mount is available as separate components The base kit mounts to the aircraft The shoe kit mounts to the GTX 3X5 Table 3 5 GTX 3X5 Vertical Remote Mount Kits GTX 335R w GPS vertical mount 010 01217 42 Install rack vertical 011 03762 00 Backplate assembly 010 02976 11 Connector kit 011 02977 01 Configuration module...

Page 36: ...ed to the doubler Torque the four supplied 10 32 stainless steel screws 20 25 in lbs Apply torque equally across all mounting screws to avoid deformation of the mounting area Use a TNC plug to connect the GPS antenna coax cable GA 37 Antenna The antenna includes four 10 32 UNF 2A x 1 00 SS 303 mounting screws and one O ring It can be necessary to use an antenna doubler Refer to applicable antenna ...

Page 37: ...ectors for the transponder antenna and TNC connectors for the GPS antenna Approved pressure altitude source 3 6 Necessary Special Tools NOTE Insertion extraction tools from ITT Cannon are all plastic The others are plastic with metal tips Some connectors use crimp contacts Use crimp tools in table 3 6 to make sure reliable crimp contact connections for the rear D sub connectors are correct Table 3...

Page 38: ...t 978 MHz and 1 5 1 at 1090 MHz TSO C66 TSO C74 or TSO C112 antennas that also meet the VSWR specification Table 3 7 Acceptable UAT 1090 Antennas Manufacturer P N Model Description Connector Type Notes Aero Antenna AT130 16 DME Transponder TNC DC Grounded Comant CI 100 DME Transponder BNC Open Circuit CI 100 2 DME Transponder TNC Open Circuit CI 105 DME Transponder BNC Open Circuit CI 105 3 DME Tr...

Page 39: ...r is TNC and the VHF connector is BNC Model Description Connector Type Manufacturer P N Garmin Order Number GA 35 GPS WAAS 1 TNC Garmin 013 00235 013 00235 Aero Antenna AT575 93G TNCF 000 RG 27 NM N A GA 36 GPS WAAS TNC Garmin 013 00244 013 00244 Aero Antenna AT575 126G TNCF 000 RG 27 NM N A GA 37 GPS WAAS XM TNC Garmin 013 00245 013 00245 Aero Antenna AT2300 126G TNCF 000 RG 27 NM N A A33W WAAS A...

Page 40: ...ion Table 3 10 Compatible ADS B Traffic FIS B Displays Model Transponder Antenna Altitude Source External GPS SBAS Position Source GPS SBAS Antenna Control Panel ADS B Traffic FIS B Display or Traffic Light Audio Panel GTX 335 X X X GTX 335R X X X X GTX 335 w GPS X X X GTX 335R w GPS X X X X GTX 345 X X X X X GTX 345R X X X X X X GTX 345 w GPS X X X X X GTX 345R w GPS X X X X X X Display FIS B Sou...

Page 41: ...ng Static Air Temp Total Air Temp Table 3 10 YES Barometric Vertical Rate Table 3 11 Indicated Airspeed Table 3 12 True Airspeed Table 3 13 Barometric Pressure Setting Table 3 14 MCP FCU Selected Altitude Table 3 15 Magnetic Heading Table 3 16 True Heading Table 3 17 Static Air Temp Table 3 18 Total Air Temp Table 3 19 NO Applicable Priority Tables START Are the ARINC 429 Sources configured as EFI...

Page 42: ...RINC 429 EFIS ADC ADC input Is the Altitude Data Select discrete configured Pressure Altitude Table 3 20 Baro Corrected Altitude Table 3 23 YES Is the Air Data Select discrete configured Pressure Altitude Table 3 10 Baro Corrected Altitude Table 3 10 YES NO NO Are Altitude Sources 1 and or 2 configured Pressure Altitude Table 3 21 Baro Corrected Altitude Table 3 24 YES Pressure Altitude Table 3 22...

Page 43: ...DB Barometric Vertical Rate from GDU 620 1 7 HSDB Barometric Vertical Rate from GDU 620 2 Priority Source 1 ARINC 429 Label 206 from an ADC 2 ARINC 429 Label 206 from an EFIS ADC 3 RS 232 from an ADC 4 RS 232 from a remote control panel 5 HSDB Indicated Airspeed from a GX000 6 HSDB Indicated Airspeed from GDU 620 1 7 HSDB Indicated Airspeed from GDU 620 2 Priority Source 1 ARINC 429 Label 210 from...

Page 44: ...S ADC 2 ARINC 429 Label 234 from an EFIS ADC 3 ARINC 429 Label 235 from an AFCS 4 ARINC 429 Label 234 from an AFCS 5 RS 232 from an ADC 6 RS 232 from a remote control panel 7 HSDB Barometric Pressure Setting from a GX000 8 HSDB Barometric Pressure Setting from GDU 620 1 9 HSDB Barometric Pressure Setting from GDU 620 2 Priority Source 1 ARINC 429 Label 102 from an AFCS 2 ARINC 429 Label 102 from a...

Page 45: ... 7 HSDB Magnetic Heading from GTN 2 8 HSDB Magnetic Heading from a GX000 9 HSDB Magnetic Heading from GDU 620 1 10 HSDB Magnetic Heading from GDU 620 2 Priority Source 1 ARINC 429 Label 314 from a heading source 2 ARINC 429 Label 314 from an AHRS 3 ARINC 429 Label 314 from an EFIS ADC 4 RS 232 from a remote control panel 5 HSDB True Heading from a GX000 Priority Source 1 ARINC 429 Label 213 from a...

Page 46: ...3 RS 232 from an ADC 4 RS 232 from a remote control panel 5 HSDB Total Air Temperature from a GX000 6 HSDB Total Air Temperature from GDU 620 1 7 HSDB Total Air Temperature from GDU 620 2 8 Outside air temperature sensor if OAT Sensor Installed is active Altitude Data Select Discrete Source Open RS 232 from a remote control panel Ground Source specified in Altitude Source Configuration 2 Priority ...

Page 47: ...trol panel 6 Optional GAE module 7 HSDB Pressure Altitude from GTN 1 8 HSDB Pressure Altitude from GTN 2 9 HSDB Pressure Altitude from a GX000 10 HSDB Pressure Altitude from GDU 620 1 11 HSDB Pressure Altitude from GDU 620 2 12 Gray code altitude 13 RS 232 from a 100 ft resolution altitude source Altitude Data Select Discrete Source Open Source specified in Altitude Source Configuration 1 Ground S...

Page 48: ...urce 1 RS 232 from a remote control panel 2 HSDB Runway Information from GTN 1 3 HSDB Runway Information from GTN 2 4 HSDB Runway Information from a GX000 5 HSDB Runway Information from GDU 620 1 6 HSDB Runway Information from GDU 620 2 Priority Source 1 RS 232 from an ADC 2 RS 232 from a remote control panel 3 HSDB Density Altitude from a GX000 4 HSDB Density Altitude from GDU 620 1 5 HSDB Densit...

Page 49: ... 5 HSDB Radio Height from GTN 2 6 HSDB Radio Height from a GX000 7 HSDB Radio Height from GDU 620 1 8 HSDB Radio Height from GDU 620 2 Priority Source 1 ARINC 429 Labels 100 306 and 307 from an EFIS ADC Priority Source 1 RS 232 from a remote control panel 2 HSDB FMS Vertical Navigation Data from a GX000 3 HSDB FMS Vertical Navigation Data from GDU 620 1 4 HSDB FMS Vertical Navigation Data from GDU...

Page 50: ...xternal GPS receivers Latitude Longitude Height above ellipsoid Horizontal and vertical position accuracy data Horizontal position integrity data North south velocity East west velocity Up down velocity Ground speed Horizontal velocity accuracy Ground track Geometric vertical rate SIL and SIL supplement RAIM alarm Geoid altitude Time Date ...

Page 51: ...raft manufacturer s type certificated antenna location and style The antenna must be installed in accordance with manufacturer instructions and or AC 43 12 2A Chapter 3 Transponder antenna considerations help the installer to select the best location for the antenna The antenna should Be attached away from major protrusions such as engines nacelles propellers and antenna masts Be as far as practic...

Page 52: ...in order of importance to get the best performance The installer should use best judgment to balance the installation guidelines The GPS antenna should Be installed as near to level as possible with respect to the normal cruise flight attitude of the aircraft Be installed in a location to minimize the effects of airframe shadowing during typical maneuvers Be installed a minimum of two feet from an...

