Garmin G600 Maintenance Manual
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Garmin G600 Maintenance Manual

Txi part 23 aml stc
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Download this manual See also: Reference Manual, Instruction Manual
G500/G600 TXi Part 23 AML STC
Maintenance Manual
Contains Instructions for Continued Airworthiness
for STC SA02571SE
Aircraft make, model, registration number, and serial
number along with the applicable STC configuration
information must be completed in Appendix A and
saved with aircraft permanent records.
190-01717-B1
November 2017
Revision 1

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  • Page 1 G500/G600 TXi Part 23 AML STC Maintenance Manual Contains Instructions for Continued Airworthiness for STC SA02571SE Aircraft make, model, registration number, and serial number along with the applicable STC configuration information must be completed in Appendix A and saved with aircraft permanent records.
  • Page 2 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 and to print one copy of this manual or of any revision...
  • Page 3 The AES file encryption software is provided “as is” with no explicit or implied warranties in respect of its properties, including, but not limited to, correctness and/or fitness for purpose. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page ii...
  • Page 4 End User (“Licensee”, “you” or “your”), on the one hand, and Garmin and its licensors and affiliated companies of Garmin and its licensors, on the other hand. The Licensed Software is licensed, not sold, to you.
  • Page 5 Term. The term of this Agreement shall commence on the Effective Date, and shall continue in perpetuity thereafter, unless terminated earlier as provided in this Section 4. b. Termination by Garmin. Garmin may immediately terminate this Agreement upon written notice to Licensee if Licensee commits a material breach of this Agreement or breaches a material term of this Agreement.
  • Page 6 No Devices or Services. Licensee acknowledges and agrees that nothing in this Agreement shall be construed as requiring Garmin to: (a) provide or supply the Devices or any other devices or hardware to Licensee; (b) grant any licenses to any software other than the Licensed Software;...
  • Page 7 Garmin concerning the Licensed Software or Documentation or Gamin's products, services, technology, techniques, processes or materials (“Feedback”). Garmin may in connection with any of its products or services freely use, copy, disclose, license, distribute and otherwise exploit such Feedback in any manner without any obligation, payment, royalty or restriction whether based on intellectual property rights or otherwise.
  • Page 8 Entire Agreement. This Agreement shall constitute the entire agreement between Garmin and you with respect to the subject matter hereof and will supersede all prior negotiations, agreements and understandings of Garmin and you of any nature, whether oral or written, with respect to such subject matter.
  • Page 9 THE DISPLAY WITH A CLEAN, LINT-FREE CLOTH AND A CLEANER THAT IS SAFE FOR ANTI-REFLECTIVE COATINGS. CAUTION Do not store any G500/G600TXi component in or near water. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page viii...

  • Page 10: Table Of Contents

    5.14 Uploading Software........................5-41 5.15 System Checks..........................5-41 APPENDIX A INSTALLATION SPECIFIC INFORMATION.......... A-1 General Information ........................A-1 LRU Information ..........................A-2 Equipment Location ........................A-3 Wire Routing - Single Engine ......................A-4 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page ix...
  • Page 11 Saved Configuration File......................A-6 Print Configuration Log........................A-6 GDU 1060 EIS Gauge Layout Template..................A-7 GDU 700P EIS Gauge Layout Template ..................A-8 A.10 GDU 700L EIS Gauge Layout Template ..................A-9 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page x...
  • Page 12 Figure 4-22 External LRU Service Message Troubleshooting .............4-31 Figure 4-23 GAD Fault Message Troubleshooting ................4-32 Figure 4-24 GAD Fault Message Troubleshooting Continued .............4-33 Figure 4-25 EIS Gauge Troubleshooting ....................4-34 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page xi...
  • Page 13 Figure 5-24 Airspeed Configuration Type ....................5-43 Figure A-1 GDU 1060 EIS Gauge Template ..................A-7 Figure A-2 GDU 700P EIS Gauge Layout Template................A-8 Figure A-3 GDU 700L EIS Gauge Layout Template ................A-9 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page xii...
  • Page 14 Advanced Airframe Specific Configuration Data – Arc Ranges........5-46 Table 5-5 Advanced Airframe Specific Configuration Data – Markings ..........5-48 Table 5-6 Air Data Test Points......................5-50 Table 5-7 Altitude Hold Check Log....................5-52 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page xiii...

  • Page 15: Introduction

    Acronyms ...........................1-3 1.1 Purpose This document is designed for use by the installing agency of the Garmin G500/G600 TXi PFD/MFD/EIS System as a Maintenance Manual and ICA in response to FAR Part 23.1529, and Part 23 Appendix G. This ICA includes information required by the operator to adequately maintain the Garmin G500/G600 TXi system installed under AML STC.

