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    190-01004-02 January 2012 Rev. C

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    GTN 625/635/650 TSO Installation Manual Page A190-01004-02 Rev. C

    Copyright 2011-2012Garmin International Inc., or its subsidiaries

    All Rights Reserved

    Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted,disseminated, downloaded or stored in any storage medium, for any purpose without the express priorwritten consent of Garmin. Garmin hereby grants permission to download a single copy of this manual

    and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed andto print one copy of this manual or of any revision hereto, provided that such electronic or printed copy ofthis manual or revision must contain the complete text of this copyright notice and provided further thatany unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

    SkyWatch and Stormscope are registered trademarks of L-3 Communications. XM is a registeredtrademark of XM Satellite Radio, Inc.

    Windows is a registered trademark of Microsoft Corporation in the United States and other countries.

    At Garmin, we value your opinion. For comments about this guide, please e-mail:[email protected].

    Garmin International, Inc.1200 E. 151st Street

    Olathe, KS 66062 USATelephone: 913-397-8200

    Aviation Dealer Technical Support Line (Toll Free): (888) 606-5482Web Site Address: www.garmin.com

    Garmin (Europe) Ltd.Liberty House

    Bull Copse RoadHounsdown Business Park

    Southampton, SO40 9RB, UK

    Telephone: 44 (0) 8708501243

    RECORD OF REVISIONS

    Revision Revision Date Description

    A 2/8/11 Initial Release

    B 4/27/11Corrected plug number and added note 8 to Figure D-16.Updated information in system functions Table 1-6. SeeCurrent Revision Description for more details.

    C 1/25/12Added ETSO information and other minor edits. See CurrentRevision Description for more details.

    mailto:[email protected]:[email protected]:[email protected]
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    Page B GTN 625/635/650 TSO Installation ManualRev. C 190-01004-02

    CURRENT REVISION DESCRIPTION

    SectionNumber

    Description of Change

    1.3.4.1 Updated modulation and frequency range of the COM transmitter.

    1.3.4.2 Updated frequency range of the COM receiver.

    1.5.1 Updated Table 1-4 with ETSO information.

    1.5.3 Added deviations for ETSO-2C40c, ETSO-C118, ETSO-C146, and ETSO-C147.

    2.1Added, To mitigate against the loss of navigation and communication, installation ofsecond navigation and/or communication system may be required.

    2.2Added, To meet requirements for Part 25, 27, and 29 aircraft, it is necessary to install asecond VHF communications radio.

    4.4 Deleted, Connector, BNC, Male, Clamp from section.

    4.9 Changed 010-2042-000 to 030-2042-000 in Table 4-5.

    5.1.2 Corrected figure of P1002 connector.

    5.1.3 Corrected figure of P1003 connector.

    5.1.4 Corrected figure of P1004 connector.

    6.6.6.1 Changed range of photocell transition from 0 to 5.

    6.9.5.4

    Added, The default value of 24 seconds is a nominal value for most aircraft. This valuecan be changed depending on the types of operations the aircraft is expected to

    encounter to Auto Standby Delay information.Added, This field should be set to the typical vertical speed climb rate of the aircraft.This number determines the rate of climb necessary for the GTN to assume lift-off fordetecting an airborne state. Refer to the Pilots Operating Handbook (POH) to determinethis value. If the POH does not include aircraft climb rate information, use the defaultvalue of 300 fpm To Altitude Climb Rate for Airborne Transition information.

    Appendix C Updated Backplate Kit Content Differences in Figure C-2.

    Appendix D

    Figure D-2, D-3 and D-4: Added fan.Figure D-5: Simplified entire figure.Figure D-9: Changed interconnect to illustrate wiring for single/dual GTNs to single/dual

    transponders, with and without TIS.Figure D-24: DeletedFigure D-25: Added SUSPEND ANNUNCIATE discrete and note 6.

    DOCUMENT PAGINATION

    Section Pagination

    Table of Contents i - viii

    Section 1 1-1 through 1-20

    Section 2 2-1 through 2-2

    Section 3 3-1 through 3-12

    Section 4 4-1 through 4-10

    Section 5 5-1 through 5-24

    Section 6 6-1 through 6-52

    Section 7 7-1 through 7-2Appendix A A-1 through A-2

    Appendix B B-1 through B-10

    Appendix C C-1 through C-8

    Appendix D D-1 through D-40

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    GTN 625/635/650 TSO Installation Manual Page i190-01004-02 Rev. C

    INFORMATION SUBJECT TO EXPORT CONTROL LAWS

    This document may contain information which is subject to the Export Administration Regulations("EAR") issued by the United States Department of Commerce (15 CFR, Chapter VII, Subchapter C) andwhich may not be exported, released, or disclosed to foreign nationals inside or outside of the UnitedStates without first obtaining an export license. A violation of the EAR may be subject to a penalty of upto 10 years imprisonment and a fine of up to $1,000,000 under Section 2410 of the Export Administration

    Act of 1979. Include this notice with any reproduced portion of this document.

    WARNING

    This product, its packaging, and its components contain chemicals known to the State ofCalifornia to cause cancer, birth defects, or reproductive harm. This notice is beingprovided in accordance with California's Proposition 65. If you have any questions orwould like additional information, please refer to our web site atwww.garmin.com/prop65.

    WARNING

    Perchlorate Materialspecial handling may apply, Seewww.dtsc.ca.gov./hazardouswaste/perchlorate.

    WARNING

    This product contains a lithium battery that must be recycled or disposed of properly.Battery replacement and removal must be performed by professional services.

    CAUTION

    To avoid damage to the GTN, take precautions to prevent Electro-Static Discharge (ESD)when handling the GTN, connectors, fan, and associated wiring. ESD damage can beprevented by touching an object that is of the same electrical potential as the GTN beforehandling the GTN itself.

    CAUTION

    The GTN 625, GTN 635 and GTN 650 has a display that is coated with a special anti-reflective coating and is very sensitive to waxes and abrasive cleaners. CLEANERSCONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It isvery important to clean the display using a microfiber cloth or with a clean, lint-free clothand an eyeglass lens cleaner that is safe for anti-reflective coatings.

    http://www.dtsc.ca.gov./hazardouswaste/perchloratehttp://www.dtsc.ca.gov./hazardouswaste/perchlorate
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    Page ii GTN 625/635/650 TSO Installation ManualRev. C 190-01004-02

    1.