Page 53: ... MASKED BY VERTICAL FIN T TAIL OR DORSAL FIN ANTENNA NOT MOUNTED LEVEL WITH RESPECT TO THE NORMAL FLIGHT ATTITUDE GOOD BETTER GREATER THAN THREE INCHES OF WINDSCREEN NORMAL FLIGHT ATTITUDE ANTENNA MUST BE ON TOP OF AIRCRAFT CENTER LINE SHOULD BE GREATER THAN TWO FEET SIDE VIEW TOP VIEW GPS ANTENNA OFFSET FROM CENTERLINE WITH TYPICAL DUAL GPS INSTALLATION ...

Page 54: ...sources e g DC motors high heat sources Wiring that must be shielded must be done as shown in appendix D Shield pigtail lengths must be less than 3 0 inches 3 15 Electrical Bonding Considerations Bond electrical equipment supporting brackets and racks to the aircraft s main structure Refer to SAE ARP 1870 section 5 when surface preparation is necessary to get an electrical bond Use a calibrated mi...

Page 55: ...b connectors on the rear of the unit The shield grounds terminate to the connector backshells For additional information Refer to section 5 for rear connector pinout and descriptions of interface connections Refer to appendix D for interconnect diagrams Refer to section 3 12 for special tools Give sufficient space for installation of cables and connectors The installer supplies and assembles all c...

Page 56: ... 10 1 7 Strain relief P3251 Strain relief P3252 115 00499 03 115 00499 00 1 8 Cover P3251 Cover P3252 115 00500 03 115 00500 00 1 9 Screw 4 40x 187 FLHP100 SS P with nylon 211 63234 06 1 10 Connector D sub HD 62 pin P3251 Connector D sub HD 15 pin P3252 330 00185 62 330 00185 15 3 11 Multiple conductor shielded cable As necessary 4 12 Shield terminator As necessary 4 5 13 Wire insulated 20 22 AWG ...

Page 57: ...h a pre installed shield drain Prepare all of the shielded cables using one of the methods shown in figure 4 1 Refer to figure 4 2 for details of the shield termination to the connector backshell 1 At the end of the shielded cable 11 strip back a 2 5 maximum length of the jacket to expose the braid 2 Remove the exposed braid 3 Carefully score the jacket 1 4 to 5 16 from the end and remove the jack...

Page 58: ... 4 Page 4 4 Preferred Method Alternate Method Figure 4 1 Shielded Cable Preparation SHIELD DRAINS AS SHORT AS PRACTICAL NO LONGER THAN 3 0 31 OF EXPOSED SHIELD 2 5 MAX 0 17 SHIELD DRAINS AS SHORT AS PRACTICAL NO LONGER THAN 3 0 31 OF EXPOSED SHIELD 2 5 MAX 0 17 ...

Page 59: ... 1 Insert flathead screws 3 through holes on the shield block 2 2 Attach to the backshell 1 3 Insert the crimped wire harness contacts 14 in the D sub connector 10 Refer to appendix D for the chosen contact location 4 Install the configuration module or GAE wires into the connector if a configuration module or GAE is used Refer to section 4 5 5 Group wires as applicable for the connector 6 Wrap th...

Page 60: ... Installation Manual Rev 4 Page 4 6 Figure 4 2 Shield Termination on Backshell Assembly 0 326 2 11 1 2 6 0 62 7 217 7 6 5 5 5 5 5 5 5 5 5 PLACE SMOOTH SIDE OF STRAIN RELIEF ACROSS CABLE BUNDLE DO NOT PLACE GROOVED SIDE ACROSS CABLE BUNDLE ...

Page 61: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 4 7 Figure 4 3 Connector and Backshell Assembly 2 127 3 7 21 9 6 2 7 675 1 5 5266 7 81 7 81 0 ...

Page 62: ... a built in configuration data storage device and interfaces to the GTX 3X5 through the same pins as the configuration module The GAE wire harness is routed out the back of the backshell and plugged into the GAE when the backplate is assembled Refer to section 5 12 and figure B 11 Refer to figure 4 4 and figure D 1 for this procedure 1 Remove 0 17 inches of insulation from the end of each wire 2 b...

Page 63: ...e 4 4 Configuration Module Installation Table 4 2 Configuration Module Kit P N 011 00979 03 Refer to Figure Description Garmin P N 1 Sub assembly potted configuration module with EEPROM 011 02178 00 2 4 conductor harness 325 00122 00 3 Socket contact crimp 22D 336 00021 01 1 2 3 ...

Page 64: ...t may need a cable longer than the physical run in the aircraft Follow the steps below for installation of the coaxial cables 1 Route the coaxial cable to the radio rack location keeping in mind the recommendations of section 3 14 2 Attach the cable in accordance with AC 43 13 1B chapter 11 section 11 3 Trim the coaxial cable to the applicable length 4 Install the coaxial connectors per the manufa...

Page 65: ... rack in the aircraft panel The screws are inserted from the inside through holes in the sides of the rack 3 Use provided screws to attach the connector s to the backplate 4 Align the backplate so the backplate screw heads pass through the keyed holes in the back of the rack 5 Use two 4 40 flat head screws to attach the GAE to the backplate if used Refer to figure B 11 6 Connect the wire harness t...

Page 66: ... to the main system rack with the nutplate kit listed in section 3 4 2 At least eight screws are required to secure the rack as shown in figure B 7 Refer to G1000 System Installation Manual Attach the connectors and optional GAE if used to the connector backplate the same way as panel mount units Refer to section 4 7 1 4 8 Panel and Standard Remote Mount Unit Installation and Removal CAUTION The a...

Page 67: ...the GTX 3X5 shoe into the base at an angle 2 Make sure the unit is fully engaged and in line with the base 3 Rotate the GTX 3X5 down flat onto the base 4 Rotate the base locking mechanism up and place the cup over the shoe 5 Rotate the knob clockwise until tight 6 Directly attach the connector backplate to the GTX 3X5 with two screws using a 3 32 hex tool Removal 1 On the base pull the knob back 2...

Page 68: ...Configuration and Control Inputs 5 6 5 4 Lighting Bus 5 7 5 5 Altitude Inputs 5 7 5 5 1 Pressure Sensor Module 5 7 5 5 2 Gray Code Altitude Input 5 8 5 6 Discrete I O 5 8 5 7 Serial Data Interfaces 5 9 5 7 1 RS 232 5 9 5 7 2 ARINC 429 5 9 5 7 3 HSDB 5 10 5 7 4 RS 422 5 10 5 8 Suppression Bus 5 10 5 9 OAT Input 5 10 5 10 Audio Output 5 11 5 11 Time Mark 5 11 5 12 Configuration Module 5 11 5 13 USB ...

Page 69: ...BLE DISCRETE 2 I O 17 XPDR FAIL 1 or CONFIGURABLE O 18 EXTERNAL SUPPRESSION I O I O C4 B1 A1 I B A O C1 I O H I O B2 A2 I R B D4 C2 O L 21 42 Ext Ident Input 7 Air Ground Input 8 Ext Standby Input 6 Lighting Bus Ext Suppression Bus Switched Power Out Power Config Reserved Altitude Gray Code Input Power Input 1 Power Ground A T A D Ground RS 232 3 Discrete I O 1 1 OAT Temp Probe RS 232 2 Keep Alive...

Page 70: ...32 IN 2 I 31 RS 232 IN 1 I 32 ALTITUDE A2 or CONFIGURABLE I 33 ALTITUDE B2 or CONFIGURABLE I 34 ALTITUDE C2 or CONFIGURABLE I 35 RESERVED I 36 EXTERNAL IDENT SELECT or CONFIGURABLE I 37 AUDIO INHIBIT 2 or CONFIGURABLE I 38 POWER CONTROL I 39 SWITCHED POWER OUT O 40 LIGHTING BUS LO I 41 AIRCRAFT GROUND 42 AIRCRAFT POWER 1 I 43 ALT ENCODER CONFIG MODULE POWER O 44 USB VBUS POWER I 45 USB GND 46 AUDI...