  • Page 16: Publications

    In addition to this manual, the following documents are recommended for performing maintenance on the G500/G600 TXi system. It is the responsibility of the owner/operator to ensure the latest applicable versions of these documents are used during operation, servicing, or maintenance of the G500/G600 TXi system.
  • Page 17 WAAS: Wide Area Augmentation System GSR: Garmin Services WXR: Weather Radar Garmin Reference System GTP: Garmin Temperature Probe GWX: Garmin Weather Radar HSI: Horizontal Situation Indicator IAS: Indicated Air Speed 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 1-3...

  • Page 18: System Description

    The G500/G600 TXi installation can provide PFD, MFD, and EIS functions. Three display models, the GDU 700P, GDU 700L, and GDU 1060 are used to convey the information. The G500/G600 TXi system utilizes engine sensors and the GEA 110 engine adapter to provide EIS functions.

  • Page 19: Table 2-1 Aml Stc Installed Sensors

    GDU. The EIS gauges include optional gauges and those required by the aircraft POH and manufacturer. This manual only provides information for the EIS sensors installed per the G500/G600 TXi AML STC. Table 2-1 lists the sensors that are maintained in this manual. Refer to the applicable maintenance data and/ or TSO manual for other sensors that are interfaced to the EIS.

  • Page 20: Figure 2-1 Entering The Configuration Mode On The Gdu

    Flight Log Download ◦ Save configuration to SD card ◦ Save error log to SD card ◦ Load configuration from SD card • Bottom/Right Slot ◦ Update Databases (faster) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-3...

  • Page 21: Save/Load Sd

    To save your aircraft configuration settings to an SD card: 1. Insert an SD card into the Top/Left slot of any GDU 1060/700 in the system 2. Power on all GDUs in the G500/G600 TXi system in configuration mode 3. From the Home screen, select SD save 4.

  • Page 22: Lru Description, Control, And Operation

    2.1.7 Electrical Load Information Electrical load information for the G500/G600 Txi system LRU’s is provided below. Appendix A of this document contains details specific to the load changes for the specific aircraft installation. Table 2-2 G500/600 TXi LRU Electrical Load...

  • Page 23: Figure 2-3 Gdu 700P Features And Controls

    MFD. Pressing the knob acts as an enter or selection of the currently highlighted information. Power Button Photocell Top Card Slot Bottom Card Slot Dual Concentric Knob Figure 2-3 GDU 700P Features and Controls 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-6...

  • Page 24: Figure 2-4 The Gdu 700L Eis Unit

    Dual Concentric Knobs - Control knobs that can be used to scroll and select through various options on the display. Pressing the knob acts as an enter or selection of the currently highlighted information. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-7...

  • Page 25: Figure 2-5 Gdu 700L Features And Controls

    ADC/AHRS LRU. Shown below is a combined PFD/MFD/EIS display. The GDU 1060 requires interface with a compatible GPS/SBAS navigator. Figure 2-6 The GDU 1060 functioning as an MFD/PFD and MFD/PFD/EIS 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-8...

  • Page 26: Figure 2-7 Gdu 1060 Features And Controls

    The GCU 485 is a panel mount remote control unit that provides an alternate method of controlling the G500/G600 TXi PFD display parameters. The GCU 485 Control Unit is available in variations containing different numbers of buttons. All variations contain three knobs in the same configuration as shown below.

  • Page 27: Figure 2-8 Gcu 485 (P/N 011-03582-01 Shown)

    GTP 56 that are connected to the GDU 1060/700P. The integrated ADAHRS utilizes GPS signals sent from the GPS/SBAS navigator. Attitude, heading, and air data can be sent using ARINC 429 digital signals to external LRUs and the GAD43/43e. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-10...

  • Page 28: Figure 2-10 Gsu 75() Adahrs Unit

    GPS/SBAS navigator. Attitude and heading data is sent using ARINC 429 digital signals to the GDU 1060/ 700P and GAD 43/43e. An RS-232 digital connection is used for maintenance and configuration information. Figure 2-11 GRS 79 AHRS Unit 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-11...

  • Page 29: Figure 2-12 Gdc 72 Adc Unit

    GTP 59 OAT probe. The GDC 72 provides pressure altitude, airspeed, vertical speed, and OAT data to the G500/G600 TXi system. The GDC 72 provides data to the G500/G600 TXi using ARINC 429 digital interfaces, as well as RS-232 for maintenance and configuration information.

  • Page 30: Figure 2-14 Gtp 59 Outside Air Temperature Probe

    The GBB 54 supplies power to the GDU 700P, internal ADAHRS, essential EIS sensors, and a single GEA 110 in the event of total electrical power loss. Figure 2-15 GBB 54 Backup Battery 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-13...

  • Page 31: Figure 2-16 Gea 110 Engine Interface

    The GEA 110 is a remote-mount engine interfacing and monitoring module used for gathering sensor input parameters from the engine and processing the signals for the G500/G600 TXi system. The GEA 110 can be mounted to the back assembly of the GDU 1060 or it can be remotely mounted in the fuselage or in the engine compartment.