    GENERAL DESCRIPTION ............................................................................................................ 1-1

    1.1 Introduction .............................................................................................................................. 1-11.2 Equipment Description ............................................................................................................. 1-11.3 Technical Specifications ........................................................................................................... 1-2

    1.3.1 Physical Characteristics........................................................................................................ 1-2

    1.3.2

    General Specifications.......................................................................................................... 1-2

    1.3.3

    GTN GPS/SBAS Specifications........................................................................................... 1-3

    1.3.4 COM Specifications (GTN 635/650 Only) .......................................................................... 1-41.3.5

    VOR Specifications (GTN 650 Only) .................................................................................. 1-5

    1.3.6 LOC Specifications (GTN 650 Only) .................................................................................. 1-51.3.7 Glideslope Specifications (GTN 650 Only) ......................................................................... 1-61.3.8 GPS/WAAS Antenna Requirements .................................................................................... 1-7

    1.4 License Requirements............................................................................................................... 1-81.5 Regulatory Compliance ............................................................................................................ 1-9

    1.5.1

    TSO Authorization and Advisory Circular References ........................................................ 1-9

    1.5.2 Non-TSO Functions ........................................................................................................... 1-101.5.3 TSO Deviations .................................................................................................................. 1-121.5.4 FCC Grant of Equipment Authorization ............................................................................ 1-141.5.5

    AFM/AFMS/POH Considerations ..................................................................................... 1-14

    1.6 GTN Databases ....................................................................................................................... 1-181.6.1 Basemap Database ............................................................................................................. 1-181.6.2 Navigation Database .......................................................................................................... 1-181.6.3 FliteChartsDatabase ........................................................................................................ 1-181.6.4 ChartView Database....................................................................................................... 1-191.6.5 SafeTaxiDatabase ............................................................................................................ 1-191.6.6 Terrain Database ................................................................................................................ 1-191.6.7 Obstacle Database .............................................................................................................. 1-19

    1.7

    Fault Detection and Exclusion (FDE) .................................................................................... 1-19

    1.8 Aviation Limited Warranty .................................................................................................... 1-202. LIMITATIONS ................................................................................................................................ 2-1

    2.1

    Installation ................................................................................................................................ 2-1

    2.1.1 GPS Antenna ........................................................................................................................ 2-12.2

    Aircraft Radio ........................................................................................................................... 2-1

    3. INSTALLATION OVERVIEW ...................................................................................................... 3-13.1 Introduction .............................................................................................................................. 3-13.2

    Minimum System Configuration .............................................................................................. 3-1

    3.2.1 VFR Installation ................................................................................................................... 3-13.2.2 IFR GPS Installation in Reciprocating, Single-Engine Aircraft 6000 lbs or Less ............... 3-13.2.3 IFR GPS Plus VOR/LOC/GS Installation ............................................................................ 3-2

    3.3 External Sensors ....................................................................................................................... 3-23.3.1

    Multiple Uncorrected Pressure Altitude Sources ................................................................. 3-2

    3.3.2 Multiple Baro-Corrected Altitude Sources........................................................................... 3-3

    3.3.3

    Multiple Heading Sources .................................................................................................... 3-3

    3.3.4 Multiple Indicated Airspeed Sources ................................................................................... 3-43.3.5 Multiple True Airspeed Sources .......................................................................................... 3-43.3.6

    Multiple VLOC Selected Course Sources ............................................................................ 3-4

    3.3.7 GPS Selected Course Sources .............................................................................................. 3-53.3.8 Total Air Temperature Sources ............................................................................................ 3-53.3.9 Static Air Temperature Sources ........................................................................................... 3-5

    3.4 Antenna Considerations ............................................................................................................ 3-63.4.1 GPS Antenna Location ......................................................................................................... 3-6

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    3.4.2 COM Antenna Location ....................................................................................................... 3-73.4.3

    VOR/LOC Antenna Location ............................................................................................... 3-9

    3.4.4 Glideslope Antenna Location ............................................................................................... 3-93.4.5 Electrical Bonding ................................................................................................................ 3-93.4.6 Interference of GPS .............................................................................................................. 3-9

    3.5 GTN 625/635/650 Mounting Considerations ......................................................................... 3-10

    3.6

    Cabling and Wiring Considerations ....................................................................................... 3-10

    3.7

    Air Circulation and Cooling ................................................................................................... 3-11

    3.8 Compass Safe Distance .......................................................................................................... 3-114.

    INSTALLATION PROCEDURES .................................................................................................. 4-1

    4.1 Unit and Accessories ................................................................................................................ 4-14.2 Optional Accessories ................................................................................................................ 4-2

    4.2.1 GPS Antenna Options .......................................................................................................... 4-24.3 Database Options ...................................................................................................................... 4-34.4 Miscellaneous Options ............................................................................................................. 4-34.5

    Optional Reference Material .................................................................................................... 4-3

    4.6 Enablement Cards ..................................................................................................................... 4-34.7 Installation Materials Required but not Supplied ..................................................................... 4-4

    4.7.1 Accessories Required but not Supplied ................................................................................ 4-44.7.2

    Materials Required but not Supplied (New Installations Only) ........................................... 4-4

    4.7.3 Optional Annunciation Panels .............................................................................................. 4-54.8 Special Tools Required ............................................................................................................. 4-54.9 Coaxial Cable Installation ........................................................................................................ 4-64.10 Equipment Mounting ................................................................................................................ 4-8

    4.10.1 Rack Installation ................................................................................................................... 4-84.10.2 GTN Unit Insertion and Removal ........................................................................................ 4-84.10.3 Unit Replacement ................................................................................................................. 4-8

    4.11 Antenna Installation and Connections ...................................................................................... 4-94.11.1

    GPS Antenna ........................................................................................................................ 4-9

    4.11.2 COM Antenna (GTN 650 Only) ........................................................................................ 4-104.11.3 NAV Antenna (GTN 650 Only) ......................................................................................... 4-10

    5.

    CONNECTOR PINOUT INFORMATION ..................................................................................... 5-1

    5.1 Pin Function List ...................................................................................................................... 5-15.1.1

    P1001 Main ConnectorMain Board ................................................................................. 5-1

    5.1.2 P1002 Connector .................................................................................................................. 5-35.1.3 P1003 COM Connector ........................................................................................................ 5-45.1.4

    P1004 NAV Connector ........................................................................................................ 5-5

    5.2 Power, Lighting, And Antennas ............................................................................................... 5-75.2.1 Power.................................................................................................................................... 5-75.2.2 Lighting Bus ......................................................................................................................... 5-75.2.3 Antennas ............................................................................................................................... 5-85.2.4

    Serial Data ............................................................................................................................ 5-8

    5.2.5 Ethernet (HSDB) ................................................................................................................ 5-12

    5.2.6

    Main Audio Output ............................................................................................................ 5-12

    5.2.7 Main Indicator .................................................................................................................... 5-125.2.8 OBS .................................................................................................................................... 5-135.2.9

    Discrete Inputs ................................................................................................................... 5-14

    5.2.10 Discrete Outputs ................................................................................................................. 5-155.2.11 TIME MARK OUT ............................................................................................................ 5-185.2.12 COM Audio (GTN 650 Only) ............................................................................................ 5-195.2.13 COM Discrete Inputs (GTN 650 Only) .............................................................................. 5-205.2.14 VOR/ILS Audio (GTN 650 Only) ..................................................................................... 5-20

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    5.2.15 VOR/ILS Discrete Inputs (GTN 650 Only) ....................................................................... 5-215.2.16

    VOR/ILS Indicator (GTN 650 Only) ................................................................................. 5-21