Page 71: ... a ground to activate If there is no asterisk the signal is an Active High 53 ALTITUDE A4 or CONFIGURABLE I 54 ALTITUDE B4 or CONFIGURABLE I 55 ALTITUDE C4 or CONFIGURABLE I 56 ALTITUDE GROUND O 57 SQUAT SWITCH or CONFIGURABLE I 58 AIR DATA SELECT or CONFIGURABLE I 59 POWER CONFIG I 60 GPS KEEP ALIVE I 61 AIRCRAFT POWER 2 I 62 AIRCRAFT POWER 2 I Pin Pin Name I O ...

Page 72: ...me I O 1 ETHERNET OUT 1B O 2 ETHERNET IN 1B I 3 ETHERNET OUT 2B O 4 ETHERNET IN 2B I 5 RS 232 OUT 4 O 6 ETHERNET OUT 1A O 7 ETHERNET IN 1A I 8 ETHERNET OUT 2A O 9 ETHERNET IN 2A I 10 RS 232 IN 4 I 11 RS 422 A O 12 RS 422 B O 13 CONFIGURABLE DISCRETE 11 I O 14 CONFIGURABLE DISCRETE 12 I O 15 RS 232 GND 4 P N N T N N P R P P 5 10 G round B I O I O A 15 1 ETHERNET OUT 1 6 11 RS 232 OUT ETHERNET OUT 2...

Page 73: ...l GPS clock and decreases initial GPS satellite acquisition time during system power up 5 3 1 Power Configuration and Control Inputs The power control inputs are for remote power on off and enabling the power auto on feature The POWER CONFIG input controls the remote on off feature The POWER CONFIG input connects to ground for remote unit installation The input is left open for panel mount unit in...

Page 74: ...n P N 011 03080 00 HSDB Refer to section 3 10 for altitude source priorities With the proper encoder the Mode S transponder transmits altitude reporting in 25 foot resolution to ground stations and other aircraft The unit must receive altitude from an applicable altitude reporting device or from the optional GAE module A parallel Gray code encoder provides altitude in 100 foot resolution For altit...

Page 75: ...en active Refer to table 6 7 and table 6 8 for discrete input and output configuration Table 5 8 Discrete Inputs and Outputs Pin Name Connector Pin I O ALTITUDE A1 or CONFIGURABLE P3251 10 I ALTITUDE A2 or CONFIGURABLE P3251 32 I ALTITUDE A4 or CONFIGURABLE P3251 53 I ALTITUDE B1 or CONFIGURABLE P3251 11 I ALTITUDE B2 or CONFIGURABLE P3251 33 I ALTITUDE B4 or CONFIGURABLE P3251 54 I ALTITUDE C1 or...

Page 76: ...cal specification when loaded with up to five standard ARINC 429 receivers The ARINC 429 inputs and outputs can be configured for different functions depending on the installation Refer to section 6 5 Table 5 10 ARINC 429 Inputs and Outputs Pin Name Connector Pin I O RS 232 OUT 1 P3251 9 O RS 232 IN 1 P3251 31 I RS 232 GND 1 P3251 52 O RS 232 OUT 2 P3251 8 O RS 232 IN 2 P3251 30 I RS 232 GND 2 P32...

Page 77: ...e GTX 3X5 Table 5 13 External Suppression Bus Pin 5 9 OAT Input The GTX 3X5 includes an OAT input used for OAT and density altitude displays TEMP PROBE IN uses a current sensor type probe such as the EDMO P N 655 PROBE or the Davtron P N C307PS The temperature input specification is 1 microamp per degree Kelvin 1uA K Connect the probe red wire to pin 25 and the black wire to pin 3 Table 5 14 OAT I...

Page 78: ... the GTX 3X5 D sub connector Connect using The wire colors are shown in table 5 17 The configuration module stores the specified aircraft installation configuration settings The optional GAE module is used to provide the pressure altitude for the transponder The GAE module also includes configuration memory function to store the installation configuration When used A separate configuration module ...

Page 79: ...res Potential damage or interference due to coupling with other cables will occur Only use the USB interface for unit configuration software updates and service while the aircraft is on the ground Do not use during normal operation or when airborne Table 5 18 USB Inputs and Outputs Pin Name Connector Pin I O USB DATA HI P3251 2 I O USB DATA LO P3251 24 I O USB VBUS POWER P3251 44 I USB GND P3251 4...

Page 80: ... sure all lighting buses are turned to their lowest adjustment before applying power to the unit The lowest adjustment prevents damage to the unit if there are any wiring errors Examine the wire harness to make sure the connection to aircraft systems and avionics equipment is correct before the unit is energized Point to point continuity must be examined to expose any faults such as shorting to gr...

Page 81: ...n this section configuration instructions are for panel mount units Refer to section 6 11 to configure remote units On a panel mount unit push and hold the ENT key and apply power to enter configuration mode Push and hold the OFF key until the unit powers off to exit configuration mode Push the FUNC key to cycle through the group pages Push the 8 or 9 key to scroll up or down on the page without a...

Page 82: ...lling a GTX 345 in a GX000 system select HSDB VOLUME To raise the volume of the transponder audio push the 8 key To lower the volume push the 9 key The range is 0 to 100 VOICE Set the voice type to MALE or FEMALE TEST AUDIO The test audio files are used to set the volume level of the transponder Selections are NONE TONE MSG 1 MSG 2 MSG 3 AUD TIMER EXPIRED ALT TRAFFIC ALERT TEST AUDIO VOICE VOLUME ...

Page 83: ...e Selections are TIMER EXPIRED ALRT PANEL MOUNT UNITS ONLY Sets timer expired alert type Selections are Figure 6 3 Audio Page 2 TRAFFIC ALERT NOTE A chime is heard if the GTX 335 is configured for TIS A traffic alerts Sets the traffic alerting type Selections are Figure 6 4 Audio Page 3 OFF MESSAGE MSG W CHIME OFF MESSAGE MSG W CHIME OFF MESSAGE MSG W CHIME ...

Page 84: ...llation Manual Rev 4 Page 6 5 6 5 Interfaces Configures inputs and outputs of RS 232 ARINC 429 discretes and HSDB interfaces Figure 6 5 Interface Group INTF DISCRETE FUNC A429 OUTPUT A429 IN CH 1 RS 422 OUTPUT RS 232 PRESENT HSDB INTERFACE PIN ...

Page 85: ...MT 2 Supports transponder interface and TIS traffic to GTN and GNS 480 CNX80 GTX 335 only Input Output GDL Supports GDL 88 interface All 2 Input Output GNS Supports GNS 400W 500W Series ADS B In weather Traffic is supported over ARINC 429 Supplies GPS data GTX 345 only Input Output CONNEXT FMT 1 Supports G3X for ADS B In weather and traffic GTX 345 only Input CONNEXT FMT 3 Supports input from a Fl...

Page 86: ...splays GPSMAP 396 496 695 696 G3X G300 GTX 335 only Output LGCY TRAFFIC Supports GDL 90 traffic interface to legacy G1000 GTX 345 only Input Output Selection Description Input Output OFF Information is not received or transmitted Input Output GNS Supports GNS 400W 500W Series ADS B In weather Traffic is supported over ARINC 429 Supplies GPS information Input Output CONNEXT FMT 1 Supports G3X for A...

Page 87: ...er to the GMX 200 and MX20 Either format also provides weather to a legacy G1000 installation Table 6 3 RS 422 Selections Figure 6 7 RS 422 Output Page Channel Input Output Selection Description RS 422 Output CONNEXT FMT 3 Supports output to Flight Stream 210 OFF Information is not transmitted MX FMT 1 Supports GMX 200 MX FMT 2 Supports MX20 ...

Page 88: ...ATA Receives altitude airspeed altitude rate and heading information from EFIS and ADC systems FLIGHT CONTROL Receives selected altitude barometric setting and non standard pitch discrete data for Bendix King KFC 225 HEADING Receives heading information MODE S CTRL PNL Receives ARINC 718 labels for ATCRBS Control and Flight ID RADIO ALTITUDE Receives radar altitude information TRAFFIC 1 Receives t...

Page 89: ...itted FORMAT 1 Mode S control panel FORMAT 2 Garmin concentrator FORMAT 3 Garmin concentrator and Mode S control panel FORMAT 4 Garmin TAS and GPS data FORMAT 5 Garmin concentrator Garmin TAS and GPS data FORMAT 6 Mode S control panel Garmin TAS and GPS data FORMAT 7 Garmin concentrator Mode S control panel Garmin TAS and GPS data FORMAT 8 Garmin TIS A 1 FORMAT 9 Garmin concentrator and Garmin TIS...

