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Garmin Part 23 AML STC Cockpit Reference Guide

1. 6 PE LISTE TS SS ETSI I PR nih 6 Minimums Bug Barometric or Radar Altimeter outlets MT c M 9 Fast ore TC a E E eb te EUN OR ARR UD E 9 A DO aa aE E A ENE AO 10 Vertical Speed EN 10 Vertical Deviation Indicator VDI asissccosobeicei risate retta RV ERR E ER tke ar rbd 11 am eacus 11 ENEE 11 OR mde un icon fiteeccn tuned tse ects Ue 12 Horizontal Situation Indicator HSI Aircraft Headmg seen 13 Adjusting the Course eegene rm unes 14 VER E RUE I RI ROUES 14 Marker Beacon Annuncattons terere treten teinte nin 16 Di due ln El a a na 16 PNT ey 0 0 AP a er eee 18 EE 18 TR en en 19 Alude Care Opiional DOE ascensus 19 Autopilot Navigation nn 19 5 9 20 abr an db qr M ota 21 CSS eee ee nee ce 22 Autopilot Mode Annundatton nene tnnt 22 ee MER 23 Garmin Sel VISION Technology OPONA seca client eR n e etx Rn cde estu 23 Displaying Garmin SVT Terrain 24 Displaying Heading on the Horizon 24 K wierder 24 Multi Function Display MED 25 Page Navigation Moving Between Pages rennes 26 Changirig Settings ler E 26 MEETS Wiel D INO 26 MED SOR REDDERET a 0 2 Map CT OUT E 28 Navigation Map 1 and Navigation Map 2 Pages 28 Decluttering DCLTR the Map Pages 29 Split SEENEN 32 190 01102 03 Rev G G500 Cockpit Refer
2. SPLIT SCREE 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 32 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP Traffic Map Page Optional TRAFFIC MAP UU Soft Keys Found on Traffic Map Page Traffic Display When a traffic alert is generated by an interface traffic system the PFD will display a traffic annunciator and the MFD will have a pop up screen displaying the detected traffic 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CLR key Press the ENT key to go to the traffic page The traffic pop up window will be removed when the traffic alert is no longer active Traffic Annunciation Traffic DIS 285 NH DTK 187 E D a AUHS WEEE D Traffic Pop Up PFD Traffic Display MFD Traffic Pop Up Window 190 01102 03 Rev G G500 Cockpit Reference Guide 33 MAP GROUP GARMIN Displaying and Operating Traffic Advisory Systems TAS HDG UP TRAFFIC MAP UN FPL OOOO STANDBY Y ALT MODE Y ADVISORY Traffic Map TAS A NOTE Depending on your traffic configuration the OPERATE and STANDBY soft keys may not be available Traffic Mode Field Altitude Mode Field 34 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP Press the ALT MODE soft key to change what traffic is displayed Pressing the BELOW NORMAL ABOVE or UNREST soft keys will determine what traffic is
3. 3606 ke Pressing the INHIBIT soft key deactivates the TERRAIN SVT PDA FLTA aural and visual alerts ADVISORY Inhibit Soft Key Press MENU for selections to hide or show Aviation Data Overlay on the Terrain page Aviation Data Overlay 38 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP Terrain Pop Up Alerts TERRAIN SUT ADUISORY 6 HDG UP zb IBENIBDPPARK E PRESS ENT TRRN PAGE PRESS CLR PREV PAGE NAVIGATION MAP 1 TERRAIN SVT 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 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 ENT key 190 01102 03 Rev G G500 Cockpit Reference Guide 39 alt WE Kid j LL x mal c gt Gi m WX GROUP GARMIN WX Group XM Weather Map Pages AM WEATHER MAP 1 EO OLO AM WEATHER MAP 2 UNI AM WEATHER MAP 3 OUR Soft Keys Found on XM Weather Map Pages A NOTE The pr
4. 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 and turn the large MFD knob to move to the NAV Status field in the PFD OPTIONS box 2 Turn the small MFD knob to select the style and press ENT WIND VECTOR NAY STATUS 190 01102 03 Rev G G500 Cockpit Reference Guide 51 gt c 2 G ee c 2 Un Un ell LL S Un m c 0 V I G m UD er AUX GROUP GARMI N Synchronization For Dual Installations Only A 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 3 Press ENT to move to the DATE TIME box or press the small MFD knob to exit the editing mode SYNCHRONIZATION CDI BARO ON Synchronization Option LL S a D _ LL un Li mE un gt un A Ce OU Ge t 52 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H AUX GROUP Setting Time Format 1 While vie
5. 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 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 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN ______WARNINGS CAUTIONS AND NOTES eo A 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 weaher product Due to time delays inherent in gathering and processing weather data for data link weather product 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 operati
6. the NOTAM soft key will be available To view the information press the NOTAM soft key CATION BE ALERT TO RUNWAY CROSSING CLEARANCES AEALBACK OF ALL RUNWAY WA INSTRUCTIONS IS REQUIRED LL lt a un ec t J Charts Page 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 FPL GROUP A NOTE The chart for the selected destination airport or approach is automatically loaded If the destination airport is in the flight plan the chart page will default to the nearest airport 66 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN FPLGROUP Viewing Details of ChartView Charts 1 While view 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 An aircraft icon will show in the lower right corner of the display if your aircraft is in the chart area The icon will have an X through it if the aircraft is not in the chart area or the GPS fix is lost Selecting Other Charts You are able to choose other charts to display based on your flight plan FPL charts of the nearest airpo