    5.2.17 RMI/OBI (GTN 650 Only) ................................................................................................ 5-235.2.18 DME Tuning (GTN 650 Only) ........................................................................................... 5-24

    6. POST INSTALLATION CONFIGURATION AND CHECKOUT PROCEDURES ..................... 6-16.1 System Configuration Overview .............................................................................................. 6-1

    6.2

    Mounting, Wiring, and Power Checks ..................................................................................... 6-1

    6.3

    Connector Engagement Check ................................................................................................. 6-2

    6.4 Configuration Mode Operations ............................................................................................... 6-26.5

    System Information Page.......................................................................................................... 6-2

    6.6 GTN Setup Page ....................................................................................................................... 6-36.6.1 ARINC 429 Configuration Page .......................................................................................... 6-36.6.2 RS-232 Configuration Page ................................................................................................. 6-76.6.3 HSDB (Ethernet) Configuration Page .................................................................................. 6-96.6.4 Interfaced Equipment Page .................................................................................................. 6-96.6.5

    Main Indicator (Analog) Configuration Page .................................................................... 6-10

    6.6.6 Lighting Configuration Page .............................................................................................. 6-116.6.7 Audio Configuration Page .................................................................................................. 6-126.6.8 Traffic Configuration Page ................................................................................................. 6-136.6.9

    Main System Configuration Page ...................................................................................... 6-13

    6.6.10 COM Configuration Page (GTN 650 Only) ....................................................................... 6-146.6.11 VOR/LOC/GS Configuration Page (650 Only) ................................................................. 6-15

    6.7 GTN Options Page ................................................................................................................. 6-166.7.1 TAWS Configuration Page (For TAWS Units Only) ........................................................ 6-166.7.2 COM Transmit Power Configuration Page ........................................................................ 6-17

    6.8 GTN Diagnostics Page ........................................................................................................... 6-186.8.1 ARINC Inputs Page ............................................................................................................ 6-186.8.2 Serial Inputs Page ............................................................................................................... 6-186.8.3

    Discrete Pages .................................................................................................................... 6-18

    6.8.4 HSDB (Ethernet) Page ....................................................................................................... 6-186.8.5 Main Indicator (Analog) Diagnostics Page ........................................................................ 6-186.8.6

    Analog Inputs Page ............................................................................................................ 6-19

    6.8.7 Power Statistics Page ......................................................................................................... 6-196.8.8

    WAAS Diagnostics Page ................................................................................................... 6-19

    6.8.9 Temperatures Page ............................................................................................................. 6-196.8.10 Error Log Page ................................................................................................................... 6-196.8.11

    Main Data Inputs Page ....................................................................................................... 6-19

    6.8.12 VOR/ILS Indicator (Analog) Page ..................................................................................... 6-196.9 External Systems .................................................................................................................... 6-20

    6.9.1 GDL 69/69A Interface Check ............................................................................................ 6-206.9.2 StormscopePage .............................................................................................................. 6-216.9.3

    Traffic Test Page ................................................................................................................ 6-22

    6.9.4 GAD 42 Configuration ....................................................................................................... 6-22

    6.9.5

    Remote Transponder Configuration ................................................................................... 6-23

    6.10 Ground Checks (Configuration Mode) ................................................................................... 6-326.10.1 Main Indicator Check (Analog Only) ................................................................................ 6-326.10.2

    VOR/ILS Indicator (Analog) Diagnostics .......................................................................... 6-32

    6.10.3 Discrete Inputs Checkout ................................................................................................... 6-336.10.4 Discrete Outputs Checkout ................................................................................................. 6-336.10.5 HSDB Provisional Wiring Checkout ................................................................................. 6-336.10.6 Crossfill Check (If Dual GTNs Installed) .......................................................................... 6-346.10.7 TAWS Audio Check (For Units with TAWS Only) .......................................................... 6-34

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    6.10.8 GAD 42 Interface Check .................................................................................................... 6-356.10.9

    Lighting Bus Interface Check ............................................................................................ 6-35

    6.10.10 Altitude Encoder or Air Data Computer Check ................................................................. 6-366.10.11 AHRS/IRU Interface Check ............................................................................................... 6-36

    6.11 Ground Checks (Normal Mode) ............................................................................................. 6-376.11.1 Display of Self-Test Data ................................................................................................... 6-37

    6.11.2

    Signal Acquisition Check ................................................................................................... 6-38

    6.11.3

    VHF COM Interference Check .......................................................................................... 6-38

    6.11.4 VHF NAV Checkout (GTN 650 Only) .............................................................................. 6-406.11.5

    VHF COM Checkout (GTN 650 Only) .............................................................................. 6-40

    6.11.6 TAWS System Check (For Units with TAWS Only) ........................................................ 6-406.12 Interface Checkout .................................................................................................................. 6-41

    6.12.1 Honeywell (Bendix/King) EFS40/50 Interface Check ....................................................... 6-416.12.2 Sandel SN 3308 Interface Check ....................................................................................... 6-416.12.3 EHSI Deviation Scaling (If HSI/CDI Is Driven by the GTN Via Serial Data) .................. 6-446.12.4

    ARINC 429 Traffic System Interface Check ..................................................................... 6-45

    6.12.5 StormscopeInterface Check ............................................................................................. 6-456.12.6 GMX 200/MX20 Interface Check ...................................................................................... 6-456.12.7 GDL 69/69A Interface Check ............................................................................................ 6-456.12.8

    VOR RMI/OBI Interface Check (650 Only) ...................................................................... 6-46

    6.12.9 DME Interface Check (GTN 650 Only) ............................................................................. 6-466.12.10 Magnetic Compass Check .................................................................................................. 6-46

    6.13 Flight Checks .......................................................................................................................... 6-476.13.1 GPS Flight Check ............................................................................................................... 6-476.13.2 VHF COM Flight Check (GTN 650) ................................................................................. 6-476.13.3 VOR Flight Check (GTN 650) ........................................................................................... 6-476.13.4 ILS Flight Check (GTN 650) ............................................................................................. 6-486.13.5 Autopilot Flight Check ....................................................................................................... 6-486.13.6

    TAWS Audio Flight Check (TAWS-equipped units only) ................................................ 6-48

    6.14 Database Check ...................................................................................................................... 6-486.15 Data Card Replacement .......................................................................................................... 6-496.16

    Software Loading ................................................................................................................... 6-49

    6.16.1 Creating a GTN Software Loader Card .............................................................................. 6-496.16.2

    GTN Software Loading ...................................................................................................... 6-50

    6.17 Documentation Checks ........................................................................................................... 6-516.17.1 Airplane Flight Manual Supplement .................................................................................. 6-51

    7.

