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Garmin G600 Pilot’s Guide
190-00601-02 Rev. E
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
•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)
1.1.1 Line 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.