7. 1 or AHRS 2 is operating exclusively in no GPS mode in no GPS mode AHRS 1 or AHRS 2 is using the AHRS 1 or AHRS 2 is using the backup GPS information GPS AHRS 1 or AHRS 2 is using the backup GPS information AHRS1 2 SRVC AHRS1 or AHRS 2 magnetic field model needs update This der on the groun GC ETM EXCEED ADAS engine trend monitor is reporting an exceedence or advisory condition ETM FAULT ADAS engine trend monitor is reporting a system fault 190 01102 03 Rev G G500 Cockpit Reference Guide 69 ALERTS GARMI H Description GAD 43 ont 70 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN ALERTS Alert Description IRUS CONFIG Error in configuration of specific LRU where lt LRU gt denotes specific LRU a manifest entry but is not in the manifest NAV1 2 FAIL PREV EXCEED ADAS engine trend monitor is reporting a previous exceedence RADAR CONTROLS DISAGREE Data does not match for 15 seconds or more SIMULATOR Sim Mode is active Do not use for navigation Out of available terrain region SVT DISABLED Terrain DB resolution too low SW MISMATCH GDU software version strings to no match Xtalk is off TDB Airframe does not support terrain database Terrain awareness unavailable For configurations using Lise TERRAIN SVT TRAFFIC FAIL TRF STBY TRK LOST WX ALERT 190 01102 03 Rev G G500 Cockpit Reference Guide 71 ALERTS GARMI H Terrain SVT Alerts Terrain DSP Terr
8. 190 01102 03 Rev G G500 Cockpit Reference Guide 41 A GARMIN Weather Legend 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 AM LTNG 3 Exit and return to the map page by pressing either the LEGEND soft key ENT key or the small MFD knob CELL MOV Displaying Surface Data and Winds Aloft While viewing any of the pages in the WX Page group if ud in the setup you chose to display SURFACE DATA VIEWING RANGE the SRFC TIME soft key will be available Pressing the SRFCTIME soft key will cycle through O the age of the information in 12 hour increments from CURRENT to 48 HR Mini Legend GFDS PAGES U While viewing any of the pages in the WX Page Group if in the setup you chose to display WINDS ALOFT DATA VIEWING RANGE the WIND DOWN and WIND E UP soft keys will be available To view winds aloft press the WIND DOWN or WIND UP soft keys to cycle through up or down the winds aloft altitudes GR OOO m m EOLO 42 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN Garmin Flight Data Services GFDS Map Pages GFDS WEATHER MAP 1 WX Bill GFDS WEATHER MAP 2 WH UBI GFDS WEATHER MAP 3 WH HOU Soft Key Fo
9. Fpl pt Info Charts U1234 5678 90 Info Rwy Freq NOTAM anes 8o S st E LES TRND ACK APTURE BACK Select Minimums MFD Soft Key Map 190 01102 03 Rev G G500 Cockpit Reference Guide 2 MAP GROUP GARMIN Map Group Navigation Map 1 and Navigation Map 2 Pages NAVIGATION MAP 1 UU NAVIGATION MAP 2 M DNI Soft Keys Found on Navigation Map Pages Moving the Map Pointer Around the Map Panning A 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 un be a o D SS Ld un A Ce OU a ei Map Pointer 3 Turn the small MFD knob to move the map pointer up and down vertically 4 Press the small MFD knob again to exit panning mode Selecting Items on the Map UBI 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 m
10. PFD GARMI N 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 A NOTE Airspeed tape markings are dependent upon configuration at the time of installation Reference the AFM POH or latest revision of the G500 Pilot s Guide for more details Groundspeed Mmo VMO VNE Trend Indicator VNO Current WE Airspeed Vs1 Vso True Airspeed Airspeed Tape Typical Airspeed Tape Markings r m EE e V se Maximum speed Vuen With landing gear extended Overspeed Indication Additional Reference Markings 4 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Reference Speeds V speeds Glide V V and V 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 the right of the airspeed scale o Glide Reference Marker Vr Reference Mark
11. aircraft latitude is greater than 75 North or 60 South NOTE Terrain SVT is standard when the Synthetic Vision Technology SVT option is installed NOTE Do not use SafeTaxi or ChartView functions as the basis for ground maneuvering SafeTaxi and ChartView functions do not comply with the requirements of AC 20 159 and are not qualified to be used as an airport moving map display AMMD SafeTaxi and ChartView are to be used by flight crew to orient themselves on the airport surface to improve pilot situational awareness during ground operations 190 01102 03 Rev G G500 Cockpit Reference Guide V A GARMIN Record of Revisions Part Number Revision Date Description 190 01102 03 5 28 09 6 18 09 10 26 09 11 30 10 8 23 11 2 14 12 12 21 12 vi G500 Cockpit Reference Guide Production Release Updated logo to meet guidelines and added Garmin to SVTTM Updated subscription information for FliteCharts and ChartView Added software version 4 00 and 5 00 functionality Added software version 6 00 functionality Minor edits Added software version 6 10 functionality 190 01102 03 Rev G GARMIN ___ TABLE OF CONTENTS Contents Warnings Cautions amp Notes 2ggesteseretus ebeket esgeebeggregE geesde ii modic ON raa E E EE A 1 Primary Flight Display PFD sin 2 D Ci P ER er a ee 4 PRICY VICE D M 5 RE
