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 7-36Textron Nav III Series Revision 3190-02128-04Compass Rose Evaluation of Magnetic Disturbances for MagnetometerCalibration Procedure (Optional)NOTEThe Magnetometer Calibration Procedure that follows in Section 7.10.3(Calibration Procedure B) must be carried out at a site that isdetermined to be free of magnetic disturbances. If it is unsure whetherthe site is ‘clean’, the technician should verify that the site is ‘clean’ byfollowing the guidance provided in Section 7.10.2. The technician mayskip Section 7.10.2 if the site condition is acceptable.Typically, a compass rose is an acceptable location to perform themagnetometer calibration procedure. However, because not allcompass roses are well maintained, even an existing compass roseshould be regularly evaluated using the method described here todetermine if it is free of magnetic disturbances. If evaluation of anexisting compass rose indicates that magnetic disturbances arepresent, then an alternative location must be found to perform theMagnetometer Calibration Procedure.A G1000-equipped airplane that has completed the pitch/roll offset compensation procedure(Procedure A-1, Section 7.10.1) can be used to evaluate a candidate site for magneticdisturbances and determine whether it is a suitable location to perform the magnetometercalibration procedure. The magnetometer calibration procedure itself contains the logic tosimultaneously survey the location for magnetic cleanliness while it is computing themagnetometer calibration parameters.In order to evaluate a candidate site, the Magnetometer Calibration Procedure must beperformed twice: once turning clockwise around the site, and once turning counter-clockwise.Both times, the procedure should be conducted as described in Section 7.10.3 of thisdocument, with the exception of the direction of turns around the site.NOTEAlthough Section 7.10.3 indicates that the Magnetometer CalibrationProcedure should be performed by making a series of clockwise turnsaround the site, the procedure can also be performed by makingcounter-clockwise turns for the purpose of evaluating the site formagnetic disturbances.If the PFD displays the “CALIBRATION SUCCESSFUL / SITE IS CLEAN” message uponcompletion of the Magnetometer Calibration Procedure in each clockwise and counter-clockwise direction, then the candidate site is sufficiently free of magnetic disturbances and isacceptable for performing the Magnetometer Calibration Procedure. It is important to obtainsuccessful result in both the clockwise and counter-clockwise directions to ensure that themagnetometer sweeps over a large enough area at the candidate site.If the PFD displays either the “MAG FIELD AT SITE NOT UNIFORM” or “MAG FIELD AT SITEDIFFERS FROM IGRF MODEL” message upon completion of the Magnetometer CalibrationProcedure in either of the two directions, then the site contains magnetic disturbances that aretoo large. PreviousNext |