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190-01499-02

GTX 3X5 Transponder TSO Installation Manual

Rev. 9

Page E-1

CS-ACNS Compliance Matrix

Appendix E CS-ACNS Compliance Matrix

E. 1 Elementary Surveillance (ELS)

...................................................................................................................

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E. 2 Enhanced Surveillance (EHS)

...................................................................................................................

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E. 3 ADS-B......................................................................................................................................................

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E.1

Elementary Surveillance (ELS)

The information in appendix E-1 is applicable to GTX 335/335R/345/345R units running software v2.05 or earlier.

Table E-1 ELS

CS-ACNS SECTION

CS-ACNS ITEM DESCRIPTION

COMPLIANCE SUMMARY

CS ACNS.D.ELS.001 Applicability

Provided that the differences listed in Appendix
D have also been addressed, then previous
compliance declarations with JAA TGL 13
Revision1 (Certification of Mode S Transponder
Systems for Elementary Surveillance)
supplemented with the additional assessments is
another Acceptable Means of Compliance.

Not applicable for the new GTX 335/335R/345/345R
units.

CS ACNS.D.ELS.010 Transponder
Characteristics

a)

The transponder(s) is (are) an approved level
2 or greater Mode S transponder(s) with
Elementary Surveillance and Surveillance
Identifier (SI) capability.

The GTX 335/335R/345/345R units are TSO Class 1 Level
2 transponder with Level C (Major) Failure classification
with SI mode capability.

b)

The transponder(s) of aircraft that have
ACAS II installed is (are) ACAS compatible.

The GTX 335/335R/345/345R units do not support an
interface with an ACAS II system therefore the Resolution
Advisory (BDS 3,0) is transmitted as all zeros.

c)

The peak pulse power available at the
antenna end of the transmission line of the
transponder is more than 125 W (21 dBW)
and not more than 500 W (27 dBW) for
aircraft that operate at altitudes exceeding 4
570 m (15 000 ft) or with a maximum
cruising speed exceeding 90 m/s (175
knots).

The GTX 335/335R/345/345R units meets the minimum
and maximum transmit power level, 125 W (21 dBW) and
500 W (27 dBW), respectively, when installed according
to the installation manual.

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Summary of Contents for GTX 335

Page 1: ...190 01499 02 June 2017 Revision 9 GTX 3X5 Transponder TSO Installation Manual ...

Page 2: ... complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited 2017 Bluetooth word mark and logos are registered trademarks owned by Bluetooth SIG Inc and any use of such marks by Garmin is under license Other trademarks and trade names are those of their respective owners Garmin is a registere...

Page 3: ...5 NV w GPS to table 1 2 GTX 3X5 Units 1 8 Updated weights for GTX 335 and GTX 345 units in table 1 4 Physical Characteristics Panel Mount Units Updated weights for GTX 335 and GTX 345 units in table 1 5 Physical Characteristics Remote Mount Units Updated Main and ADS B boot block part numbers in table 1 14 Applicable P Ns 3 2 Added GTX 345 NV and GTX 345 NV w GPS to table 3 1 GTX 3X5 Configuration...

Page 4: ...ction in table 6 8 Discrete Outputs 6 6 Updated figure 6 13 Unit Group Updated information in Enhanced Surveillance section for clarity 6 7 Added figure 6 23 Keypad Backlight and Minimum Level Page Added figure 6 24 Photocell Transition Slope and Offset Page Added figure 6 25 Lighting Bus Input Voltage Page Added figure 6 26 Default Backlight and Contrast Offset Page 6 9 Updated figure 6 36 ADS B ...

Page 5: ...N 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 REFER TO GARMIN S WEBSITE WWW GARMIN COM PROP65 WARNING PERCHLORATE MATERIAL SPECIAL HANDLING CAN APPLY REFER TO WWW DTSC CA GOV HAZARDOUSWASTE PERCHLORATE NOTE All screen shots used in ...

Page 6: ...4 Optional Accessories 3 7 3 5 Necessary Installation Materials and Accessories Not Supplied 3 9 3 6 Necessary Special Tools 3 9 3 7 Transponder Antenna 3 10 3 8 GPS Antenna Requirements 3 11 3 9 Minimum Systems Configuration 3 12 3 10 GTX Input Source Priority 3 13 3 11 ADS B In Considerations 3 22 3 12 Bluetooth Considerations GTX 345R Only 3 23 3 13 Field Enablements 3 23 3 14 GPS SBAS Paramete...

Page 7: ...8 Sensors 6 21 6 9 ADSB 6 27 6 10 Diagnostics 6 32 6 11 Remote Unit Configuration 6 33 6 12 Ground Check GPS Reception Check 6 33 6 13 Ground Check Transponder 6 34 6 14 Software Installation Procedure 6 34 7 CONTINUED AIRWORTHINESS 7 1 APPENDIX A DATA FORMATS A 1 A 1 RS 232 Air Data Input Format A 1 A 2 ARINC 429 Input Formats A 5 A 3 ARINC 429 Output Formats A 9 APPENDIX B GTX 3X5 MECHANICAL DRA...

Page 8: ...ash Message Indicator Page 6 16 Figure 6 19 Bluetooth Page 6 16 Figure 6 20 EHS Page 6 16 Figure 6 21 Display Group 6 17 Figure 6 22 Display Backlight and Minimum Level Page 6 18 Figure 6 23 Keypad Backlight and Minimum Level Page 6 18 Figure 6 24 Photocell Transition Slope and Offset Page 6 19 Figure 6 25 Lighting Bus Input Voltage Page 6 19 Figure 6 26 Default Backlight and Contrast Offset Page ...

Page 9: ...wer Configuration Typical Interconnect D 3 Figure D 2 GTX 345 G1000 Interconnect D 5 Figure D 3 GTX 335 G1000 Interconnect D 7 Figure D 4 GTX 3X5 GNS 480 CNX80 Interconnect D 8 Figure D 5 GTX 335 GTN 6XX 7XX Typical Interconnect D 9 Figure D 6 Single Dual GTX 335 Single GTN 6XX 7XX Interconnect D 10 Figure D 7 GTX 345 GTN 6XX 7XX Typical Interconnect D 11 Figure D 8 GTX 345 Single Dual GTN 6XX 7XX...

Page 10: ...r Antennas 3 11 Table 3 9 Minimum System Configuration 3 12 Table 3 10 Compatible ADS B Traffic FIS B Displays 3 12 Table 3 11 Air Data Select Source Priority 3 14 Table 3 12 Barometric Vertical Rate Source Priority 3 15 Table 3 13 Indicated Airspeed Source Priority 3 15 Table 3 14 True Airspeed Source Priority 3 15 Table 3 15 Barometric Pressure Setting Source Priority 3 16 Table 3 16 MCP FCU Sel...

Page 11: ...ark Outputs 5 11 Table 5 17 Configuration Module Inputs and Outputs 5 12 Table 5 18 USB Inputs and Outputs 5 12 Table 6 1 RS 232 Channel 1 through Channel 3 Selections 6 6 Table 6 2 RS 232 Channel 4 Selections 6 7 Table 6 3 RS 422 Selections 6 8 Table 6 4 ARINC 429 Inputs 6 9 Table 6 5 ARINC 429 Outputs 6 10 Table 6 6 HSDB Formats 6 11 Table 6 7 Discrete Inputs 6 12 Table 6 8 Discrete Outputs 6 13...

Page 12: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page xi List of Tables Table C 9 Remote Control C 12 Table C 10 TIS A Displays C 13 Table E 1 ELS E 1 Table E 2 EHS E 7 Table E 3 ADS B E 9 ...