12. 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 the 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 o
13. anata 74 Terrain Obstacle Symbols EEN 15 Det ele ee AIDC CR 15 AMPAVX Weather Symbols and Product AG coire trim ture ethica dioe tet 76 SOS Eo CREE i vil G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN PRIMARY FLIGHT DISPLAY PFD Introduction This reference guide covers the operation of the GDU 620 as integrated in the G500 Avionics Display System The G500 Avionics Display System is an avionics suite that combines primary flight instrumentation navigational information and a moving map all displayed on dual 6 5 inch color screens The G500 system is composed of sub units or Line Replaceable Units LRUs LRUs have a modular design and can be installed directly behind the instrument panel or in a separate avionics bay if desired This design greatly eases troubleshooting and maintenance of the G500 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 systems operation For more details on the G500 system refer to the latest revision of the G500 Pilots Guide P N 190 01102 02 GARMIN PFD MFD A NOTE Certain G500s have the left side display configured as the MFD 190 01102 03 Rev G G500 Cockpit Reference Guide 1 PRIMARY FLIGHT DISPLAY PFD GARMI N Primary Flight Display PFD 2 gt ct a z e Bn TE gt Ce lt x Ce
14. as Primary Flight Display PFD Airspeed Tape Displays Groundspeed GS Airsoeed Trend Current Airspeed and True Airspeed TAS Markings dependent upon installation configuration Wind Vector Displays direction and speed of wind Outside Air Temperature OAT Displays the current outside air temperature 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 oS 9 9 X9 2 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Heading Select Key Press HDG and turn PFD knob to set heading bug Course Select Key Press CRS and turn PFD knob to set the course of the selected source VOR1 VOR2 GPS1 or GPS2 Altitude Select Key Press ALT and turn PFD knob to set altimeter bug V S Vertical Speed Select Key Press V S and turn PFD knob to set V S bug Barometer Select Key Press BARO and turn PFD knob to change barometric setting PFD Knob Turn PFD knob to change bug settings Heading Bug Course Altitude Bug V S Bug and Barometer setting Soft Keys Used to select available options on PFD or MFD SD Card Slots Upper and Lower The upper slot is used for updating databases or software the lower slot is for the database card Soft Key Labels Located on the bot
15. bug setting portion of the Altitude Bug will be displayed at the top or bottom of the altitude tape if the selected altitude bug is off of the tape Altitude Bug Setting Altitude Bug WU lage Altitude Bug 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 SE F Deviation of Within 1000 ft Within 200 ft 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 J I Ad mE Gi ebe Un J gt lt Pointer Fast Slow Scale Fast Slow Scale and Pointer 190 01102 03 Rev G G500 Cockpit Reference Guide 9 PRIMARY FLIGHT DISPLAY PFD GARMI N 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 Alt
16. 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 MED 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 f Auto is selected turn the large MFD knob to highlight the Display Level Brightness value Turn the small MFD knob to 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 Viewing Charts and Panning 1 While viewing the Charts page of the FPL Page Group press the RNG Range keys to zoom in and 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 190 01102 03 Rev G G500 Cockpit Reference Guide 65 m Gi eil c n CH gt un gt Gi m FPL GROUP GARMIN Viewing NOTAMS In the event there is an active NOTAM Notice to Airmen for a particular chart
17. 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 190 01102 03 Rev G G500 Cockpit Reference Guide A WARNINGS CAUTIONS AND NOTES GARMIN Warnings Cautions amp Notes WARNING Navigation and terrain separation must NOT 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 terrai
18. to 15 channels Recalling a Preset Channel While viewing the XM Radio page press the PRESETS soit key and press the wi preset soft key for the desired stored channel such as PS1 To move to the next group of presets press the MORE soft key ORT AUX GROUP POSITION R m ES m m m m m 58 G500 Cockpit Reference Guide 190 01102 03 Rev G A GARMIN Position Reporting Page POSITION REPORTING x HOOUOUEO Soft Key Found on Position Reporting Page POSITION REPORTING STATUS TIME UNTIL TRANSMIT REPORTING STATUS REPORTS IN QUEUE SETTINGS REPORT TYPE PERIOD POSITION REPORTING OOOOO8O at cum 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 Fight Following or Standard m m m m m Co m 190 01102 03 Rev G G500 Cockpit Reference Guide 59 A GARMIN Iridium amp Phone Page IRIDIUM PHONE MAP Wx guum Soft Keys Found on Iridium Phone Page IRIDIUM PHONE STATUS CALL TIME PHONE STATUS CALL SUPPRESSION Status Window PHONEBOOK NAME Phonebook PHONE NUMBER Catalog Icon Volume Level To IRIDIUM PHONE IX 1 OCDOOUUS DIA EN NBEN SENE ALERTS Iridium Phone Page For detailed use of the Iridium Phone sy