  • Page 32: Figure 2-17 Gad 43 (Left) And Gad 43E (Right)

    The GAD 43e provides all of the functions of the GAD 43. In addition, it allows the G500/G600 TXi to receive data from marker beacon receivers, synchro (ARINC 407) ADF receivers, DME systems, and analog radar altimeters.

  • Page 33: Figure 2-18 Engine Annunciator

    The carburetor temperature probe is a Type-K thermocouple (Chromel and Alumel) probe. Figure 2-19 Carburetor Temperature Probe 2.2.15.3 Oil Temperature Probe The oil temperature probe is a Type-K thermocouple (Chromel and Alumel) probe. Figure 2-20 Oil Temperature Probe 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-16...

  • Page 34: Figure 2-21 Fuel Flow Sensor Ft-60 (Left) And Ft-90 (Right)

    2.2.15.7 P-Lead RPM Pickup A wire with two parallel resistors in-line connects from each P-lead, at the Magneto or the ignition switch, to the GEA 110 to sense RPM. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 2-17...

  • Page 36: Servicing Information

    3.2 Servicing Information There are no servicing requirements for the G500/G600 TXi system. In the event of a system or LRU failure, troubleshoot the G500/G600 TXi system in accordance with Section 4. 3.2.1 Periodic Maintenance Instructions G500/G600 TXi system LRUs are designed to detect internal failures. A thorough self-test is executed automatically upon application of power to the units, and built-in tests are continuously executed while the LRUs are operating.
  • Page 37 Garmin. Every 2000 Flight hours or Electrical Bonding Perform an electrical bonding check of the G500/G600 TXi 10 years, Check system LRUs in accordance with Section 3.5. whichever comes first It is recommended that the cooling fan on the GDU 1060/700 be replaced every 3000 fan operating hours.

  • Page 38: Visual Inspection

    Aluminum Foil Tape (non-metallic aircraft only) Any aluminum foil tape used in the G500/G600 TXi installation for grounding of a GSU 75/75B, GDC 72, GRS 79, GAD 43/43e, or GEA 110 (see Appendix A of this document) must be inspected every 12 calendar months.

  • Page 39: Rvsm Periodic Maintenance (Socata Tbm 700/850 Only)

    If measured resistance is greater than applicable values in the following table, bonding must be improved to meet applicable requirements for a new installation in accordance with Section 4 of the G500/G600 TXI Part 23 AML STC Installation Manual. Table 3-2 Electrical bonding requirements...

  • Page 40: Overhaul Period

    The system does not require overhaul at a specific time period. Power on self-test and continuous BIT will monitor the health of the G500/G600 TXi system. If any LRU indicates an internal failure, the unit may be removed and replaced. See of this document for fault 3.8 Special Inspection Requirements...

  • Page 41: Data Relative To Structural Fasteners

    3.10 Data Relative to Structural Fasteners Data relative to structural fasteners, such as type, torque, and installation requirements can be found in Section 5 of this manual. 3.11 Additional Instructions None. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 3-7...

  • Page 42: Troubleshooting

    Appendix A of this document or with the aircraft’s permanent records. 4.1 General System Troubleshooting Before troubleshooting the G500/G600 TXi system, use the Configuration log tool to print the current configuration log to ensure that system configuration settings match those recorded in the aircraft’s permanent records.

  • Page 43: Connector Information

    Maintenance log 4.1.1 System Maintenance Log The G500/G600 TXi system has a maintenance and error log that can be accessed or printed to assist with system maintenance and troubleshooting. The maintenance and error log can be accessed using the following procedure: 1.

  • Page 44: Figure 4-2 Gdu 700P Connectors

    J4/P4 - 78 pin female contact HD-D-sub • J5/P5 - TNC connector (Not Used) • J6/P6 - TNC connector (Not Used) • J7/P7 - TNC connector Figure 4-2 GDU 700P Connectors 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-3...
  • Page 45 ETHERNET OUT 2A MAGNETOMETER PWR OUT ETHERNET IN 3A RS-232 OUT 2 ETHERNET OUT 3A RS-232 OUT 1 ETHERNET IN 4A CONFIG MODULE DATA * Denotes active low 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-4...
  • Page 46 TIME MARK IN 2A DISC IN 3 HI TIME MARK IN 2B DISC IN 4 HI TIME MARK IN 1A RS-485 4A TIME MARK IN 1B RS-485 4B 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-5...
  • Page 47 DISC IN 6 LO ARINC 429 OUT 4B DISC IN 7 LO ARINC 429 OUT 5A DISC IN 8 LO ARINC 429 OUT 5B J7/P7Connector Name BACKUP GPS ANT 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-6...

  • Page 48: Figure 4-3 Gcu 485 Connector

    RS-232 IN 1 RS-232 OUT 2 RS-232 IN 2 POWER GROUND SIGNAL GROUND AIRCRAFT_POWER_1 SIGNAL GROUND AIRCRAFT_POWER_2 RESERVED LIGHTING BUS HI LIGHTING BUS LO RESERVED* RESERVED POWER GROUND 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-7...