Page 13: ... 1 14 2 Design Assurance Levels 1 15 1 14 3 Transmitter Grant of Equipment Authorization 1 16 1 15 License Requirements 1 16 1 16 Reference Documents 1 17 1 1 Scope NOTE Garmin recommends installation of the GTX 3X5 by a Garmin authorized installer Garmin will not be liable for damages that result from improper or negligent installation of the GTX 3X5 to the extent permitted by law Mechanical and ...

Page 14: ...w GPS GTX 345 NV GTX 345 NV w GPS Mode S ES X X X X X X X X X X X ARINC 429 data concentrator X X X X X X X X X X X ADS B In with alerting UAT and 1090 MHz X X X X X X Connext via Bluetooth X X X X X X FIS B X X X X X X TIS traffic X X X X X ADS B In and TAS TCAS traffic integration X X X X X X HSDB forwarding X X X X X X Pressure sensor module optional X X X X X X X X X X X Flight timers X X X X ...

Page 15: ...Radar Beacon System BDS Comm B Data Selector CDTI Cockpit Display of Traffic Information CFR Code of Federal Regulations CG Center of Gravity CONUS Continental United States CS ACNS Certification Specification and Acceptable Means of Compliance for Airborne Communication Navigation and Surveillance CSA Conflict Situational Awareness DC Direct Current DME Distance Measuring Equipment ELS Elementary...

Page 16: ...craft ADS R and TIS B information from ground stations Traffic information received from these transmissions supply compatible ADS B In data to CDTIs to show the pilot 1 4 3 Installation Approval for ADS B Systems The conditions and tests necessary for TSO approval of the GTX 3X5 are minimum performance standards It is the responsibility of the installer to determine if the aircraft installation c...

Page 17: ...evel in some locations The GTX 345 supplies the data to compatible displays Depending on the CDTI it can show NOTAM includes TFRs AIRMET SIGMET SUA METAR TAFs PIREP Winds Temps Aloft Regional NEXRAD CONUS NEXRAD 1 6 TIS System Capabilities The GTX 335 supplies information about nearby traffic through the FAA provided radar based TIS Advisory traffic information is shown on a compatible Garmin disp...

Page 18: ... 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 15 15 O 1 1 I O 1 2 4 Gray code altitude input 3 I 3 1 1 Suppression bus I O 1 1 1PPS O 1 1 OAT input I 1 1 Audio output O 1 1 Configuration module GAE modul...

Page 19: ...ty Report X 1 7 Common Usage GICB Capability Report X 1 8 MSSS GICB Capability Report 1 of 5 X 1 9 MSSS GICB Capability Report 2 of 5 X 1 A MSSS GICB Capability Report 3 of 5 X 1 B MSSS GICB Capability Report 4 of 5 X 1 C MSSS GICB Capability Report 5 of 5 X 1 D MSSS MSP Capability X 2 0 Aircraft Identification X 2 1 Aircraft Registration X 4 0 Selected Vertical Intention X 5 0 Track and Turn Repo...

Page 20: ...measured from face of aircraft panel to rear of connector backshells 10 07 inches 256 mm GTX 335 weight unit only 2 1 lb 0 95 kg GTX 335 with GPS weight unit only 2 2 lb 1 00 kg GTX 335 with rack backplate and connectors 2 9 lb 1 32 kg GTX 335 with GPS with rack backplate and connectors 3 0 lb 1 36 kg GTX 345 weight unit only 2 3 lb 1 04 kg GTX 345 with GPS weight unit only 2 5 lb 1 13 kg GTX 345 ...

Page 21: ...ht with vertical remote mount backplate and connectors 3 3 lb 1 50 kg GTX 335R weight with GX000 remote mount nut plates backplate and connectors 2 7 lb 1 22 kg GTX 335R with GPS weight with GX000 remote mount nut plates backplate and connectors 2 9 lb 1 32 kg GTX 345R weight unit only 2 2 lb 1 00 kg GTX 345R with GPS unit only 2 3 lb 1 04 kg GTX 345R weight with standard mounting tray backplate a...

Page 22: ...top 30 From bottom 10 Characteristic Specification Dimensions 1 12 x 0 62 x 0 57 inches 28 4 x 15 7 x 14 5 mm Weight 0 8 ounces with mounting hardware and harness Operating Temperature 40 F to 158 F 40 C to 70 C Altitude 30 000 feet maximum Voltage Supplied by GTX 3X5 transponder Current Supplied by GTX 3X5 transponder Resolution 1 foot Characteristic Specification Transmitter frequency 1090 MHz 1...

Page 23: ...z Modulation Binary pulse position Data rate 1 Mbps Sensitivity 81 dBm for 90 MSR Characteristic Specification Number of channels 15 12 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...

Page 24: ...Characteristic 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 ...

Page 25: ...ware v2 05 or earlier the units are Level 2 els 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 2ens 3 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 th...

Page 26: ...RTCA DO 229D 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 Ty...

Page 27: ...ls Table 1 17 Complex Hardware Design Assurance Levels 1 Developed to DO 178B level B equivalent process 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 re...

Page 28: ...ements The 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 aviati...

Page 29: ...Receiver System 004 00287 00 G1000 System Installation Manual 190 00303 00 GTX 3X5 Environmental Qualification Form 005 00752 02 GTX 3X5 Mode A C Lock Enablement Guide 190 01499 21 GTX 3X5 Pilot s Guide 190 01499 00 GTX 3X5 Series Transponder G1000 Pilot s Guide 190 01499 01 GTX 3X5 Transponder Control Enablement Guide 190 01499 22 GTX 3X5 Transponder Installation Tool Guide 190 01499 30 Document ...

Page 30: ...are necessary by the TSOs in section 1 14 Installation 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 associate...

Page 31: ...12 3 10 GTX Input Source Priority 3 13 3 11 ADS B In Considerations 3 22 3 12 Bluetooth Considerations GTX 345R Only 3 23 3 13 Field Enablements 3 23 3 14 GPS SBAS Parameters 3 23 3 15 Antenna Considerations 3 24 3 15 1 Transponder Antenna 3 24 3 15 2 GPS Antenna 3 25 3 16 Electrical Bonding 3 27 3 17 Cabling and Wiring 3 27 3 18 Electrical Bonding Considerations 3 27 3 19 Cooling Requirements and...

Page 32: ... 03 G1000 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 Vertical GTX 335R GPS Remote X 011 03301 40 010 01215 40 010 01215 43 G1000 GTX 345 Panel X 011 03302 00 010 01216 00 010 01216 01 GTX 345 NV Panel X 011 03302 20 010 01216 20 010 01216 21 GTX 345 GPS Panel X X 011 03302 40 010 01216 40 010 01216 41 GTX 345 N...

Page 33: ...1214 41 Install rack 115 01771 01 1 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 01 1 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 In...

Page 34: ...stall rack G1000 115 02250 00 Backplate assembly 011 02976 01 Connector kit 011 02977 00 Configuration module 011 00979 03 Product information kit K00 00598 05 GTX 345 010 01216 01 Install rack 115 01771 01 1 Backplate assembly 011 02976 00 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 03 GTX 345 w GPS 010 01216 41 Install rack 115 01771 01 1 Backpl...

Page 35: ...771 01 1 Backplate assembly 011 02976 01 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 04 GTX 345R w GPS vertical mount 010 01217 42 Install rack vertical 011 03762 00 Backplate assembly 011 02976 11 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 04 GTX 345R w GPS G1000 mount 010 01217 43 Install rack ...

