Home

Garmin Part 23 AML STC Cockpit Reference Guide

1. 62 XM Radio Page Optional 63 Position Reporting Page 65 Iridium Phone Page Optional 66 System Status Page 68 Flight Plan Group 69 Active Flight Plan Page 69 Viewing Your Active Flight Plan 69 Waypoint Information Page 70 Charts Page Optional 71 Chart Information
2. 80 Terrain SVT Alerts 81 Symbols 82 Map Page Symbols 82 SafeTaxi Symbols 83 Traffic Symbols 83 Terrain Obstacle Symbols 85 Map Toolbar Symbols 86 XM WX Weather Symbols and Product Age 87 Miscellaneous Symbols 88 1 G500 600 Cockpit Reference Guide 190 0060
3. 71 Selecting a Chart 71 Selecting Other Charts 72 Viewing Charts and Panning 72 Viewing Details of ChartView Charts 73 Setting Minimums 73 Changing Day Night View 73 Viewing NOTAMs ChartView Only 74 Alerts 75 On Screen Alerts 75 TAWS B Alerts
4. 29 Decluttering DCLTR the Map Pages 30 Split Screen Page Optional 34 Traffic Map Page Optional 35 Terrain TAWS B Page 41 viii G500 600 Cockpit Reference Guide 190 00601 03 Rev G TABLE OF CONTENTS TABLE OF CONTENTS Terrain Pop Up Alerts 43 WX Group 44 XM Weather Map Pages 44 Customizing the Weather Map 44 Changing Forecast Time
5. 17 Autopilot AP 19 GAD 43 Attitude 19 Heading 20 Altitude Capture Optional Upgrade 20 Autopilot Navigation 20 GPSS 21 Flight Director Display 22 Vertical Speed Control 22 Autopilot Mode Annunciations 23 Additional Features
6. 46 Changing Weather Altitude 46 Garmin Flight Data Services GFDS Map Pages 47 FIS B Weather Map Pages 49 Customizing the Weather Map 49 Weather Radar Optional 51 Weather Radar Map Page 51 Airborne Color Weather Radar 52 Aux Group 55 External Video Page Optional 55 System Setup Page 56 XM Information Page Optional
7. ii Introduction 1 Primary Flight Display PFD 2 Airspeed Tape 4 Altitude Tape 6 Barometric Pressure 6 Minimums Bug Barometric or Radar Altimeter 7 Altitude Bug 9 Fast Slow Indication 9 Wind Vectors 10 Vertical Speed V S 10
8. 24 Synthetic Vision Technology 24 Displaying SVT Terrain 25 Displaying Heading on the Horizon 25 Displaying Airport Signs 25 Multi Function Display MFD 26 Page Navigation Moving Between Pages 27 Changing Settings within a Page 27 Default Map Page 27 MFD Soft Key Map 28 Map Group 29 Navigation Map 1 and Navigation Map 2 Pages
9. ADS B and TCAS Status and Altitude Filter Selected Vector Motion and Duration Turn Cursor Knob for Next Target Map Orientation Range Rings Ownship Icon Range Ring Radius Basic Directional Traffic 4000 ft Below and Climbing Traffic Motion Vector NOTE ADS B targets will be shown as the filled in icon when they are within 6NM laterally and 1200 ft vertically of the ownship otherwise they are shown as the hollow icons 40 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE ADS B Target Selection Traffic targets displayed on the dedicated traffic page may be selected in order to obtain additional information about a traffic target 1 Press the small MFD knob to start target selection 2 Turn the small or large MFD knobs to step through selection of the available targets 3 Press the small MFD knob to stop target selection Press the DESELECT key to stop selection and or clear target selection ADS B Status ADS B Status displays the current status of traffic application Off Surface Airborne Fail Test or N A TAS TCAS TCAD Status This shows the current operating mode status of an interfaced TAS TCAS TCAD system STBY GND APR OPER or FAIL ADS B Motion Vector When Absolute Motion Vectors are selected the vectors extending from the traffic targets depict the target reported track and speed over the ground When Relative Motion
10. Display of External Video Source Map Display Current Video Source External Video 2 The External Video page will show the external video on the top half of the MFD and a Navigation Map will be shown on the lower half 35 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE Traffic Map Page Optional Soft Keys Found on Traffic Map Page OPERATE STANDBY MOTION ALT MODE DESELECT STANDBY ABSOLUTE RELATIVE OFF DURATION BACK BELOW NORMAL ABOVE UNRSTD OPR STBY Traffic Display When a traffic alert is generated by an interfaced traffic system the PFD will display a traffic annunciator and the MFD will have a pop up screen displaying the detected traffic if not viewing the Traffic page To remove the pop up press the CLR key Press the ENT key to go to the traffic page The traffic pop up window will be removed when the traffic alert is no longer active PFD Traffic Display MFD Traffic Pop Up Window Traffic Pop Up Traffic Traffic Annunciation 36 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE Displaying and Operating Traffic Advisory Systems TAS Traffic Advisory Off Scale Aircraft is Out of Range 1200 ft Above and Climbing Operating Mode Proximity Advisory Aircraft is 5000 ft Above and Descending Range Ring Non Threat Traffic Traffic Advisory 1200 ft Above and Climbing Ownship S
11. Alerts with multiple messages are configurable at installation and are installation dependent Alerts for the default configuration are indicated with asterisks 81 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Terrain SVT Alerts Alert Type PFD MFD Alert Annunciation Aural Message GPS signal re established None Terrain System Available Terrain System Test Successful None Terrain System test OK Terrain System Test in Progress None Terrain Alerting is disabled None No GPS position Excessively degraded GPS signal Terrain System Not Available Terrain SVT System Test Fail Terrain System Failure Alert Type PFD MFD Alert Annunciation Aural Message FLTA Terrain Caution RTC C ITI C Caution Terrain Terrain FLTA Terrain Caution RLC C ILI C Caution Wire Wire FLTA Terrain Warning RTC W ITI W Warning Terrain Terrain FLTA Terrain Warning RLC W ILI W Warning Wire Wire FLTA Obstacle Caution ROC C IOI C Caution Obstacle Obstacle FLTA Obstacle Warning ROC W IOI W Warning Obstacle Obstacle 82 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS Symbols Map Page Symbols Symbol Description Unknown Airport Non towered Non serviced Airport Towered Non serviced Airport Non towered Serviced Airport Towered Serviced Airport
12. Low Wing Prop High Wing Prop Jet Piston Rotorcraft Turbine Rotorcraft Default Map Cursor Measuring Cursor MFD Wind Vector w valid GPS solution Parallel Track Waypoint Restricted Prohibited Warning Alert TFR Temporary Flight Restrictions MOA Class B Airspace De Emphasized Smart Airspace Class C Airspace De Emphasized Smart Airspace Class D Airspace De Emphasized Smart Airspace Airspace Altitude Label Upper Lower Limits User Waypoint 2009 2015 Garmin Corporation Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 or 866 739 5687 Fax 913 397 8282 Garmin AT Inc 2345 Turner Rd SE Salem Oregon 97302 U S A Tel 503 581 8101 or 800 525 6726 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton SO40 9RB U K Tel 44 0 870 850 1243 Fax 44 0 238 052 4004 Garmin Corporation No 68 Jangshu 2nd Road Xizhi Dist New Taipei City 221 Taiwan R O C Tel 886 2 2642 9199 Fax 886 2 2642 9099 Garmin Singapore Pte Ltd 46 East Coast Road 05 06 Eastgate Singapore 428766 Tel 65 63480378 Fax 65 63480278 www garmin com Part Number 190 00601 03 Rev G
13. NOTAM Detail Select Header Plan Profile Minimums AUX continued AUX ALERTS TRND ACK CAPTURE BACK Iridium Phone Dial Hang Up Vol Keys 1234 5678 90 Answer Weather Map 1 Weather Map 2 Weather Map 3 Legend FCST Time XM WX Alt Dn WX Alt Up Weather Radar Mode Control Horizon Vertical Back WX Legend FCST Time XM WX Alt Dn WX Alt Up Legend FCST Time XM WX Alt Dn WX Alt Up DB ACTV DB SYNC LRU Wpt Info INFO MAP Rwy Freq APT DIR WX NOTAM Navigation Map 1 Declutter Map Traffic Topo Terrain Navigation Map 2 Declutter Map Traffic Topo Terrain Traffic View Inhibit Terrain 360 Arc Split Screen Declutter Map Traffic Topo Terrain MAP Softkeys depend on configuration 29 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP NAV PAGES Map Group Navigation Map 1 and Navigation Map 2 Pages Soft Keys Found on Navigation Map Pages Moving the Map Pointer Around the Map Panning NOTE Panning can be used in Terrain pages to view elevation levels 1 While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group press the small MFD knob A flashing arrow map pointer will appear in the center of the map page 2 Turn the large MFD knob to move the map pointer left and right horizontally 3 Turn the small MFD knob to move the map pointer up and down vertically
14. Soft Surface Serviced Airport Soft Surface Non serviced Airport Private Airport Heliport Intersection LOM compass locator at outer marker NDB Non directional Radio Beacon VOR VOR DME ILS DME or DME only VORTAC TACAN 83 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS SafeTaxi Symbols Symbol Description Helipad Airport Beacon Under Construction Zones Designated Water Areas Traffic Symbols TAS Symbol Description Other Traffic Proximity Advisory PA Traffic Advisory TA Traffic Advisory Off Scale TAS TCAS Traffic Symbols TIS Symbol Description Proximate Traffic other than TA traffic Traffic Advisory TA Traffic Advisory Off Scale TIS Traffic Symbols 84 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS Symbol Description Basic Non Directional Traffic White in Air Brown on Ground Basic Directional Traffic White in Air Brown on Ground Basic Off scale Selected Traffic Proximate Non Directional Traffic Proximate Directional Traffic Proximate Off scale Selected Traffic Non Directional Alerted Traffic Off Scale Non Directional Alerted Traffic Directional Alerted Traffic Off Scale Directional Alerted Traffic Non Directional Surface Vehicle Directional Surface Vehicle ADS B Traffic Symbols 85 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOL
15. ii consumable parts such as batteries unless product damage has occurred due to a defect in materials or workmanship iii damage caused by accident abuse misuse water flood fire or other acts of nature or external causes iv damage caused by service performed by anyone who is not an authorized service provider of Garmin or v damage to a product that has been modified or altered without the written permission of Garmin In addition Garmin reserves the right to refuse warranty claims against products or services that are obtained and or used in contravention of the laws of any country THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES WHETHER EXPRESS IMPLIED OR STATUTORY INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE STATUTORY OR OTHERWISE THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS WHICH MAY VARY FROM STATE TO STATE IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL SPECIAL INDIRECT OR CONSEQUENTIAL DAMAGES WHETHER RESULTING FROM THE USE MISUSE OR INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU Garmin retains the exclusive right to repair or replace with a new or newly overhauled replacement product the product or software or offer a full refund of the purchase price at its sole d
16. the Vertical Speed tape Current Vertical Speed Vertical Speed Bug Setting Vertical Speed Bug Vertical Speed Vertical Speed Warning Indication Vertical Speed Minimum Vertical Speed Maximum 11 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Vertical Deviation Indicator VDI The Vertical Deviation Indicator is displayed for ILS and GPS approaches with vertical guidance The GPS approach glidepath is shown in magenta G and indicator while the ILS approach glideslope is shown in green G and indicator GPS Approach Vertical Deviation Source Vertical Deviation Indicator ILS Approach Temperature Display The outside air temperature is displayed to the left of the HSI The air data computer calculates the temperature based on temperature probe and pitot static inputs The units C or F and temperature reference are selected on the AUX SYSTEM SETUP page The temperature reference can be selected to one of the following choices Static Air Temperature SAT This is the calculated temperature of the stationary static outside air Conceptually this is the temperature that would be read on a thermometer floating stationary at the current location Total Air Temperature TAT This is the calculated temperature of the outside air as it moves past the aircraft including the rise in temperature due to air compression
