1-2Garmin G500H Pilot’s Guide 190-01150-02 Rev. JForewordSec 1SystemSec 2PFDSec 3MFDSec 4HazardAvoidanceSec 5AdditionalFeaturesSec 6Annun.& AlertsSec 7SymbolsSec 8GlossaryAppendix AAppendix BIndex• GNS 480, CNX80, GNS 400W series, GNS 500W series, GTN 600series, GTN 700 series, or a compatible GPS Navigator• Temperature Probe (such as the GTP 59)• GMU 44 Magnetometer• GEA 71 Engine/Airframe UnitInterfaces to various other aircraft systems and equipment are supported,including:• GAD 43/43e Adapter• GDL 69/69A Satellite Data Link Receiver• GDL 88H ADS-B Transceiver• GSR 56 Satellite Data Link Receiver• NavCom - Garmin GTR/GNC or SL30 COM/NAV radios, or selected 3rd-party radios• Autopilot/Flight Director• ADF• Garmin GTS or GTX traffic awareness systems, or selected 3rd partydevices• Audio Panel• Garmin GWX radar systems or selected 3rd party radars• Radar Altimeter• Video Sources• Stormscope®1.1.1 Standard System Line Replaceable Units (LRU)This guide covers the operation of the GDU 620 display as integrated inthe G500H system. The G500H Avionics Display System is an avionics suitedesigned to replace the traditional flight instrument cluster. The system combinesprimary flight instrumentation, navigational information, and a moving map alldisplayed on dual color screens. The G500H system is composed of sub-units orLine Replaceable Units (LRUs). LRUs have a modular design, which greatly easestroubleshooting and maintenance of the G500H system. A failure or problemcan be isolated to a particular LRU, which can be replaced quickly and easily.