19. A GARMIN G500 Cockpit Reference Guide 2009 2012 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of system software version 6 10 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 040 9RB U K Tel 44 0 870 850 1243 Fax 44 0 238 052 4004 Garmin Corporation No 68 Zhangshu 2nd Road Xizhi Dist New Taipei City 221 Taiwan R O C Tel 886 02 2642 9199 Fax 886 02 2642 9099 Garmin Singapore Pte Ltd 46 East Coast Road 05 06 Eastgate Singapore 428766 Tel 65 3480378 Fax 65 63480278 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
20. Beacon Location Marker Beacons eise dn H Medea a a Miscompare Annunciations For complete description and conditions of miscompare annunciations see the G500 Pilots Guide P N 190 01102 02 gt ct B A e Bn SS TE gt Ce t Ce Pitch Miscompare Roll Miscompare Miscompare Annunciations 16 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Switching Between Navigation Sources ws wg y VLOC CDI gt NAVIGATOR 1 1 2 1 2 NE CE GPS L d VLOC WA NAVIGATOR 2 LCD gt NAVIGATOR 2 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 VORI and VOR2 or GPS1 and GPS2 J gt wd SA L G s Un J gt lt A NOTE Verify the navigation source by the indication on the HSI A NOTE The selected navigator is the source for all PFD and MFD functions except for bearing pointers and external TAWS PFD annunciations 190 01102 03 Rev G G500 Cockpit Reference Guide 17 PRIMARY FLIGHT DISPLAY PFD GARMI H Autopilot AP The G500 is able to interface to certain autopilot systems to provi
21. FF 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 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 LIL lt a D m LL un e LL be un gt un A Ce OU us t DEL Dt 48 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H AUX GROUP Aux Group External Video Page Optional EXTERNAL VIDEO AUX EO OODD Soft Keys Found on System Setup Page Setting Brightness Contrast and Saturation Levels The 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 or VIDEO 2 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 v
22. LIGHT DISPLAY PFD GARMI N 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 aircrafts 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 ground G500 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 Roll Pointer pointing towards the sky Roll Scale Zero Pointer gt lt Ae A c Bn ee TE gt c E cc e Roll Scale i G500 Attitude Indicator with a Sky Pointer Configuration in a Left Turn 12 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD 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 displacemen
23. O soft key to view information about the highlighted waypoint 3 Press the small MFD knob to return to the Active Flight Plan page 190 01102 03 Rev G G500 Cockpit Reference Guide 63 FPL GROUP GARMIN Waypoint Information Page Soft Keys Found on Waypoint Information Page WAYPOINT INFORMATION UN TUS IDENT FACILITY CITY fw m P l DO AURORA PAUL 3 in fa po Pd GE 219 WOODBURN b MOLALLA GERVA ROK MOUNT ANGEL HAVER HOBGU WAYPOINT INFORMATION maA IT WW ADVISORY Waypoint Information Page 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 counterclockwise to obtain drop down menus for FPL Nearest and Recent Press the RWY FREQ soft key to view runway and frequency information about the waypoint 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 to scroll down the page Press the WX soft key if available to view METARS or TAFs for the waypoint G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN FPLGROUP Charts Page Optional Soft Keys Found on Charts Page CHARTS Setting Minimums 1 While viewing the Charts page of the FPL Page Group MENU key to display the Options menu and press ENT 2 Turn the small MFD
24. S source is available Additionally ADF is available if an ADF source is installed c 2c J Bearing 2 YE Pointer gt mE GPS Level SS Current Navigation of Service et Source Bearing 1 Pointer Eel Bearing 1 Se Source Bearing 2 Bearing 1 Bearing 2 Source Pointer Icon Pointer Icon Bearing Pointers on the HSI 14 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD OCN GE ENR GPS2 TERM VOR1 APR VOR2 LNAV LOC LNAV V LOC2 LNAVIVNAV LPV LP MSG OBS LOI SUSP PFD HSI Annunciations CDI Source The CDI Source on the HSI will display which navigation source is selected Navigation sources available GPS1 VOR1 or LOCT Navigation sources available GPS2 VOR2 or LOC2 if a second source is available GPS Mode The GPS Mode annunciation on the HSI will be the same as what is annunciated on the interfaced GPS unit See the GPS GNS Pilots Guide for a description of each mode GPS Advisory MSG Displays when a new advisory message is displayed on the GNS LOI Loss of Integrity Displays when GPS integrity is lost J gt we lt SA C lis mr un J gt lt Suspend OBS Displays when OBS mode is activated SUSP Displays when automatic waypoint sequencing on the interfaced GPS unit is suspended 190 01102 03 Rev G G500 Cockpit Reference Guide 15 GARMIN Marker Beacon Annunciations Marker Beacon Location Marker
25. TION 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 display 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 display using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION When interfaced with a GSR 56 Iridium transceiver only one SD card may be present in the GDU 620 and it must be the lower slot CAUTION Garmin would like to remind pilots flying with GDL 69 69A equipped aircraft that TFRs are only advisory and are not a replacement for thorough preflight briefing on TFR times