17. 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY CDI Source The CDI Source on the HSI will display which navigation source is selected Navigation sources available GPS1 VOR1 or LOC1 Navigation sources available GPS2 VOR2 or LOC2 if a second source is available GPS Mode The GPS Mode annunciation on the HSI indicates the current CDI scaling of the GPS navigator See the GPS navigator pilot s guide for a description of each mode GPS Advisory MSG Displays when a new advisory message is displayed on the GPS navigator LOI Loss of Integrity Displays when GPS integrity is lost Suspend OBS Displays when OBS mode is activated SUSP Displays when automatic waypoint sequencing on the interfaced GPS unit is suspended Marker Beacon Annunciations Marker Beacon Location Marker Beacon Location Marker Beacons Current Beacon Icon Standard Icon Blink Inner Marker Middle Marker Outer Marker 17 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Miscompare Annunciations For complete description and conditions of miscompare annunciations see the G500 600 Pilot s Guide P N 190 00601 02 Pitch and Roll Miscompare Pitch Miscompare Roll Miscompare Miscompare Annunciations 18 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Switching Betwee
18. 4 Press the small MFD knob again to exit panning mode Selecting Items on the Map 1 While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group while the map pointer is active move the map pointer to highlight a waypoint 2 Press ENT to display information about the highlighted waypoint 3 Press the INFO soft key if available to view more information about the highlighted waypoint 4 Press the WX soft key if available to view TAF and METAR information Press the small MFD knob again to return to the map Map Pointer 30 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP SETUP OPTIONS Decluttering DCLTR the Map Pages There are four levels of decluttering DCLTR DCLTR 1 DCLTR 2 and DCLTR 3 DCLTR shows the most detail while DCLTR 3 removes most detail While viewing Navigation Map 1 or Navigation Map 2 page of the Map Page Group press the DCLTR soft key Each successive press of the DCLTR soft key will toggle through the declutter levels Turning on Map Overlays While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group press the MAP soft key Select the Traffic TOPO or Terrain overlays by pressing the appropriate soft key Measuring Distances 1 While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group press MENU 2 Turn the large MFD knob or the small MFD knob to highlight Measure Bearing Distance and then
19. Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP IRIDIUM PHONE Creating Entries into Phonebook 1 While viewing the Iridium Phone page of the Aux Group press the small MFD knob to activate the cursor 2 Turn the large MFD knob to highlight the phonebook catalog icon Turn the small MFD knob to display phonebook 3 If the name already exists it will be displayed in the drop down menu If you are adding a new entry highlight New Entry Press ENT 4 Turn the small MFD knob to enter each letter of the name Press ENT 5 Turn the large MFD knob to move to enter the phone number Turn the small MFD to enter each number Press ENT Deleting Entries into Phonebook 1 Press the small MFD knob to activate the cursor and then turn the large MFD knob to select the Phone Book Catalog icon 2 Turn the small MFD knob to display the contents of the Phone Book Catalog and highlight the desired entry Press ENT to select the catalog entry 3 Turn the large MFD knob to highlight the DELETE key Press ENT to delete the catalog entry Press the small MFD knob again to cancel the selection cursor Editing a Phone Book Catalog Entry 1 Press the small MFD knob to activate the cursor and then turn the large MFD knob to select the Phone Book Catalog icon 2 Turn the small MFD knob to display the contents of the Phone Book Catalog and highlight the desired entry Press ENT to select the catalog entry 3 Us
20. Vectors are selected the vectors extending from the traffic targets display how the traffic target is moving relative to your aircraft These vectors are calculated using the traffic target s track and ground speed and your aircraft s track and ground speed These two values are combined to depict where the traffic target is moving purely with respect to your aircraft and give a forecast of where the traffic target will be relative to your aircraft in the near future NOTE Absolute motion vectors are the same color as the traffic target Relative motion vectors are yellow for TAs and otherwise are green The annunciation on the bottom of the dedicated traffic page indicates which vector type is selected and their length NOTE Relative motion vectors are not available on the ground 41 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP TERRAIN TAWS B PAGE MAP GROUP Terrain TAWS B Page Optional Soft Keys Found on Terrain TAWS B Page VIEW 360 ARC INHIBIT Garmin provides the following Terrain TAWS selections based upon your system configuration WARNING Do not use Terrain SVT information for primary terrain avoidance Terrain SVT is intended only to enhance situational awareness NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 North or 60 South NOTE Terrain SVT is standard when the Synthetic Vision Technology SVT option is installed The TAWS option will
21. Vertical Deviation Indicator VDI 11 Temperature Display 11 DME Indication 12 Clock Timer 12 Attitude Indicator 12 Horizontal Situation Indicator HSI Aircraft Heading 13 Adjusting the Course Pointer 14 HSI Bearing Pointers 14 Marker Beacon Annunciations 16 Miscompare Annunciations
22. adjust the tilt of the antenna up or down Monitor the displayed tilt value in the TILT field The range of tilting the antenna is DN 15 to UP 15 2 Press the small MFD knob to confirm selection 53 G600 Cockpit Reference Guide 190 00601 03 Rev F WX GROUP WX GROUP WEATHER RADAR Adjusting the Antenna Bearing 1 Press the small MFD knob and turn the large MFD knob to move to the BEARING field 2 Adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field The range of the bearing is R45 to L45 3 Press the ENT key to remove the cursor When scanning horizontally a bearing line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the CONTROL soft key 2 Press the BRG soft key Sector Scan GWX Radars Only 1 Press the small MFD knob and turn the large MFD knob to move to the SECTOR SCAN field 2 Turn the small MFD knob to select FULL 60 40 or 20 scan 3 If desired readjust the Bearing Line to change the center of the Sector Scan Turn the large MFD knob to move cursor to the BEARING field and turn the small MFD knob to adjust the line Adjusting Gain WARNING Changing the gain in Weather Mode Garmin GWX units only causes precipitation intensity to be displayed as a color not representative of the true intensity Remember to
23. an AOPA authorized representative has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you April 2015 Printed in the U S A i G500 600 Cockpit Reference Guide 190 00601 03 Rev G AVIATION LIMITED WARRANTY All Garmin avionics products are warranted to be free from defects in materials or workmanship for two years from the date of purchase for new Remote Mount and Panel Mount products one year from the date of purchase for new portable products and any purchased newly overhauled products six months for newly overhauled products exchanged through a Garmin Authorized Service Center and 90 days for factory repaired or newly overhauled products exchanged at Garmin in lieu of repair Within the applicable period Garmin will at its sole option repair or replace any components that fail in normal use Such repairs or replacement will be made at no charge to the customer for parts or labor provided that the customer shall be responsible for any transportation cost This warranty does not apply to i cosmetic damage such as scratches nicks and dents
24. and friction at the current airspeed Difference from International Standard Atmosphere ISA This is the difference between SAT and standard ISA temperature at the current altitude This provides an indication of how much warmer colder the temperature is from a standard atmosphere 12 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY DME Indication DME information is displayed in a window in the lower left corner of the PFD The distance to the station and the NAV source used are shown Selected DME DME Information Set Hold for Selected DME DME Hold Annunciation DME Indication Clock Timer The Clock Timer function displays a clock or timer window in the lower left corner of the PFD Show Hide Timer Show Hide Clock Select Clock Select Timer Start StopTimer Reset Timer Clock and Timer Functions Attitude Indicator The standby mechanical Attitude Indicator in your aircraft is either a Ground Pointer or a Roll Pointer configuration The GDU 620 Attitude Indicator has been configured in either a Ground Pointer or a Roll Pointer configuration to match the configuration of your aircraft s standby Attitude Indicator In an aircraft with an Attitude Indicator that has a Ground Pointer the pointer above the roll scale shifts with the roll or bank angle of the aircraft to keep the Roll Scale Zero Pointer pointing towards the grou
25. aviation database 13 Soft Key Labels Located on the bottom screen of the PFD and MFD Selection is done by pressing the corresponding soft key Soft keys that are available have the labels shown as white text on a black background Soft keys that are selected have the labels shown as black text on a gray background Soft keys that are unavailable have the labels shown as gray text on a black background 14 Horizontal Situation Indicator HSI Displays the Selected Heading Box Current Heading Turn Rate Markings and Heading Trend 15 Vertical Speed Tape Displays Vertical Speed and the Vertical Speed Bug 16 Barometric BARO Setting Displays the current setting of barometric pressure 17 Radar Altimeter Display Displays current height above ground from the radar altimeter Brown band in altitude tape represents the ground 18 Fast Slow Indicator See your AFM for details on operation 19 Roll Pointer and Slip Skid Indicator The slip skid indicator is the bar beneath the roll pointer The indicator moves with the roll pointer and laterally away from the pointer to indicate lateral acceleration slip skid 20 Altitude Tape Displays Current Altitude Altitude Trend Altitude Bug Altitude or Radar Altimeter Minimums Bug and BARO setting 21 Marker Beacon Marker Beacon Indicator 22 Clock or Timer window 4 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISP
26. be predicated upon the use of the terrain function The GDU 620 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness warning system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The Garmin GDU 620 has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the GDU 620 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING The altitude calculated by GPS receivers is geometric height above Mean Sea Level and could vary significantly f
27. change the display level value for which the display will automatically switch from Day Night brightness 5 Press the MFD knob to save the selected value 74 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP FPL GROUP CHARTS PAGE Viewing NOTAMs ChartView Only In the event there is an active NOTAM Notice to Airmen for a particular chart the NOTAM soft key will be available To view the information press the NOTAM soft key Charts Page 75 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Alerts Contact your Garmin dealer for service if any of the following alerts appear Refer to the Airplane Flight Manual and ADAS ETM documentation in the event that Engine Trend Monitor ETM alerts are displayed On Screen Alerts Alert Description ADC1 ALT EC ADC Altitude Error Correction is unavailable GDC is reporting that altitude correction is unavailable AHRS1 GPS AHRS 1 or AHRS 2 is not receiving any GPS information AHRS 1 or AHRS 2 is operating exclusively in no GPS mode AHRS 1 or AHRS 2 is using the backup GPS information AHRS1 2 SRVC AHRS1 or AHRS 2 magnetic field model needs update This appears on the ground only AHRS1 2 TAS AHRS1 or AHRS 2 is not receiving true airspeed from ADC ALT KEY INOP The ALT key is disabled ALT NO COMP No data from on or more altitude sensors ARINC 429 CONFIG ARINC 429 configuration error ARINC 708 CONFIG ARINC 70
28. for primary terrain avoidance Terrain SVT is intended only to enhance situational awareness CAUTION The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin GDU 620 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the GDU 620 can be misused or misinterpreted and therefore become unsafe CAUTION The Garmin GDU 620 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and pilot s authority to operate this device under FAA FCC regulations CAUTION The GDU 620 PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings NOTE Do not rely solely upon data link services to provide Temporary Flight Restriction TFR information Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control NOTE Inter