  • Page 49: Gdc 72

    RESERVED RESERVED SIGNAL GROUND SIGNAL GROUND RS 232 OUT 1 SIGNAL GROUND RS 232 IN 1 SIGNAL GROUND RESERVED SIGNAL GROUND RESERVED AIRCRAFT GROUND 1 SIGNAL GROUND 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-8...
  • Page 50 SPARE CONFIG MODULE GROUND AIRCRAFT GROUND 2 SYS ID 1* SIGNAL GROUND DISCRETE IN 3* RESERVED DISCRETE IN 4 RESERVED DISCRETE IN 2* *Indicates active low 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-9...

  • Page 51: Figure 4-5 View Of J751 Connector Looking At Gsu 75()

    RS-232 AHRS 3 GROUND RS-232 IN ADC 1 RS-232 AHRS 1 GROUND RS-232 OUT AHRS 2 MAGNETOMETER GROUND RS-232 IN AHRS 2 AIRCRAFT GROUND 1 RS-232 AHRS 2 GROUND 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-10...
  • Page 52 CONFIG MODULE GROUND AIRCRAFT GROUND 2 SYS ID 1* RS-232 ADC 2 GROUND DISCRETE IN 3* RESERVED DISCRETE IN 4 RESERVED DISCRETE IN 2* *Indicates active low 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-11...

  • Page 53: Grs 79

    ARINC 429 IN 3B RESERVED SIGNAL GROUND SIGNAL GROUND RESERVED SIGNAL GROUND RESERVED SIGNAL GROUND RS-232 OUT 2 MAGNETOMETER GROUND RS-232 IN 2 AIRCRAFT GROUND 1 SIGNAL GROUND 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-12...
  • Page 54 SPARE CONFIG MODULE GROUND AIRCRAFT GROUND 2 SYS ID 1* SIGNAL GROUND DISCRETE IN 3* RESERVED DISCRETE IN 4 RESERVED DISCRETE IN 2* *Indicates active low 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-13...

  • Page 55: Figure 4-7 Gad 43/43E J431/P431 Connector Looking At Unit

    PITCH AC OUT HI AIRCRAFT POWER 1 (60 mV/deg or 200 mV/deg) ROLL AC OUT LO AIRCRAFT POWER 2 (54 mV/deg or 200 mV/deg) *Indicates active low 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-14...

  • Page 56: Figure 4-8 Gad 43E J432/P432 Connector Looking At Unit

    DME EXT TUNE M1/MD/M3 IN PRESELECT ADDR 0 / AP DISC SW DME EXT TUNE K800/KA/K0 IN PRESELECT ADDR 1 DME EXT TUNE K400/KE/K1 IN GROUND DME EXT TUNE K200/KC/K2 IN 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-15...

  • Page 57: Figure 4-9 Gad 43E J433/P433 Connector Looking At Unit

    FD ROLL LEFT OUT (GND) FD PITCH UP IN/GS #2 +FLAG FD PITCH DOWN IN/GS #2 -FLAG FD ROLL RIGHT IN/GS #1 +FLAG FD ROLL LEFT IN/GS #2 -FLAG 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-16...

  • Page 58: Figure 4-10 Gea 110 Connectors

    RS 485 2A RS 485 1A AV PWR IN 2 RESERVED DISCRETE OUT 2 RS 485 2B RS 485 1B DISCRETE IN 5 SYS ID #1 SYS ID #2 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-17...

  • Page 59: Figure 4-12 Gea 110 J1102/P1102 Connector Looking At Unit

    +5 VDC OIL PRESSURE (-) FUEL PRESSURE (-) +12 VDC DISCRETE IN 2 MANIFOLD PRESSURE (-) FUEL QUANTITY 1 / DISCRETE IN 4 GENERAL PURPOSE 3 (-) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-18...
  • Page 60 GENERAL PURPOSE 6 (-) SHUNT 1 (+) SHUNT 2 (+) SPARE RPM IN 1 (-) +5 VDC RPM IN 2 (-) BUS 3 CONFIG MOD DATA CONFIG MOD GND 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-19...

  • Page 61: Figure 4-13 Gbb 54 J541/P541 Connector

    Pin # Function POWER IN POWER IN GROUND STANDBY GROUND GROUND BATTERY POWER BATTERY POWER POWER IN GROUND RS-232 TX RS-232 RX PWR ON REQ GROUND BATTERY POWER 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-20...

  • Page 62: G500/G600 Txi Part 23 Aml Stc Maintenance Manual

    GDU or GDC unit. 3-Conductor Shielded Cable Conductor Color Name White Probe Power Lead Blue Resistive Element HI Orange Resistive Element LO 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-21...