26. Viewing Range Off to 50 nm e Lat Lon Viewing Range Off to 2500 nm e Field of View On or Off e NEXRAD Data Viewing Range Off to 2000 nm e NEXRAD Cell Movement Range Off to 2000 nu A NEXRAD Legend e XM Lightning Viewing Range Off to 2000 nm Traffic Mode Off All Traffic TA PA TA Only SafeTaxi Viewing Range Range Off to 10 Nm e RWY Extension Range Range Off to 10 Nm e INT NDB Viewing Range Range Off to 50 Nu e VOR Viewing Range Range Off to 500 Nm e Class B TMA Range Off to 2000 nm e Class C TCA Range Off to 500 nm dei e Class D Range Off to 500 Nm e Restricted Range Off to 500 uv e MOA Military Range Off to 500 uv e Other Adiz Range Off to 500 nm e TFR Range Off to 2500 nm MAP gt 0 G d c n un m EH c 0 O lt un e Airways Off All LO Only HI Only 190 01102 03 Rev G G500 Cockpit Reference Guide 3 TT z Q c TY TY Ce O Vi T am Vi a o Ce da ef ct MAP GROUP GARMI N Split Screen Page Optional SPLIT SCREEN UO8O0 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 aircratt 1 While viewing the Map function turn the small MFD knob to the third page of the map group Display of External Video Source ss TRACK UP A D NEWBERG TFR ln Vu WOODBURN NEON Gm Ze Map Display
27. 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 50 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 discretion SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY Online Auction Purchases Products purchased through
28. ain awareness display unavailable D SVT System Test Dem Terrain System Failure FLTA Terrain Warning TERRAIN Warning Terrain Terrain FLTA Obstacle Caution OBSTACLE Caution Obstacle Obstacle FLTA Obstacle Warning OBSTACLE Warning Obstacle Obstacle 72 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN SYMBOLS Symbols Map Page Symbols ry Description Non towered Non serviced Airport o Set Towered Non serviced Airport 0 Non towered Serviced Airport 0 Towered Serviced Airport O O aseene 8 emn EN EN NAMEN Intersection LOM compass locator at outer marker NDB Non directional Radio Beacon Un lt UJ r N 190 01102 03 Rev G G500 Cockpit Reference Guide 73 SYMBOLS GARMIN SafeTaxi Symbols Symbol Description LS Under Construction Zones Unpaved Unpaved Parkinge Areas Traffic Symbols Description Highest to Lowest Priority mu Traffic Advisory TA In Range E M Traffic Advisory TA Out of Range Symbol un r o EC gt un Proximity Advisory PA NM Other Traffic 74 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN SYMBOLS Terrain Obstacle Symbols Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less Height is greater Height is greater 1000 AGL than 1000 AGL than 1000 AGL than 1000 AGL RASE AAA EEE NOTE Obstacles wil
29. already enabled press the SYN TERR soft key IB WwW Press the APTSIGNS soft key Press the BACK soft key to return to the previous page UJI 24 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N MULTI FUNCTION DISPLAY MFD Multi Function Display MFD TERRAIN ETE 1000rr M j NAVIGATION HAP 1 DCLTR HAP ALERTS OOO 000 OO G 6 O Multi Function Display MFD A NOTE Certain G500s have the left side display configured as the MFD 3 c D c c un J gt lt Page Group Position 9 Enter 2 Page Group Clear Page Labels 1 Menu 2 SD Card Slots 2 Range Select 5 Soft Key Labels 3 Map Scale 6 Soft Keys Map Orientation D Large MFD Knob Select Page Group 15 Wind Vector Small MFD Knob Select Page 190 01102 03 Rev G G500 Cockpit Reference Guide 25 MULTI FUNCTION DISPLAY MFD GARMI H Page Navigation Moving Between Pages MAP Bill Page Group Page Turn Large MFD knob 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 A 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 Press the small MFD knob to activate editing Turn the large MFD knob to select the desired item Turn t
30. and locations Always confirm TFR data through official sources and contact your Flight Service Station FSS for interpretation of TFR data NOTE Interference 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 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN ______WARNINGS CAUTIONS AND NOTES NOTE All visual depictions contained within this document including screen images of the G500 bezel displays are subject to change and may not reflect the most current G500 system Depictions of equipment may differ slightly from the actual equipment 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 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
31. ap 28 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP 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 VIN 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 e 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 press ENT 3 Turn the large MFD knob or small MFD knob to move the map pointer The distance bearing and coordinates are displayed at the top of the screen SNOILdO dfil3S dNOd Distance Bearing and Coordinates Display Measuring Map Pointer 4 Press ENT to reset the distance and bearing values 5 Press the small MED knob to stop measuring 190 01102 03 Rev G G500 Cockpit Reference Guide 29 un ef le ef Lid un E Ce OU ef E UBI MAP GROUP GARMIN Customizing Maps 1 While viewing Navigation Map 1 or Nav
