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Provides descriptions of all installed G1000 LRUs and associated components, including their functions and specifications.
Explains the multi-bus electrical system architecture post-STC installation, including power sources for equipment.
Provides an overview of the G1000 system's configuration mode for technicians, including its purpose and capabilities.
Details the process of loading G1000 software and configuration files, emphasizing the importance of correct part numbers.
Outlines the steps to start the G1000 system in configuration mode for initial setup and diagnostics.
Ensures compatibility between hardware part numbers and the G1000 system software image before installation.
Summarizes procedures for loading G1000 software and configuration files, serving as a central guide for maintenance.
Details the step-by-step process for loading system software and configuration files into the G1000 system.
Outlines the procedure for obtaining and loading various databases required for G1000 system functionality.
Defines operating limitations and maintenance requirements for continued airworthiness as per STC and applicable regulations.
Lists systems and items requiring tests or checks at specific intervals, aligned with existing inspection programs.
Details visual inspection procedures for G1000 equipment, checking for corrosion, damage, and proper attachment.
Outlines electrical bonding tests required for G1000-equipped aircraft, split into Phase 3 and Phase 4 tests.
Verifies primary and secondary power sources, data paths, and Ethernet connections for G1000 LRUs.
Verifies engine data availability and validity for ITT and torque, including test equipment and procedures.
Checks AHRS, airspeed, and altitude miscompare monitors to ensure proper system operation.
Explains system annunciations and failure indications, including invalid data fields and their common causes and solutions.
Provides troubleshooting guidance for TAWS annunciations, including causes and recommended solutions for system failures.
Addresses troubleshooting for SVS/Pathways software features, detailing symptoms and recommended actions for failures.
Focuses on troubleshooting the GFC 700 AFCS, highlighting key items for diagnosing faults within LRUs.
Covers general troubleshooting for AFCS annunciations and common AP DISC problems, with specific resolution steps.
Provides detailed removal and reinstallation procedures for GDU 1050A and GDU 1550 displays.
Provides removal and reinstallation procedures for the GIA 63W Integrated Avionics Units, including connector and rack checks.
Provides procedures for LRU replacement, configuration, and testing of GDU 1050A/1550 displays.
Details LRU replacement procedures and tests for the GMA 1347D Audio Panel.
Provides LRU replacement procedures and tests for GIA 63W Integrated Avionics Units.
Details LRU replacement procedures and tests for the GEA 71 Engine/Airframe Unit.
Provides LRU replacement procedures and tests for GTX transponders.
Details LRU replacement procedures and tests for GSU 75B ADAHRS units.
Provides LRU replacement procedures and air data tests for the GDC 7400 unit.
Details LRU replacement procedures and calibration for GRS 77/7800 AHRS and GMU 44 Magnetometer.
Outlines calibration procedures for GSU, GRS, and GMU units, including pitch/roll offset and magnetometer calibration.
Performs functional checks for TAWS-B and TAWS-A systems, including audio alerts and GPS signal verification.
Verifies correct LRU software part numbers and versions against the General Arrangement drawing after replacement.
Tests display failure conditions for MFD and PFD, verifying reversion mode and data retention.
Tests single and dual GPS failure conditions, verifying loss of signal and associated annunciations.
Details failure conditions for GIA 1, GIA 2, and dual GIA failures, outlining expected results and troubleshooting steps.
Verifies the proper operation of G1000 backup communication paths on PFD1, ensuring no system alert messages.
Verifies the proper operation of the GFC 700 AFCS after maintenance, including pre-flight tests and switch checks.
General| Manufacturer | Garmin |
|---|---|
| Display Type | LCD |
| Resolution | 1024 x 768 pixels (XGA) |
| Power Supply | 28 VDC |
| Operating Temperature | −20°C to +55°C |
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