Garmin G600 manual Line Replaceable Units LRU, Sec System

		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	Glossary
		Appendix A
	Appendix B	Index

•GNS 480, CNX80, GNS 400W series, or GNS 500W series, or a compatible GPS Navigator

•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)

1.1.1Line Replaceable Units (LRU)

This guide covers the operation of the GDU 620 display as integrated in the G600 system. The G600 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 G600 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 G600 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.

1-2 Garmin G600 Pilot’s Guide 190-00601-02 Rev. E