Page 90: ...tions are YES NO Table 6 6 HSDB Formats Figure 6 10 HSDB Interface Page Interface Description GDU 620 Controls HSDB communication with the GDU 620 GTN 6XX 7XX GTS 8X5 and GX000 GTN GTS GX000 Indirect A429 TCAS The GTX receives traffic inputs from the GIA instead of TAS TCAS in GX000 installations where TAS TCAS is connected to a GIA This interface is not shown on the display ...

Page 91: ... Off P3251 57 This input determines the on ground status of the aircraft It is active low and a ground on this input can be configured to mean On Ground or In Air AIR DATA Off P3251 58 Switches between two ARINC 429 ADC sources or two EFIS ADC sources Source 1 and 2 are set during configuration Source 1 is used when the discrete is open and Source 2 is used when the discrete is grounded ALT DATA A...

Page 92: ...3252 If the unit needs service soon this discrete will switch between open and ground for the first 30 seconds after power up If after 30 seconds there is no detection of ADS B In Out failures the discrete opens The discrete will ground if any ADS B In Out failures are detected after 30 seconds TRFC STBY Off All discrete outputs on P3251 Commands TAS TCAS standby operate Discrete output operation ...

Page 93: ...t Settings Figure 6 13 Unit Group FIS B PROCESSING GTX 345 ONLY To receive ADS B weather data select ENABLED Figure 6 14 FIS B Processing Page UNIT BLUETOOTH INSTALLATION ID TEMPERATURE UNITS ALTITUDE UNITS FIS B PROCESSING ALTITUDE ALERT DEVIATION VFR ID RESTORE PAGES ON POWER UP ...

Page 94: ...d Temperature Units Page INSTALLATION ID NOTE The Installation ID Select discrete overwrites the configuration setting Selects the ID number for the transponder Set the Installation ID to 1 in single installations Set the primary transponder Installation ID to 1 and the secondary transponder to 2 in dual installations VFR ID Sets the VFR squawk code for your country Range in octal is 0000 7777 Fig...

Page 95: ...o generate an altitude alert Range is 200 ft to 999 ft RESTORE PAGES ON POWER UP PANEL MOUNT UNITS ONLY To save the selected pages set in normal operating mode as the new default page settings next time the unit is power up select YES Figure 6 17 Altitude Alert Deviation and Restore Page BLUETOOTH GTX 345 ONLY To transmit information to a PED using Bluetooth select ENABLED Figure 6 18 Bluetooth Pa...

Page 96: ...brightness levels match the lighting levels of other equipment in the panel under night conditions Figure 6 19 Display Group DISP OFFSET LIGHTING BUS INPUT VLTG MINIMUM LEVEL KEYPAD BACKLIGHT MINIMUM LEVEL DISPLAY BACKLIGHT SLOPE PHOTOCELL TRANSITION SLOPE OFFSET DEFAULT BACKLIGHT OFFSET DEFAULT CONTRAST OFFSET ...

Page 97: ...brighter the minimum brightness PHOTOCELL TRANSITION Sets a point on the lighting bus When the lighting bus is below this point the GTX 3X5 uses the photocell to adjust the display brightness The range is 5 to 50 PHOTOCELL SLOPE Sets the sensitivity of the photocell input level Adjusting the slope higher results in a greater display brightness change for a given increase in the photocell input lev...

Page 98: ...down for any given lighting bus input level This field has a range of 0 to 100 Use the offset setting to match lighting curves with other equipment in the panel DEFAULT BACKLIGHT OFFSET Manually sets the default backlight offset value from 10 to 99 DEFAULT CONTRAST OFFSET Manually sets the default contrast offset value from 50 to 50 ...

Page 99: ... Manual Rev 4 Page 6 20 6 8 Sensors Figure 6 21 Sensor Group SNSR OAT SENSOR INSTALLED ALTITUDE SOURCE 1 ALTITUDE SOURCE 2 GPS 1 SRC INTGRTY LAT OFST LON OFST GPS 2 SRC INTGRTY LAT OFST LON OFST INTERNAL ALT ENCODER INSTALLED INTERNAL AHRS ORIENTATION ...

Page 100: ... uses both altitude sources if set The GTX uses any altitude source in priority order if no altitude sources are selected Refer to section 3 10 Sets the primary altitude source Selections are ALTITUDE SOURCE 2 Sets the secondary altitude source Selections are Figure 6 23 Altitude Source Page NONE RS232 1 RS232 2 RS232 3 A429 1 A429 2 HSDB GTX 345 only GILLHAM ALT ENC NONE RS232 1 RS232 2 RS232 3 A...

Page 101: ...nterline of the aircraft in meters Selections are LON OFST Sets the distance of the GPS antenna from the nose of the aircraft in meters Selections are GPS 2 SRC Sets the secondary GPS source Selections are INTGRTY Sets the integrity for the secondary GPS Selections are LAT OFST Sets the secondary GPS lateral offset in meters Selections are NONE INTRNL RS232 1 RS232 2 RS232 3 RS232 4 GTX 345 Only A...

Page 102: ...e CEILING Sets aircraft maximum altitude between 8 000 feet and 30 000 feet TEST POINTS Sets the number of test points used to calibrate the GAE module The range is 3 to 20 The maximum number of test points are limited by the aircraft ceiling setting Figure 6 25 Internal Alt Encoder Page INTERNAL ALT ENCODER ADJUSTMENT Sets the GAE module altitude to match the primary altitude display Figure 6 26 ...

Page 103: ... the centerline of aircraft When setting the yaw angle a positive angle indicates the GTX 345 is rotated clockwise from the longitudinal axis of the airplane line from nose to tail A negative angle indicates the GTX 345 is rotated counterclockwise Refer to figure 6 27 Figure 6 27 Setting the Yaw Angle Figure 6 28 Internal AHRS Orientation Page Nose Right Wing Positive Yaw Angle Nose Right Wing Pos...

Page 104: ...5 6 9 ADSB Figure 6 29 ADS B Group ADSB 1090ES IN CAPABLE UAT IN CAPABLE AIRCRAFT WIDTH AIRCRAFT LENGTH ACFT MAX A S ACFT CATGRY UAT OUT RMT CONTROL 1090ES OUT CONTROL ADS B IN PROCESSING ALLOW PILOT TO EDIT FLT ID DEFAULT FLT ID ADDRESS AIRCRAFT TAIL NUMBER FLT ID PREFIX ...

Page 105: ... with a maximum gross weight less than 15 500 lbs Selections are ACFT MAX A S Sets the maximum airspeed of the aircraft Selections are Figure 6 30 Aircraft Category and Max Airspeed Page AIRCRAFT LENGTH Sets aircraft length in meters AIRCRAFT WIDTH Sets aircraft width in meters UNKNOWN LIGHT SMALL HIGH PERFORMANCE ROTORCRAFT GLIDER LIGHTER THAN AIR ULTRALIGHT UAV UNKNOWN 75 kt 150 kt 300 kt 600 kt...

Page 106: ...ections are UAT OUT RMT CONTROL Not available with GDL 88 software v3 33 or earlier Figure 6 32 1090ES Out Control and UAT Out Remote Control Page 1090ES IN CAPABLE Select YES if the aircraft can receive 1090ES ADS B messages UAT IN CAPABLE Select YES if the aircraft can receive UAT ADS B messages Figure 6 33 1090ES In Capable and UAT In Capable Page Enabled Pilot Set Disabled ...

Page 107: ...et the ICAO address to either octal or hex format If the tail number is recognized as a US registered tail number the ICAO address will be pre filled by the GTX It only needs to be compared to the aircraft registration records Selections are Figure 6 35 Aircraft Tail Number and Address Page ALLOW PILOT TO EDIT FLT ID Select YES to let the pilot change the flight ID Figure 6 36 Allow Pilot to Edit ...

Page 108: ...tion Manual Rev 4 Page 6 29 DEFAULT FLT ID Sets the default flight ID used in normal mode FLIGHT ID PREFIX Sets the flight ID prefix with the carrier abbreviation For example Garmin AT is GAT Figure 6 37 Default Flight ID and Flight ID Prefix Page ...