Page 36: ...The standard rack P N 115 01771 01 is the functional equivalent of P N 115 01771 00 GTX 345 NV w GPS 010 01216 61 Install rack 115 01771 01 Backplate assembly 011 02976 01 Connector kit 011 02977 01 Configuration module 011 00979 03 Product information kit K00 00598 03 Unit Kit P N Item P N Notes ...

Page 37: ... 2 GX000 System Rack The GTX 3X5 has an optional mount and hardware for GX000 installations Table 3 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 Item P N Pressure sensor module 011 03080 00 Item P N GTX ...

Page 38: ... can be attached 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 If it is necessary to use an antenna doubler refer to the ap...

Page 39: ... 9 BNC connectors for the transponder antenna 10 TNC connectors for the GPS antenna 11 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 co...

Page 40: ...VSWR 1 7 1 at 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 ...

Page 41: ...r the XM connector 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 N...

Page 42: ...B Traffic FIS B Displays Model Transponde r 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 Source Format ADS B Traffic Sour...

Page 43: ...oll Angle Mach Table 3 11 YES Barometric Vertical Rate Table 3 12 Indicated Airspeed Table 3 13 True Airspeed Table 3 14 Barometric Pressure Setting Table 3 15 MCP FCU Selected Altitude Table 3 16 Magnetic Heading Table 3 17 True Heading Table 3 18 Static Air Temp Table 3 19 Total Air Temp Table 3 20 Roll Angle Table 3 35 Mach Table 3 36 NO Applicable Priority Tables START Are the ARINC 429 Source...

Page 44: ...titude Data Select discrete configured Pressure Altitude Table 3 21 Baro Corrected Altitude Table 3 24 YES Is the Air Data Select discrete configured Pressure Altitude Table 3 11 Baro Corrected Altitude Table 3 11 YES NO NO Are Altitude Sources 1 and or 2 configured Pressure Altitude Table 3 22 Baro Corrected Altitude Table 3 25 YES Pressure Altitude Table 3 23 Baro Corrected Altitude Table 3 26 N...

Page 45: ... GX000 6 HSDB 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 lab...

Page 46: ...from an EFIS 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...

Page 47: ... from GTN 1 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...

Page 48: ...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 and is active Altitude Data Select Discrete Source Open Source specified in altitude source configuration 1 Ground Source specified in altitude source conf...

Page 49: ...a remote control 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 configuratio...

Page 50: ...S Priority Source 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 Internally calculated from pressure a...

Page 51: ... from GTN 1 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 da...

Page 52: ...ains a GDL 88 ADS B In must be disabled in the GTX 345 In dual GTX 345 installations that connect through HSDB one GTX 345 must have ADS B In disabled Priority Source 1 ARINC 429 label 325 from an AHRS 2 ARINC 429 label 325 from an EFIS ADC 3 RS 232 from a remote control panel 4 HSDB AHRS data from a GX000 5 HSDB AHRS data from GDU 620 1 6 HSDB AHRS data from GDU 620 2 Priority Source 1 ARINC 429 ...

Page 53: ... 13 Field Enablements Transponder Control and Mode A C Lock field enablements are available with software v2 05 or later For more information refer to GTX 3X5 Mode A C Lock Enablement Guide and GTX 3X5 Transponder Control Enablement Guide 3 14 GPS SBAS Parameters The GTX 3X5 receives the following information from internal and external GPS receivers Latitude Longitude Height above ellipsoid Horizo...

Page 54: ...ircraft 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 1 Be attached away from major protrusions such as engines nacelles propellers and antenna masts 2 Be as far as ...

Page 55: ...ted in order of importance to get the best performance The installer should use best judgment to balance the installation guidelines The GPS antenna should 1 Be installed as near to level as possible with respect to the normal cruise flight attitude of the aircraft 2 Be installed in a location to minimize the effects of airframe shadowing during typical maneuvers 3 Be installed a minimum of two fe...

Page 56: ...NAS ANTENNA 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 57: ...nergy sources e g DC motors high heat sources 4 Wiring that must be shielded must be done as shown in appendix D 5 Shield pigtail lengths must be less than 3 0 inches 3 18 Electrical Bonding Considerations Bond electrical equipment supporting brackets and racks to the aircraft s main structure When surface preparation is necessary to get an electrical bond refer to SAE ARP 1870 section 5 To measur...

Page 58: ...are made through the D sub connectors on the rear of the unit The shield grounds terminate to the connector backshells For additional information For rear connector pinout and descriptions of interface connections refer to section 5 For interconnect diagrams refer to appendix D For special tools refer to section 3 15 Give sufficient space for installation of cables and connectors The installer sup...

Page 59: ... P3251 Shield block P3252 117 00147 01 117 00147 00 2 3 Screw 4 40 x 250 FLHP100 SS P nylon 211 63234 08 2 6 Screw 4 40x 375 PHP SS P with nylon 211 60234 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 pi...

Page 60: ... shield termination to the connector backshell refer to figure 4 2 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 jacket to leave the braid exposed 4 Connect a 20 or 22 AWG wire 13 to the exposed shield of the prepared cable assembly Refer to figu...

Page 61: ...n Manual Rev 9 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 62: ...ure 4 3 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 For the chosen contact location refer to appendix D 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 ...

Page 63: ...re 190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 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 2 127 3 7 21 9 6 2 7 675 1 5 5266 7 81 7 81 0 ...

Page 64: ...Installation Procedure 190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 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 65: ... The GAE module has 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 For this procedure refer to figure 4 4 and figure D 1 1 Remove 0 17 inches of insulation from the e...

Page 66: ...Page 4 9 Figure 4 4 Configuration Module Installation Table 4 2 Configuration Module Kit P N 011 00979 03 Figure 4 4 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 67: ...ads or other obstructions prevent the unit from fully engaging in the rack For drawing dimensions necessary to prepare the cutouts for the GTX 3X5 unit refer to figure B 9 For drilling the mounting holes the GTX 3X5 mounting rack may be used as a template NOTE Step 3 can be done before or after the wire harness is installed in the aircraft 1 Install the rack in a rectangular hole or gap between un...

Page 68: ... of the unit 2 Attach the vertical remote mount shoe to the unit with the four screws provided 3 Torque screws to 15 16 in lbs 4 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 7 4 GX000 Integrated Flight Decks The GTX 3X5 G1000 rack is mounted to the main system rack with the nutplate kit listed in section 3 4 2 ...

Page 69: ...Installation Procedure 190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page 4 12 Figure 4 5 GAE Assembly GARMIN ALTITUDE ENCODER ...

Page 70: ...re the position of the retention mechanism is correct it can be necessary to insert the hex drive tool into the access hole and turn the hex drive tool counterclockwise until it fully stops Insertion 1 Slide unit in until it stops approximately 3 8 inch short of the final position 2 Insert a 3 32 hex drive tool into the access hole at the bottom of the unit face 3 Push on the left side of the beze...

Page 71: ...n 1 Insert the toe of 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 bas...

Page 72: ...6 5 3 1 Power 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 10 5 7 3 HSDB 5 10 5 7 4 RS 422 5 10 5 8 Suppression Bus 5 11 5 9 OAT Input 5 11 5 10 Audio Output 5 11 5 11 Time Mark 5 11 5 12 Configuration Module...

Page 73: ...O 16 CONFIGURABLE 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 23...

Page 74: ... RS 232 IN 3 I 30 RS 232 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 POWE...

Page 75: ...s the signal is an Active Low discretes 52 RS 232 GND 1 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 76: ...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 ETHERNET IN 2 ETHERNET IN ...

Page 77: ...d 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 installation The POWER CONTROL connection controls the POWER CONTROL input This is used as a remote power on off contr...

