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Garmin G600 Pilot’s Guide
190-00601-02 Rev. B
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
Navigator
•Temperature Probe (such as the GTP 59)
•GMU 44 Magnetometer
•GTX 330/330D Mode S Transponder (optional)
•GDL 69A Satellite Data Link Receiver (optional)
•SL30 NavCom (optional)
•Autopilot (optional)
•ADF (optional)
•Traffic (optional: TAS and TIS)
•Audio Panel (optional)
1.1.1 Line Replaceable Units (LRU)
This guide covers the operation of the GDU 620 as integrated in the G600
system. The G600 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” 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.