Page 109: ... 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 30 6 10 Diagnostics Figure 6 38 Diagnostics Group DIAG LCD RS232 OAT INPT LT BUS DISCRETE INPUT STATE UNIT PHOTO A429 SRC 2 GPS SRC 1 HSDB ...

Page 110: ...ormation for troubleshooting purposes Information includes Discrete input state Lighting bus voltages Photocell voltages Outside air temperature Display temperature RS 232 channels ARINC 429 channels GPS Source 1 and GPS Source 2 status HSDB status GTX 345 Gillham input state Figure 6 39 Diagnostics Page ...

Page 111: ...nits without a display Selections are the same as for panel mount units The GTX 3X5 Install Tool P N 006 A0271 01 is available at Garmin s Dealer Resource Center A USB A plug to USB B plug cable not provided is necessary Figure 6 40 USB A and USB B Connectors To use the GTX 3X5 Install Tool 1 Remove power from the unit 2 Connect the USB A to USB B cable between the computer and the USB B receptacl...

Page 112: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 33 Figure 6 41 Aircraft Configuration Page Figure 6 42 Airframe Configuration Page ...

Page 113: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 34 Figure 6 43 Unit Configuration Page Figure 6 44 Interface Configuration Page Serial ...

Page 114: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 35 Figure 6 45 Interface Configuration Page A429 Figure 6 46 Interface Configuration Page Discretes ...

Page 115: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 36 Figure 6 47 Interface Configuration Page HSDB Figure 6 48 Sensors Configuration Page GAE ...

Page 116: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 37 Figure 6 49 Sensors Configuration Page GPS Figure 6 50 Sensors Configuration Page Internal AHRS ...

Page 117: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 38 Figure 6 51 Sensors Configuration Page Additional Sensors Figure 6 52 Audio Configuration Page ...

Page 118: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page 6 39 Figure 6 53 Display Configuration Page Panel Mount Units Only ...

Page 119: ... LAT LON continues to match the known reference 5 Repeat steps 3 and 4 for the following frequencies 6 For VHF radios that include 8 33 kHz channel spacing include the following frequencies in addition to those in step 5 7 Repeat steps 2 through 6 for all remaining COM transceivers in the aircraft 8 Turn on the TCAS system and make sure the GPS position remains valid if the aircraft is TCAS equipp...

Page 120: ...e options to be updated 4 Under Step 3 Start Upload select the Upload key 5 Wait for the upload to complete Individual files will be marked as complete as they are installed 6 Under Step 1 Select a File select the Browse key and locate the Main System software file containing the GTX 3X5 3X5R software previously downloaded 7 Under Step 2 Upload Options select the remaining options to be updated 8 ...

Page 121: ...nsponder TSO Installation Manual Rev 4 Page 7 1 7 CONTINUED AIRWORTHINESS Other than for regulatory periodic functional checks maintenance of the GTX 3X5 is on condition only Periodic maintenance of the GTX 3X5 is not required ...

Page 122: ...itude Format 1 Sentence The GTX 3X5 is capable of receiving the following 10 byte message from the altitude serializer ALT sp 12345 CR Where ALT ASCII characters sp space 0x20 12345 altitude in feet CR carriage return 0x0D A 1 3 Altitude Format 3 Sentence The GTX 3X5 is capable of receiving the following 17 byte message from GAE modules altitude serializers and altitude converters RMS sp 12345T 12...

Page 123: ...acters sign 78 represents outside air temperature Celsius ZG 90 CR LF ZG ASCII characters sign 90 represents true air temperature Celsius ZL234 CR LF ZL ASCII characters 234 represents heading degrees from north ZQ345 CR LF ZQ ASCII characters 345 represents error log reason indicator ZR678 CR LF ZR ASCII characters 678 represents checksum ETX Where STX start transmit character 0x02 CR carriage re...

Page 124: ... heading degrees from north GP89012 CR LF GP ASCII characters 89012 represents fuel used left or Single tenths gallons GR6789 0 CR LF GR ASCII characters 6789 0 represents fuel remaining gallons 1 Ga 1234 CR LF Ga ASCII characters sign 12 34 represents barometric corrected altitude tens of feet Gb56 78 CR LF Gb ASCII characters 56 78 represents current barometric pressure setting inches Hg G 901 C...

Page 125: ...acters sign 901 represents vertical speed tens of ft minute SL234 CR LF SL ASCII characters 234 represents heading degrees from north Sa 1234 CR LF Sa ASCII character sign 1234 represents barometric corrected altitude tens of feet Sb56 78 CR LF Sb ASCII character 56 78 represents current barometric pressure setting inches Hg S 901 CR LF S ASCII character 901 represents checksum ETX Where STX start...

Page 126: ...y Shown B 4 Figure B 4 GTX 345R GPS Standard Remote Mount Dimensions and CG Shown B 5 Figure B 5 GTX 3X5 Vertical Remote Mount B 6 Figure B 6 GTX 3X5 Vertical Remote Mount Dimensions and CG B 7 Figure B 7 G1000 Mount Rack Assembly with GTX 345R GPS Shown B 8 Figure B 8 G1000 Mounting Rack Dimensions and CG with GTX 345R GPS Shown B 9 Figure B 9 GTX 3X5 Panel Cutout Detail B 10 Figure B 10 GTX 3X5 ...

Page 127: ...1214 01 011 03300 00 Sub Assy GTX335 011 02977 00 011 00979 03 115 01771 01 011 02976 00 Panel 4 5 114 3 2 81 0 8 20 010 01214 21 011 03300 20 Sub Assy GTX335 NV 011 02977 00 011 00979 03 115 01771 01 011 02976 00 Panel 4 5 114 3 2 81 0 8 20 010 01214 41 011 03300 40 Sub Assy GTX335 GPS 011 02977 00 011 00979 03 115 01771 01 011 02976 01 Panel 4 5 114 3 2 81 0 8 20 010 01216 00 011 03302 00 Sub As...

Page 128: ...ure B 2 GTX 345 GPS Panel Mount Dimensions and CG Shown 44 11 1 6 99 177 4 65 16 5 1 68 42 5 RACK ALIGNMENT DIMPLES 1 73 43 8 33 8 3 1 65 41 9 BEZEL 82 20 8 DIM C 6X C SINK FOR 6 32 FLAT HEAD SCREW 6 25 158 8 BEZEL 6 30 160 0 8 62 218 8 10 09 256 3 9 61 244 0 DIM B DIM A VENT ...

Page 129: ...15 01 011 03301 00 Sub Assy GTX335R 011 02977 00 011 00979 03 115 01771 00 011 02976 00 Remote 4 8 120 3 3 84 0 8 20 010 01215 40 011 03301 40 Sub Assy GTX335R GPS 011 02977 00 011 00979 03 115 01771 00 011 02976 01 Remote 4 9 124 3 2 81 0 8 20 010 01217 00 011 03303 00 Sub Assy GTX345R 011 02977 01 011 00979 03 115 01771 00 011 02976 00 Remote 5 0 127 3 0 76 0 8 20 010 01217 40 011 03303 40 Sub A...

Page 130: ...nder TSO Installation Manual Rev 4 Page B 5 Figure B 4 GTX 345R GPS Standard Remote Mount Dimensions and CG Shown 44 11 1 65 16 5 49 12 5 6 99 177 4 33 8 3 DIM C 10 09 256 3 54 13 6 9 61 244 0 DIM A DIM B VENT 1 72 43 8 6 30 160 0 ...

Page 131: ...Assy GTX335R 011 02977 00 011 00979 03 011 03762 00 011 02976 10 Remote 5 5 140 2 7 69 1 0 25 010 01215 42 011 03301 40 Sub Assy GTX335R GPS 011 02977 00 011 00979 03 011 03762 00 011 02976 11 Remote 5 5 140 2 8 71 0 9 23 010 01217 02 011 03303 00 Sub Assy GTX345R 011 02977 01 011 00979 03 011 03762 00 011 02976 10 Remote 5 6 142 2 7 69 0 9 23 010 01217 42 011 03303 40 Sub Assy GTX345R GPS 011 029...

Page 132: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page B 7 Figure B 6 GTX 3X5 Vertical Remote Mount Dimensions and CG B A 1 03 26 1 4 00 101 6 8 00 203 2 875 22 23 C ...