    PERIODIC MAINTENANCE ......................................................................................................... 7-1

    7.1 Equipment Calibration .............................................................................................................. 7-17.2 VOR Checks ............................................................................................................................. 7-17.3 Cleaning .................................................................................................................................... 7-17.4 Battery Replacement................................................................................................................. 7-1

    Appendix A

    ENVIRONMENTAL QUALIFICATION FORM.......................................................... A-1

    Appendix B GTN DATA FORMAT .................................................................................................. B-1

    B.1

    RS-232 Aviation Data Format ................................................................................................. B-1

    B.1.1 Electrical Interface ................................................................................................................... B-1B.1.2 General Output Format ............................................................................................................ B-1B.1.3

    Output Sentence Type 1 .......................................................................................................... B-1

    B.1.4 Output Sentence Type 2 .......................................................................................................... B-3B.2 GTN RS-232 FUEL/AIR DATA INPUT FORMAT .............................................................. B-5B.2.1 Electrical Interface ................................................................................................................... B-5B.2.2 Shadin Altitude Sentence......................................................................................................... B-5B.2.3 Icarus Altitude Sentence .......................................................................................................... B-5

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    B.2.4 Shadin Fuel Flow Sentence ..................................................................................................... B-6B.2.5

    ARNAV/EI Fuel Flow Sentence ............................................................................................. B-6

    B.2.6 Shadin Fuel/Air Data Computer Sentence ............................................................................... B-7Appendix C MECHANICAL DRAWINGS ....................................................................................... C-1

    C.1 Drawing List ............................................................................................................................ C-1Appendix D INTERCONNECT DIAGRAMS.................................................................................... D-1

    D.1

    Drawing List ............................................................................................................................ D-1

    LIST OF FIGURES

    Figure 3-1. GPS Antenna Installation Considerations .............................................................................. 3-8Figure 4-1. Coaxial Cable Installation ...................................................................................................... 4-6

    Figure 6-1. Configuration Mode Page ...................................................................................................... 6-2Figure 6-2. System Information Page ........................................................................................................ 6-2Figure 6-3. GTN Setup Page ..................................................................................................................... 6-3Figure 6-4. ARINC 429 Configuration Page ............................................................................................ 6-3Figure 6-5. RS-232 Configuration Page ................................................................................................... 6-7Figure 6-6. HSDB Port Utilization Page ................................................................................................... 6-9

    Figure 6-7. Interfaced Equipment Page .................................................................................................... 6-9Figure 6-8. Main Indicator (Analog) Configuration Page ...................................................................... 6-10Figure 6-9. Lighting Configuration Page ................................................................................................ 6-11Figure 6-10. Photocell Configuration Page ............................................................................................. 6-11

    Figure 6-11. Lighting Bus Configuration Page ....................................................................................... 6-12Figure 6-12. Audio Configuration Page .................................................................................................. 6-12Figure 6-13. Select Test Sound Page ...................................................................................................... 6-12Figure 6-14. Traffic Configuration Page ................................................................................................. 6-13Figure 6-15. Main System Configuration Page ...................................................................................... 6-13Figure 6-16. Measurement of GPS Antenna Vertical Offset .................................................................. 6-14Figure 6-17. COM Configuration Page ................................................................................................... 6-14Figure 6-18. VOR/LOC/GS Configuration Page .................................................................................... 6-15Figure 6-19. GTN Options Page ............................................................................................................. 6-16

    Figure 6-20. TAWS Configuration Page ................................................................................................ 6-16Figure 6-21. Configure TAWS Audio Page ............................................................................................ 6-17Figure 6-22. COM Transmit Power Configuration Page ........................................................................ 6-17

    Figure 6-23. GTN Diagnostics Page ....................................................................................................... 6-18Figure 6-24. External Systems Page ....................................................................................................... 6-20

    Figure 6-25. GDL 69/69A Configuration Page ...................................................................................... 6-20Figure 6-26. Stormscope Page ................................................................................................................ 6-21Figure 6-27. Stormscope Configuration Page ......................................................................................... 6-21

    Figure 6-28. Stormscope Test Page ........................................................................................................ 6-21Figure 6-29. Stormscope Test Menu Page .............................................................................................. 6-21Figure 6-30. Traffic Test Page ................................................................................................................ 6-22Figure 6-31. GAD 42 Configuration Page .............................................................................................. 6-22Figure 6-32. XPDR Configuration Page ................................................................................................. 6-23

    Figure 6-33. XPDR Input/Outputs Page ................................................................................................. 6-23

    Figure 6-34. Remote XPDR Configuration Page .................................................................................... 6-28

    Figure 6-35. Microsoft Windows Calculator .......................................................................................... 6-30Figure 6-36. XPDR Audio Configuration Page ...................................................................................... 6-31Figure 6-37. Main Indicator (Analog) Diagnostics Page ........................................................................ 6-32

    Figure 6-38. VOR/ILS Indicator (Analog) Diagnostics Page .................................................................. 6-32Figure 6-41. HSDB Port Status Page ...................................................................................................... 6-33Figure 6-39. Discrete Inputs Page ........................................................................................................... 6-33Figure 6-40. Discrete Outputs Page ........................................................................................................ 6-33Figure 6-42. Audio Configuration Page .................................................................................................. 6-34

    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    Figure 6-43. GAD 42 Configuration Page .............................................................................................. 6-35Figure 6-44. Lighting Configuration Page .............................................................................................. 6-35

    Figure 6-45. Main Data Inputs Page ....................................................................................................... 6-36Figure 6-46. Updates Page ...................................................................................................................... 6-50Figure C-1. GTN 625/635/650 CG and Mounting Rack Dimensions ..................................................... C-3Figure C-3. GTN 625/635/650 Recommended Panel Cutout Dimensions .............................................. C-5

    Figure C-4. GTN 625/635/650 Mounting Rack and Tab Alignment Detail ............................................ C-6

    Figure C-5. GTN 6XX Connector Layout DetailRear View ............................................................... C-7

    Figure D-1. GTN System Interface Diagram ........................................................................................... D-3

    Figure D-2. GTN 650 Typical Installation ............................................................................................... D-4Figure D-3. GTN 625 Typical Installation ............................................................................................... D-6Figure D-4. GTN 6XX Power Lighting Configuration Interconnect ....................................................... D-8Figure D-5. GTN 6XXAntenna Interconnect....................................................................................... D-9Figure D-6. GTN 6XXMain Indicator Interconnect .......................................................................... D-12Figure D-7. GTN 6XX - Autopilot Interconnect ................................................................................... D-13

    Figure D-8. GTN 6XX - Traffic Interconnect ........................................................................................ D-14Figure D-9. GTN 6XXTransponder Interconnect .............................................................................. D-15Figure D-10. Dual GTN to Single GDU Interconnect ........................................................................... D-19Figure D-11. GTN 6XX - ARINC 429 EFIS Interconnect .................................................................... D-20

    Figure D-12. GTN - GDL 69/69A Interconnect .................................................................................... D-22Figure D-13. Audio Panel Interconnect ................................................................................................. D-23Figure D-14. GTN 6XX - Air Data/IRU/AHRS RS-232 Interconnect .................................................. D-25Figure D-15. GTN 6XX - Air Data/IRU/AHRS ARINC 429 Interconnect ........................................... D-27Figure D-16. GTN 6XX - GAD 42 Interconnect ................................................................................... D-28Figure D-17. VOR/ILS Indicator Interconnect ...................................................................................... D-29Figure D-18. GTN - RMI OBI Interconnect .......................................................................................... D-30Figure D-19. GTN 6XXWX-500 Interconnect .................................................................................. D-31Figure D-20. GTN 650 - DME Interconnect .......................................................................................... D-32