32. channel at a time in the active category 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 p W RY eS e UT En Press ENT to save the selection or press the small MFD knob to cancel selection gt c ae G ow c Ay un mt un WI AL 4 c Un ES gt G m 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 Turn the small MFD knob to move to the desired channel LA 4 Press ENT to make that channel the active channel Press the small MFD to end editing COBOOUD Ul 190 01102 03 Rev G G500 Cockpit Reference Guide 57 A GARMIN Volume While viewing the XM Radio page of the Aux Group press the VOL soft key Press the VOL4 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 soit key Press and hold a preset soft key such as PS1 until it Sch blinks You are able to preset up
33. ctor 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 gt c Gi sd lo c U m ES LL ed c gt z mi o WARNING Changing the gain in Weather Mode GWX 68 only causes precipitation intensity to be displayed as a color not representative of the MX true intensity Remember to return the gain setting to Calibrated for a viewing the actual intensity of precipitation 1 Press the small MED knob and turn the large MED knob to move to the GAIN field 2 Turn the small MED 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 V 3 Press the ENT key to remove the cursor UOUUUUG 4 To restore the gain to the calibrated position press the GAIN CAL soft key 190 01102 03 Rev G G500 Cockpit Reference Guide 47 AUX GROUP GARMI N 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 O
34. de 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 It 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 soit key and verity that the autopilot disconnects normally NOTE If the AP TEST soft key is held for longer than one second the test will not run 4 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 D will be displayed on the PFD and the autopilot will automatically disconnect RIMARY FLIGHT DISPLAY o NOTE Only appears with the installation of an optional GAD 43 Adapter Check Attitude Annunciation 18 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Heading Ihe 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
35. 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 9700 to 2700 ft NORMAL Displays traffic from 2700 to 2700 ft ABOVE Displays traffic from 2700 to 9700 ft UNREST All traffic is displayed unrestricted from 9700 ft A NOTE Some traffic systems will not enter standby mode while airborne 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 Verity 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 gt J Gi Ad c d j oe gt T1 E A m gt Gi m Traffic Annunciation on PFD 190 01102 03 Rev G G500 Cockpit Reference Guide 35 MAP GROUP GARMIN TIS Traffic The Traffic Map Page is configured to show surrounding TIS traffic data in relation to the aircrafts 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
36. ditions are removed by following the steps in Displaying SVT Terrain 190 01102 03 Rev G G500 Cockpit Reference Guide 23 gt ct n A e SS TE gt Ce t Ce as PRIMARY FLIGHT DISPLAY PFD GARMI H The following features are part of the Synthetic Vision Technology For more details refer to the G500 Pilots Guide Rev C or later e Flight Path Marker Airport Signs Horizon Heading Marks e Runway Display e Terrain Obstacle Display and Alerting Water e Three dimensional Traffic e Zero Pitch Line e Wind Vectors e Altitude Minimums Bug A NOTE SVT may be deactivated under certain conditions such as loss of heading Once condition is resolved 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 Garmin SVT Terrain Press the PFD soft key Press the SYN VIS soft key Press the SYN TERR soft key Press the BACK soft key to return to the previous page 2 3 4 Displaying Heading on the Horizon Press the PFD soft key Press the SYN VIS soft key 3 lf not already enabled press the SYN TERR soft key Press the HRZN HDG soft key 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 lf not
37. e 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 autopilots 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 emulate 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 HOLD FOR HDG BUG EX P HOLD HOG FOR GPSS HDG EA A GPSS OFF GPSS ON GPSS Mode Control gt St e H CO el Bn ebe TE gt Ce E Ce e H 20 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD 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 port
38. eferences 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 Turn the large MFD knob to Weather Setup Press ENT 2 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 3 Press ENT to confirm your selection 4 Toreturn to the XM Weather Map page press the small MFD knob un LE a Ce LE lt x LE Dei A Ce OU P E oO Es m Oo oO EOLO 40 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN WXxGRouP XM Weather Items WX Page Menu Weather Setup Menu Item Selections Available Frz Lvl Data Viewing Range Off 50 NM to 2000 NM Winds Aloft Data Viewing Range Off 50 NM to 2000 NM Current 12 HR 24 HR 36 HR and Surface Data Time A8 up Winds Aloft Altitude Surface 3000 FT to 42000 FT County Data Viewing Range Off 50 NM to 2000 NM Cydone Data Viewing Range Off 50 NM to 2000 NM on c e c My 2A S gt L LL EM m gt Gi A un A NOTE Due to similarities in color schemes it is not possible to display NEXRAD Data and Echo Top Data at the same time UU A NOTE Due to similarities in color schemes it is not possible to display Echo Top Data and Cloud Top Data at the same time ERES SE aM SEREG