29. on GFDS and how to register see the latest revision of the G500 600 Pilot s Guide P N 190 00601 02 After registering you are able to display GFDS data 1 While viewing any one of the three pages of the WX Group press the MENU button 2 Highlight GFDS Data Request and press the ENT button to display the GFDS DATA REQUEST page 48 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP GFDS PAGES Coverage Area Coverage Area Distances Remaining FPL Next 50 NM Next 500 NM Width of Coverage 50 NM 500 NM Update Rate Off 60 Minutes Cancel Manual Request Status of Request Manual Request GFDS Data Request Page Configuring GFDS Data Request Page 1 Turn the large MFD knob to the Coverage box Press ENT to select or deselect the coverage areas Selected coverage areas are denoted by a green check mark 2 Turn the large MFD knob to the Auto Request box and press ENT to change the update rate to either OFF or ON 3 Turn the large MFD knob to the Manual Request box and press ENT to either send request or cancel current request 4 Press the small MFD knob to return to the GFDS page 49 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP FIS B WEATHER PAGES FIS B Weather Map Pages Soft Keys Found on FIS B Weather Map Pages LEGEND FCST TIME WX Alt Dn WX Alt Up NOTE The preferences set on FIS B Weather Map pages are unique to e
30. the previous page Displaying Heading on the Horizon 1 Press the PFD soft key 2 Press the SYN VIS soft key 3 If not already enabled press the SYN TERR soft key 4 Press the HRZN HDG soft key 5 Press the BACK soft key to return to the previous page Displaying Airport Signs 1 Press the PFD soft key 2 Press the SYN VIS soft key 3 If not already enabled press the SYN TERR soft key 4 Press the APTSIGNS soft key 5 Press the BACK soft key to return to the previous page 26 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MULTI FUNCTION DISPLAY MFD MULTI FUNCTION DISPLAY Multi Function Display MFD 1 2 3 4 5 6 7 Multi Function Display MFD NOTE In some models or installations the PFD and MFD and their controls are switched to the other side 1 Soft Keys 2 Large MFD knob Use to move between page groups 3 Small MFD knob Use to move within page groups 4 Enter Validates or confirms a menu selection or data entry 5 Clear Erases information cancels entries or removes page menus Pressing and holding the CLR key displays the first page of the Map Group 6 Menu Displays configuration items for each page of the page groups 7 Range Select Changes the range on the map pages Up arrow zooms out down arrow zooms in Also aids in scrolling up and down text pages 27 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MULTI FUNCTION DISPLAY MFD MULT
31. using the VS key on the PFD The vertical speed mode may be alternately engaged or disengaged by pressing and holding the VS key on the PFD bezel Engage Disengage VS Bug 23 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Autopilot Mode Annunciations Some autopilots support mode annunciations located at the top of the PFD Refer to the Airplane Flight Manual and autopilot system documentation for details on the autopilot mode annunciations When autopilot annunciations are displayed at the top of the PFD the Nav Status information will be located to the left of the HSI NAV STATUS Style 2 Active Mode Autopilot Status Armed Mode Active Mode Armed Mode Roll Modes Pitch Modes Autopilot Annunciations 24 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Additional Features Synthetic Vision Technology Synthetic Vision Technology SVT is offered as a feature to the G500 600 SVT is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilot s perspective SVT information is shown on the PFD SVT offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red Obstacle Zero Pitch Line SVT Soft Key
32. wind speed Selecting NAV Status Styles When selected Nav Status information is displayed on the PFD either on the top of the display Style 1 or to the left of the HSI Style 2 1 While viewing the System Setup page of the AUX page group press the small MFD knob to activate the cursor 2 Turn the large MFD knob to highlight the desired NAV Status value 3 Turn the small MFD knob to select the style and press ENT 58 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP SYSTEM SETUP PAGE Selecting Temperature Reference 1 While viewing the System Setup page of the AUX page group press the small MFD knob to activate the cursor Turn the large MFD knob to highlight the desired Temp Reference value 2 Turn the small MFD knob to select the Temp Reference type and press ENT Figure 3 44 Outside Air Temperature Selection Synchronization For Dual Installations Only NOTE The SYNCHRONIZATION option will only be available if a second GDU 620 is installed 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to the desired field in the SYNCHRONIZATION box 2 Turn the small MFD knob to turn ON or OFF synchronization of the CDI Turn the large MFD knob to move to the BARO setting Turn the small MFD knob to turn the synchronization of the barometer ON or OFF Turn the small MFD knob to turn the synchronization of data
33. 00 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP SETUP OPTIONS SafeTaxi Optional SafeTaxi is an enhanced feature that gives greater map detail when zooming in on airports at close range The airport display on the map reveals runways with numbers taxiways with identifying letters numbers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges When the aircraft location is within the screen boundary including within SafeTaxi ranges an airplane symbol is shown on the navigation map views for enhanced positional awareness This database is updated on a 56 day cycle NOTE Do not use SafeTaxi or ChartView functions as a basis for ground maneuvering SafeTaxi and ChartView functions have not been qualified to be used as an Airport Moving Map Display AMMD SafeTaxi and ChartView are intended to improve pilot situational awareness during ground operations and should only be used by the flight crew to orient themselves on the airport surface 34 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP SPLIT SCREEN PAGE Split Screen Page Optional Soft Keys Found on Split Screen Page External Video is an optional function that displays video provided by an externally mounted video source on the aircraft 1 While viewing the Map function turn the small MFD knob to the third page of the map group
34. 1 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Introduction This reference guide covers the operation of the GDU 620 as integrated in the G500 and G600 Avionics Display Systems The G500 and G600 Avionics Display Systems are avionics suites that combine primary flight instrumentation navigational information and a moving map all displayed on dual 6 5 inch color screens The G500 and G600 systems are 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 or 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 For more details on the G500 and G600 systems refer to the latest revision of the G500 600 Pilot s Guide P N 190 00601 02 PFD MFD NOTE In some models or installations the PFD and MFD and their controls are switched to the other side 2 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Primary Flight Display PFD 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 16 17 18 19 20 21 22 Primary Flight Display PFD 1 Airspeed Tape Displays Gro
35. 8 configuration error AUD NOT AVAIL Audio system is not available AUD SYS FAIL Audio system has failed CAL LOST Registry reports that the GDU 620 has lost calibration data CNFG MISMATCH GDU 1 2 airframe configuration settings disagree CNFG MODULE Failure of configuration module 76 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Alert Description DATALINK GDL 88 ADS B Failure Unable to transmit ADS B messages GDL 88 ADS B fault ADS B fault UAT receiver ADS B fault 1090 receiver GDL 88 needs service GDL 88 ADS B is not transmitting position Check GPS devices GDL 88 control panel input fault Check transponder mode GDL 88 ADS B fault Pressure altitude source inoperative GDL 88 external traffic system inoperative or connection lost GDL 88 configuration module needs service GDL 88 is inoperative or connection to GDU is lost GDL 88 CSA failure GDL 88 external traffic system has a low battery GDL 88 external traffic system in standby for more than 60 seconds DATA LOST Pilot stored data was lost Recheck data and settings DB ERR Database found on top card DB SYNC COMPLETE Database sync complete DB SYNC DISABLED No database card found to receive databases DB SYNC ERROR Not enough space to receive one or more databases DIAG MODE System is in Diagnostic Mode DSCRT CONFIG D
36. ADAR Airborne Color Weather Radar WARNING Begin transmitting only when it is safe to do so If transmitting on the ground is necessary ensure that no personnel or objects are within the minimum safe distance from the radar antenna For Garmin GWX radars the minimum safe distance may be up to 14 feet For 3rd party radars refer to the radar pilot s guide or other manufacturer documentation to determine the minimum safe dis tance CAUTION In Standby Mode the antenna is parked at the center line It is always recommended to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 Turn the large MFD knob to select the last page of the WX Page Group 2 Press the MODE soft key 3 If the aircraft is on the ground press the STANDBY soft key to initiate the warm up period After the warm up is complete the radar enters Standby Mode After the aircraft is airborne press the WEATHER soft key OR If the aircraft is already airborne press the WEATHER or GROUND soft key The warm up period is initiated after which the radar begins transmitting The horizontal scan is initially displayed Press the BACK soft key then the VERTICAL soft key to scan vertically 4 Press the RNG keys to select the desired range Adjusting Antenna Tilt 1 Press and turn the small MFD knob to
37. Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP XM WEATHER PAGES XM Weather Items WX Page Menu Weather Setup Menu Item Adjustment Map Orientation North Up Track Up NEXRAD Data Viewing Range Off 10 NM to 500 NM NEXRAD Legend On Off Source US Canada Echo Top Data Viewing Range Off 10 NM to 500 NM Cloud Top Data Viewing Range Off 10 NM to 500 NM Lightning Data Viewing Range Off 10 NM to 500 NM Cell Mov Data Viewing Range Off 10 NM to 500 NM SIG AIR Viewing Range Off 10 NM to 500 NM PIREPS Data Viewing Range Off 10 NM to 500 NM METAR Data Viewing Range Off 10 NM to 500 NM Surface Data Viewing Range Off 10 NM to 500 NM Frz Lvl Data Viewing Range Off 10 NM to 500 NM Wnds Aloft Data Viewing Range Off 10 NM to 500 NM County Data Viewing Range Off 10 NM to 500 NM TFR Data Viewing Range Off 10 NM to 500 NM AIREPS Data Viewing rnage Off 10 NM to 500 NM Icing Data Viewing Range Off 10 NM to 500 NM Turbulence Data Viewing Range Off 10 NM to 500 NM Cyclone Data Viewing Range Off 50 NM to 500 NM NOTE Due to similarities in color schemes it is not possible to display NEXRAD Data and Echo Top Data at the same time NOTE Due to similarities in color schemes it is not possible to display Echo Top Data and Cloud Top Data at the same time 46 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP XM WEATHER PAGES Weather Lege
38. ENT key TAWS B Pop Up Alert TAWS B alerts typically employ a CAUTION or a WARNING alert severity level or both When an alert is issued visual annunciations are displayed and aural alerts are simultaneously issued Refer to the Alerts section of this guide for more information on alerts both visual and aural When an alert is issued annunciations appear on the PFD and MFD TAWS page only If the TAWS B Page is not displayed at the time a pop up alert appears on the MFD To acknowledge the pop up alert and return to the currently viewed page press the CLR key To acknowledge the pop up alert and go to the TAWS B page press the ENT key 44 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP XM WEATHER PAGES WX Group XM Weather Map Pages Soft Keys Found on XM Weather Map Pages LEGEND FCST TIME WX Alt Dn WX Alt Up NOTE The preferences set on XM Weather Map pages are unique to each page Customizing the Weather Map 1 While viewing any of the XM Weather Map pages in the WX Page Group press the MENU key to display the page menu Press ENT 2 Turn the small MFD knob to select Weather Setup 1 or Weather Setup 2 and press ENT 3 Turn the large MFD knob to select desired item to change Turn the small MFD knob to set the preference of the weather feature option 4 Press ENT to confirm your selection 5 To return to the XM Weather Map page press the small MFD knob 45 G500 600