    Figure D-21. GTN 650Remote DME Interconnect............................................................................ D-33Figure D-22. Parallel 2 of 5 DME Tuning ............................................................................................. D-34Figure D-23. Parallel Slip Code DME Tuning Interconnect .................................................................. D-35

    Figure D-24. Reserved ........................................................................................................................... D-36Figure D-25. GPS Annunciator Interconnect ......................................................................................... D-37

    Figure D-26. NAV Source Select Annunciator Interconnect ................................................................. D-38Figure D-27. TAWS Interconnect .......................................................................................................... D-39Figure D-28. Switches Interconnect ....................................................................................................... D-40

    LIST OF TABLES

    Table 1-1. GTN Units ............................................................................................................................... 1-1Table 1-2. GTN Current Specifications .................................................................................................... 1-6Table 1-3. Approved GPS/SBAS Antennas .............................................................................................. 1-7

    Table 1-4. TSO Authorization .................................................................................................................. 1-9

    Table 1-5. Non-TSO Functions ............................................................................................................... 1-10

    Table 1-6. System Functions ................................................................................................................... 1-11Table 4-1. Catalog Part Numbers .............................................................................................................. 4-1Table 4-2. Standard Kit Accessories ......................................................................................................... 4-1

    Table 4-3. Replacement Fan Parts ............................................................................................................ 4-1Table 4-4. Recommended Crimp Tools (or Equivalent) ........................................................................... 4-5Table 4-5. Socket Contact Part Numbers .................................................................................................. 4-7Table B-1. Type 1 Output Sentence Format ............................................................................................ B-2Table B-2. Type 2 Output Sentence Format ............................................................................................ B-4

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    GTN 625/635/650 HARDWARE MOD LEVEL HISTORY

    The following table identifies hardware modification (Mod) Levels for the GTN 625, GTN 635, andGTN 650. Mod Levels are listed with the associated service bulletin number, service bulletin date, andthe purpose of the modification. The table is current at the time of publication of this manual (see date onfront cover) and is subject to change without notice. Authorized Garmin Sales and Service Centers areencouraged to access the most up-to-date bulletin and advisory information on the Garmin Dealer

    Resource web site at www.garmin.com using their Garmin-provided user name and password.

    Mod LevelService Bulletin

    NumberService Bulletin

    DatePurpose of Modification

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    1. GENERAL DESCRIPTION

    1.1 Introduction

    This manual is applicable for units with main software version 2.00 or later. This manual describes thephysical, mechanical, and electrical characteristics, as well as instructions and other conditions andlimitations for installation and approval of the GTN units. Refer to Section2,Limitations, for additional

    information and other considerations.NOTE

    Except where specifically noted, references made to GTN will equally apply to theGTN 625, GTN 635, and GTN 650. All screen shots used in this document are current atthe time of publication. Screen shots are intended to provide visual reference only. Allinformation depicted in screen shots, including software file names, versions, and partnumbers, is subject to change and may not be up to date.

    Table 1-1. GTN Units

    Model Part Number Color

    GTN 625 010-00811-00 BLACKGTN 635 010-00812-00 BLACK

    GTN 650010-00813-00 BLACK

    010-00889-00 GRAY

    1.2 Equipment Description

    The GTN 625 is a GPS/SBAS unit and may be approved for IFR en route, terminal, non-precision, andprecision approach operations. The GTN 625 meets the requirements of the TSO specified inTable 1-4.

    The GTN 635 includes all of the features of the GTN 625 in addition to an airborne VHF communicationstransceiver. The GTN 635 meets the requirements of the TSO specified inTable 1-4.

    The GTN 650 includes all of the features of the GTN 625 in addition to an airborne VHF communications

    transceiver and airborne VOR/localizer (LOC) and glideslope (G/S) receivers. The GTN 650 meets therequirements of the TSO specified inTable 1-4.

    CAUTION

    The GTN has a display that is coated with a special anti-reflective coating that is verysensitive to waxes and abrasive cleaners. CLEANERS CONTAINING AMMONIAWILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean thedisplay using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safefor anti-reflective coatings.

    CAUTION

    The use of ground-based cellular telephones while aircraft are airborne is prohibited by

    FCC rules. Due to potential interference with onboard systems, the use of ground-basedcell phones while the aircraft is on the ground is subject to FAA regulation 14CFR 91.21. FCC regulation 47 CFR 22.925 prohibits airborne operation of ground-based cellular telephones installed in or carried aboard aircraft. Ground-based cellulartelephones must not be operated while aircraft are off the ground. When any aircraftleaves the ground, all ground-based cellular telephones on board that aircraft must beturned off. Ground-based cell phones that are on, even in a monitoring state, can disruptGPS/SBAS performance.

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    1.3 Technical Specifications

    1.3.1 Physical Characteristics

    Characteristics Specifications

    Bezel Height 2.65 in. (67 mm)

    Bezel Width 6.25 in. (159 mm)

    Rack Height (Dimple-to-Dimple) 2.665 in. (68 mm)

    Rack Width 6.300 in (160 mm)

    Depth Behind Panel with Connectors (Measured fromface of aircraft panel to rear of connector backshells)

    11.25 in. (286 mm)

    GTN 625 Weight (Unit only) 4.2 lb (1.90 kg)

    GTN 625 Weight (Installed with rack and connectors) 5.4 lb (2.48 kg)

    GTN 635 Weight (Unit only) 4.8 lb (2.18 kg)

    GTN 635 Weight (Installed with rack and connectors) 6.2 lb (2.82 kg)

    GTN 650 Weight (Unit only) 5.5 lb (2.48 kg)

    GTN 650 Weight (Installed with rack and connectors) 7.0 lb (3.20 kg)

    1.3.2 General Specifications

    Characteristics Specifications

    Operating Temperature Range

    -20 C to +55 C. For more details seeEnvironmental Qualification Form on theDealers Only page on www.garmin.com. See

    Appendix A for part numbers.

    Humidity 95% non-condensing

    Altitude Range -1,500 ft to 50,000 ft

    Input Voltage Range - All Units (Main Connector) 11 to 33 VDC

    Input Voltage Range (COM Connector on GTN 650) 11 to 33 VDC

    GTN Current Draw Refer toTable 1-2

    Superflag Power Requirements 320 mA maximum per superflag output

    Environmental TestingSee Environmental Qualification Form on theDealers Only page on www.garmin.com. See

    Appendix A for part numbers.

    The display on the GTN is a sunlight readable LCD display.