  • Page 63: Troubleshooting Flow Charts

    This section provides troubleshooting flow charts for most system failures and alert messages. It is recommended that system troubleshooting and repair only be completed by a Garmin dealer. If a specific alert or fault condition is not listed, or the fault still exists after completing the given corrective action, contact Garmin Aviation Technical Support at the number listed for your specific region on the “Support”...

  • Page 64: Figure 4-14 Gdu Alert Message Troubleshooting

    If fa u lt s till e x is ts , c o n ta c t G a rm in . Figure 4-14 GDU Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-23...

  • Page 65: Figure 4-15 Gdu Config And Battery Alert Message Troubleshooting

    Section 5.1.4 or from saved SD from saved SD Section 5.1.5 card card If fault still exists, contact Garmin. Figure 4-15 GDU Config and Battery Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-24...

  • Page 66: Figure 4-16 Pfd Alert Message Troubleshooting

    Part 23 AML Inspect NAV Installation Manual wiring, (P/N:190-01717- connections, and B3) for more configuration information) settings If fault still exists, contact Garmin. Figure 4-16 PFD Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-25...

  • Page 67: Figure 4-17 Ahrs/Adc Alert Message Troubleshooting

    AHRS unit in connections, and 01717-B3) 01717-B3) accordance with wiring. G500/G600 Txi AML STC installation manual If fault still exists, contact Garmin. Figure 4-17 AHRS/ADC Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-26...

  • Page 68: Figure 4-18 Terrain Alert Message Troubleshooting

    V erify T errain database coverage If fau lt s till ex is ts , co n ta ct G arm in . Figure 4-18 Terrain Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-27...

  • Page 69: Figure 4-19 Traffic Alert Message Troubleshooting

    If fa u lt s till e x is ts , c o n ta c t G a r m in . Figure 4-19 Traffic Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-28...

  • Page 70: Figure 4-20 Audio/Weather Alert Message Troubleshooting

    Troubleshoot in accordance with Troubleshoot in audio device accordance with maintenance audio device manual maintenance manual If fault still exists, contact Garmin. Figure 4-20 Audio/Weather Alert Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-29...

  • Page 71: Figure 4-21 External Lru Failure Message Troubleshooting

    If f a u lt s t ill e x is t s , c o n t a c t G a r m in . Figure 4-21 External LRU Failure Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-30...

  • Page 72: Figure 4-22 External Lru Service Message Troubleshooting

    If fau lt s till e x ists , c o n ta c t G a rm in . Figure 4-22 External LRU Service Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-31...

  • Page 73: Figure 4-23 Gad Fault Message Troubleshooting

    If fa u lt s till e x is ts , c o n ta c t G a rm in . Figure 4-23 GAD Fault Message Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-32...

  • Page 74: Figure 4-24 Gad Fault Message Troubleshooting Continued

    If fa u lt s till e x is ts , c o n ta c t G a rm in . Figure 4-24 GAD Fault Message Troubleshooting Continued 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-33...

  • Page 75: Figure 4-25 Eis Gauge Troubleshooting

    EMI shield Replace fuel flow transducer If fault still exists, contact Garmin. Figure 4-25 EIS Gauge Troubleshooting 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 4-34...

  • Page 76: Equipment Maintenance And Checkout Procedures

    5.10.2 Re-Installation ..........................5-29 5.10.3 Checkout...........................5-29 5.11 Backup GPS Antenna ........................5-29 5.11.1 Removal ...........................5-30 5.11.2 Installation ..........................5-30 5.11.3 Checkout...........................5-30 5.12 EIS Sensors .............................5-31 5.12.1 Carburetor/Induction Air Temperature ..................5-32 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-1...
  • Page 77 This section provides the procedures to remove, replace, or install required and optional LRUs that are part of the G500/G600 TXi system. Refer to Section 4 for the definition of connectors and pin functions for G500/G600 TXi system LRUs. Before performing any maintenance on the G500/G600 TXi system all information in Appendix A must be filled out.

  • Page 78: Gdu 1060/700

    5.1 GDU 1060/700 QTY ITEM PART NUMBER DESCRIPTION NOTES Figure 5-1 GDU 1060 Installation 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-3...

  • Page 79: Figure 5-2 Gdu 700P Installation

    1. Ensure the current configuration is saved to an SD card in accordance with the instructions contained in Section 2.1.6. 2. Turn off the GDU and remove power for the GDU. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-4...

  • Page 80: Cooling Fan Replacement

    Cooling Fan Replacement NOTE The GDU cooling fan replacement kit (P/N: K00-01080-00) must be obtained from an authorized Garmin dealer. In order for the GDU warranty to remain valid this procedure must be accomplished by an authorized Garmin dealer. NOTE Resetting the fan operation hours requires the use of an Installer unlock card.