39. ERT Possible severe weather ahead WX RADAR Weather radar has failed WX RDR SERVICE Weather radar needs service WXR INPUT FAULT Weather radar is not receiving one or more inputs 80 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS TAWS B Alerts Alert Type PFD MFD Alert Annunciation Aural Message Excessive Descent Rate Warning EDR W Pull Up FLTA Terrain Warning RTC W ITI W Terrain Ahead Pull Up Terrain Ahead Pull Up or Terrain Terrain Pull Up Pull Up FLTA Obstacle Warning ROC W IOI W Obstacle Ahead Pull Up Obstacle Ahead Pull Up or Obstacle Obstacle Pull Up Pull Up FLTA Wire Warning ILI W RLC W Wire Ahead Pull Up Wire Ahead Pull Up or Wire Wire Pull Up Pull Up FLTA Terrain Caution RTC C ITI C Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain FLTA Obstacle Caution ROC C IOI C Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle FLTA Wire Caution ILI C RLC C Wire Ahead Wire Ahead or Caution Wire Caution Wire Premature Descent Alert Caution PDA Too Low Terrain Voice Callout VCO 500 None Five Hundred Excessive Descent Rate Caution EDR C Sink Rate Negative Climb Rate Caution NCR C Don t Sink or Too Low Terrain
40. FPL GROUP ACTIVE FLIGHT PLAN Flight Plan Group Active Flight Plan Page Soft Keys Found on Active Flight Plan Page Viewing Your Active Flight Plan The active flight plan as received from the active GPS unit is shown on the first page of the Flight Plan page group No changes to the flight plan can be made from the GDU 620 All flight plan changes must be made from the GPS unit Active Flight Plan Page 1 While viewing the Active Flight Plan page of the FPL Page Group press the small MFD knob and then turn the large MFD knob to highlight waypoints in the flight plan 2 Press the INFO soft key to view information about the highlighted waypoint 3 Press the small MFD knob to return to the Active Flight Plan page 70 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP FPL GROUP WAYPOINT INFO PAGE Waypoint Information Page Soft Keys Found on Waypoint Information Page WX NOTAM Facility Type Map Window Map Region Lat Lon Map Orientation Bearing amp Distance to Wpt from Present Position Info Map Soft Key Airport Directory Soft Key Facility Identifier Facility Name Facility Location Wpt Weather Info Soft Key Rwy Freq Soft Key Waypoint Information Page 1 While viewing the Waypoint Information page of the FPL Page Group press the small MFD knob and then turn the small MFD knobs to enter or select the waypoint You can also turn the small MFD knob counterclockwis
41. G500 600 Cockpit Reference Guide 2008 2015 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of system software version 7 00 or later Some differences in operation may be observed when comparing the information in this manual to later software versions Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton SO40 9RB U K Tel 44 0 870 850 1243 Fax 44 0 238 052 4004 Garmin Corporation No 68 Jangshu 2nd Road Xizhi Dist New Taipei City 221 Taiwan R O C Tel 886 02 2642 9199 Fax 886 02 2642 9099 www garmin com At Garmin we value your opinion For comments about this guide please e mail Techpubs Salem garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyr
42. I FUNCTION DISPLAY Page Navigation Moving Between Pages Page Group Turn Large MFD knob Page Turn Small MFD knob 1 Turn the large MFD knob to move between page groups 2 Turn the small MFD knob to change pages within the page group NOTE Page Group and Page are shown at the bottom of the MFD Changing Settings within a Page 1 Press the MENU key and make the necessary adjustments with the large MFD knob and small MFD knobs 2 Press the small MFD knob to activate editing 3 Turn the large MFD knob to select the desired item 4 Turn the small MFD knob to change the highlighted value 5 Press ENT to accept displayed value or press the small MFD knob to cancel selection or exit the editing mode Default Map Page Press and hold the CLR key to return to the first page of the MAP group 28 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MULTI FUNCTION DISPLAY MFD MULTI FUNCTION DISPLAY MFD Soft Key Map The soft keys available depend on the page displayed and the features available The soft key Alerts is present on the far right position on all MFD pages System Setup Default Unit RA Test Dflt Spd XM Info Lock XM Radio Channel CH CH DIR CH Category CAT CAT ALL Volume Mute Vol Vol Presets PS1 PS2 PS15 System Status Position Reporting Send FPL Active Fpl Info External Video Video 1 Video 2 Setup Charts
43. LAY Airspeed Tape The upper left portion of the PFD display provides Groundspeed Airspeed Trend Current Airspeed and True Airspeed information Current Airspeed is normally shown in white on the black pointer The Trend Indicator magenta line indicates what the airspeed will be in six seconds if the current acceleration is maintained If the current acceleration will cause the airspeed to exceed Vne in six seconds the airspeed is displayed in yellow If the current airspeed exceeds Vne the pointer changes to red with white text NOTE Airspeed tape markings are dependent upon configuration at the time of installation Reference the AFM or POH or latest revision of the G500 600 Pilot s Guide for more details Mmo Vmo Vne Vno Vfe Vs0 Vs1 Groundspeed Trend Indicator True Airspeed Current Airspeed Typical Airspeed Tape Markings Airspeed Tape Overspeed Overspeed Indication Additional Reference Markings VYSE VMCA White triangle See AFM POH Maximum speed with landing gear extended Reference Speeds 5 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY V speeds Glide Vr VX and VY default values are set during the installation process but can be changed and turned on off from the System Setup page on the first page of the Aux page group When active on the V speeds are displayed at their respective locations to th
44. ROUP SETUP OPTIONS Map Setup Options Group Selections MAP Orientation North Up Track Up DTK up HDG up North Up At Off to 500 NM Auto Zoom On or Off Land Data On or Off Track Vector Length Off to 20 mins Wind Vector On or Off Enhanced Range Ring On or Off Topo Data On or Off Topo Scale On or Off TERRAIN Data On or Off Obstacle Viewing Range Off to 15 NM Power Line Viewing Range Off to 15 NM Lat Lon Viewing Range Off to 500 NM Selected Alt Range Arc On or Off WEATHER NEXRAD Data Viewing Range Off to 500 NM NEXRAD Cell Movement On or Off NEXRAD Legend On or Off NEXRAD Source US or Canada XM Lightning Viewing Range Off to 500 NM TRAFFIC Traffic Mode Off All Traffic TA PA TA Only AVIATION SafeTaxi Viewing Range Range Off to 2 5 NM RWY Extension Range Range Off to 2 5 NM INT NDB Viewing Range Range Off to 15 NM VOR Viewing Range Range Off to 150 NM Class B TMA Range Off to 500 NM Class C TCA Range Off to 150 NM Class D Range Off to 150 NM Restricted Range Off to 150 NM MOA Military Range Off to 150 NM Other Adiz Range Off to 150 NM TFR Range Off to 500 NM Airways Off All LO Only HI Only Smart Airspace On or Off Show Airspaces All Below 18000ft Below 3000ft Airspace Labels On or Off 33 G5
45. S Terrain Obstacle Symbols Unlighted Obstacle Height is less than 1000 ft AGL Lighted Obstacle Height is less than 1000 ft AGL Unlighted Obstacle Height is greater than 1000 ft AGL Lighted Obstacle Height is greater than 1000 ft AGL Tower Windmill Grouped Obstacles Power Line The notes grouped obstacles NOTE Obstacles will be removed from the Terrain TAWS page when range RNG exceeds 10 nm Threat Location Unlighted Obstacle Projected Flight Path 1000 ft 100 ft Threshold Terrain more than 1000 ft below the aircraft altitude Black Terrain between 100 ft and 1000 ft below the aircraft altitude Yellow Terrain above or within 100 ft below the aircraft altitude Red Terrain Altitude Color Correlation 86 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS Map Toolbar Symbols Symbol Description Terrain Proximity Enabled and Available Indicator Terrain Proximity Enabled and Not Available Indicator Point Obstacle Enabled and Available Indicator Point Obstacle Enabled and Not Available Indicator Wire Obstacles Enabled and Available Indicator Wire Obstacles Enabled and Not Available Indicator StormScope StormScope Enabled and Not Available Indicator Traffic Enabled and Available Indicator Traffic Enabled and Not Available Indicator 87 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS XM W
46. X Weather Symbols and Product Age The broadcast rate represents the interval at which XM WX Satellite Radio broadcasts new signals that may or may not contain new weather data It does not represent the rate at which weather data is updated or new content is received by the Data Link Receiver Weather data is updated at intervals that are defined and controlled by XM WX Satellite Radio and its data vendors The product label in the legend will turn yellow at half the expiration time and grey when expired Expired products will not be shown on the display Weather Product Expiration Time Minutes NEXRAD NEXRAD and Echo Top are Mutually Exclusive 30 Echo Top Cloud Top and Echo Top Mutually Exclusive NEXRAD and Echo Top Mutually Exclusive 30 Cloud Top Cloud Top and Echo Top Mutually Exclusive 60 XM Lightning 30 Cell Movement 30 SIGMETs AIRMETs 60 METARs 90 City Forecast 90 Surface Analysis 60 Freezing Levels 120 Winds Aloft 90 County Warnings 60 PIREPS 90 TFRs 60 AIREPS 90 Icing 90 Turbulence 180 Cyclone Warnings 60 NOTE Product age is not displayed for individual reports of AIRMETs SIGMETs City Forecasts County Warnings Cell Movement and TFRs Product generation time is displayed for Freezing Level and Winds Aloft instead of valid time 88 G500 600 Cockpit Reference Guide 190 00601 03 Rev G SYMBOLS SYMBOLS Miscellaneous Symbols Symbol Description
47. ach page Customizing the Weather Map 1 While viewing any of the FIS B Weather Map pages in the FIS B Page Group press the MENU key to display the page menu 2 Turn the small MFD knob to select Weather Setup and press ENT 3 Turn the large MFD knob to select the desired item to change Turn the small MFD knob to set the preference of the weather feature option 4 Press ENT to confirm your selection 5 To return to the FIS B Weather Map page press the small MFD knob 50 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP FIS B WEATHER PAGES FIS B Weather Items WX Page Menu Weather Setup Menu Item Adjustment Map Orientation North Up Track Up NEXRAD Data Viewing Range Off 10 NM to 500 NM NEXRAD Legend On Off Source CONUS Regional Combined SIG AIR Viewing Range Off 10 NM to 500 NM PIREPS Data Viewing Range Off 10 NM to 500 NM METAR Data Viewing Range Off 10 NM to 500 NM Wnds Aloft Data Viewing Range Off 10 NM to 500 NM TFR Data Viewing Range Off 10 NM to 500 NM 51 G600 Cockpit Reference Guide 190 00601 03 Rev F WX GROUP WX GROUP WEATHER RADAR Weather Radar Optional Weather Radar Map Page Soft Keys Found on Weather Radar Map Page Weather Alert GWX only Control Window Operating Mode Operating Mode Precipitation Scale Weather Radar 52 G600 Cockpit Reference Guide 190 00601 03 Rev F WX GROUP WX GROUP WEATHER R
48. again to deactivate Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system automatically switches to Standby Mode Altitude Compensated Tilt ACT GWX 70 only Altitude Compensated Tilt ACT automatically adjusts the tilt to compensate for altitude changes as you climb or descend Turbulence Detection GWX 70 only optional Turbulence Detection activates a feature that detects and displays severe turbulence Turbulence Detection is inactive at ranges greater that 160 NM This optional feature requires a separate enablement See your dealer for details If Turbulence Detection is enabled and available Turbulence Detection will be reported as Inactive in any of the following conditions Scan orientation is not Horizontal Scan range is greater than 160 NM Radar mode is not Weather Ground Clutter Suppression GCS GWX 70 only optional Ground Clutter Suppression reduces the amount of returns as a result of highly reflective objects on the ground such as buildings or cities while maintaining the intensity and size of weather returns his optional feature requires a separate enablement See your dealer for details 55 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP SYSTEM SETUP PAGE AUX GROUP Aux Group External Video Page Optional Soft Key Found on External Video Page Setting Brightness Contrast and Saturation Levels T