    Characteristics Specifications

    Display Size 4.9 inch diagonal

    Active Area 4.46 inches (W) x 1.98 inches (H)

    Resolution 600 x 708 pixels

    Viewing Angle

    Left: 45Right: 35

    Up: 10

    Down: 30

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    1.3.3 GTN GPS/SBAS Specifications

    Characteristics Specifications

    Number Of Channels 15 (12 GPS and 3 GPS/WAAS/SBAS)

    Frequency 1575.42 MHz L1, C/A code

    Sensitivity (Acquisition, No Interference)-134.5 dBm GPS

    -135.5 dBm WAAS

    Sensitivity (Drop Lock) -144 dBmDynamic Range > 20 dB

    Lat/Lon Position Accuracy

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    1.3.4 COM Specifications (GTN 635/650 Only)

    1.3.4.1 COM Transmitter Specifications

    Characteristics Specifications

    Classes 3, 4, 5, 6

    Microphone InputTwo inputs, standard carbon or dynamic mic with integrated

    preamp providing minimum 70 mVRMS into 1000 loadModulation Capability 85% with 100 to 1000 mVRMS microphone input at 1000 Hz

    Modulation

    AM double-sided

    Emission Designator: 6K00A3E (118136.975 MHz)

    5K60A3E (118136.992 MHz)

    Frequency Range118.000 to 136.975 MHz, 25 kHz channel spacing

    118.000 to 136.992 MHz, 8.33 kHz channel spacing

    Frequency Tolerance +/-2ppm from -40C to +70C

    Output Power10 Watt Mode: 10 watts minimum16 Watt Mode: 16 watts minimum

    Duty Cycle 100%

    16W: Recommended 25% (5 seconds on/15 seconds off,15 seconds on/45 seconds off, etc.)

    Carrier Noise Level At least 35 dB (SNR).

    Stuck Mic Time-Out 30 seconds time-out, reverts to receive

    Demodulated Audio DistortionLess than 5% distortion when the transmitter is at 85%modulation at 350 to 2500 Hz

    Sidetone 1.4 Vrms into a 500 load

    1.3.4.2 COM Receiver Specifications

    Characteristics Specifications

    Classes C and E

    Frequency Range118.000 to 136.975 MHz, 25 kHz channel spacing118.000 to 136.992 MHz, 8.33 kHz channel spacing

    Headset Audio Output 100 mW minimum into a 500 load

    Audio Response Less than 6 dB of variation between 350 and 2500 Hz.

    Audio Distortion Less than 5% at rated output power

    AGC CharacteristicsLess than 3 dB of variation in the audio output from -93 to -13

    dBm (power absorbed by a 50 load)

    Sensitivity

    SINAD on all channels is greater than 6 dB when the RF level is

    2 uV (hard) or -107 dBm (power absorbed by a 50 load)modulated 30% at 1000 Hz at rated audio output power

    Squelch Automatic squelch with manual override

    Selectivity

    6 dB BW is greater than +7 kHz for 25 kHz channeling.

    60 dB BW is less than 22 kHz for 25 kHz channeling.6 dB BW is greater than 3.5 kHz for 8.33 kHz channeling.

    60 dB BW is less than 7.37 kHz for 8.33 kHz channeling.

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    1.3.5 VOR Specifications (GTN 650 Only)

    Characteristics Specifications

    Receiver Audio Sensitivity At -103.5 dBm (S+N)/N is not less than 6 dB.

    Course Deviation Sensitivity -103.5 dBm or less for 60% of standard deflection.

    Flag

    The VOR Course Deviation Flag must be flagged when:

    RF signals are absent.

    9960 Hz modulation is absent.either one of the two 30 Hz modulations are absent.

    the level of a standard VOR deviation test signal producesless than a 50% of standard deflection.

    AGC CharacteristicsFrom -99 dBm to -13 dBm input of a Standard VOR Audio TestSignal, audio output level does not vary more than 3 dB.

    Spurious Response Greater than 60 dB.

    VOR OBS Bearing AccuracyThe bearing information as presented to the pilot does not have anerror in excess of 2.7 as specified by RTCA DO-196 and EuroCAEED-22B.

    Audio Output A minimum 100 mW into a 500 load.

    Audio ResponseLess than 6 dB of variation between 350 and 2500 Hz. In voicemode, an IDENT tone of 1020 Hz Ident Tone is attenuated at least20 dB down.

    Audio DistortionThe distortion in the receiver audio output does not exceed 10% atall levels up to 100 mW.

    Selectivity 6 dB BW is greater than 16.5 kHz. 69 dB BW is less than 36 kHz.

    1.3.6 LOC Specifications (GTN 650 Only)

    Characteristics Specifications

    Receiver Audio Sensitivity At -103.5 dBm (S+N)/N is not less than 6 dB.

    Course Deviation SensitivityAt -103.5 dBm, deviation output is not to be less than 60% ofstandard deflection when a LOC deviation test signal is applied.

    Flag

    The VOR/LOC Course Deviation Flag is flagged when:

    RF signals are absent.

    9960 Hz modulation is absent.one of the two 30 Hz modulations is absent.

    the level of a standard VOR deviation test signal producesless than a 50% of standard deflection.

    AGC CharacteristicsFrom -99 dBm to -13 dBm input of a Standard VOR Audio TestSignal, audio output level does not vary more than 3 dB.

    Selectivity6 dB BW is greater than 9 kHz

    69 dB BW is less than 36 kHz

    Standard Deflection

    With a standard deflection FLY LEFT condition (90 Hz dominant),the output is +90 mV 9 mV.

    With a standard deflection FLY RIGHT condition (150 Hzdominant), the output is -90 mV 9 mV.

    Spurious Response Greater than 60 dB.

    VOR OBS Bearing AccuracyThe bearing information as presented to the pilot does not have anerror in excess of 2.7 as specified by RTCA DO-196 and EuroCAEED-22B.

    Audio Output A minimum 100 mW into a 500 load.

    Audio ResponseLess than 6 dB of variation between 350 and 2500 Hz. In voicemode, an IDENT tone of 1020 Hz Ident Tone is attenuated at least20 dB down.

    Audio DistortionThe distortion in the receiver audio output does not exceed 10% atall levels up to 100 mW.

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    1.3.7 Glideslope Specifications (GTN 650 Only)

    Characteristics Specifications

    Sensitivity -87 dBm or less for 60% of standard deflection.

    Centering Accuracy 0 0.01183 ddm or 0 10.14 mV

    Selectivity

    The course deviation is 0 ddm .0091 ddm when using the Glideslope

    Centering Test Signal as the RF frequency is varied 17 kHz from theassigned channel.

    At frequencies displaced by 132 kHz or greater, the input signal is atleast 60 dB down.

    Standard Deflection

    With a standard deflection FLY DOWN condition (90 Hz dominant),the output is -78 mV 7.8 mV.

    With a standard deflection FLY UP condition (150 Hz dominant), theoutput is +78 mV 7.8 mV.

    Flag

    The unit flags when:

    the level of a standard VOR deviation test signal produces50% or less of standard deflection of the deviation indicator.

    150 Hz modulation is absent.

    90 Hz modulation is absent.90 Hz and 150 Hz modulations are both absent.

    RF signals are absent.