Page 78: ...several different sources Gray code inputs RS 232 serial inputs ARINC 429 inputs The optional GAE module Garmin P N 011 03080 00 HSDB For altitude source priorities refer to section 3 10 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 o...

Page 79: ...250 milliamp when active For discrete input and output configuration refer to table 6 7 and table 6 8 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...

Page 80: ...nputs and outputs can be configured for different functions depending on the installation Refer to section 6 5 Pins P3252 5 10 and 15 are on the GTX 345 only Table 5 9 RS 232 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 P3251 51 RS 232 OUT 3 P3251 7 O RS 232 IN 3 P3251 ...

Page 81: ...Ethernet Inputs and Outputs 5 7 4 RS 422 The RS 422 interface conforms to the electrical specifications of EIA standard RS 422 Table 5 12 RS 422 Outputs Pin Name Connector Pin I O ARINC 429 OUT A P3251 5 O ARINC 429 OUT B P3251 6 O ARINC 429 IN 1A P3251 27 I ARINC 429 IN 1B P3251 28 I ARINC 429 IN 2A P3251 48 I ARINC 429 IN 2B P3251 49 I Pin Name Connector Pin I O ETHERNET OUT 1A P3252 6 O ETHERNE...

Page 82: ... N 655 PROBE or the Davtron P N C307PS The temperature input specification is 1 microamp per degree Kelvin 1uA K Connect the probe positive wire to pin 25 and negative wire to pin 3 For wire designations refer to the manufacturer s specifications Table 5 14 OAT Input and Output 5 10 Audio Output The audio output is used to provide aural traffic alerts The output is capable of 100 mW into a 500 ohm...

Page 83: ...ation When used A separate configuration module is not necessary Table 5 17 Configuration Module Inputs and Outputs 5 13 USB Interface CAUTION USE THE USB CABLE SHIPPED WITH THE UNIT DO NOT LENGTHEN OR TIE UP IN BUNDLES WITH OTHER ELECTRICAL WIRES POTENTIAL DAMAGE OR INTERFERENCE DUE TO COUPLING WITH OTHER CABLES WILL OCCUR Only use the USB interface for unit configuration software updates and ser...

Page 84: ... Lock Enablement Guide 6 2 Mounting Wiring and Power Checks CAUTION MAKE 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...

Page 85: ...optional GAE module operates as a configuration module In this section configuration instructions are for panel mount units To configure remote units refer to section 6 11 To enter configuration mode on a panel mount unit push and hold ENT and apply power Push and hold OFF until the unit powers off to exit configuration mode Push FUNC to cycle through the group pages Push 8 or 9 to scroll up or do...

Page 86: ...ransponder select XPDR If installing a GTX 345 in a GX000 system select HSDB Volume To raise the volume of the transponder audio push 8 To lower the volume push 9 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 Figure 6 2 Audio Page NONE TONE MSG 1 MSG 2 MSG 3 AUD TIMER EXPIRED ALRT ...

Page 87: ...tions are Timer Expired Alrt Panel Mount Units Only Configures 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 Configures the traffic alerting type Selections are Figure 6 4 Audio Page 3 OFF MESSAGE MSG W CHIME GTX 335 ONLY OFF MESSAGE MSG W CHIME OFF MESSAGE MSG W CHIME GTX 335 ONLY ...

Page 88: ...02 GTX 3X5 Transponder TSO Installation Manual Rev 9 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 A429 OUTPUT A429 IN RS 422 OUTPUT RS 232 HSDB INTERFACE ...

Page 89: ...l Input Output REMOTE FMT 2 Supports transponder interface and TIS traffic to GTN GNS 480 CNX80 and G1000 NXi GTX 335 only Input Output GDL Supports GDL 88 interface All 2 Input Output GNS Supports GNS 400W 500W Series ADS B In weather GTX 345 only Traffic is supported over ARINC 429 Supplies GPS and HAT data GTX 345 1 All 4 Input Output CONNEXT FMT 1 Supports G3X for ADS B In weather and traffic ...

Page 90: ...n the source of the data All Output TIS A OUT FMT Transmits TIS A traffic for non certified displays GPSMAP 396 496 695 696 G3X G300 GTX 335 only Output LGCY TRAFFIC Supports GDL 90 traffic interface to G1000 GTX 345 only Output MAPMX Supports Garmin AHRS units All 1 3 Input AVIATION FMT 2 Provides internal GPS data to the GTR All 5 Input Output Selection Description Input Output OFF Information i...

Page 91: ...format also provides weather to a G1000 installation Table 6 3 RS 422 Selections 1 Supported with software v2 05 or later Figure 6 7 RS 422 Output Page Channel Input Output Selection Description Notes RS 422 Output OFF Information is not transmitted CONNEXT FMT 3 Supports output to Flight Stream 210 MX FMT 1 Supports GMX 200 MX FMT 2 Supports MX20 OPT LGCY ADSB Supports third party display of ADS ...

Page 92: ...43A Receives GPS information from ARINC 743A EFIS AIR DATA 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 RADIO ALTITUDE Receives radar altitude information TRAFFIC 1 Receives traffic information f...

Page 93: ...used Figure 6 9 A429 Output Page Format Description Notes OFF Information is not transmitted FORMAT 1 Transponder Control Format 1 1 FORMAT 2 Garmin FORMAT 3 Garmin Transponder Control Format 1 1 2 FORMAT 4 Garmin TAS and GPS data 3 FORMAT 5 Garmin concentrator Garmin TAS and GPS data 3 FORMAT 6 Transponder Control Format 1 Garmin TAS GPS Data 3 FORMAT 7 Garmin Transponder Control Format 1 Garmin ...

Page 94: ...ed to the GTX 345 Selections are YES NO Table 6 6 HSDB Formats Figure 6 10 HSDB Interface Page Interface Description G500 G600 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 displ...

Page 95: ...trol format remote or transponder formats is used to control the transponder SQUAT 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 ...

Page 96: ... 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 or P3252 Commands TAS TCAS standby operate Discrete output operation automatically sets through TAS TCAS input configuration GTX 345 only ...

Page 97: ...6 6 Unit 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 EHS INSTALLATION ID TEMPERATURE UNITS ALTITUDE UNITS FIS B PROCESSING ALTITUDE ALERT DEVIATION VFR ID RESTORE PAGES ON POWER UP FLASH MESSAGE INDICATOR BLUETOOTH ...

Page 98: ...Figure 6 15 Altitude and 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 Configures the VFR squawk code for your country Ra...

Page 99: ...the unit is power up select YES Figure 6 17 Altitude Alert Deviation and Restore Page Flash Message Indicator Panel Mount Units Only Software v2 05 and Later To have MSG flash when a new alert occurs select YES If No is selected the MSG indicator is visible when an alert is active but does not flash Figure 6 18 Flash Message Indicator Page Bluetooth GTX 345 Only To transmit information to a PED us...

Page 100: ... NOTE Make sure the brightness levels match the lighting levels of other equipment in the panel under night conditions Figure 6 21 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 101: ...um brightness Figure 6 22 Display Backlight and Minimum Level Page Keypad Backlight Configures the source for the keypad backlight control and adjustment Select PHOTOCELL if the lighting level uses ambient lighting Select LIGHTING BUS if an input from the lighting bus is used to dim the keypad Minimum Level Configures the minimum brightness of the keypad The range is 0 to 100 The higher the number...

Page 102: ... in the panel Figure 6 24 Photocell Transition Slope and Offset Page Lighting Bus Input Vltg Configures the voltage of the lighting bus source Selections are Figure 6 25 Lighting Bus Input Voltage Page Display and Bezel Key Lighting Slope Configures the sensitivity of the display or bezel keys for any given lighting bus input level Set the slope higher for a brighter display for a given increase i...