49. bases ON or OFF 3 Press ENT to move to the DATE TIME box or press the small MFD knob to exit the editing mode Synchronization Option 59 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP SYSTEM SETUP PAGE AUX GROUP Setting Time Format 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob Turn the large MFD knob to the desired field in the DATE TIME box The only items that are able to be modified is the TIME FORMAT and TIME OFFSET The date and time are coordinated with the GPS 2 Turn the small MFD knob to display your choices of LOCAL 12hr LOCAL 24hr and UTC Universal Time Coordinated Turn the small MFD knob to the desired format and press ENT to confirm your selection Setting Time Offset 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob Turn the large MFD knob to the time offset portion of the DATE TIME box 2 Use the small MFD knob and large MFD knob to edit the time offset 3 Press ENT to confirm your selection Press the small MFD knob to exit the editing mode To convert UTC to local time a time offset must be chosen See the table below to determine the time offset Time Zone Standard Local Time Offset Daylight Saving Time Offset Atlantic 4 hours 3 hours Eastern 5 hours 4 hours Central 6 hours 5 hours Mountain 7 hours 6 hours Pacific 8 hours 7 hours Alaskan 9 hour
50. d then the CH or CH soft keys to increment up or down one channel at a time in the active category 5 Press CHNL and then the DIR CH soft key to directly select a channel in the active channel field Turn the small MFD knob and large MFD knob to select desired channel 6 Press ENT to save the selection or press the small MFD knob to cancel selection Selecting a Channel within a Category 1 Press CATGRY to highlight the category window 2 Press CAT or CAT to cycle through the different categories or turn the small MFD knob to the category and press ENT 3 Turn the small MFD knob to move to the desired channel 4 Press ENT to make that channel the active channel 5 Press the small MFD to end editing 64 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP XM RADIO PAGE Volume While viewing the XM Radio page of the Aux Group press the VOL soft key Press the VOL or VOL soft keys or turn the small MFD knob to increase or decrease radio volume Press the small MFD knob when done adjusting To mute the radio press the MUTE soft key To restore the radio volume press MUTE again or the VOL or VOL soft keys Storing a Preset Channel While viewing the XM Radio page you may set a preset for the Active Channel Press the PRESETS soft key Press and hold a preset soft key such as PS1 until it blinks You are able to preset up to 15 channels Recalling a Preset Channel While
51. de tape if the selected altitude bug is off of the tape Altitude Bug Altitude Bug Altitude Bug Setting The Altitude Bug provides visual and aural altitude alerting Aural alerting occurs within 200 feet or 1000 feet as configured of the Altitude Bug setting or when deviating beyond 200 feet of the bug Within 1000 ft Within 200 ft Deviation of 200ft Altitude Bug Indications Fast Slow Indication The Fast Slow indication from an external system may be optionally displayed on the left side of the PFD Refer to the Airplane Flight Manual for instructions on using the Fast Slow indications Pointer Fast Slow Scale Fast Slow Scale and Pointer 10 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Wind Vectors The PFD will display a Wind Vector Field to the left of the HSI when configured by the user There are four different styles of wind vector displays available Refer to the System Setup page in the AUX Group section of this guide for instructions on selecting wind vector style Wind Vectors can only be calculated when the aircraft is in the air Wind Vector Field Wind Vector Display Vertical Speed V S The Vertical Speed Tape and Vertical Speed Bug are displayed below the Altitude Tape For aircraft with vertical speed operating limitations red bands showing Vertical Speed Maximum and Minimum ranges will be shown on the left side of
52. e right of the airspeed scale Glide Reference Marker Vr Reference Marker Vx Reference Marker Vy Reference Marker Reference Speeds The labels for the reference markers may vary as configured during installation Reference Marker V1 Reference Marker Vr Reference Marker V2 Reference Marker Alternate Reference Speeds 6 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Altitude Tape The upper right portion of the PFD displays the Altitude Bug setting Current Altitude Altitude Trend Altitude Minimums Bug and the current BARO Setting The Altitude Trend indicates what the altitude will be in six seconds if the current vertical speed is maintained Altitude Bug Setting Altitude Trend BARO Setting Current Altitude Altitude Tape Altitude Bug Altitude Minimums Bug Barometric Pressure The Barometric Pressure BARO setting is displayed at the bottom of the altitude tape To change the BARO setting press the BARO key and turn the PFD knob to the desired pressure To select standard pressure 29 92in 1013 mb press the PFD knob To return to the previous setting press the PFD knob again 7 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Minimums Bug Barometric or Radar Altimeter For altitude awareness an Altitude Minimums Bug commonly referred to as the Minimums Bu
53. e the large MFD knob and small MFD knobs to make changes to the name or number Press ENT to save the changes Press the small MFD knob again to cancel the selection cursor Making a Phone Call 1 While viewing the Iridium Phone page enter a phone number using the KEYS soft key rotary knobs or select one from the Phone Book catalog 2 Press the DIAL key 3 After completing the call press the HANG UP key 68 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP SYSTEM STATUS PAGE System Status Page Soft Keys Found on System Status Page The System Status page of the AUX Page group shows the status serial number and version of LRUs as well as the effectivity information There are no menu options In the LRU Status column a green check means the unit is present and operating properly while a red X indicates an absence or failure System Status 1 While viewing the System Status page of the Aux Page Group press the DB ACTV soft key and turn the small MFD knob to view the list of the databases loaded into the GDU 620 Press the small MFD knob to exit 2 Press the DB SYNC soft key synchronize databases with a second LRU Press the small MFD knob to exit 3 Press the LRU soft key and turn the small MFD knob to scroll through the status serial number and version of each LRU Press the small MFD knob to exit 69 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP
54. e to obtain drop down menus for FPL Nearest and Recent 2 Press the RWY FREQ soft key to view runway and frequency information about the waypoint 3 Press the APT DIR soft key if available to view the airport directory information such as facility hours noise abatement pattern etc Press the small MFD knob and turn to scroll down the page if available 4 Press the WX or WX NOTAM soft key if available to view METARs TAFs or NOTAMs for the waypoint 71 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP FPL GROUP CHARTS PAGE Charts Page Optional Soft Keys Found on Charts Page Chart Information FliteCharts FliteCharts resemble the paper version of FAA published terminal procedures charts The charts are displayed with high resolution and in color for applicable charts The database contains procedure charts for the United States only This database is updated on a 28 day cycle FliteCharts is disabled 180 days after the expiration date and is no longer available for viewing upon reaching the disable date ChartView Optional with Enablement Card ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of approach charts and on airport diagrams ChartView requires an enablement card The ChartView database is updated
55. ference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 feet away from the source of the interference should alleviate the condition NOTE All visual depictions contained within this document including screen images of the GDU 620 bezel and displays are subject to change and may not reflect the most current GDU 620 system Depictions of equipment may differ slightly from the actual equipment v G500 600 Cockpit Reference Guide 190 00601 03 Rev G WARNINGS CAUTIONS AND NOTES WARNINGS CAUTIONS AND NOTES NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 North or 60 South NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Terrain SVT is standard when the Synthetic Vision Techno
56. g can be set the source of data for minimums alerting can be selected to either barometric altitude or radar altitude if installed When active and within 2500 feet of the selected minimums altitude the minimums bug setting is displayed to the bottom left of the altimeter When set a bug appears parked at the bottom of the altitude tape and moves up the tape as the set altitude comes into view When the aircraft altitude descends to within 2500 feet of the selected altitude minimums setting the minimums box appears with the altitude value in cyan text Once in range the Minimums Bug appears in cyan on the altitude tape A portion of the Minimums Bug will be displayed at the bottom of the altitude tape if the selected altitude minimums bug is off of the tape When the aircraft is within 100 feet of the selected altitude minimums setting the bug and the altitude text turn white Once the aircraft reaches the selected altitude minimums setting the bug and the altitude text turn yellow and the aural alert Minimums minimums is heard one time Minimums Annunciations using BARO for Source Minimums Box Minimums Bug Bug and text are cyan within 2500 ft Bug and text are white within 100 ft Bug and text are yellow when altitude reached Alerting is inhibited while the aircraft is on the ground and also if a value has been set for altitude alerting until the aircraft reaches 150 feet above the setting f
57. ger than one second the test will not run CAUTION Do not use the autopilot if the AP TEST key fails to disconnect the autopilot Autopilot Disconnect When the GDU 620 attitude monitors have detected an AHRS malfunction or the inability to actively monitor the AHRS a Check Attitude annunciation will be displayed on the PFD and the autopilot will automatically disconnect NOTE Only appears with the installation of an optional GAD 43 Adapter Check Attitude Annunciation 20 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Heading The GDU 620 heading bug may be used in conjunction with the Heading mode of supported autopilots When the autopilot is in heading mode and the heading bug is adjusted in the normal manner and the autopilot will turn to and maintain the selected heading Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot heading mode Selected Heading Box on HSI Altitude Capture Optional Upgrade Adjust the altitude bug in the normal manner when using the altitude capture interface Some autopilot installations support arming and disarming of the selected altitude using the ALT key on the PFD The PFD knob window will indicate when this function is available The selected altitude may be alternately armed or disarmed by pressing and holding the ALT key on the PFD beze
58. he desired field of the SYSTEM DISPLAY UNITS box 2 Turn the small MFD knob to display your choices of MAGNETIC or TRUE measurement for navigating Press ENT to confirm your selection and move to the next preference or press the small MFD knob to exit editing mode Setting Pressure Units 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to the desired field of the SYSTEM DISPLAY UNITS box 61 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP SYSTEM SETUP PAGE AUX GROUP 2 Turn the small MFD knob to display your choices of INCHES in or HECTOPASCALS hpa for your barometric pressure units Press ENT to confirm your selection and move to the next preference or press the small MFD knob to exit editing mode Setting Temperature Units 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to the desired field of the SYSTEM DISPLAY UNITS box 2 Turn the small MFD knob to display your choices of CELSIUS C or FAHRENHEIT F for the temperature Press ENT to confirm your selection and press the small MFD knob to exit editing mode Data Link 1 Press the small MFD knob and turn the large MFD knob to move to the Data Link box 2 Turn the small MFD knob to display your choices of the available WX TFR Source Press ENT to confirm your selection Press t
