Garmin G500 Pilots Guide - Page 18
Line Replaceable Units LRU - avionics suite
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Foreword System Sec 1 PFD Sec 2 MFD Sec 3 Features Avoidance Hazard • GNS 480, CNX80, GNS 400W series, or GNS 500W series GPS Navigator • Temperature Probe (such as the GTP 59) • GMU 44 Magnetometer • GTX 330/330D TIS-B Traffic (optional) • GDL 69A Satellite Data Link Receiver (optional) • SL30 NavCom (optional) • Autopilot/Flight Director (optional) • ADF (optional) • Traffic (optional: TAS and TIS) • Audio Panel (optional) • GAD 43 Adapter (optional) • GWX 68 Weather Radar (optional) 1.1.1 Line Replaceable Units (LRU) This guide covers the operation of the GDU 620 as integrated in the G500 system. The G500 Avionics Display System is an advanced technology 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 6.5 inch color screens. The G500 system is composed of sub-units or Line Replaceable Units (LRUs). LRUs have a modular design and can be installed directly behind the instrument panel or in a separate avionics bay if desired. This design greatly eases troubleshooting and maintenance of the G500 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. Sec 4 Additional Sec 5 & Alerts Annun. Sec 6 Symbols Sec 7 Appendix A Glossary Sec 8 Index Appendix B 1-2 Garmin G500 Pilot's Guide 190-01102-02 Rev. B