  • Page 81: Figure 5-3 Integrated Adc Module Installation

    2. Mark pitot and static lines with ‘P’ and ‘S’, if not already marked, near ADC connections. REF. FITTING, 1/8-27 ANPT TYP. 2 PLCS REF. 011-03457-00 ADC MODULE, GDU 700/1060 DISPLAY REF. THUMB SCREW Figure 5-3 Integrated ADC Module Installation 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-6...

  • Page 82: Configuration Module Replacement

    Replace all deficient components if any of these conditions are found. 6. Connect harness to new configuration module. 7. Install new configuration module in connector backshell(6) and re-install cover(7). 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-7...

  • Page 83: Figure 5-4 Configuration Module Installation

    Section 5.1.4. Following the master configuration module replacement, the system ID will have changed. Any feature unlocks and databases will need to be re-issued for the new system ID by a Garmin dealer. To return the system to service from this condition perform the following steps:...

  • Page 84: Re-Installation

    5. Ensure that Master is selected on the GDU that has been chosen to act as the master configuration module. 6. At this point the G500/G600 TXi system will have a new system ID. System features will need to be unlocked and the system databases will need to be re-installed. The System ID must be updated on Flygarmin.com and then new databases can be downloaded.

  • Page 85: Gcu 485

    3. Turn counter-clockwise until the pawl-latches are able to rotate to a horizontal position. 4. Remove the unit from the panel. 5. Disconnect the electrical connector from the back of the unit. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-10...

  • Page 86: Re-Installation

    3. Tighten the pawl latches with a 3/32” hex drive tool inserted through holes in GCU 485 face plate. 4. Torque the latches to 20 +/-2 in-lbs. 5. Restore power to the unit. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-11...

  • Page 87: Eis Annunciator

    5. Push to release the snap tabs in the switch housing and gently pull the connector out of the module. Figure 5-7 EIS Caution and Warning Annunciator Installation 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-12...

  • Page 88: Re-Installation

    3. Tighten the mounting screws until the module is fully seated in the housing. 4. Rotate the cap back into position on the module and gently press until secured. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-13...

  • Page 89: Gdc 72

    Figure 5-8 GDC 72 Installation (Sheet Metal Shelf Example) 5.4.1 Removal Removal of the GDC 72 Air Data Computer can be accomplished using the following procedure: 1. Remove power to the GDC 72. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-14...

  • Page 90: Checkout

    Perform a static and pitot system leak test in accordance with the aircraft manufacturers specification and/ or applicable regulations. In accordance with 14 CFR Part 43 Appendix E, paragraph (b)(2), Garmin specifies a test procedure equivalent to Part 43 Appendix E, paragraph (b)(1) with two exceptions. The tests of sub-paragraphs (iv) (Friction) and (vi) (Barometric Scale Error) are not applicable because the digital outputs of the GDC 72 are not susceptible to these types of errors.

  • Page 91: Gsu 75(), Grs 79

    5.5.1 Removal Removal of the GSU 75() or GRS 79 can be accomplished using the following procedure: 1. Remove power to the unit. 2. Disconnect electrical connector. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-16...

  • Page 92: Installation

    Perform a static and pitot system leak test in accordance with the aircraft manufacturers specification and/ or applicable regulations. In accordance with 14 CFR Part 43 Appendix E, paragraph (b)(2), Garmin specifies a test procedure equivalent to Part 43 Appendix E, paragraph (b)(1) with two exceptions. The tests of sub-paragraphs (iv) (Friction) and (vi) (Barometric Scale Error) are not applicable because the digital outputs of the GSU 75() are not susceptible to these types of errors.

  • Page 93: Gad 43/43E

    GAD 43/43e or if the software is updated, a GDU installer unlock card is necessary to configure the new unit. Figure 5-10 GAD 43 Installation (Sheet Metal Shelf Example) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-18...

  • Page 94: Removal

    3. Navigate to Interfaces → Adapter → Settings 4. Configure interface settings per the printed configuration log. 5. Perform checkout procedures in Section 6.2 and Section 6.7 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev.

  • Page 95: Gea 110

    5.7 GEA 110 Figure 5-11 GEA 110 Installation (Mounted Directly to Airframe Example) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-20...

  • Page 96: Figure 5-12 Gea 110 Installation (Mounted On A Tray Example)

    Figure 5-12 GEA 110 Installation (Mounted on a Tray Example) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-21...
  • Page 97 Perform the following checkout procedure only if the GEA was replaced or did not initially pass the checkout procedure above: 1. EIS Ground Checks as described in Section 6.5 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3).

  • Page 98: Gbb 54

    5.8 GBB 54 Figure 5-13 GBB 54 Installation (Sheet Metal Shelf Example) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-23...

  • Page 99: Removal

    7. Insert battery cover (2) with gasket (3) and battery pack (4) into housing (5). 8. Insert the four bolts (1) and nuts (7). 9. In cross-tightening sequence, torque bolts (1) to 40 to 60 in-lbs. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-24...

  • Page 100: Gmu 44

    Removal, re-installation, or replacement of the GMU 44 will require a recalibration of the AHRS which requires the use of a GDU installer unlock card. In addition, any removal or 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-25...