39. ence Guide vii I LO r rmi um m e Ki r rr Ki un un ew E LA ben a OQ V LL O LA aad E me TABLE OF CONTENTS GARMI N Tatie Map Page Optional RR eR 33 cg GE 3 PO E A saan seanceaeeuee 39 MK OUD RER RC RER ee 40 ES OT 40 CUSTOMIZING EEN 40 Displaying Surface Data and Winds Aloft 42 Garmin Flight Data Services GFDS Map Pages 43 Weather Radar Optional in 45 Weamer Radar Map PUE eee RE rtt tcp mde itr etnies E iub eps IUE 45 Aname Color Weather an ne Era I Ea HR Rm 46 ipe cir Met ee one 49 BER OR Page OPa EE 49 SO 50 XM Information Page Optional seen 56 AN RER 57 giu B Iv RIRs c 29 TUS TI CBE E 60 Ecc sae he te E E 62 GE Plan GORE a a te nou 63 EE a Tr iU gd ET 63 Viewing Tour Mr E un 63 p ers Du A I D ONE OT 64 CO PO nesoetea A A eeeeiee cers 65 SA a a 65 Changing Day Night View 65 Viewing Char ana uttter toe tta mena E otn tute ec setae rtm tesa Peau 65 ro Ii CIE cT Ur 66 Danis A 66 Viewing Details of ChartViewTM Charts nente trennen 67 su netur RAI c PER Om Umm 67 EECHER 68 Dil ES O A A A AAA E AT EET 69 Bi Ee GE 69 OS NETS 72 up mec 13 ys eR es raj Siac cere T 13 BEER 74 AC een LOS MEM T
40. er Vx Reference Marker Vy Reference Marker Reference Speeds The labels for the reference markers may vary as configured during installation a Reference Marker Ski V2 Reference Marker ARMIS V1 Reference Marker Alternate Reference Speeds J gt d Ul Cc lis un J gt lt 190 01102 03 Rev G G500 Cockpit Reference Guide 5 gt et e H A el Bn TE gt Ce Ce e H PRIMARY FLIGHT DISPLAY PFD GARMI N 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 Bug Altitude Trend Current Altitude Altitude Minimums Bug BARO Setting Altitude Tape 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 6 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Minimums Bug Barometric or Radar Altimeter For altitude awareness an Altitude Minimums Bug commonl
41. ey 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 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 46 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H AUX GROUP 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 Se
42. f the SYSTEM DISPLAY UNITS box Ld lt ER Li x A Oe T x lt lt x LL EL BE CT LT LI LI 54 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H AUX GROUP 2 Turn the small MFD knob to display your choices of INCHES In or HECTOPASCALS kPa 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 MED 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 Radar Altimeter Test A 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 Pilots Guide P N 190 01102 02 gt gt lt CY ES My x aad gt RA TEST m gt CY m WE RA TEST Annunciation on PFD If the unit fails the self test the RA FAIL annunciation will appear on the PED RA FAIL Annunciation on PFD ERIGE GERERE 190 01102 03 Re
43. for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and GDU 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 Communications and Sirius and XM are trademarks of Sirius XM Radio Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively AODA 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 an AOPA authorized representative has been advised of the possibility of such damages User agrees not t
44. hat are able to be modified STATUS SERIAL NUMBER VERSION AVIATION REGION AVIATION CYCLE AVIATION EFFECTIVE AVIATION EXPIRES AIRPORT DIRECTORY REGION AIRPORT DIRECTORY CYCLE AIRPORT DIRECTORY EFFECTIVE AIRPORT DIRECTORY EXPIRES SYSTEM STATUS ER OOU D E BOO DBASE ALERTS System Status Page 1 While viewing the System Status page of the Aux Page Group press the LRU soft key and turn the small MED knob to scroll through the status serial number and version of each LRU Press the small MFD knob to exit 2 Press the DBASE 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 62 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN FPLGROUP Flight Plan Group Active Flight Plan Page ACTIVE FLIGHT PLAN Soft Keys Found on Active Flight Plan Page Viewing Your Active Flight Plan The active flight plan as received from the active GNS 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 GNS unit MINIMUMS SOURCE ALTITUDE ACTIVE LEG INFO ACTIVE LEG ESA ROUTE ESA FS EE d FLIGHT PLAN PLAN Active ae os 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 INF
45. he small MFD knob to change the highlighted value Ke W RY 00 NANA NA NA UJI Press ENT to accept displayed value or press the small MFD knob to cancel selection or exit the editing mode gt t l a A el e um UJ lt E zT Default Map Page Press and hold the CLR key to return to the first page of the MAP group 26 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N MULTI FUNCTION DISPLAY MFD 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 avMap1 NavMap2 Split Screen Traffic Terrain Standby Dedutter Dedutter emm Operate View Map Map Map Alt Mod 360 Traffic Traffic Traffic t Mode Arc Topo Topo Topo Below Inhibit Terrain Terrain Terrain Normal Above ES Unrest GFDS Nem Map 1 GFDS Wee Map 2 GFDS Weck i Map3 Wx Radar XM Weather 1 XMWeather2 XM Weather 3 E Legend Lp Legend Legend Control SRFC Time XM Wind Down Horizon Vertical Wind Up Back Video 1 l CH CAT Mute P5 Video 2 RA Test CH CAT Vol pS Setup Dflt Spd DIR CH ALL Vol External System F Info XM dio Video Setup Zi besse E Default Unit Channel Category Volume Presets PS15 3 c D c c A I un Y gt lt continued System Status Position Reporting Iridium Phone a Send ei Up DBASE i Active