59. he following steps can be applied to either Video 1 or Video 2 1 While viewing the External Video Page of the Aux Page Group press the desired video soft key VIDEO 1 VIDEO 2 or FULL 2 Press the SETUP soft key The BRIGHTNESS in the CURRENT box will flash Turn the small MFD knob to change the brightness of the video output 3 Turn the large MFD knob to CONTRAST and turn the small MFD knob to change the contrast level of the video output 4 Turn the large MFD knob to SATURATION and turn the small MFD knob to change the saturation level of the video output 5 Press the small MFD knob to exit out of the setup mode Setting the Zoom Level of the Video Output 1 While viewing the External Video Page of the Aux Page Group press the small MFD knob 2 Press the RNG Range keys to zoom in and out The range of the zoom feature is 1x up to 10x 3 Press the small MFD knob to exit Video Soft Keys Setup Soft Key Full Soft Key 56 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP SYSTEM SETUP PAGE System Setup Page Soft Keys Found on System Setup Page Setting Brightness and Mode 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob The LEVEL in the DISPLAY BRIGHTNESS box will flash 2 Turn the small MFD knob to brighten or dim the display 3 Press ENT when you reach the desired level NOTE When LEVEL is changed the MODE defau
60. he small MFD knob to exit editing mode Radar Altimeter Test NOTE Not all radar altimeters have the test function Press the RA TEST soft key if available to activate the radar altimeter test An RA TEST annunciation will be displayed on the PFD For more information on the Radar Altimeter and its settings see the latest revision of the G500 600 Pilot s Guide P N 190 00601 02 RA TEST Annunciation on PFD If the unit fails the self test the RA FAIL annunciation will appear on the PFD RA FAIL Annunciation on PFD 62 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP XM RADIO PAGE XM Information Page Optional Soft Key Found on XM Information Page While viewing the Aux Group turn the small MFD knob to display the XM Information screen This page contains the Data Radio and Audio Radio IDs The only option on this page is to LOCK in your information once your subscription has been activated XM Information Page 63 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP XM RADIO PAGE AUX GROUP XM Radio Page Optional Soft Keys Found on XM Radio Page TO Selecting a Channel 1 While viewing the XM Radio page of the Aux Page Group press the small MFD knob and then turn the small MFD knob to highlight the desired channel 2 Press ENT to make the highlighted channel the Active Channel 3 Press the small MFD knob to end editing 4 Press CHNL an
61. ight notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin GDU 620 are trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc SkyWatch is a registered trademark of L 3 Avionics Systems and SiriusXM is a registered trademark of Sirius XM Radio Inc Iridium is a registered trademark of Iridium Communications Inc Canadian radar data provided by Environment Canada United States radar data provided by NOAA European radar data collected and provided by Meteo France AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fitness for a particular purpose The information is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances including negligence shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or
62. ing sent to the GDU PIT NO COMP No data from one or more pitch attitude sensors PREV EXCEED ADAS engine trend monitor is reporting a previous exceedence RADAR CONTROLS DISAGREE Data does not match for 15 seconds or more REGISTER GFDS Data services are inoperative GFDS is not registered ROL NO COMP No data from one or more roll attitude sensors RS 232 CONFIG RS 232 configuration error RS 485 CONFIG RS 485 configuration error 79 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Alert Description SIMULATOR Sim Mode is active Do not use for navigation STORMSCOPE Stormscope either reports a failure or has timed out SVT DISABLED Out of available terrain region Terrain DB resolution too low SW MISMATCH GDU software version strings to no match Xtalk is off TAWS External TAWS not available Internal TERRAIN SVT alerting enabled External TAWS configuration mismatch TDB Airframe does not support terrain database TERRAIN DSP Terrain awareness unavailable For configurations using TAWS B or TERRAIN SVT TRAFFIC CONFIG ADS B traffic data does not match configuration TRAFFIC FAIL Traffic device has failed Traffic data will no longer be displayed TRAFFIC STDBY Traffic device is in standby mode while airborne TRK LOST GPS1 TRK lost HSI defaulted to GPS2 TRK TRK TRAFFIC Heading lost Traffic is now based on track WX AL
63. iscrete output configuration error ENG SENSOR UNIT 1 2 Configuration error Communication with sensors is halted Communication with sensors lost FAN 1 2 FAIL Cooling fan 1 or 2 has failed ETM CAPTURE ADAS engine trend monitor is recording trend data ETM EXCEED ADAS engine trend monitor is reporting an exceedence or advisory condition 77 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Alert Description ETM FAULT ADAS engine trend monitor is reporting a system fault FAN 1 2 FAIL Cooling fan 1 2 has failed Unit may operate at extreme temperatures Extended operation at high temperatures is not recommended as damage to the GDU may occur PFD MFD coloration may be incorrect Backlight may dim to reduce power and heat GAD 43 Gyro Emulation Type Mismatch Fault Yaw Rate Scale Factor Mismatch Fault GDU AHRS Monitor Fault Pitch Deviation Fault Roll Deviation Fault Yaw Rate Deviation Fault AHRS A429 Attitude Timeout Fault AHRS A429 Attitude Invalid Fault AHRS Pitch Out of Range Fault AHRS Attitude Invalid Fault AHRS A429 Heading Timeout Fault AHRS A429 Heading Invalid Fault Reference Timeout Fault Application SCI Integrity Fault Configuration Integrity Fault AC Reference Lost Calibration Integrity Fault Unit Fault Power Supply Fault GAD 43 communication lost GAD 43E CONFIG GAD 43e configuration err
64. iscretion SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY Online Auction Purchases Products purchased through online auctions are not eligible for warranty coverage Online auction confirmations are not accepted for warranty verification To obtain warranty service an original or copy of the sales receipt from the original retailer is required Garmin will not replace missing components from any package purchased through an online auction International Purchases A separate warranty may be provided by international distributors for devices purchased outside the United States depending on the country If applicable this warranty is provided by the local in country distributor and this distributor provides local service for your device Distributor warranties are only valid in the area of intended distribution Devices purchased in the United States or Canada must be returned to the Garmin service center in the United Kingdom the United States Canada or Taiwan for service To obtain warranty service contact your local Garmin Authorized Service Center For assistance in locating a Service Center near you visit the Garmin web site at http www garmin com or contact Garmin Customer Service at 866 739 5687 ii G500 600 Cockpit Reference Guide 190 00601 03 Rev G WARNINGS CAUTIONS AND NOTES WARNINGS CAUTIONS AND NOTES Warnings Cautions amp Notes WARNING Navigation and terrain separation must NOT
65. l Arm Disarm Altitude Bug Autopilot Navigation The GDU 620 acts as a switching source between the installed navigation sources e g GPS VLOC 1 2 The navigation source that is displayed on the HSI is sent to the autopilot Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot navigation functions 1 Set your navigation source and HSI to the desired course 2 Engage your autopilot in navigation mode 3 Control your autopilot navigation through the navigation source and the HSI 21 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY GPSS The GDU 620 will send the GPSS commands from the displayed GPS source to the autopilot For example if GPS 1 is displayed on the HSI the GPSS commands from GPS 1 will be sent to the autopilot Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot s GPSS function NOTE GPSS commands are not sent to the autopilot when a VLOC source is displayed on the HSI In installations that use GPSS emulation in combination with the heading mode of the autopilot GPSS mode may be toggled on off with an external switch or by pressing and holding the HDG key on the PFD If the installation uses the HDG key on the PFD the PFD knob window will display the GPSS HDG mode options NOTE The GDU 620 has the ability to emu
66. late GPSS roll steering for autopilots that do not support GPSS The GDU 620 emulates GPSS by sending headings to the autopilot that guide turn anticipation GPSS OFF GPSS ON GPSS Mode Control When GPSS mode is on the heading bug on the HSI changes to a hollow outline and a crossed out heading bug appears in the PFD Knob Mode Indicator indicating that the autopilot is not coupled to the heading bug The bug is still controllable and may still be used by the pilot for reference GPSS is annunciated in the lower left portion of the PFD The GPSS mode annunciation depends on the location of the NAV STATUS information as shown in the following figure NAV Status Style 1 NAV Status Style 2 GPSS Mode Annunciations 22 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Flight Director Display Flight director commands are presented as a single cue flight director on the PFD SVT Off SVT On Flight Director Bars Showing Aircraft Pitch Vertical Speed Control The GDU 620 vertical speed bug may be used to control vertical speed with certain autopilots Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the vertical speed mode if available Adjust the vertical speed bug in the normal manner when using the vertical speed mode interface Some autopilot installations support engaging disengaging the vertical speed mode
67. logy SVT option is installed The TAWS option will take precedence over Terrain SVT NOTE Do not use SafeTaxi FliteCharts or Chartview functions as the basis for ground maneuvering SafeTaxi FliteCharts and Chartview functions have not been qualified to be used as an airport moving map display AMMD SafeTaxi FliteCharts and Chartview are intended to improve pilot situational awareness during ground operations and should only be used by the flight crew to orient themselves on the airport surface vi G500 600 Cockpit Reference Guide 190 00601 03 Rev G Record of Revisions Part Number Revision Date Description 190 00601 03 A B C D E F G 6 12 08 6 1 09 10 26 09 11 30 10 8 23 11 10 23 12 4 10 15 Production release Revision reflects functionality added with SW version 3 00 Added SVT TAWS B Terrain Proximity Wind Vectors Minimums Bug GAD 43 and Weather Radar information Updated subscription information for FliteCharts and ChartView Added changes to reflect v4 00 and v5 00 software changes Added changes to reflect v6 00 software changes Added changes to reflect v6 11 software changes Added changes to reflect software version 7 00 G500 and G600 CRG s are combined vii G500 600 Cockpit Reference Guide 190 00601 03 Rev G TABLE OF CONTENTS TABLE OF CONTENTS Contents Warnings Cautions amp Notes
68. lts to MANUAL If MODE is set the AUTO the LEVEL will adjust in response to ambient light or a lighting bus as configured during installation Setting Airspeed References 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob Turn the large MFD knob to move to the desired field in the AIRSPEEDS box 2 Turn the small MFD knob to change the speeds and to also turn the speeds ON or OFF When the speeds are turned ON they are shown near the bottom of the Airspeed Tape if airspeed is zero Airspeed References V Speed References on Airspeed Tape NOTE At any time during the setting of your airspeed references pressing the DFLT SPD soft key will restore the unit to its initial configuration 57 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP SYSTEM SETUP PAGE AUX GROUP Selecting Wind Vector Styles 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to the field in the PFD OPTIONS box 2 Turn the small MFD knob to select the styles available for displaying wind vectors Each style shows direction and velocity of the wind Style 1 Style 2 Style 3 Style 4 Style 1 Displays headwind and crosswind components Style 2 Displays total wind direction and speed Style 3 Displays total wind direction with headwind and crosswind speed components Style 4 Displays total wind direction in degrees with