  • Page 101: Removal

    5. Perform the Checkout procedure in Section 5.9.3. 5.9.3 Checkout Perform the following calibration procedures and checks found in Section 6 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3) to return the aircraft to service: 1. Magnetometer Calibration.

  • Page 102: Figure 5-15 Gmu 44 Installation (Universal Mount Example)

    Figure 5-15 GMU 44 Installation (Universal Mount Example) 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-27...

  • Page 103: Gtp 59

    To remove the GTP 59, perform the following procedure: 1. Remove power to the ADC unit. 2. Remove mounting nut(1) shown in Figure 5-16. 3. Remove GTP from hole. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-28...

  • Page 104: Backup Gps Antenna

    2. Install washer(2) and nut(1) and torque to specifications in Figure 5-16. 5.10.3 Checkout Perform the checkout procedure in Section 6.3.2 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3). 5.11 Backup GPS Antenna The backup GPS antenna is designed for installation on top of an existing instrument panel glare shield.

  • Page 105: Figure 5-18 Backup Gps Antenna Installation (Removable Installation Example)

    Install the backup GPS antenna in the reverse order of the removal procedure. 5.11.3 Checkout Perform the Backup GPS checkout procedure as described in Section 6.3.6 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3). 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev.

  • Page 106: Eis Sensors

    (AN/MS). After removing or replacing any EIS sensor perform the EIS ground checkout procedure for the specific sensor that was affected in Section 6.5 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3) CAUTION Check hose routing for sharp bends.

  • Page 107: Figure 5-19 Carburetor Temperature Sensor Installation Example

    Figure 5-19 Carburetor Temperature Sensor Installation Example CAUTION Fuel and air passages must remain free of contaminants during work near and around the carburetor. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-32...

  • Page 108: Figure 5-20 Oil Temperature Sensor Installation Example

    7, Safetying of Chapter 7, Aircraft Hardware, Control Cables and Turnbuckles of advisory circular AC 43.13-1B, Aircraft Inspection and Repair. Figure 5-20 Oil Temperature Sensor Installation Example 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-33...

  • Page 109: Table 5-1 Pressure Sensor Equipment List

    Manifold pressure, oil pressure, and fuel pressure sensor installations are similar. Garmin pressure sensors with a brass housing are limited to aircraft with operational ceilings up to 25,000 feet. Garmin pressure sensors with a stainless steel housing may be used on all aircraft on the AML.

  • Page 110: Figure 5-21 Brass Sensor Installation, Coupling Mount Example

    Figure 5-21 Brass Sensor Installation, Coupling Mount Example 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-35...

  • Page 111: Figure 5-22 Stainless Steel Sensor Installation, Housing Mount Example

    Figure 5-22 Stainless Steel Sensor Installation, Housing Mount Example 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-36...

  • Page 112: Fuel Flow

    Methods, Techniques, and Practices defined in Chapter 4, Metal Structure, Welding and Brazing of advisory circular AC 43.13-1B, Aircraft Inspection and Repair are acceptable. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-37...

  • Page 113: Figure 5-23 Fuel Flow Transducer Installation

    110. Connection can be made at the magneto or the ignition switch. To replace the P-Lead wire, remove the old section of wire and replace the entire wire and parallel resistors in accordance with the P-Lead installation instructions contained in the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3).

  • Page 114: Calibration

    Analog NAV Calibration Analog Nav calibration requires the use of an Installer unlock card. If it becomes necessary to re-calibrate the Analog Nav, refer to the calibration procedure contained in the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3) 5.13.4...

  • Page 115: External Systems (Weather Radar) Calibration

    External Systems (Weather Radar) Calibration Weather radar calibration requires the use of an Installer unlock card. If it becomes necessary to re- calibrate the weather radar, refer to the calibration procedure contained in the G500/G600 TXi Part 23 AML STC Installation Manual (P/N: 190-01717-B3).

  • Page 116: Uploading Software

    7. Follow the on-screen display instructions. 5.15 System Checks Periodic system checks that do not require a Garmin dealer to perform are contained in this section. For complete system checkout procedures see Section 6 of the G500/G600 TXi Part 23 AML STC Installation Manual (P/N:190-01717-B3).

  • Page 117: Table 5-2 Lru Status Indicators

    5.15.1.2 System Summary The Home page in configuration mode of the GDU 700P/1060 contains a Summary button that provides information for each configured LRU as part of the G500/G600 TXi System. 1. Open the system summary (Home → Summary). 2. Verify that all configuration settings listed are consistent with the printed configuration log.

  • Page 118: Figure 5-24 Airspeed Configuration Type

    9. Change the airspeed until the PFD airspeed tape pointer is at the top of the white band (Vfe). 10. Verify that the top of the white arc/band on the standby ASI and PFD airspeed tape are at the same airspeed value. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-43...