Page 103: ...O Installation Manual Rev 9 Page 6 20 Default Backlight Offset Manually configures the default backlight offset value from 10 to 99 Default Contrast Offset Manually configures the default contrast offset value from 50 to 50 Figure 6 26 Default Backlight and Contrast Offset Page ...

Page 104: ...ev 9 Page 6 21 6 8 Sensors Figure 6 27 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 ALT ENCODER ADJUSTMENT INTERNAL AHRS ORIENTATION INTERNAL AHRS CALIBRATION ...

Page 105: ... GTX 3X5 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 Configures the primary altitude source Selections are Altitude Source 2 Configures the secondary altitude source Selections are Figure 6 29 Altitude Source Page NONE RS232 1 RS232 2 RS232 3 A429 1 A429 2 HSDB GTX 345 only GILLHAM ALT ENC NONE RS232...

Page 106: ... Selections are Lat Ofst Configures the distance from the antenna and the centerline of the aircraft in meters Selections are Lon Ofst Configures the distance of the GPS antenna from the nose of the aircraft in meters Selections are GPS 2 Src Configures the secondary GPS source Selections are Intgrty Configures the integrity for the secondary GPS Selections are NONE INTRNL RS232 1 RS232 2 RS232 3 ...

Page 107: ...odule is connected to the backplate Ceiling Configures aircraft maximum altitude between 8 000 feet and 30 000 feet Test Points Configures 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 31 Internal Alt Encoder Page Internal Alt Encoder Adjustment Configures the GAE module altitud...

Page 108: ... of the unit relative to 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 33 Figure 6 33 Setting the Yaw Angle Figure 6 34 Internal AHRS Orientation Page Nose Right Wing Positive Yaw A...

Page 109: ... Installation Manual Rev 9 Page 6 26 Internal AHRS Calibration GTX 345 Only Calibrate the internal AHRS to level 0 pitch and 0 roll The Internal AHRS Orientation must be set and the aircraft must be level before beginning this procedure Figure 6 35 Internal AHRS Calibration Page ...

Page 110: ...installed It is not necessary to install a certified ADS B In system NOTE The GDL format must be configured to modify UAT OUT RMT CONTROL Figure 6 36 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 ADDRESS AIRCRAFT TAIL NUMBER FLT ID PREFIX ACFT STALL SPEE...

Page 111: ...ge Acft Stall Method Configures which type of action is taken in the event of a stall Selections are Acft Stall Speed If the aircraft category is set to Light Small or High Performance stall speed selections are 30 kts to 200 kts in 1 kt increments Figure 6 38 Aircraft Stall Method and Stall Speed Page Aircraft Length Configures aircraft length in meters UNKNOWN LIGHT SMALL HIGH PERFORMANCE ROTORC...

Page 112: ...s are UAT Out Rmt Control Not available with GDL 88 software v3 33 or earlier Figure 6 40 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 41 1090ES In Capable and UAT In Capable Page Unknown 34 0 mt 52 0 mt 80 0 mt 23 0 mt 38 0 mt 59 5 ...

Page 113: ...tail number Address Set 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 43 Aircraft Tail Number and Address Page Allow Pilot To Edit Flt ID Select YES to let the pilot change the flight ID Figure 6 44...

Page 114: ...r TSO Installation Manual Rev 9 Page 6 31 Default Flt ID Configures the default flight ID used in normal mode Flight ID Prefix Configures the flight ID prefix with the carrier abbreviation For example Garmin AT is GAT Figure 6 45 Default Flight ID and Flight ID Prefix Page ...

Page 115: ...uration Checkout 190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page 6 32 6 10 Diagnostics Figure 6 46 Diagnostics Group DIAG LCD RS232 OAT INPT LT BUS DISCRETE INPUT STATE UNIT PHOTO A429 SRC 2 GPS SRC 1 HSDB ...

Page 116: ...5 and GTX 345 units with an optional internal GPS receiver 1 Make sure the LAT LON on the ADS B Out page matches with a known reference 2 Select 121 150 MHz on the COM transceiver to be tested 3 Transmit for a period of 35 seconds 4 Make sure the 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 spacin...

Page 117: ... airborne state place the GTX 3X5 in Ground Test mode Ground Test mode overrides the air ground logic to transmit as if the GTX is airborne This mode has a duration of one power cycle To enable Ground Test mode press and hold CRSR while applying power to the unit Ground Test mode can be enabled by the GTX 3X5 Install Tool on the State page FAR 91 413 provides guidance for the transponder check 6 1...

Page 118: ... GTX 3X5 Transponder TSO Installation Manual Rev 9 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 119: ...essage is received per second A 1 2 Altitude 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 a...

Page 120: ...I characters 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 carri...

Page 121: ...resents 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 ...

Page 122: ...I characters 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...

Page 123: ...50 ms 200 ms 325 Roll Angle 50 ms 200 ms 332 Body Lateral Acceleration 60 ms 240 ms 333 Body Normal Acceleration 60 ms 240 ms 340 Inertial Yaw Rate 20 ms 80 ms 365 Inertial Vertical Velocity 40 ms 160 ms Label Data Transmission Rate Periodic Timeout 203 Altitude 62 5 ms 250 ms 204 Baro Corrected Altitude 1 62 5 ms 250 ms 205 Mach 125 ms 500 ms 206 Indicated Airspeed 125 ms 500 ms 210 True Airspeed...

Page 124: ...ms 121 GNSS Longitude Fine 200 ms 2000 ms 130 Horizontal Protection Limit 200 ms 2000 ms 133 Vertical Protection Limit 200 ms 2000 ms 136 Vertical Figure of Merit 200 ms 2000 ms 140 UTC Fine 200 ms 2000 ms 141 UTC Fine Fractions 200 ms 2000 ms 142 Vertical Velocity Figure of Merit 200 ms 2000 ms 145 Horizontal Velocity Figure of Merit 200 ms 2000 ms 150 UTC 200 ms 2000 ms 165 Vertical Velocity 200...

Page 125: ...500 ms 500 ms 210 True Airspeed 50 ms 50 ms 211 Total Air Temperature 2000 ms 2000 ms 212 Altitude Rate 250 ms 250 ms 213 Static Air Temperature 2000 ms 2000 ms 234 Baro Setting hPa 500 ms 500 ms 235 Baro Setting in Hg 500 ms 500 ms 306 Joystick Waypoint Latitude 500 ms 500 ms 307 Joystick Waypoint Longitude 500 ms 500 ms 314 True Heading 200 ms 200 ms 320 Magnetic Heading 200 ms 200 ms 325 Roll A...

Page 126: ...345 Label Data Transmission Rate Periodic Timeout 314 True Heading 50 ms 200 ms 320 Magnetic Heading 50 ms 200 ms Label Data Transmission Rate Periodic Timeout 013 TCAS Display Control 100 ms 400 ms 015 Altitude Select Limits 100 ms 400 ms 016 Mode S Control Panel Data 100 ms 400 ms 024 Tandem Control Word See Note 1 See Note 1 031 ATCRBS Control 100 ms 400 ms 233 Flight ID Data Word 1 5000 ms 200...

Page 127: ...Rate Periodic Timeout 016 TCAS Mode Sense 500 ms 2000 ms 130 Intruder Range 500 ms NA 131 Intruder Altitude 500 ms NA 132 Intruder Bearing 500 ms NA 270 Vertical RA 500 ms 2000 ms 274 TCAS Output 500 ms 2000 ms 350 TCAS Fault Summary 500 ms 2000 ms 357 Request to Send End of Transmission 500 ms NA Label Data Transmission Rate Priority Order 273 GNSS Sensor Status 200 ms 1 76 GNSS Altitude 200 ms 2...