Page 133: ...m A inch mm Dim B inch mm Dim C inch mm G1000 mount 011 03301 00 Sub Assy GTX335R 011 02977 00 011 00979 03 115 02250 00 011 02976 00 G1000 5 3 135 3 2 81 0 7 18 G1000 mount 011 03301 40 Sub Assy GTX335R GPS 011 02977 00 011 00979 03 115 02250 00 011 02976 01 G1000 5 3 135 3 2 81 0 8 20 G1000 mount 011 03303 00 Sub Assy GTX345R 011 02977 01 011 00979 03 115 02250 00 011 02976 00 G1000 5 4 137 3 0 ...

Page 134: ...Mounting Rack Dimensions and CG with GTX 345R GPS Shown 2X 38 9 7 2X 48 12 2 2X 96 24 4 3X 44 11 1 3X 3 35 85 1 1 70 43 1 1 75 44 4 DIM C NUT PLATE REMOVED FOR CLARITY THIS SIDE 10 48 266 3 10 00 254 0 14 3 6 6 30 160 1 DIM A DIM B VENT NO BLOCK 6 90 175 3 7 26 184 5 38 9 7 48 12 2 96 24 4 ...

Page 135: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 4 Page B 10 Figure B 9 GTX 3X5 Panel Cutout Detail ...

Page 136: ... Figure B 10 GTX 3X5 Connector and Vent Locations Figure B 11 Optional Garmin Altitude Encoder CONNECTORS VENT GTX BACKPLATE PANEL MOUNT G1000 REMOTE BACK PLATE ASSEMBLY 011 02976 00 011 02976 01 CONNECTOR KIT 011 02977 00 011 02977 01 OPTIONAL ALTITUDE SENSOR 011 03080 00 ...

Page 137: ...MENT COMPATIBILITY AND CONFIGURATION C 1 ADS B In Displays C 2 C 2 GPS Sources C 3 C 3 Altitude Sources C 4 C 4 Audio Panels C 5 C 5 Radar Altimeters C 6 C 6 Heading Reference Sources C 6 C 7 Traffic Sensors GTX 345 Only C 8 C 8 Bluetooth C 9 C 9 Remote Control C 9 C 10 TIS A Display C 10 ...

Page 138: ...3 RS 232 ADSB TFC GNS Supports traffic only also includes GPS data from the GNS 400W 500W ADSB TFC WX GNS Supports both traffic and weather that includes GPS data from the GNS 400W 500W Series ARINC 429 ADSB TFC TRAFFIC Supports ADS B traffic without TAS TCAS ADSB TFC w TCAS TRAFFIC Supports ADS B traffic w TAS TCAS correlation G950 G1000 RS 232 GDL 90 LGCY TRAFFIC Supports GTX 345R installations ...

Page 139: ...udes GPS data Refer to table C 9 LGCY REMOTE 1 1 4 OR LGCY REMOTE 2 2 4 Internal N A N A Refer to section 6 8 GTN 6XX 7XX RS 232 ADS B OUT ADS B FMT 1 HSDB ADS B In Source GTX GTN Enabled Applicable to GTX 345 installations only GNS 400W 500W RS 232 ADSB TFC GNS Applicable to GTX 345 installations only Note that the primary purpose of this interface is for ADS B In Data however this format also in...

Page 140: ...tem is installed GDC 74 N A ADC ADC GDU 620 GENERAL Speed HIGH EFIS AIR DATA Speed HIGH EFIS AIR DATA Speed HIGH GTN 6XX 7XX GTX Mode S 1 OR GTX w TIS 2 REMOTE FMT 1 1 OR REMOTE FMT 2 2 REMOTE FMT 1 1 OR REMOTE FMT 2 2 This configuration is primarily for purposes of transponder remote control however this configuration also provides altitude data Refer to table C 9 GAE 12 N A Garmin Altitude Encod...

Page 141: ... F ADC 2000 interface to the GTX not both N A ADC Speed LOW ADC Speed LOW Trans Cal Industries IA RS232 X N A ALT FMT 1 100 ft ALT FMT 1 100 ft SSD120 25 ft or lower encoding ALT FMT 1 25 ft ALT FMT 1 25 ft Applicable to installations with the SSD120 unit configured for 25ft or lower encoding 100 ft encoding ALT FMT 1 100 ft ALT FMT 1 100 ft Applicable to installations with the SSD120 unit configu...

Page 142: ...tallations only Collins AHC 85E ARINC 429 AHRS 2 Speed HIGH AHRS 2 Speed HIGH Garmin G950 G1000 ARINC 429 GEN PURPOSE N A EFIS AIR DATA 3 Speed HIGH Refer to STC installation guidance GRS 77 ARINC 429 N A AHRS 2 Speed HIGH AHRS 2 Speed HIGH GAD 42 ARINC 429 N A HEADING 1 Speed LOW HEADING 1 Speed LOW Applicable to GTX 3X5 installations only GDU 620 ARINC 429 GENERAL EFIS AIR DATA 3 Speed HIGH EFIS...

Page 143: ...affic 5 Installation with TIS traffic GTX 335 only Honeywell Bendix King EFIS 40 50 SG 465 ARINC 429 N A HEADING 1 Speed LOW HEADING 1 Speed LOW Applicable to GTX 3X5 installations only Sandel SN3500 ARINC 429 AHRS 2 Speed LOW AHRS 2 Speed LOW SN3308 AHRS 2 Speed LOW AHRS 2 Speed LOW Manufacturer Model Configuration Parameter Interfacing Equipment Configuration GTX 335 Configuration Setting GTX 34...

Page 144: ...on Primary TX 1 TRAFFIC 1 Speed HIGH Output 2 Transponder 1 Communication Primary RX 1 FORMAT 4 Speed HIGH Data format includes Garmin TAS Pressure Altitude Source Primary RX Magnetic Heading Source Primary RX GPS Position Velocity Time Source Primary RX Transponder 1 Communication Primary RX 1 FORMAT 5 Speed HIGH Data format includes Garmin TAS as well as Garmin concentrator required for G1000 N ...

Page 145: ...th a FS 110 210 installation RS 422 Output CONNEXT FMT 3 Manufacturer Model Data Format Interface Configuration GTX 335 Configuration Setting GTX 345 Configuration Setting Notes Garmin GTN 6XX 7XX RS 232 GTX Mode S REMOTE FMT 1 REMOTE FMT 1 Installations with no TIS GTX w TIS REMOTE FMT 2 N A Installations with TIS GNS 480 RS 232 GTX REMOTE FMT 1 REMOTE FMT 1 Installations with no TIS GTX w TIS RE...

Page 146: ...primary purpose of this interface is for remote control however this format also includes TIS A data Refer to table C 9 GDU 620 ARINC 429 GTX 330 FORMAT 8 GNS 400W 500W Series ARINC 429 GARMIN GTX 330 FORMAT 8 GNS 480 RS 232 GTX w TIS REMOTE FMT 2 Note that the primary purpose of this interface is for remote control however this format also includes TIS A data Refer to table C 9 G950 G1000 RS 232 ...

Page 147: ...D 12 Figure D 8 GTX 345 Single Dual GTN 6XX 7XX Interconnect D 14 Figure D 9 GTX 335 345 GDL 88 Interconnect D 16 Figure D 10 GTX 345 Traffic Sensor Interconnect D 17 Figure D 11 GTX 345 Single and Dual 400W 500W Series D 18 Figure D 12 GTX 3X5 Audio Interconnect D 19 Figure D 13 GTX 3X5 Radio Altimeter Interconnect D 20 Figure D 14 GTX 3X5 AHRS Heading Source D 21 Figure D 15 GTX 3X5 Switches and...

Page 148: ...ed cables are shown for reference only In dual GTX transponder installations each transponder must be grounded through separate ground terminal stud locations on the aircraft If practical power and ground wires should be routed separately for each transponder Route grounds and wire separately to improve safety if there is a wiring or grounding system failure Designations for ground connections Shi...