69. n Navigation Sources GPS NAVIGATOR 2 VLOC NAVIGATOR 2 GPS NAVIGATOR 1 VLOC NAVIGATOR 1 CDI Sources The Course Deviation Indicator CDI can display two sources of navigation GPS or NAV VOR or LOC Press the CDI soft key to toggle between the available CDI modes GPS or VOR If a second GPS source or NAV source is available pressing the 1 2 soft key will toggle the navigation sources VOR1 and VOR2 or GPS1 and GPS2 NOTE Verify the navigation source by the indication on the HSI NOTE The selected navigator is the source for all PFD and MFD functions except for bearing pointers and external TAWS PFD annunciations 19 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Autopilot AP The G500 600 is able to interface to certain autopilot systems to provide the functions described in this section Please refer to your particular Airplane Flight Manual and autopilot documentation for specific information and operating instructions GAD 43 Attitude If the GAD 43 Adapter is providing attitude to the autopilot test the disconnect mechanism prior to each flight in the following manner 1 Allow all avionics to complete power up and begin normal operation 2 Engage the autopilot while on the ground 3 Press and release the AP TEST soft key and verify that the autopilot disconnects normally NOTE If the AP TEST soft key is held for lon
70. nd Roll Pointer Roll Scale Zero Pointer Roll Scale Attitude Indicator with a Ground Pointer Configuration in a Left Turn In an aircraft with an Attitude Indicator that has a Sky Pointer the pointer below the roll scale shifts with the roll or bank angle of the aircraft to keep the 13 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Roll Pointer pointing towards the sky Roll Scale Roll Scale Zero Pointer Roll Pointer Attitude Indicator with a Sky Pointer Configuration in a Left Turn The Slip Skid Indicator is the bar beneath the roll pointer The indicator moves with the roll pointer and moves laterally away from the pointer to indicate lateral acceleration Slip skid is indicated by the location of the bar relative to the pointer One bar displacement from the roll pointer is equivalent to one ball displacement on a traditional Slip Skid Indicator Slip Skid Indicator Roll Pointer Slip Skid Indicator Roll Scale Zero Horizontal Situation Indicator HSI Aircraft Heading The top of the HSI displays current heading current GPS track magenta diamond heading trend and turn rate markings The heading trend indicates the rate of turn Marking for rate of turn are provided at half standard 1 5 sec and standard 3 sec rate 14 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Cur
71. nd A mini legend can be displayed on the XM Weather Map page upper right hand corner for the weather products you selected in the setup menu To view a full page legend 1 While viewing any of XM Weather Map pages in the WX Page Group press the LEGEND soft key 2 Turn the small MFD knob or large MFD knob to view the entire legend 3 Exit and return to the map page by pressing either the LEGEND soft key ENT key or the small MFD knob Changing Forecast Time 1 When the Surface Data products Surface Analysis and City Forecasts are displayed the time period for these forecasts can be changed with the FCST TIME soft key 2 Press the FCST TIME soft key to cycle through the age of the information in 12 hour increments from CURRENT to 48 HR Changing Weather Altitude 1 When Winds Aloft Turbulence or Icing products are displayed the altitude for these forecasts can be selected with the WX Alt Up Dn soft keys 2 Press the WX Alt Dn or WX Alt Up soft keys to cycle through the available forecast periods as shown on the right side of the weather page Mini Legend 47 G500 600 Cockpit Reference Guide 190 00601 03 Rev G WX GROUP WX GROUP GFDS PAGES Garmin Flight Data Services GFDS Map Pages Soft Key Found on GFDS Weather Map Pages Requesting Garmin Flight Data Services GFDS Prior to requesting GFDS information an access code and system ID will need to be assigned For more information
72. on a 14 day cycle ChartView is disabled 70 days after the expiration date and is no longer available for viewing upon reaching the disable date Selecting a Chart 1 While viewing the Charts page of the FPL Page Group press the SELECT soft key to change the airport or chart 2 Turn the small and large MFD knobs to select the airport identifier and press ENT to accept the selected airport 3 Turn the large MFD knob to select the desired chart 4 Press ENT to display the desired chart NOTE The chart for the selected destination airport or approach is automatically loaded If no flight plan is entered the chart page will default to the nearest airport 72 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP FPL GROUP CHARTS PAGE Selecting Other Charts You are able to choose other charts to display based on your flight plan FPL charts of the nearest airport NRST or recently selected airports RECENT 1 While viewing the Charts page of the FPL Page Group press the SELECT soft key 2 Turn the small MFD knob counterclockwise 3 Turn the small MFD knob to show FPL NRST or RECENT 4 Turn the large MFD knob to highlight the desired airport then press ENT Display Charts From Flight Plan Display Charts Of Nearest Airport Display Charts From Recent Choices Viewing Charts and Panning 1 While viewing the Charts page of the FPL Page Group press the RNG Range keys to zoom in and
73. or Communication halted GATE MODE Automated testing is on GDL 69 GDL 69 69A has failed 78 G500 600 Cockpit Reference Guide 190 00601 03 Rev G ALERTS ALERTS Alert Description GEO LIMITS AHRS too far North South no magnetic compass GPS1 2 FAIL No GPS1 or GPS2 data is available GPS 1 2 PPS FAIL The PPS signal has not been received in more than 5 seconds GSR FAIL The GSR 56 has failed GWX CONFIG GWX configuration error Configuration service required GWX SERVICE GWX need service Return unit for repair HDG FAULT AHRS 1 magnetometer fault has occurred HDG LOST HDG features disabled or defaulted to GPS1 TRK HTAWS External HTAWS not available Internal TERRAIN HSVT alerting enabled External HTAWS configuration mismatch IAS NO COMP No data from one or more airspeed sensors lt LRU gt CONFIG Error in configuration of specific LRU where lt LRU gt denotes specific LRU lt LRU gt COOLING Specific LRU has poor cooling reducing power usage lt LRU gt DB ERR Database for specific LRU is corrupt lt LRU gt KEYSTK lt LRU gt lt KEY gt is stuck lt LRU gt SERVICE Specific LRU needs service lt LRU gt VOLTAGE lt LRU gt has low voltage reducing power usage MANIFEST GDU has received product data for an LRU that should have a manifest entry but is not in the manifest NAV1 2 FAIL No navigation receiver 1 or 2 data NO RADAR DATA No data is be
74. or the alert 8 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY To set the altitude for the Minimums Bug 1 While viewing the Active Flight Plan page of the FPL Group press the small MFD knob to activate the cursor and turn the large MFD knob to the Source selection 2 Turn the small MFD knob to select Off BARO or RAD ALT 3 Turn the large MFD knob to the ALTITUDE portion of the MINIMUMS section 4 Turn the small MFD knob to enter the desired altitude Press the ENT key to confirm selection 5 When finished press the small MFD knob to exit the MINIMUMS box The Minimums Bug can also be set from the Charts page of the FPL 1 While viewing the Charts page of the FPL Group press the MENU key and select Set Minimums from the Options menu 2 Turn the small MFD knob to select Off BARO or RAD ALT 3 Press the ENT key to move to enter altitude Turn the small MFD knob to enter the desired altitude Press the ENT key to confirm selection Brown band represents the ground Radar Altimeter Value Minimums Annunciations using RAD ALT for Source 9 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Altitude Bug The Altitude Bug is displayed on the Altitude Tape at the selected altitude bug setting A portion of the Altitude Bug will be displayed at the top or bottom of the altitu
75. out 2 Press the small MFD knob to enter the panning mode and activate scroll bars on the edges of the chart 3 Turn the large MFD knob to move around the chart horizontally and turn the small MFD knob to move vertically 4 Press the small MFD knob to cancel the scroll bars and exit panning 73 G500 600 Cockpit Reference Guide 190 00601 03 Rev G FPL GROUP FPL GROUP CHARTS PAGE Viewing Details of ChartView Charts 1 While viewing the Charts page of the FPL Page Group press the DETAIL soft key 2 Press the HEADER PLAN PROFILE or MINIMUMS soft keys to view detailed sections for the chart for those topics Setting Minimums 1 While viewing the Charts page of the FPL Page Group press the MENU key to display the Options menu and press ENT 2 Turn the small MFD knob to select the source BARO or RAD ALT Press the ENT key 3 Turn the small MFD knob to select the altitude Press ENT to set the altitude Changing Day Night View 1 While viewing the Charts page of the FPL Page Group press the MENU key to display the Options menu 2 Turn the small MFD knob to Chart Setup Press ENT The Color Scheme option will be highlighted 3 Turn the small MFD knob to select Day Auto Night Press the small MFD knob to save the selected value and return to the Charts page 4 If Auto is selected turn the large MFD knob to highlight the Display Level Brightness value Turn the small MFD knob to
76. press ENT 3 Turn the large or small MFD knobs to move the map pointer The distance bearing and coordinates are displayed at the top of the screen Distance Bearing and Coordinates Display Measuring Map Pointer 4 Press ENT to reset the distance and bearing values 5 Press the small MFD knob to stop measuring 31 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP SETUP OPTIONS Customizing Maps 1 While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group press the MENU key Map Setup Option Menu 2 Press the ENT key to enter the setup page The selected group will be flashing 3 Turn the small MFD knob to activate the drop down menu and to move within available groups Map Weather Traffic or Aviation Available Groups 4 Press the ENT key to select the group and set your preferences 5 Turn the large MFD knob to move between fields 6 Turn the small MFD knob to display available options Press the ENT key to select your preference and move to the next option 7 When completed with setting preferences press the small MFD knob to return to the Navigation Map 1 page 8 Repeat the above steps to set preferences for the remaining groups NOTE In the Map Options Setup section the selected range is defined as the map range below which the display feature will be visible 32 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP G
77. rent Heading Turn Rate Markings Heading Trend Current GPS Track HSI Heading Markings NOTE If magnetic heading is lost GPS ground track will be displayed in place of heading Adjusting the Course Pointer Press the CRS key and turn the PFD knob to select a course for a VOR ILS or OBS mode course HSI Bearing Pointers NOTE The Bearing Pointer for navigation source 1 BRG1 will be an arrow with a single line The Bearing Pointer for navigation source 2 BRG2 will be an arrow with a double line To toggle between the available bearing pointers press the PFD soft key then the BRG soft key and then the BRG1 or BRG2 soft keys The BRG1 soft key cycles through modes NAV1 and GPS1 Additionally ADF is available if an ADF source is installed The BRG2 soft key cycles through modes NAV2 and GPS2 if a second NAV or GPS source is available Additionally ADF is available if an ADF source is installed 15 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY Selected source for BRG 1 bearing pointer BRG2 Pointer BRG1 Pointer Selected source for BRG 2 bearing pointer Bearing Pointers on the HSI CDI Source GPS Mode GPS Advisory Suspend MSG LOI OBS SUSP GPS1 GPS2 VOR1 VOR2 LOC1 LOC2 OCN ENR TERM APR LNAV LNAV V LNAV VNAV LPV LP LP V 1 00nm 0 30nm LOI PFD HSI Annunciations 16 G500 600 Cockpit Reference Guide 190
78. return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Press the small MFD knob and turn the large MFD knob to move to the GAIN field 2 Turn the small MFD knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the ENT key to remove the cursor 4 To restore the gain to the calibrated position press the GAIN CAL soft key 54 G600 Cockpit Reference Guide 190 00601 03 Rev F WX GROUP WX GROUP WEATHER RADAR Antenna Stabilization 1 To activate or deactivate the antenna stabilization press the CONTROL soft key 2 Press the STAB ON soft key to activate antenna stabilization or press the STAB OFF soft key to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH GWX Weather Radar only WATCH Weather Attenuated Color Highlight which helps identify possible shadowing effects of short range cell activity identifying areas where radar return signals are weakened or attenuated by intense precipitation or large areas of lesser precipitation and may not fully reflect the storm behind the storm To activate the WATCH feature press the CONTROL soft key Press the WATCH soft key Press the WATCH soft key