    Table 1-2. GTN Current Specifications

    LRU14 Volt Current Draw 28 Volt Current Draw

    Typical Maximum Typical Maximum

    GTN 625

    Main Connector 1.6 A [1] 2.8 A [2] 0.8 A [1] 1.5 A [2]

    GTN 635

    Main Connector 1.6 A [1] 2.8 A [2] 0.8 A [1] 1.5 A [2]

    COM Connector 0.45 A5.66 A (16W COM)4.02 A (10W COM)

    0.21 A2.33 A (16W COM)

    1.76 A (10W COM)

    GTN 650

    Main Connector 1.6 A [1] 2.8 A [2] 0.8 A [1] 1.5 A [2]

    COM Connector 0.45 A5.66 A (16W COM)4.02 A (10W COM)

    0.21 A2.33 A (16W COM)

    1.76 A (10W COM)

    NAV Connector 0.60 A 1.16A [2] 0.30 A 0.58 A [2]

    [1] The specified current draw is with the display backlight set to 100% and the fan operatingat low speed. If the superflags are connected, their current draw must be added inaddition to the specified current.

    [2] The specified current draw does not include the superflags. If connected, their currentdraw must be added to the specified current. The superflags will supply up to 320 maeach regardless of the input voltage.

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    1.3.8 GPS/WAAS Antenna Requirements

    Antenna performance is critical to the GPS/SBAS operation. The antennas listed inTable 1-3provideacceptable performance with the GTNs.

    Table 1-3. Approved GPS Antennas

    Model/Description Conn Type Mfr Part Number

    Garmin

    OrderNumber

    GA 35, GPS/WAAS[1]

    TNCGarmin 013-00235-( )

    013-00235-( )Aero Antenna AT575-93G( )-TNCF-000-RG-27-NM

    GA 36, GPS/WAAS TNCGarmin 013-00244-( )

    013-00244-( )Aero Antenna AT575-126G( )-TNCF-000-RG-27-NM

    GA 37, GPS/WAAS/XM TNCGarmin 013-00245-( )

    013-00245-( )Aero Antenna AT2300-126G( )-TNCF-000-RG-27-NM

    A33W, WAAS Antenna TNCGarmin 013-00261-( )

    013-00261-( )Aero Antenna AT575-332G( )- TNCF-000-RG-27-NM

    GPS/VHF AntennaTNC/BNC

    [2]Comant CI-2580-200 N/A

    GPS/VHF AntennaTNC/BNC

    [2]Comant CI-2728-200 N/A

    GPS/XM/VHF AntennaTNC/TNC/BNC

    [3]Comant CI-2580-410 N/A

    GPS/XM/VHF AntennaTNC/TNC/BNC

    [3]Comant CI-2728-410 N/A

    GPS/WAAS Antenna TNC Comant CI-428-200 N/A

    GPS/XM Antenna TNC/TNC Comant CI-428-410 N/A

    [1] Same mounting hole pattern as GA 56, but GA 35 antenna has a physically larger footprint.

    [2] The antenna connector is a TNC type. The VHF connector is a BNC type.

    [3] The antenna connector is a TNC type. The XM connector is a TNC type. The VHF connector is aBNC type.

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    1.4 License Requirements

    The Telecommunications Act of 1996, effective February 8, 1996, provides the FCC discretion toeliminate radio station license requirements for aircraft and ships. The GTN 6XX installations mustcomply with current transmitter licensing requirements. In the US, to find out the specific details onwhether a particular installation is exempt from licensing, please visit the FCC web sitehttp://wireless.fcc.gov/aviation. If an aircraft license is required, make application for a license on FCCform 404, Application for Aircraft Radio Station License. The FCC also has a fax-on-demand service toprovide forms by fax. Outside the US, contact the responsible telecommunication authority. TheGTN 625, 635, and 650 owner accepts all responsibility for obtaining the proper licensing before usingthe transceiver. The maximum transmitting power, modulation identification, and frequency bandinformation may be required for licensing and are detailed in Section 1.4.4.

    CAUTION

    The VHF transmitter in this equipment is guaranteed to meet Federal CommunicationsCommission acceptance over the operating temperature range. Modifications notexpressly approved by Garmin could invalidate the license and make it unlawful tooperate the equipment.

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    1.5 Regulatory Compliance

    1.5.1 TSO Authorization and Advisory Circular References

    The conditions and tests required for TSO approval of this article are minimum performance standards. Itis the responsibility of those installing this article either on or within a specific type or class of aircraft todetermine that the aircraft installation conditions are within the TSO standards. TSO articles must have

    separate approval for installation in an aircraft. The article may be installed only in compliance with 14CFR part 43 or the applicable airworthiness requirements.

    All GTN unit functions are design approved under the TSO. Unauthorized changes or modifications toany GTN unit product may void the compliance to required regulations and authorization for continuedequipment usage.

    Table 1-4. TSO Authorization

    [1] [2]

    FunctionTSO/ETSO/SAE/RTCA/EUROCAE

    Class/Type

    Applicable SW P/NsApplicable CLD

    P/Ns

    GTN6

    25

    GTN6

    35

    GTN6

    50

    C ILS Glideslope ReceivingEquipment

    TSO-C34e

    DO-192ETSO-2C34f

    ED-47B

    006-B0082-11 through -1( )006-B1026-01 through -0( )

    006-C0124-00through

    006-C0124-0( )

    006-C0134-22through

    006-C0134-2( )

    006-C0135-22through

    006-C0135-2( )

    CILS Localizer ReceivingEquipment

    TSO-C36eDO-195

    ETSO-2C36fED-46B

    A006-B0082-11 through -1( )006-B1026-01 through -0( )

    C C

    VHF Radio CommunicationTransmitting Equipment Operatingwith the Radio Frequency Range117.975-137 MHz

    ETSO-2C37eED-23B

    3456

    006-B1061-02 through -0( )006-B1026-01 through -0( )

    C C

    VHF Radio CommunicationReceiving Equipment Operatingwithin the Radio Frequency

    Range 117.975137 MHz

    ETSO-2C38eED-23B

    DE

    006-B1061-02 through -0( )006-B1026-01 through -0( )

    C VOR Receiving Equipment

    TSO-C40cDO-196

    ETSO-2C40cED-22B

    006-B0082-11 through -1( )006-B1026-01 through -0( )

    I I IAirborne ATC TransponderEquipment

    TSO-C74dDO-144A

    ETSO-C74dDO-144

    A 006-B1026-01 through -0( )

    I I IAirborne Passive ThunderstormDetection Equipment

    TSO-C110aETSO-C110a

    DO-191006-B1026-01 through -0( )

    I I IAir Traffic Control Radar BeaconSystem/Mode Select

    ATCRABS/Mode S

    TSO-C112cDO-181D

    ETSO-2C112bED-73B

    006-B1026-01 through -0( )

    C C C Multipurpose Electronic DisplaysTSO-C113

    ETSO-C113AS 8034

    IIIIII

    006-B1026-01 through -0( )

    I I ITraffic Collision AvoidanceSystem (TCAS) AirborneEquipment

    TSO-C118ETSO-C118

    DO-197006-B1026-01 through -0( )