Page 128: ...nder to TCAS interface specified in ARINC 735 also known as the XT bus Table A 12 TAS Output Labels Label Data Transmission Rate 100 Selected Course 1 200 ms 203 Altitude 100 ms 204 Baro Corrected Altitude 1 100 ms 206 Indicated Airspeed 100 ms 210 True Airspeed 100 ms 211 Total Air Temperature 100 ms 213 Static Air Temperature 100 ms 306 Joystick Waypoint Latitude 500 ms 307 Joystick Waypoint Lon...

Page 129: ...abel immediately when it is received 2 The GTX only transmits this label when the data is valid Label Data Transmission Rate 130 Intruder Range 500 ms 131 Intruder Altitude 500 ms 132 Intruder Bearing 500 ms 274 TCAS Output 500 ms 313 Own Aircraft Track Angle 500 ms 350 TCAS Fault Summary 500 ms 357 End of Transmission 500 ms 371 GA Equipment Identifier 500 ms Label Data Transmission Rate 024 Tand...

Page 130: ...y using a variant of the TCAS to display interface specified in ARINC 735 Table A 15 Traffic Labels Label Data Transmission Rate 130 Intruder Range 500 ms 131 Intruder Altitude 500 ms 132 Intruder Bearing 500 ms 203 Own Aircraft Pressure Altitude 500 ms 313 Own Aircraft True Hack 500 ms 314 Own Aircraft True Heading 500 ms 353 ADS B Alerts and Status 500 ms 354 TAS TCAS TCAD Status 500 ms 357 Requ...

Page 131: ...nt Assembly B 4 Figure B 4 GTX 3X5R GPS Standard Remote Mount Dimensions and Center of Gravity B 5 Figure B 5 GTX 3X5 Vertical Remote Mount B 6 Figure B 6 GTX 3X5 Vertical Remote Mount Dimensions and Center of Gravity B 7 Figure B 7 GTX 3X5R GPS G1000 Mount Rack Assembly B 8 Figure B 8 GTX 3X5R GPS G1000 Mounting Rack Dimensions and Center of Gravity B 9 Figure B 9 GTX 3X5 Panel Cutout Detail B 10...

Page 132: ...GTX 345 Sub Assy GTX 345 w GPS Sub Assy GTX 345 NV Sub Assy GTX 345 NV w GPS 011 02977 00 011 00979 03 115 01771 01 011 02976 00 011 02977 00 011 00979 03 115 01771 01 011 02976 00 011 02977 00 011 00979 03 115 01771 01 011 02976 00 011 02977 00 011 00979 03 115 01771 01 011 02976 01 011 02977 01 011 00979 03 115 01771 01 011 02976 00 011 02977 01 011 00979 03 115 01771 01 011 02976 01 011 02977 0...

Page 133: ...90 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page B 3 GTX 3X5 Mechanical Drawings Figure B 2 GTX 3X5 GPS Panel Mount Dimensions and Center of Gravity 5 10 17 03 6 0 6 1 25 7 6 5 0 0 9 17 ...

Page 134: ...03301 40 010 01217 00 011 03303 00 010 01217 40 011 03303 40 Sub Assy GTX 335R Sub Assy GTX335R w GPS Sub Assy GTX345R Sub Assy GTX345R w GPS 011 02977 00 011 00979 03 011 02977 00 011 00979 03 011 02977 01 011 00979 03 011 02977 01 011 00979 03 115 01771 01 115 01771 01 115 01771 01 115 01771 01 011 02976 00 011 02976 01 011 02976 00 011 02976 01 Remote Remote Remote Remote 4 8 120 4 9 124 5 0 12...

Page 135: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page B 5 GTX 3X5 Mechanical Drawings Figure B 4 GTX 3X5R GPS Standard Remote Mount Dimensions and Center of Gravity 0 0 0 9 17 ...

Page 136: ... 03301 00 Sub 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 GTX34...

Page 137: ...lation Manual Rev 9 Page B 7 GTX 3X5 Mechanical Drawings Figure B 6 GTX 3X5 Vertical Remote Mount Dimensions and Center of Gravity 1 81 45 8 6 56 166 7 60 15 3 1 22 31 1 74 18 7 9 29 236 0 B A 1 03 26 1 4 00 101 6 8 00 203 2 875 22 23 C 11 4 290 ...

Page 138: ... ASSEMBLY MOUNT TYPE DIM 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 0297...

Page 139: ...Figure B 8 GTX 3X5R GPS G1000 Mounting Rack Dimensions and Center of Gravity 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 6 90 175 3 7 26 184 5 38 9 7 48 12 2 96 24 4 ...

Page 140: ...190 01499 02 GTX 3X5 Transponder TSO Installation Manual Rev 9 Page B 10 GTX 3X5 Mechanical Drawings Figure B 9 GTX 3X5 Panel Cutout Detail ...

Page 141: ... B 11 GTX 3X5 Mechanical Drawings Figure B 10 GTX 3X5 Connector and Vent Locations Figure B 11 Optional Garmin Altitude Encoder CONNECTORS VENT BACK PLATE ASSEMBLY 011 02976 00 011 02976 01 CONNECTOR KIT 011 02977 00 011 02977 01 OPTIONAL ALTITUDE ENCODER 011 03080 00 ...

Page 142: ...ion Appendix C Equipment 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 6 C 5 Radar Altimeters C 6 C 6 Heading Reference Sources C 7 C 7 Traffic Sensors GTX 345 Only C 9 C 8 Bluetooth C 10 C 9 Remote Control C 11 C 10 TIS A Display C 12 ...

Page 143: ...0W 500W Series 3 RS 232 ADSB TFC GNS Supports control of ADS B Traffic only also includes GPS data from the GNS 400W 500W ADSB TFC WX GNS Supports weather and control of ADS B traffic also includes GPS data from the GNS 400W 500W 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 TRA...

Page 144: ... 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 only software version 2 10 and earlier or GTX 335 345 software version 2 11 and later Note that the primary purpose of this interface is for ADS B In Data howeve...

Page 145: ...ystem 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 Enc...

Page 146: ... ADC 200 N A ADC FMT 1 ADC FMT 1 F ADC 2000 N A ADC FMT 1 ADC FMT 1 Either the RS 232 or ARINC 429 data format can be used for the Shadin 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 configu...

Page 147: ...ta Format GTX 3X5 Configuration Setting Garmin SL10 SL10MS SL10M SL10S SL15 SL15M GMA 340 GMA 347 GMA 35 GMA 350 Analog Audio Audio XPDR Honeywell Bendix King KMA 24 KMA 24H 70 71 KMA 26 DMA 28 PS Engineering PMA 6000 PMA 7000 Series PMA 8000 Series Manufacturer Model Data Format Interface Configuration GTX 3X5 Configuration Free Flight RA 4500 ARINC 429 N A RADIO ALTITUDE Garmin GRA 55 5500 Honey...

Page 148: ...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 GDU 620 ARINC 429 GENERAL EFIS AIR DATA 3 Speed HIGH EFIS AIR DATA 3 Speed HIGH Note that this interface also provides altitude data Refer to table C 3 GTN 6XX 7XX RS 232 GTX Mode S 4 OR GTX w TIS 5 REMOTE FMT 1 4 OR REMOTE FMT 2 5 REMOTE FMT 1 4 OR REMOTE FMT 2 5 This configuratio...