Page 149: ...ENNA XPDR ANTENNA P325 XPDR XPDR ANTENNA GPS ANTENNA AIRCRAFT POWER 42 AIRCRAFT GND 41 XPDR AVIONICS BUS 14 28VDC AIRCRAFT GROUND 3A USB VBUS POWER USB DATA HI USB DATA LO USB GROUND 44 2 24 45 POWER CONTROL 38 GPS KEEP ALIVE 60 UNSWTCH BAT BUS 14 28VDC 19 EXISTING LIGHTING BUS 5VDC 14VDC 28VDC OR 5VAC 40 RED YEL BLK WHT RED GRN BLK WHT S LIGHTING BUS LO LIGHTING BUS HI VBUS D D GND USB TYPE B REC...

Page 150: ...MODULE WIRE HARNESSES ARE NOT INTERCHANGEABLE WIRE COLOR IN MODULE WIRE HARNESS DESIGNATES FUNCTION CONNECT MODULE WIRE HARNESS TO GTX 3X5 ACCORDING TO WIRE COLOR REFER TO SECTION 5 3 1 FOR DETAILS GPS KEEP ALIVE IS RECOMMENDED FOR GPS INSTALLS IF NOT CONNECTED GPS MAY TAKE UP TO 20 MINUTES TO OBTAIN A GPS FIX REFER TO SECTION 5 4 FOR LIGHTING BUS CONNECTIONS GPS KEEP ALIVE MUST BE CONNECTED TO TH...

Page 151: ...2 GND 5 39 19 S P3471 S S 18 s EXTERNAL SUPPRESSION 1 RS 232 RX 8 64 63 RS 232 GND 8 S 5 P3252 15 RS 232 TX 4 RS 232 GND 4 RS 422 Port 3A RS 422 Port 3B 28 27 S 11 12 RS 422 A RS 422 B S S A429 TX 3A 74 75 A429 TX 3B S 48 49 A429 RX 2A A429 RX 2B S 2 CONFIG MODULE PWR CONFIG MODULE GND CONFIG MODULE DATA CONFIG MODULE CLK 43 23 22 1 RED YEL BLK WHT CONFIG MODULE 4 GTS 8XX P8001 S 24 23 25 A429 TX ...

Page 152: ...L TRAFFIC SYSTEM IS INSTALLED USE ANY AVAILABLE ARINC 429 PORT THIS MUST BE CONFIGURED BY THE INSTALLER GTS 8XX SHOWN AS AN EXAMPLE REFER TO EXTERNAL TRAFFIC SENSORS FOR ALTERNATE EXTERNAL TRAFFIC SYSTEM OPTIONS GTX 345 PROVIDES AUTOMATIC CONTROL OF OPERATE STANDBY BASED ON AIRBORNE STATUS GTX 3X5 INSTALL TOOL PROVIDES TRAFFIC SELF TEST DISCRETE FOR EXTERNAL TRAFFIC VALIDATION THIS DIAGRAM PROVIDE...

Page 153: ...S 53 55 54 AIRCRAFT POWER 42 30 RS 232 RX 2 RS 232 TX 2 8 51 RS 232 GND 2 RS 232 TX 5 RS 232 RX 5 SIGNAL GROUND GIA 63 2 2P603 S 53 55 54 31 RS 232 RX 1 RS 232 TX 1 9 52 RS 232 GND 1 RS 232 TX 5 RS 232 RX 5 RS 232 GND 5 S S 18 s EXTERNAL SUPPRESSION 1 CONFIG MODULE PWR CONFIG MODULE GND CONFIG MODULE DATA CONFIG MODULE CLK 43 23 22 1 RED YEL BLK WHT CONFIG MODULE GTS 8XX P8001 S 25 A429 RX 2A 5 S ...

Page 154: ...QE OR EQUIVALENT DASHED LINES AND AREAS REPRESENT TRANSPONDER 2 AND GNS 480 CNX80 2 INSTALLATION DETAILS GNS 480 CNX80 1 P5 GTX 3X5 2 22 42 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 RS 232 OUT 6 RS 232 IN 6 RS 232 GND 6 S GTX 3X5 2 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 GNS 480 CNX80 2 2 22 42 RS 232 OUT 6 RS 232 IN 6 RS 232 GND 6 1 PANEL MOUNTED DPDT SWITCH XPDR 1 XPDR 2 14 EXT STANDBY...

Page 155: ...D 3 RS 232 OUT 1 RS 232 IN 1 SIGNAL GROUND P3251 XPDR AVIONICS BUS 28VDC or 14 VDC 3A XPDR ANT XPDR ANTENNA P325 XPDR CONFIG MODULE PWR CONFIG MODULE GND CONFIG MODULE DATA CONFIG MODULE CLK 43 23 22 1 USB VBUS POWER USB DATA HI USB DATA LO USB GROUND 44 2 24 45 s RED YEL BLK WHT RED GRN BLK WHT USB TYPE B RECEPTACLE CONFIG MODULE 1 VBUS D D GND SHIELD RS 232 OUT HI RS 232 OUT LO ALTITUDE ENCODER ...

Page 156: ...eet 2 of 2 CONFIG MODULE REQUIRES WIRE HARNESS P N 325 00122 00 PRESSURE SENSOR CONFIG MODULE REQUIRES WIRE HARNESS P N 325 00421 00 MODULE WIRE HARNESSES ARE NOT INTERCHANGEABLE WIRE COLOR IN MODULE WIRE HARNESS DESIGNATES FUNCTION CONNECT MODULE WIRE HARNESS TO GTX 3X5 ACCORDING TO WIRE COLOR REFER TO SECTION 5 3 1 FOR DETAILS 1 2 ...

Page 157: ...R SINGLE INSTALLATION AUDIO INHIBIT I O PIN IS CONFIGURABLE REFER TO PIN CONFIGURATION SECTION FOR DETAILS GTN 6XX 7XX GTX 335 27 8 46 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 RS 232 OUT 1 RS 232 IN 1 SIGNAL GROUND s P1001 TAWS AUDIO ACTIVE 35 37 AUDIO INHIBIT GTX 335 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 37 AUDIO INHIBIT 7 RS 232 IN 2 RS 232 OUT 2 26 45 RS 232 GND 2 s P3251 P3251 GTN...

Page 158: ...S 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 RS 232 OUT 1 RS 232 IN 1 s SIGNAL GROUND 27 8 46 P3251 P3252 s RS 232 OUT HI RS 232 OUT LO ALTITUDE ENCODER AUDIO IN HI AUDIO IN LO AUDIO PANEL 31 RS 232 IN 1 52 RS 232 GND 1 s 46 AUDIO OUT HI 47 AUDIO OUT LO AIRCRAFT POWER 21 AIRCRAFT POWER 42 XPDR AVIONICS BUS 28VDC or 14 VDC 22 AWG 3A 22 AWG XPDR ANT XPDR ANTENNA P325 XPDR CONFIG MODULE 1 USB VBUS POWER...

Page 159: ...eet 2 of 2 CONFIG MODULE REQUIRES WIRE HARNESS P N 325 00122 00 PRESSURE SENSOR CONFIG MODULE REQUIRES WIRE HARNESS P N 325 00421 00 MODULE WIRE HARNESSES ARE NOT INTERCHANGEABLE WIRE COLOR IN MODULE WIRE HARNESS DESIGNATES FUNCTION CONNECT MODULE WIRE HARNESS TO GTX 3X5 ACCORDING TO WIRE COLOR REFER TO SECTION 5 3 1 FOR DETAILS 1 2 ...

Page 160: ...P1002 2 7 6 1 ETHERNET IN 1A ETHERNET OUT 1A ETHERNET IN 1B ETHERNET OUT 1B s s ETHERNET OUT 3A ETHERNET IN 3A ETHERNET OUT 3B ETHERNET IN 3B 26 25 23 24 P1001 TAWS AUDIO ACTIVE 35 37 AUDIO INHIBIT GTN TAWS UNITS ONLY 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 RS 232 OUT 1 RS 232 IN 1 s SIGNAL GROUND 27 8 46 P3251 P3252 P1001 s P1002 2 7 6 1 ETHERNET IN 1A ETHERNET OUT 1A ETHERNET IN 1B ETHERNE...

Page 161: ... 7XX IS THE ONLY INSTALLED GPS NAVIGATOR OR GPS NAVIGATOR 1 IN A DUAL GPS NAVIGATOR INSTALLATION CONFIGURE GTN 6XX 7XX AS GTN 1 BY LEAVING SYSTEM ID P1002 10 NOT CONNECTED WHEN THE GTN 6XX 7XX IS GPS NAVIGATOR 2 IN A DUAL GPS INSTALLATION CONFIGURE GTN 2 BY GROUNDING SYSTEM ID P1002 10 TO THE SHIELD BLOCK TAWS AUDIO INHIBIT FOR GTN 6XX 7XX TAWS UNITS ONLY 1 2 ...