79. roduct may be significantly older than the indicated weather product age WARNING For safety reasons GDU 620 operational procedures must be learned on the ground WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G500 600 Pilot s Guide Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G500 600 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING Exceeding 200 deg second in pitch or roll may invalidate AHRS attitude provided to the GDU 620 Exceeding 450 KIAS may invalidate ADC information provided to the GDU 620 WARNING Because of anomalies in the earth s magnetic field operating the G500 600 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude and between longitude 75 West and 120 West An area north of 70 North latitude and between longitude 85 East and 114 West An area south of 55 South latitude between longitude 120 East and 165 East iv G500 600 Cockpit Reference Guide 190 00601 03 Rev G WARNINGS CAUTIONS AND NOTES WARNINGS CAUTIONS AND NOTES WARNING Do not use Terrain SVT information
80. rom the altitude displayed by pressure altimeters such as the output from the GDC 74A B Air Data Computer or other pressure altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the GDU 620 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G500 or G600 system must be updated regularly in order to ensure that the information remains current Pilots using an outdated database do so entirely at their own risk iii G500 600 Cockpit Reference Guide 190 00601 03 Rev G WARNINGS CAUTIONS AND NOTES WARNINGS CAUTIONS AND NOTES WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the GDU 620 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather p
81. s Horizon Heading Mark SVT Terrain Flight Path Marker Airport Sign Terrain Threat Synthetic Vision Imagery NOTE SVT will become disabled if the databases necessary to display SVT are unavailable generating a GDU DB ERR or SVT DISABLED alert or AHRS or GPS data is unavailable SVT may be restored once the fail conditions are removed by following the steps in Displaying SVT Terrain 25 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY The following features are part of the Synthetic Vision Technology For more details refer to the G500 600 Pilot s Guide Rev G or later Flight Path Marker Airport Signs Horizon Heading Marks Runway Display Terrain Obstacle Display and Alerting Water Three dimensional Traffic Zero Pitch Line Wind Vectors Altitude Minimums Bug NOTE SVT may be deactivated under certain conditions such as loss of heading Once the condition is resolved SVT may restart automatically otherwise to reactivate SVT press the PFD soft key followed by the SYN VIS soft key then the SYN TERR soft key NOTE SVT features are not a substitute for standard course and altitude deviation information using the CDI VSI and VDI Displaying SVT Terrain 1 Press the PFD soft key 2 Press the SYN VIS soft key 3 Press the SYN TERR soft key 4 Press the BACK soft key to return to
82. s 8 hours Hawaiian 10 hours 9 hours 60 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP SYSTEM SETUP PAGE MFD Display Units NOTE At any time during the setting of your preferences pressing the DFLT UNIT soft key will restore the settings for brightness synchronization time format time offset and display units to the initial settings NOTE The corresponding GPS navigator must also be set to match the selection chosen distance speed NAV angle pressure and temperature units on the GDU 620 Setting Distance and Speed Units 1 Press the small MFD knob and turn the large MFD knob to move to the MFD DISPLAY UNITS box 2 Turn the small MFD knob to display your choices of IMPERIAL METRIC and NAUTICAL units for distance and speed displayed on MFD Press ENT to confirm your selection Press the small MFD knob to exit editing mode Setting Altitude and Vertical Speed Units 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to the desired field of the MFD DISPLAY UNITS box 2 Turn the small MFD knob to display your choices of FEET or METRIC units for altitude and vertical speed Press ENT to confirm your selection Press the small MFD knob to exit editing mode Setting Nav Angle 1 While viewing the System Setup Page of the Aux Page Group press the small MFD knob and turn the large MFD knob to move to t
83. tacles Wires will be removed from the Terrain TAWS page when range RNG exceeds 10 NM While viewing the Terrain TAWS B page of the Map Page Group press the VIEW soft key and then press the 360 or ARC soft keys to select the desired view 360 or ARC Soft Keys Pressing the INHIBIT soft key deactivates the PDA FLTA aural and visual alerts See AFMS for guidance on inhibiting TAWS Inhibit Soft Key Press MENU for selections to hide or show Aviation Data Overlay on the Terrain page NOTE Installations with a valid external TAWS B source will not display the INHIBIT key Aviation Data Overlay 43 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP TERRAIN TAWS B PAGE MAP GROUP Terrain Pop Up Alerts TERRAIN SVT Pop Up Alert on MFD TAWS B Pop Up Alert on MFD TERRAIN SVT Pop Up Alert TERRAIN SVT alerts typically employ a CAUTION or a WARNING alert severity level or both When an alert is issued visual annunciations are displayed and aural alerts are simultaneously issued Refer to the Alerts section of this guide for more information on alerts both visual and aural When an alert is issued annunciations appear on the PFD and MFD TAWS page only If the TERRAIN SVT Page is not displayed at the time a pop up alert appears on the MFD To acknowledge the pop up alert and return to the currently viewed page press the CLR key To acknowledge the pop up alert and go to the TERRAIN SVT page press the
84. take precedence over Terrain SVT NOTE TAWS alerts will be generated by the GPS TAWS unit on the PFD if an external TAWS unit is installed and interfaced to the G500 600 TERRAIN PROXIMITY is a non TSO C151b certified terrain awareness system Do not confuse Terrain Proximity with TAWS TAWS is TSO C151b certified and Terrain Proximity is not Terrain Proximity does not provide warning annunciations or voice alerts it only provides color indications on map displays when terrain and obstacles are within a certain altitude threshold from the aircraft TERRAIN SVT refers to a subset of Class B TAWS that meets the terrain alerting requirements outlined in Section 7 b of AC 23 26 Terrain SVT is a non TSO C151b certified terrain awareness system Do not confuse Terrain SVT with TAWS TAWS is TSO C151b certified and Terrain SVT is not Terrain SVT is a subset of Class B TAWS that provides a 42 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TERRAIN TAWS B PAGE Class B TAWS FLTA functionality including visual alerting and aural alerting Terrain SVT is provided with the Synthetic Vision functionality and not marketed separately Garmin Terrain SVT is available in GDU 620 v3 00 or later with SVT enabled TAWS B is an optional feature developed that meets the terrain alerting and ground proximity requirements for Class B TAWS system as defined in TSO C151b Viewing Terrain NOTE Obs
85. uide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE TIS Traffic The Traffic Map Page is configured to show surrounding TIS traffic data in relation to the aircraft s current position and altitude without clutter from the basemap Aircraft orientation on this map is always heading up unless there is no valid heading TIS receives traffic information from ground stations and is updated every five seconds The GDU 620 displays up to eight traffic targets within a 7 5 NM radius from 3000 feet below to 3500 feet above the requesting aircraft Displaying TIS Traffic While viewing the Traffic Page of the Map Page Group press the OPERATE soft key to begin displaying traffic TIS OPER is displayed in the upper left hand corner of the MFD NOTE TIS is disabled when a Traffic Advisory System TAS is installed Traffic Advisory Aircraft is 1200 feet above climbing and moving in the direction of the line Operating Mode Proximity Advisory Aircraft is 3000 feet above descending and moving in the direction of the line 39 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE ADS B Traffic Optional The ADS B traffic page provides an enhanced display of traffic from a compatible ADS B In system Available ADS B traffic features may include individual target selection and other details such as type direction groundspeed and motion Selected Traffic Info
86. undspeed GS Airspeed Trend Current Airspeed and True Airspeed TAS Markings dependent upon installation configuration 2 Wind Vector Displays direction and speed of wind 3 Heading Select Key Press HDG and turn PFD knob to set heading bug 4 Course Select Key Press CRS and turn PFD knob to set the course of the selected source VOR1 VOR2 GPS1 or GPS2 5 Altitude Select Key Press ALT and turn PFD knob to set altimeter bug 6 V S Vertical Speed Select Key Press V S and turn PFD knob to set V S bug 7 Barometer Select Key Press BARO and turn PFD knob to change barometric setting 3 G500 600 Cockpit Reference Guide 190 00601 03 Rev G PRIMARY FLIGHT DISPLAY PFD PRIMARY FLIGHT DISPLAY 8 Outside Air Temperature SAT TAT or ISA Displays the current outside air temperature 9 NAV Status Window NAV Style 2 Shown Displays which GPS is selected as the Active Source Active Waypoint WPT and Distance to Waypoint DIS NAV Style 1 Not Shown displays Active Source WPT DIS Desired Track DTK and Current Track TRK at top of screen 10 PFD Knob Turn PFD knob to change bug settings Heading Bug Course Altitude Bug V S Bug and Barometer setting 11 Soft Keys Used to select available options on PFD or MFD 12 SD Card Slots Upper and Lower The lower slot is used for the supplemental database card including aviation database updates The upper slot may be used to update the internal
87. viewing the XM Radio page press the PRESETS soft key and press the preset soft key for the desired stored channel such as PS1 To move to the next group of presets press the MORE soft key 65 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP POSITION REPORTING Position Reporting Page Soft Key Found on Position Reporting Page Position Reporting Page Position Reporting Status The Status window shows the time until the next data transmission and the status of the reporting system Settings Window 1 While viewing the Position Reporting page press the small MFD knob 2 Turn the large MFD knob to change the report type to either AFF Automatic Flight Following or Standard 66 G500 600 Cockpit Reference Guide 190 00601 03 Rev G AUX GROUP AUX GROUP IRIDIUM PHONE Iridium Phone Page Optional Soft Keys Found on Iridium Phone Page Volume Level Status Window Phonebook Catalog Icon Name and Phone Number Field Iridium Phone Page For detailed use of the Iridium Phone system see the latest revision of the G500 600 Pilot s Guide P N 190 00601 02 Call Suppression 1 While viewing the Iridium Phone page press the small MFD knob 2 Turn the large MFD knob to select the Call Suppression type of Off On or On During APR MAPR TERM The last setting will suppress call during approaches missed approaches or during terminal procedures 67 G500 600 Cockpit
88. ymbol Non Bearing Traffic System is Unable to Determine Bearing Aircraft Distance is 8 0 NM 1100 ft Above and Descending Traffic Map TAS NOTE Depending on your traffic configuration the OPERATE and STANDBY soft keys may not be available Traffic Mode Field Altitude Mode Field NOTE Some traffic systems will not enter standby mode while airborne 37 G500 600 Cockpit Reference Guide 190 00601 03 Rev G MAP GROUP MAP GROUP TRAFFIC PAGE Press the ALT MODE soft key to change what traffic is displayed Pressing the BELOW NORMAL ABOVE or UNRSTD soft keys will determine what traffic is displayed The selection is shown in the altitude mode field The values below define what each altitude mode displays relative to the altitude of the aircraft Soft Key Description BELOW Displays traffic from 9900 to 2700 ft NORMAL Displays traffic from 2700 to 2700 ft ABOVE Displays traffic from 2700 to 9900 ft UNRSTD All traffic is displayed unrestricted from 9900 ft TAS Test Mode On Ground 1 While viewing the Traffic Map Page of the Map Page Group press the MENU key and select Test Mode from the menu 2 Verify that a traffic message is shown next to the altitude tape on the PFD and that the traffic pop up is displayed on the MFD After a few seconds test mode is exited automatically by the traffic system Traffic Annunciation Traffic Annunciation on PFD 38 G500 600 Cockpit Reference G

Garmin Part 23 AML STC Cockpit Reference Guide

Contents

Download Pdf Manuals

Related Search

Related Contents