Page 149: ... Rev 9 Page C 8 Equipment Compatibility and Configuration 1 Heading information only 2 Attitude and heading information 3 Altitude airspeed altitude rate and heading information 4 Installation with no TIS traffic 5 Installation with TIS traffic GTX 335 only ...

Page 150: ... Traffic Display Destination Primary TX 1 TRAFFIC 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 concentrat...

Page 151: ... 920 ARINC 429 Input Controller Discrete Intruder File Protocol ARINC 735 TRAFFIC 5 Speed HIGH L3 Comm SKY 497 SKY 899 ARINC 429 Input N A TRAFFIC 2 Speed HIGH Manufacturer Model Data Format Input Output GTX 345 Configuration Setting Notes Garmin Internal Bluetooth N A Bluetooth Enabled Flight Stream 110 210 RS 232 Input CONNEXT FMT 3 Both the RS 232 input and RS 422 output are required internal B...

Page 152: ...onfiguration 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 REMOTE FMT 2 N A Installation with TIS G950 G1000 RS 232 GTX 33 1 OR GTX 33ES 2 REMOTE FMT 1 3 OR LGCY REMOTE 1 4 REMOTE FM...

Page 153: ...T 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 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 ...

Page 154: ...ect D 11 Figure D 8 GTX 345 Single Dual GTN 6XX 7XX Interconnect D 13 Figure D 9 GTX 335 345 GDL 88 Interconnect D 14 Figure D 10 GTX 345 Traffic Sensor Interconnect D 15 Figure D 11 GTX 345 Single and Dual 400W 500W Series D 19 Figure D 12 GTX 3X5 Audio Interconnect D 20 Figure D 13 GTX 3X5 Radio Altimeter Interconnect D 21 Figure D 14 GTX 3X5 AHRS Heading Source D 22 Figure D 15 GTX 3X5 Switches...

Page 155: ...nd associated 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 conn...

Page 156: ...PS SBAS ANTENNA 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...

Page 157: ...25 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 FOR DETAILS REFER TO SECTION 5 3 1 GPS KEEP ALIVE IS RECOMMENDED FOR GPS INSTALLS IF NOT CONNECTED GPS MAY TAKE UP TO 5 MINUTES TO OBTAIN A GPS FIX FOR LIGHTING BUS CONNECTIONS REFER TO SECTION 5 4 GPS KEEP ALIVE MUST BE CONN...

Page 158: ... 5 RS 232 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 ...

Page 159: ...DING TO UNIT USE ANY AVAILABLE ARINC 429 PORT THIS MUST BE CONFIGURED BY THE INSTALLER GTS 8XX SHOWN AS AN EXAMPLE FOR ALTERNATE EXTERNAL TRAFFIC SYSTEM OPTIONS REFER TO EXTERNAL TRAFFIC SENSORS 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 PROVIDES AN OVERVIEW OF ...

Page 160: ...1 1P603 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...

Page 161: ...P N 7201SYZQE 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 ...

Page 162: ...RS 232 GND 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...

Page 163: ...ESS DESIGNATES FUNCTION CONNECT MODULE WIRE HARNESS TO GTX 3X5 ACCORDING TO WIRE COLOR FOR DETAILS REFER TO SECTION 5 3 1 DASHED AREAS INDICATE ADDITIONAL INTERCONNECTS FOR DUAL INSTALLATION AND ARE NOT REQUIRED FOR SINGLE INSTALLATION AUDIO INHIBIT I O PIN IS CONFIGURABLE FOR DETAILS REFER TO SECTION 5 6 1 2 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...

Page 164: ...MUTE 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 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 V...

Page 165: ...rconnect Sheet 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 FOR DETAILS REFER TO SECTION 5 3 1 1 2 ...

Page 166: ...TN 6XX 7XX 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 MUTE 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...

Page 167: ...CTED 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 ADS B FORMAT 2 SHOULD BE USED FOR BOTH INTERFACES 1 2 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...

Page 168: ...7 34 33 SKY 899 42 43 A429 TX B A429 TX A TRAFFIC SENSOR ARINC 429 A429 RX B A429 RX A A429 OUT 1B A429 OUT 1A 6 5 48 EXTERNAL SUPPRESSION 18 89 93 s EXTERNAL SUPPRESSION 54 55 68 1 TRFC TEST 15 TRFC STBY 16 2 23 STBY OPERATE TEST MODE 85 82 21 19 74 75 P8002 P8001 23 24 25 26 P1 P1 GARMIN L3 COMM HONEYWELL P10 KTA 870 810 KTA 970 910 4 s SQUAT SWITCH 88 24 3 6 AUDIO HI AUDIO LO 20 21 89 90 91 92 ...

Page 169: ... IN 1A 28 27 A429 TX B A429 TX A TRAFFIC SENSOR ARINC 429 EXTERNAL SUPPRESSION 18 s EXTERNAL SUPPRESSION 54 55 68 TRFC TEST 15 TRFC STBY 16 2 23 STBY OPERATE TEST MODE HONEYWELL P10 KMH 820 880 KMH 920 980 s AUDIO MUTE 58 OTHER ALERTING SYSTEMS TERRAIN ANNUNCIATOR S 116 117 22 20 21 AUDIO LOW AUDIO HIGH EXISTING WIRING TO AUDIO PANEL ADV INHIBIT TERRAIN WARN TERRAIN CAUTION 8 4 1 9 2 ...

Page 170: ... PORT ONLY RS 232 PORT 4 CAN BE USED FOR THIS CONNECTION IF THE EXTERNAL TRAFFIC SENSOR WAS INTERFACED TO THE AUDIO PANEL THESE WIRES SHOULD BE CAPPED AND STOWED ONLY THE GTX 345 SHOULD BE INTERFACED TO THE AUDIO PANEL THIS DISCRETE IS TO DRIVE THE SENSITIVITY LEVEL FOR THE TRAFFIC SYSTEM FOR SPECIFIC G950 G1000 INSTALLATIONS THIS DISCRETE IS NOT NECESSARY TO CONNECT TO THE GTX 345 UNLESS THE GTX ...

Page 171: ...ED THE TERRAIN ANNUNCIATOR SIGNALS DRIVE THE AUDIO MUTE INPUT TO THE GTX WITH THE APPLICATION OF TWO ADDITIONAL DIODES P N 1N4007 IF OTHER SYSTEMS INTERFACE TO THE ADV INHIBIT P10 22 THEY SHOULD BE REMOVED FROM P100 22 AND INTERFACED TO THE GTX AS SHOWN IF THE EGPWS IS NOT ENABLED THE AUDIO WIRING CAN BE CAPPED AND STOWED AND THE TERRAIN ANNUNCIATOR SIGNALS WITH THE DIODES DO NOT NEED TO BE CONNEC...

Page 172: ... 232 OUT 2 8 51 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...

Page 173: ...TED AFTER MIXING 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 MUTE 46 47 37 32 31 GND LUG T 39 19 32 31 AUDIO PANEL ANALOG AUDIO IN LO AUDIO IN HI EXTERNAL AUDIO INHIBIT DISCRET...

Page 174: ...gs NOTES Figure 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 175: ...ARMIN GDU 620 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 GA...

Page 176: ...ELVIN RESPONSE SUITABLE MODELS ARE EDMO 655 AND DAVTRON C307PS DISCRETE I O PINS ARE CONFIGURABLE REFER TO SECTION 6 5 THE SQUAT SWITCH INPUT CAN BE USED TO CONTROL AIR GROUND STATUS THE INPUT SENSE CONFIGURATION IS DESCRIBED INTABLE 6 8 GTX 3X5 P3251 37 AUDIO CANCEL TRAFFIC CANCEL 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...