Page 162: ...TERFACES GTX 335 345 GDL 88 P3251 TIME MARK A RS232 2 GND 4 22 RS232 2 RX 45 26 50 7 RS232 3 GND RS232 3 TX P881 TIME MARK 1 PPS A OUT S S GTX 335 345 PROVIDING GPS POSITION TO GDL 88 GDL 88 PROVIDING GPS POSITION TO GTX 335 345 GTX 335 345 GDL 88 P3251 RS232 2 TX RS232 2 GND 45 7 50 29 RS232 3 RX RS232 3 GND P881 S S TIME MARK B 26 3 TIME MARK 1 PPS A OUT S S 1 ...

Page 163: ...ES RS 232 4 IS THE ONLY PORT THAT SUPPORTS THIS CONNECTION GTX 345 P3251 A429 IN 1B A429 IN 1A 28 27 s GTS 8XX SKY 497 34 33 SKY 899 44 45 A429 TX B A429 TX A TRAFFIC SENSOR ARINC 429 GTX 345 P3252 RS 232 4 TX RS 232 4 RX 5 10 s 20 22 RS 232 3 RX RS 232 3 TX TRAFFIC SENSOR RS 232 RS 232 3 GND 21 RS 232 4 GND 15 A429 RX B A429 RX A A429 OUT 1B A429 OUT 1A 6 5 48 EXTERNAL SUPPRESSION 18 89 93 s EXTE...

Page 164: ...1 RS 232 GND 2 GNS 400W 500W 1 P4001 P5001 GTX 345 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 5 ARINC 429 OUT A 6 ARINC 429 OUT B GNS 400W 500W 2 P4001 P5001 RS232 OUT 1 RS232 IN 1 56 57 29 RS 232 IN 3 RS 232 OUT 3 7 50 RS 232 GND 3 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 RS232 OUT 1 RS232 IN 1 56 57 30 RS 232 IN 2 RS 232 OUT 2 8 51 RS 232 GND 2 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 5 ARINC 429 OUT A 6 A...

Page 165: ...NG RESISTORS ARE INSTALLED SHIELDS FOR AUDIO CABLES SHOULD BE GROUNDED AT ONE END WITH LEADS LESS THAN 3 0 INCHES AND LEFT FLOATING AT THE OTHER END GARMIN SL 10 15 SERIES BOTTOM GMA 340 GMA 347 GMA 35 GMA 350 J1 P3471 P3501 GTX 3X5 P3251 AUDIO OUT HI AUDIO OUT LO AUDIO INHIBIT 46 47 37 32 31 GND LUG T 39 19 32 31 AUDIO PANEL ANALOG AUDIO IN LO AUDIO IN HI EXTERNAL AUDIO INHIBIT DISCRETE GND CONNE...

Page 166: ...gure D 13 GTX 3X5 Radio Altimeter Interconnect ONLY APPLICABLE TO FREE FLIGHT RA 4500 P N 84560 X2 XXXX GTX 3X5 P3251 A429 IN 1B A429 IN 1A 28 27 s FREE FLIGHT RA 4500 12 11 GARMIN GRA 55 5500 52 55 HONEYWELL KRA 405B B C A429 TX B A429 TX A RADIO ALTIMETER ARINC 429 P1 J5501 P1 1 1 ...

Page 167: ...20 3 20 GARMIN GAD 42 13 14 A429 TX B A429 TX A HEADING SOURCE ARINC 429 1 GARMIN GRS 77 12 27 HONEYWELL EFIS 40 50 SG 465 47 20 COLLINS AHC 85E 16 14 AVIDYNE EXP5000 700 00006 22 21 A429 TX B A429 TX A HEADING SOURCE ARINC 429 ASPEN EFD1000 26 27 SANDEL SN3308 11 29 SANDEL SN3500 30 15 P1 P1 P2 P4652B P3 P732 P771 P421 P6202 A429 IN 1B A429 IN 1A 28 27 s 1 s GTX 3X5 P3251 A429 IN 1A GARMIN GNS 4X...

Page 168: ...ONSE SUITABLE MODELS ARE EDMO 655 AND DAVTRON C307PS DISCRETE I O PINS ARE CONFIGURABLE REFER TO SECTION 6 6 THE SQUAT SWITCH INPUT CAN BE USED TO CONTROL AIR GROUND STATUS THE INPUT SENSE CONFIGURATION IS DESCRIBED IN TABLE 6 8 GTX 3X5 P3251 37 AUDIO MUTE TRAFFIC MUTE 36 EXT IDENT IDENT PRI 58 AIR DATA SELECT AIR DATA SELECT SQUAT SWITCH 57 ALT S OAT PROBE IN OAT PROBE OUT 3 25 1 2 3 XPDR 1 14 EX...

Page 169: ...NN 40 22 A429 TX B A429 TX A AIR DATA COMPUTER ARINC 429 SHADIN 8800T 7 15 ACK Technologies A 30 7 14 SHELL TRANS CAL IA RS232 X SSD 120 4 9 5 CONFIG JUMPERS 1 2 7 8 SHADIN F ADC 200 F ADC 2000 6 9 s GARMIN GDC 74 29 30 B D SPIRENT 90004 003 27 9 Bendix King HONEYWELL KDC 481 U i Bendix King HONEYWELL KDC 281 5 6 14 POWER 1 SHADIN ADC 2000 7 8 2 3 4 DB15 P3 DB9 J5 DB15 J2 DB9 P741 P2811 P4811 J1 J...

Page 170: ...F INSTALLED RS 232 SPLICE MUST BE MADE ADJACENT TO GTX 1 CONNECTOR AS SHOWN CONFIGURE ENCODER OUTPUT TO TRIMBLE GARMIN 9600 BPS FORMAT IF USING RS 232 SOFTWARE METHOD LIMIT STRAP LENGTH TO SPECIFIED LENGTH IN THE MANUFACTURER S INSTALLATION MANUAL POWERING SAE 5 35 THROUGH THE SWITCHED OUTPUT IS OPTIONAL ALTITUDE MAY BE INPUT ON RS 232 IN 1 RS 232 IN 2 OR RS 232 IN 3 1 2 3 4 5 6 ...

Page 171: ...UT 1 56 30 GNS 400W 500W 1 P4001 P5001 GTX 335 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 5 ARINC 429 OUT A 6 ARINC 429 OUT B GNS 400W 500W 2 P4001 P5001 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 ARINC 429 IN 1A ARINC 429 IN 1B 48 49 5 ARINC 429 OUT A 6 ARINC 429 OUT B SINGLE GNS 400W 500W SERIES P3251 P3251 s s s s DISCRETE OUT 11 15 TIS A SELECT 1 RS 232 2 RX s RS 232 3 GND 51 s RS232 OUT 1 56 30 RS 232 ...

Page 172: ...N TO CONFIGURE PORT 4 FOR RS 422 OPERATION IF PORT 4 IS USED AS AN RS 422 PORT RS 232 PORT 4 CANNOT BE USED GTX 345 345R P3251 RS 232 3 RX 29 s 6 RS 232 3 TX GARMIN FS 110 210 RS 232 3 GND 50 RS 422 TX A 11 s 4 RS 422 RX A RS 422 RX B 10 RS 422 TX B 12 s s P3252 P301 5 15 GROUND AIRCRAFT POWER BT LINK 1A AIRCRAFT GROUND 1 1 P3252 GTX 345 MX20 GMX 200 RS 422 PORT 4A RS 232 PORT 4B 23 4 S 11 12 RS 4...

Page 173: ... D 27 Figure D 20 GTX 335 GDU 620 Interconnect GDU 620 1 P4001 P5001 GTX 335 DISCRETE OUT 26 15 TIS A SELECT ARINC 429 IN 7A ARINC 429 IN 7B 4 26 5 ARINC 429 OUT A 6 ARINC 429 OUT B P3251 s GDU 620 2 P4001 P5001 DISCRETE OUT 26 ARINC 429 IN 7A ARINC 429 IN 7B 4 26 s S ...

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