Contents - Table Of Contents
- Table Of Contents
- Table Of Contents
- Table Of Contents
- Table Of Contents
- Table Of Contents
- INTRODUCTION
- Organization
- Definitions/Abbreviations
- Units of Measure
- Section 1 1-1 –
- SYSTEM DESCRIPTION
- Figure 2-2, Transponder
- Figure 2-3 GSU-75 ADAHRS with Connector and Mounting Tray
- Figure 2-4, GDL 69A SXM Datalink
- G1000 Optional Interfaces
- G1000 Normal Mode
- Section 2 2-1 –
- SOFTWARE AND CONFIGURATION
- Figure 3-1, SET>ACTV Diagram
- Figure 3-2, Loss of Communication
- G1000 System Software Information
- Figure 3-5, GSU Configuration Settings Storage
- Configuration Mode
- Figure 3-6, Garmin Unit S/N Location
- G1000 Software/Configuration Procedure
- System Software and Configuration Load
- Figure 3-8 – Airframe Group Selection
- Figure 3-9 – Airframe Change Confirmation
- Feature Enablement
- Aircraft Registration Number Entry
- Configuration Manager
- Splash Screen Loading
- Figure 3-10, MFD Aux - Database Page DB Transfer
- Configuration of Navigation Map for Traffic System
- Interface Confirmation
- Section 3 3-1 –
- Servicing Information
- Maintenance Intervals
- Electrical Bonding Test
- GSU 75 Earth Magnetic Field Updates
- Section 4 4-1–
- TROUBLESHOOTING
- System Annunciations
- G1000 Alerting System
- Synthetic Vision and Pathways Troubleshooting
- Backup Communications Path Checks
- GDU 105X Troubleshooting
- GDU 105X Alerts
- GTX Troubleshooting
- GDL69A SXM Troubleshooting (if installed)
- GSU 75 and GMU 44 Troubleshooting
- Figure 5-5, Magnetometer Interference Test
- Table 5-3, Magnetometer Interference Test Sequence
- GSU 75 Troubleshooting
- Software/Configuration Troubleshooting
- Backshell/Backplate Connectors
- Section 5 5-1 –
- EQUIPMENT REMOVAL & INSTALLATION
- GDU 1054B/1050
- GDL 69A SXM (if installed)
- Figure 6-1, Configuration Module Installation
- Figure 6-2, GSU 75 Configuration Module Installation
- Section 6 6-1 –
- GARMIN G1000 LRU REPLACEMENT/CONFIGURATION & TESTING
- Figure 7-1, G1000 Normal Mode Check
- GMA 1347 Audio Panel
- GIA 63W Integrated Avionics Unit
- Figure 7-2, Aux – GPS Status Page (MFD)
- GEA 71 Engine/Airframe Unit
- Figure 7-3, Normal Engine Instrument Markings (MFD)
- GTX 335R, GTX 345R, or GTX 33 Transponder
- Figure 7-4, Aircraft Registration
- GSU 75 ADAHRS (if installed)
- GDC 74A Air Data
- Table 7-1, Altitude Test Points
- Table 7-2, Airspeed Test Points
- GRS 77 and GMU 44 Magnetometer (if installed)
- GMU 44 Magnetometer
- GSU/GRS/GMU Calibration Procedures
- Table 7-4, Required GRS/GMU Calibrations
- Figure 7-5, GRS/GMU Calibration, Pitch/Roll Offset
- Figure 7-6, GRS/GMU Calibration, Engine Run-Up
- Figure 7-7, Normal Mode AHRS Check
- GDL 69A or GDL 69A SXM Data Link (if installed)
- GSA 81 Servos (if installed)
- Garmin Traffic Systems (GTS 800) (if installed)
- Section 7 7-1–
- SUBSYSTEM FUNCTIONAL CHECKS
- ChartView Functional Check
- SafeTaxi Functional Check
- DME Functional Check
- Section 8 8-1 –
- G1000 SYSTEM RETURN TO SERVICE PROCEDURE
- Figure 9-2, PFD Power-up System Annunciations
- Figure 9-3, PFD Normal Operation
- Display Failure Test
- Reversion Mode Check
- GPS Signal Acquisition
- GPS Failure Test
- GIA Failure Test
- GEA Functional Check
- G1000 Backup Path Test
- Appendix A
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G1000 Supplemental Maintenance Manual Page 7-8Textron Nav III Series Revision 3190-02128-047.3 GIA 63W Integrated Avionics UnitOriginal GIA 63W(s) ReinstalledNo software or configuration loading is required if the removed GIA is re-installed in its originalposition (GIA1 and GIA2 in their original racks). This does not include units that were returnedfor repair as their software and configuration files are deleted during the repair testing process.Continue to the return-to-service checks in Section 9.Original GIA 63Ws Swapped for TroubleshootingNo software loading is required if the originally installed GIA units are re-installed in oppositepositions (GIA1 and GIA2 in opposite unit racks). However, configuration loading is required.See Section 7.3.1.New, Repaired or Exchange GIA 63W(s) InstalledIf a new, repaired or exchange GIA 63W is installed, the correct software and configuration filesmust be loaded to the unit. See Section 7.3.1.LRU Replacement Procedure GIA1 or GIA21. Open the MFD, PFD (ESS BUS), and PFD (AVN BUS 1) circuit breakers.2. Remove Garmin SD/MMC/FS 510 cards from bottom slots of the MFD and PFD ifpresent.3. Apply power to the G1000 system by connecting external power to the aircraft toenergize the aircraft.4. Turn on Avionics electrical busses.5. Power on the MFD and PFD in configuration mode.6. Using the PFD, scroll to the LRU replacement page.7. Activate the cursor and select GIA1 or GIA2, whichever was replaced in the LRUdropdown box.8. Press the CHK All softkey.9. Press the Load softkey.10. Press ENT to acknowledge the process was complete.11. Select Com1 or 2 (as applicable) in the LRU dropdown box.12. Press the CHK All softkey.13. Press the Load softkey.14. Press ENT to acknowledge the process was complete.15. Select GPS1 or 2 (as applicable) in the LRU dropdown box.16. Press the CHK All softkey.17. Press the Load softkey.18. Press ENT to acknowledge the process was complete.19. Select Nav1 or 2 (as applicable) in the LRU dropdown box.20. Press the CHK All softkey.21. Press the Load softkey.22. Press ENT to acknowledge the process was complete. |