  • Page 119: Table 5-3 Airspeed Test Points

    ±3 ±2.0 ±3 ±2.0 ±5 ±2.0 ±5 ±2.0 ±5 ±3.0 ±6 Notes: [1] If available, the aircraft or instrument manufacturer’s data should be referenced for standby tolerances. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-44...
  • Page 120 8. Starting at the current airspeed, decrease the airspeed to zero, stopping at all of the relevant airspeeds listed in Table 5-3 (airspeeds above Vne should not be checked). Verify that the PFD and standby ASI values are within the tolerances indicated. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-45...

  • Page 121: Table 5-4 Advanced Airframe Specific Configuration Data - Arc Ranges

    Overlap between set to OFF. WHITE/ standard operational 2-Limitations GREEN and flaps If WHITE and GREEN arcs overlap, operational ranges configure to the range they overlap within. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-46...
  • Page 122 If variable with altitude, set to Variable operating mach and set overspeeds in accordance with number appendix E.5 in G500/G600 TXi Part 23 AML STC Intsallation Manual. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-47...

  • Page 123: Table 5-5 Advanced Airframe Specific Configuration Data - Markings

    Pitot-static System #1, Pitot-static System #2, and calibration of the AM-250, must meet the criteria in the following sections. The air data tests and surface checks are required within the previous 24 months. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-48...
  • Page 124 If either the pilot or co-pilot air data system does not meet the tolerances specified, maintenance checks should be performed on the air data system or the Pitot-static system. 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-49...

  • Page 125: Table 5-6 Air Data Test Points

    20009 to 20103 20026 to 20086 20056 20035 to 20129 20035 to 20129 20052 to 20112* 20000 20082* 20277 to 20371 20277 to 20371 20294 to 20354 20324 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-50...
  • Page 126 If the aircraft fails to hold altitude to this tolerance, repeat the check ensuring that the airspeed remains constant and the air remains stable during the entire test. If the test still fails, perform maintenance checks on the G600 TXi system, then repeat the test. RVSM operations are prohibited until the autopilot is capable 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev.

  • Page 127: Table 5-7 Altitude Hold Check Log

    En route to: Pilot Co-pilot Time (hr:min) Altitude (ft) Airspeed (kt) Altitude (ft) Airspeed (kt) 0:00 0:05 0:10 0:15 0:20 0:25 0:30 0:35 0:40 0:45 0:50 0:55 1:00 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page 5-52...

  • Page 128: Appendix A Installation Specific Information

     GDU3  1060  700P  700L  MFD  PFD  EIS  GDU4  1060  700P  700L  MFD  PFD  EIS 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-1...

  • Page 129: Lru Information

    GDC 74( ) #2 011-0_____-_______ GTP 59 #1 011-00978-________ GTP 59 #2 011-00978-________ GAD 43/43e 011-0_____-_______ GEA 110 #1 011-03454-________ GEA 110 #2 011-03454-________ GCU 485 011-03582-________ GBB 54 011-03456-________ 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-2...

  • Page 130: Equipment Location

    GDC 72( ) #2 GDC 74( ) #1 GDC 74( ) #2 GTP 59 #1 GTP 59 #2 GAD 43/43e GEA 110 #1 GEA 110 #2 GBB 54 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-3...

  • Page 131: Wire Routing - Single Engine

    Wire Routing – Single-Engine The following diagram depicts the wire routing for the G500/G600 LRUs throughout the aircraft structure for a single-engine aircraft: 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-4...

  • Page 132: Wire Routing - Twin Engine

    Wire Routing – Twin-Engine The following diagram depicts the wire routing for the G500/G600 LRUs throughout the aircraft structure for a twin-engine aircraft: 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-5...

  • Page 133: Saved Configuration File

    Saved Configuration File The G500/G600 TXi system configuration must be saved to an SD card and placed with the permanent aircraft maintenance records. For instructions on saving the aircraft configuration file to an SD card refer to Section 2.1.6. It is recommended that the SD card be taped or otherwise secured to this page in the location marked below.

  • Page 134: Gdu 1060 Eis Gauge Layout Template

    A.8 GDU 1060 EIS Gauge Layout Template (E G T / C H T ) ( E G T / C H T ) Figure A-1 GDU 1060 EIS Gauge Template 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-7...

  • Page 135: Gdu 700P Eis Gauge Layout Template

    A.9 GDU 700P EIS Gauge Layout Template ( E G T /C H T ) (E G T /C H T ) Figure A-2 GDU 700P EIS Gauge Layout Template 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-8...

  • Page 136: Gdu 700L Eis Gauge Layout Template

    A.10 GDU 700L EIS Gauge Layout Template (EGT/CHT) (EGT/CHT) Figure A-3 GDU 700L EIS Gauge Layout Template 190-01717-B1 G500/G600 TXi Part 23 AML STC Maintenance Manual Rev. 1 Page A-9...

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