Page 177: ... 2000 MS CONN 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...

Page 178: ... TO GTX 2 IF 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 179: ...IES RS232 OUT 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...

Page 180: ...e D 18 GTX 345 345R Flight Stream Interconnect CIRCUIT BREAKER SHOULD BE LABELED AS SHOWN 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 ...

Page 181: ...RT 4 FOR RS 422 OPERATION IF PORT 4 IS USED AS AN RS 422 PORT RS 232 PORT 4 CANNOT BE USED P3252 GTX 345 MX 20 GMX 200 RS 422 PORT 4A RS 422 PORT 4B 26 11 S 11 12 RS 422 A RS 422 B S P2001 29 9 RS 232 IN 4 PORT CONFIG HI 1 1 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 O...

Page 182: ...CS ACNS D ELS 010 Transponder Characteristics a The transponder s is are an approved level 2 or greater Mode S transponder s with Elementary Surveillance and Surveillance Identifier SI capability The GTX 335 335R 345 345R units are TSO Class 1 Level 2 transponder with Level C Major Failure classification with SI mode capability b The transponder s of aircraft that have ACAS II installed is are ACA...

Page 183: ...compatible control device e g GTN 6XX 7XX GX000 GNS 480 2 The pressure altitude corresponding to within plus or minus 38 m 125 ft on a 95 per cent probability basis with the pressure altitude information referenced to the standard pressure setting of 1013 25 hectopascals used on board the aircraft to adhere to the assigned flight profile The pressure altitude ranges from minus 300 m 1 000 ft to th...

Page 184: ...l interference 6 Emergency status is reported in DF 5 and 21 replies 7 The data link capability report 7 BDS register 10 Data Link Capability Report is provided 8 The common usage GICB capability report 8 BDS register 17 Common Usage Ground Initiated Comm B Capability Report is provided 9 The ICAO 24 bit aircraft address 9 ICAO 24 bit aircraft address is provided in DF 11 squitters 10 Aircraft tha...

Page 185: ...d status is set to airborne The GTX 335 335R 345 345R units will report the airborne state in FS fields 4 5 20 21 and the CA field of DF 11 Furthermore DF 11 provides the additional capability of identifying if the aircraft didn t know the air ground state by transmitting a CA code of 6 or 7 which still translates to an AIRBORNE state CS ACNS D ELS 025 Altitude Source a The reported pressure altit...

Page 186: ... The flight crew is notified when transmission of pressure altitude is inhibited via the annunciation of ON or Standby mode on the front panel or remotely on a compatible control device 5 To select the transponder to the standby or OFF condition 5 The GTX 335 335R 345 345R units are equipped with an OFF and STBY key Remotely installed units are controlled serially and provide a means to place the ...

Page 187: ...r is installed simultaneous operation of transponders is prevented Dual transponder installations are configured by the installer A compatible control device e g GTN 6XX 7XX or a compatible external standby input discrete ensures that only one transponder can be in a state other than standby CS ACNS D ELS 055 ICAO 24 bit Aircraft Address The ICAO 24 bit aircraft address assigned by the competent a...

Page 188: ...section provides standards for airborne Mode S EHS installations which provide on request through Mode S replies elicited by Mode S interrogations airborne parameters in addition to parameters provided by ELS installations compliant with Section 2 See CS ACNS D EHS 015 c See CS ACNS D EHS 015 a 8 c b This certification specification is applied together with Mode S Elementary Surveillance certifica...

Page 189: ...cated Airspeed or Mach No 6 Indicated Airspeed and Mach No are transmitted in BDS 6 0 by the GTX 7 Vertical rate Barometric Altitude rate or Inertial vertical velocity When barometric altitude rate field is provided it is derived solely from barometric measurement 7 Vertical Rate Barometric altitude rate and Inertial Vertical Velocity are transmitted in BDS 6 0 by the GTX 8 Barometric Pressure Set...

Page 190: ...ss than 5000 hrs using the MTBF rates or 2 0E 04 failure rate CS ASNS SECTION CS ACNS DESCRIPTION COMPLIANCE SUMMARY CS ACNS D ADSB 001 Applicability This section provides standards for 1090 MHz Extended Squitter ES ADS B Out installations Information only no compliance statement necessary CS ACNS D ADSB 010 ADS B Out System Approval The equipment contributing to the ADS B Out function is approved...

Page 191: ...a is sourced from transponder internal configuration settings 4 4 a Airborne Horizontal Position Latitude and Longitude a Supported in BDS 0 5 Airborne Position b Airborne Navigation Integrity Category NIC b Supported in BDS 0 5 Airborne Position c Airborne Surface Navigation Accuracy Category for Position NACp c Supported in BDS 6 2 Target State and Status and 6 5 Aircraft Operational Status d Ai...

Page 192: ... source 7 7 a Emergency Status a Supported in BDS 6 1 Emergency Priority Status b Emergency Indication b Data is sourced from current Mode A code status The Mode A code is entered and displayed via the GTX panel or a compatible control device 8 1090 ES Version Number 8 Supported in BDS 6 5 Aircraft Operational Status Bits 41 43 are populated with 2 9 9 a Airborne velocity over Ground East West and...

Page 193: ...gth width of Aircraft 15 Supported in BDS 6 5 Aircraft Operational Status Subtype 1 Data sourced from transponder configuration 16 GPS Antenna Longitudinal Offset 16 Supported in BDS 6 5 Aircraft Operational Status Subtype 1 Data sourced from transponder configuration 17 17 a Geometric Altitude a Supported in BDS 0 9 Airborne Velocity b Geometric Altitude Quality GVA b Supported in BDS 6 5 Aircraf...

Page 194: ...Approval The ADS B transmit unit is approved and it is integrated in the Mode S transponder The GTX 3X5 units have TSOA and meet TSO C112d and TSO C166b with granted deviations CS ACNS D ADSB 035 ICAO 24 bit Aircraft address The ICAO 24 bit aircraft address is implemented as specified in CS ACNS D ELS 055 The ICAO address is programmed as part of the transponder configuration by the installer and ...

Page 195: ...in and radio altitude when possible The on the ground status cannot be set my manual action CS ACNS D ADSB 070 Horizontal Position and Velocity Data Sources a The horizontal position is derived from GNSS data Horizontal position data will be derived from approved GPS sources b The GNSS receiver based horizontal position and velocity data source is approved and performs as a minimum horizontal posi...

Page 196: ...s is provided to indicate the non operational status or failure of the ADS B Out system without undue delay ADS B Out failure indications are provided on the GTX front panel panel annunciators or to a compatible control device any time the ADS B Out system constitutes a failure CS ACNS D ADSB 100 Integrity a The ADS B Out system integrity is designed commensurate with a major failure condition for...

Page 197: ...h a minor failure condition for the transmission of other data parameters GTX 3X5 is designed to meet design assurance level C which exceeds the minor failure classification for TSO C166b 3 b loss of ADS B Out transmission as a minor failure condition CS ACNS D ADSB 105 Continuity The ADS B Out system continuity is designed to an allowable qualitative probability of remote The GTX 3X5 units have a...

Page 198: ...te ARINC 743 and total latency contribution 200 ms Position solution update delay until the next solution overwrite is relayed to the transponder 1000 ms 1 Hz update rate The GTX 3X5 introduces an additional total latency of 250 ms to the ADS B Out system Therefore the total latency of the ADS B Out system with a 1 Hz rate GPS source and the listed assumptions is 1450 ms CS ACNS D ADSB 120 Horizon...

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