What to do if Software File Mismatch Alert appears on Garmin Autopilot System?
If a Software File Mismatch Alert appears on your Garmin Autopilot System's PFD, verify that the correct software file part number and version were loaded to the LRU. Also, check that the correct Card Loader was used during the load process. If issues persist, try reloading the software to the LRU.
What to do if configuration file load fails on Garmin Autopilot System?
If the configuration file load fails on your Garmin Autopilot System, first ensure that the required criteria are fulfilled. Next, verify that the LRU is reporting data on the System Status page and check the data path wiring. Try loading the configuration file again with a different card, making sure not to touch the MFD during the process. Confirm that the LRU part number is compatible with the Card Loader. If the issue continues, replace the LRU.
How to troubleshoot MFD or PFD displays that do not power up on a Garmin Autopilot System?
If the MFD or PFD displays of your Garmin Autopilot System do not power up, first ensure that all necessary criteria are met. Then, check that power is present at the display backshell connector. If the issue persists, consider replacing the display.
General| Type | Autopilot System |
|---|---|
| Manufacturer | Garmin |
| Applicability | General Aviation Aircraft |
| Display Size | N/A (integrated with existing displays) |
| Resolution | N/A (integrated with existing displays) |
| Features | Yaw Damper |
| Compatibility | Garmin G1000 |
| Functions | Altitude Hold |
| Approach Capabilities | ILS, LPV, LNAV/VNAV, LNAV, VNAV |
| Control Modes | Heading |
| Display Integration | Integrated with Garmin Avionics Displays |
| Certification | FAA |
| Operating Temperature | -20°C to +55°C |
| Interface | ARINC 429, CAN bus |
| Weight | Various components, consult install manual for specific weights |
| Power Consumption | Consult install manual for specific power consumption |
Defines the ICA for Garmin G1000/GFC700 in Hawker Beechcraft King Air.
Details the components of the G1000 integrated cockpit system and GFC700 AFCS.
Describes the Primary Flight Displays (PFD) and Multi-Function Display (MFD) units.
Details the GIA 63W Integrated Avionics Units and their interfaces.
Describes the GDC 7400 Air Data Computer and its function.
Details the GRS 77 AHRS and its role in providing attitude and heading.
Details the procedure for starting the G1000 system in Normal Mode.
Explains reversionary mode for display information in case of failure.
Provides an overview of the configuration mode for avionics technicians.
Outlines the procedure for creating a software loader card for the G1000 system.
Describes how to perform a final software review after loading procedures.
Lists the mandatory maintenance intervals and checks for continued airworthiness.
Details systems and items requiring tests or checks at specific intervals.
Provides procedures for Phase 3 and Phase 4 electrical bonding checks.
Verifies primary/secondary power sources and data path integrity.
Checks AHRS, airspeed, and altitude miscompare monitors for accuracy.
Identifies messages indicating a data path failure within the GDU or GIA units.
Provides basic troubleshooting guidance for LRU failures.
Guides troubleshooting for individual engine/airframe sensor failures.
Provides troubleshooting steps for TAWS system annunciation issues.
Describes symptoms and troubleshooting actions for SVS/Pathways feature issues.
Provides troubleshooting steps for the GFC 700 Autopilot.
Lists common annunciations and their resolution for the AFCS system.
Step-by-step procedure for testing PFD and MFD functionality.
Lists calibration procedures and criteria for GRS 77 and GMU 44 units.
Performs functional checks for TAWS-B and TAWS-A systems.
Required checks to verify proper configuration for RVSM airspace operation.
Verifies avionics configuration matches requirements for RVSM.
Visual inspection criteria for the RVSM critical region around static ports.
Procedure for inspecting static port height using a gauging assembly.
Perform Air Data Test to ensure RVSM compliance.
Verifies autopilot's ability to maintain altitude during RVSM cruise.
Verifies proper operation of the GFC 700 AFCS after maintenance.
Verifies the GFC 700 automatic pre-flight test and aural alert.
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