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    [1] [2]

    FunctionTSO/ETSO/SAE/RTCA/EUROCAE

    Class/Type

    Applicable SW P/Ns Applicable CLD P/Ns

    GTN6

    25

    GTN6

    35

    GTN6

    50

    C C

    Equipment that PreventsBlocked Channels in 2-wayRadio Communications due toUnintentional Transmissions

    TSO-C128aDO-207

    ETSO-2C128ED-67

    006-B1061-02 through -0( )006-B1026-01 through -0( )

    006-C0124-00through

    006-C0124-0( )

    006-C0134-22through

    006-C0134-2( )

    006-C0135-22

    through006-C0135-2( )

    C C C

    Stand-Alone AirborneNavigation Equipment using theGPS Augmented by theSatellite Based AugmentationSystem

    TSO-C146cDO-229D

    ETSO-C146DO-229B

    3006-B0339-10 through -1( )006-B1026-01 through -0( )

    I I ITraffic Advisory System (TAS)

    Airborne Equipment

    TSO-C147ETSO-C147

    DO-197AA 006-B1026-01 through -0( )

    C C CTerrain Awareness WarningSystems (TAWS)

    TSO-C151bETSO-C151b

    B 006-B1026-01 through -0( )

    C C C Electronic Map DisplayEquipment for GraphicalDepiction of Aircraft Position

    TSO-C165DO-257AETSO-C165

    006-B1026-01 through -0( )

    C C

    VHF Radio CommunicationsTransceiver EquipmentOperating with RadioFrequency Range 117.975 to137.000 MHz

    TSO-C169aDO-186B

    006-B1061-02 through -0( )006-B1026-01 through -0( )

    [1] CComplete TSO

    [2] IIncomplete TSO - The incomplete TSOs/ETSOs are for an incomplete system. The GTN must beinterfaced to units with applicable TSO/ETSO authorizations to be a complete TSO/ETSO system.The installer should verify that non-Garmin interfaced devices listed in this manual have been

    authorized under appropriate TSO/ETSO to assure the installed system will comply with theTSO/ETSO requirements.

    1.5.2 Non-TSO Functions

    Table 1-5. Non-TSO Functions

    Function Applicable SW P/N Applicable CLD P/Ns

    XM Satellite Radio Weather DisplayThe GTN 625/635/650 displays weather products whenconnected to Garmin GDL 69 Series XM Radio Receiver.

    006-B1026-01 through -0( ) 006-C0134-22 through -2( )

    XM Satellite Radio Audio EntertainmentThe GTN 625/635/650 displays channel information andcontrol audio output from Garmin GDL 69 Series.

    006-B1026-01 through -0( ) 006-C0134-22 through -2( )

    Traffic Display/Control (TIS)

    The GTN 625/635/650 requests and displays traffic data fromGTX Mode S Transponder. 006-B1026-01 through -0( ) 006-C0134-22 through -2( )

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    Table 1-6. System Functions

    System FunctionDO-178B

    Level

    Operating System B

    Touchscreen Display and Control B

    GPS/SBAS Navigation Information and CDI/VDI Output B

    VHF DME Navigation Information and VHF CDI/VDI Output B

    VHF Communication B

    Display of VOR/LOC/Glideslope information B

    Roll Steering Command Output C

    TAWS (Class B) Functionality C

    Display of terrain and moving map B

    Display of flight plan information B

    Display of traffic (TIS/TAS/TCAS I) data D

    Display of marker beacon, data from passive lightning detection equipment, XM weather and audioentertainment data.

    C

    Processing of passive lightning detection, TIS, marker beacon, and XM weather and audio data D

    Remote Transponder Communication C

    HSDB Data Forwarding B

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    1.5.3 TSO/ETSO Deviations

    TSO/ETSO Deviation

    TSO-C34e

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    TSO-C36e

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from TSO to use RTCA/DO-178B instead of earlier versions of RTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    TSO-C40c

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label,TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    ETSO-2C40c 1. Garmin was granted a deviation from the ETSO to have a deflection response of 0.5 to 2.7 seconds.

    TSO-C74d

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    TSO-C110a

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    4. Garmin was granted a deviation from the TSO not to mark the computer software level(s) on the unit.

    TSO-C112c

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    TSO-C113

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    4. Garmin was granted a deviation from the TSO not to mark the computer software level(s) on the unit.

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    TSO/ETSO Deviation

    TSO-C118

    1. Garmin was granted a deviation from the TSO not to mark the computer software level(s) on the unit.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-197A instead of RTCA/DO-197 as theMinimum Operational Performance Standards.

    3. Garmin was granted a deviation from the TSO to mark product name, part number, serial number and astatement on the units nameplate label TSO-C146c Class 3, See IM for Addl Appliance Approvals , instead o

    Product Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, weight and Software Part Number.

    4. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    5. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    ETSO-C1181. Garmin was granted a deviation from the ETSO to use RTCA-DO-197A instead of RTCA/DO-197 as theMinimum Operational Performance Standards.

    TSO-C128a

    1. Garmin was granted a deviation from the TSO to mark product name, part number, serial number andstatement on the units nameplate label, TSO-C146c Class 3, See IM for Addl Appliance Approvals, instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, Weight and Software Part Number.

    2. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    3. Garmin was granted a deviation from the TSO to use RTCA/DO-178B instead of earlier versions ofRTCA/DO-178 to demonstrate compliance for the verification and validation of the computer software.

    TSO-C146c

    1. Garmin was granted a deviation from RTCA/DO-229D to use a 10 degree vertical viewing angle below thelower display edge.

    2. Garmin was granted a deviation from RTCA/DO-229D to use GPS antennas that meet Garmin minimumperformance specifications.

    3. Garmin was granted a deviation from the TSO to mark product name, part number, serial number and astatement on the units nameplate label TSO-C146c Class 3, See IM for Addl Appliance Approvals , instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, weight and Software Part Number.

    4. Garmin was granted a deviation from the TSO to use RTCA/DO-160F instead of earlier versions of RTCA/DO160 as the standard for Environmental Conditions and Test Procedures of Airborne Equipment.

    ETSO-C146

    1. Garmin was granted a deviation from the ETSO to use RTCA/DO-229D instead of RTCA/DO-229B as theMinimum Operational Performance Standards.

    2. Garmin was granted a deviation from RTCA/DO-229D to use a 10 degree vertical viewing angle below thelower display edge.

    TSO-C147

    1. Garmin was granted a deviation from the TSO not to furnish each person receiving a unit copies of the data inparagraphs 3(a)(10) through (12) of the TSO.

    2. Garmin was granted a deviation from the TSO not to display a visual Traffic annunciation for the duration ofthe traffic alert.

    3. Garmin was granted a deviation from the TSO to mark product name, part number, serial number and astatement on the units nameplate label TSO-C146c Class 3, See IM for Addl Appliance Approvals , instead oProduct Type, TSO Numbers, Equipment Class, Dev (deviation), Environmental Categories, Date ofManufacture, weight and Software Part Number.

    4. Garmin was granted a