Pilot's Guide

1-2
Garmin G500H Pilot’s Guide
190-01150-02 Rev. F
Foreword
Sec 1
System
Sec 2
PFD
Sec 3
MFD
Sec 4
Hazard
Avoidance
Sec 5
Additional
Features
Sec 6
Annun.
& Alerts
Sec 7
Symbols
Sec 8
GlossaryAppendix A
Appendix B
Index
• Temperature Probe (such as the GTP 59)
• GMU 44 Magnetometer
• GDL 69/69A Satellite Data Link Receiver (optional)
• GSR 56 Satellite Data Link Receiver (optional)
• SL30 NavCom (optional)
• Autopilot/Flight Director (optional)
• ADF (optional)
• Garmin GTS or GTX traffic awareness systems, or selected 3rd party
devices (optional)
• Audio Panel (optional)
• GAD 43 Adapter (optional)
• Garmin GWX systems or selected 3rd party radar (optional)
1.1.1 Line Replaceable Units (LRU)
This guide covers the operation of the GDU 620 display as integrated in
the G500H system. The G500H Avionics Display System is an avionics suite
designed to replace the traditional flight instrument cluster. The system combines
primary flight instrumentation, navigational information, and a moving map all
displayed on dual color screens. The G500H system is composed of sub-units or
Line Replaceable Units (LRUs). LRUs have a modular design, which greatly eases
troubleshooting and maintenance of the G500H system. A failure or problem
can be isolated to a particular LRU, which can be replaced quickly and easily.
Each LRU has a particular function, or set of functions, that contributes to the
system’s operation.