Garmin G500 Manual
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Page 61
2-21190-01102-02 Rev. DGarmin G500 Pilot’s Guide ForewordSec 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 2.6.2 Turn Rate Indicator The Turn Rate Indicator is located directly above the rotating compass card. Tick marks to the left and right of the lubber line denote half-standard and standard turn rates. A magenta Turn Rate Trend Vector shows the current turn...
Page 62
2-22Garmin G500 Pilot’s Guide190-01102-02 Rev. D 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 NOTE: The ILS Localizer and Glideslope deviation indicators will indicate full-scale deflection for the GNS 480 navigator at the second dot. The GNS 400W/500W series navigators will indicate full-scale deflection at the edge of the display. 2.7.1 Changing CDI Sources The...
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2-23190-01102-02 Rev. DGarmin G500 Pilot’s Guide ForewordSec 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 1) Press the CDI soft key to toggle between GPS and VOR/LOC source type. 2) Press 1-2 soft key to toggle between the 1 and 2 navigators of the GPS or VOR/ LOC sources. 3) Verify the navigation source by the indication on the HSI and in the upper left corner of the PFD....
Page 64
2-24Garmin G500 Pilot’s Guide190-01102-02 Rev. D 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 2.7.3 Vertical Deviation Indicator (VDI) The Vertical Deviation (Glideslope) Indicator (VDI) appears to the left of the VSI whenever an ILS frequency is tuned in the active NAV field. A green diamond acts as the VDI Indicator, like a...
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2-25190-01102-02 Rev. DGarmin G500 Pilot’s Guide ForewordSec 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 2.7.4 Auto-Slewing The G500 system is designed to interface with GNS navigator units and also manage up to four different CDI course pointers (GPS1, NAV1, GPS2, NAV2) independently. The G500 will automatically slew the NAV course pointer to the correct final...
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2-26Garmin G500 Pilot’s Guide190-01102-02 Rev. D
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
Example of activating Auto-Slewing in the G500:
Course Pointer slewed to 218° for the ILS
Figure 2-33 Auto-Slewing HSI with ILS Loaded and Shown with the Corresponding
Approach Plate
1) The aircraft is flying vectors to final on an active ILS approach,...
Page 67
2-27190-01102-02 Rev. DGarmin G500 Pilot’s Guide
ForewordSec 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
Course Pointer slewed to 313° for the Backcourse
Figure 2-34 Auto-Slewing HSI with Localizer Backcourse Loaded and Shown with the
Corresponding Approach Plate
2.8 Supplemental Flight Data
2.8.1 Bearing Pointers
Two Bearing Pointers can be displayed on the HSI for NAV...
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2-28Garmin G500 Pilot’s Guide190-01102-02 Rev. D 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 • GPS is the bearing source and an active waypoint is not selected • ADF is selected and a signal is not received (if you have an ADF that supports a valid flag then the bearing pointer will be removed. If your ADF system does not include a valid flag then the bearing...
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2-29190-01102-02 Rev. DGarmin G500 Pilot’s Guide ForewordSec 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 2.8.2 Temperature Display The Outside Air Temperature (OAT) is displayed to the left of the HSI. The O AT can be displayed in ºF or ºC, which is configured in the Aux System Setup Page. The temperature is derived from the Temperature Probe on the aircraft. The...
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2-30Garmin G500 Pilot’s Guide190-01102-02 Rev. D 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 2.9 radar altimeter When an optional Radar Altimeter is installed, the altitude received from the radar altitude will be displayed on the PFD. NOTE: See the Radar Altimeter documentation for details on the radar altimeter performance and limitations....