46. ideo 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 Pa ge 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 gt c 2 G ee c 2 Un Un _ LL S Un m c m m gt G m BRIGHTNESS CONTRAST Setup Soft Key SATURATION Video Soft Keys Z N zf EO AUX BOooooo Y VIDEO 2 Y y ALERTS External Video Setup Umm 190 01102 03 Rev G G500 Cockpit Reference Guide 49 AUX GROUP GARMIN System Setup Page SYSTEM SETUP A Wn 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 defaults 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 Set
47. igation Map 2 of the Map Page Group press the MENU key The option Map Setup will flash PAGE MENU OPTIONS Press the MFD knob to return to base page 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 the Navigation Map 1 page 8 Repeat the above steps to set preferences for the remaining groups A NOTE In the Map Options Setup section the selected range is defined as the map range below which the display feature will be visible 30 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP Map Setup Options Group Selections Orientation North Up Track Up DTK up HDG up e North Up At Off to 2500 nm e Auto Zoom On or Off e Land Data On or Off Track Vector Length Off to 20 mins e Wind Vector On or Off Nav Range Ring On or Off Topo Data On or Off Topo Scale On or Off e TERRAIN Data On or Off TERRAIN Scale On or Off e Obstacle
48. ion 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 Flight Director Display Flight director commands are presented as a single cue flight director on the FFD Q x SVT Off SVT On Flight Director Bars Showing Aircraft Pitch 190 01102 03 Rev G G500 Cockpit Reference Guide 21 J gt d mE C s mr un J gt lt gt ct E a e Bn TE gt Ce lt x Ce as PRIMARY FLIGHT DISPLAY PFD GARMI N 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 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 HOLD HOLD TO DISENG TO ENGAGE a EIS MEA Engage Disengage VS Bug 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 de
49. itude Tape For aircraft with vertical speed operating limitations red bands showing gt lt x E 2 e Gd Vertical Speed Maximum and Minimum ranges will be shown on the left side of U the Vertical Speed tape Li gt cc Vertical Speed ES GH Vertical See mW Speed Bug Current Vertical Speed Vertical Speed Minimum Vertical Speed Bug Setting Vertical Speed Vertical Speed Warning Indication 10 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Vertical Deviation Indicator VDI The Vertical Deviation Indicator is displayed for GPS and ILS 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 Vertical Deviation Indicator GPS Approach ILS Approach Outside Air Temperature OAT The Outside Air Temperature as sensed from the temperature probe on the aircraft is displayed to the left of the HSI This temperature is used in calculating the true airspeed J gt Ad mE Gi ebe Un J gt lt 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 DME Information DME Hold Annunciation Selected DME Set Hold for Selected DME DME Indication 190 01102 03 Rev G G500 Cockpit Reference Guide 11 PRIMARY F
50. l be removed from the Terrain page when range A RNG exceeds 10 nm Potential Impact Point Projected Flight Path y TOUN a Unlighted Obstacle Terrain more than 1000 ft below the aircraft altitude Black Un lt UJ r un Terrain Altitude Color Correlation Map Toolbar Symbols Symbol Description Maximum Zoom Indicator 4 Terrain Proximity Enabled and Available Indicator Ka Terrain Proximity Enabled and Not Available Indicator Traffic Enabled and Available Indicator CG Traffic Enabled and Not Available Indicator 190 01102 03 Rev G G500 Cockpit Reference Guide 75 SYMBOLS GARMIN XM WX 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 Symbol Expiration Time Broadcast Rate Minutes Minutes foe EEE He 5 Bem 9 Momm o fs DB m o o DE ese 9 a m o n B e DM eme Freezing Levels Description un E ES gt un County Warnings Cyclone Warnings NOTE Product age is not displayed for individual reports of AIRMETs SIGMETs City Forecasts County Warnings Cell Movement and TFRs Product ge
51. 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 bezel HOLD TO ARH p ALT A Arm Disarm Altitude Bug Autopilot Navigation Ihe 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 190 01102 03 Rev G G500 Cockpit Reference Guide 19 J gt d mE G lis mr GA J gt lt PRIMARY FLIGHT DISPLAY PFD GARMI H GPSS The GDU 620 will send the GPSS commands from the displayed GPS source to the autopilot For exampl
52. n airplane symbol is shown on the navigation map views for enhanced positional awareness This database is updated on a 56 day cycle jw ChartView Optional with Enablement Card 5 ChartView resembles the paper version of Jeppesen terminal procedures charts 3 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 The ChartView database is updated 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 A 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 68 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN ALERIS Alerts A NOTE Contact your Garmin dealer for service if any of the following alerts appear On Screen Alerts Alert Description ADC Altitude Error Correction is unavailable ADC1 ALT EC E GDC is reporting that altitude correction is unavailable AHRS 1 or AHRS 2 is not a AE any GPS information AHRS1 GPS AHRS 1 or AHRS 2 is operating AHRS
53. n 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 from the altitude displayed by pressure altimeters such as the output from the GDC 74A B Air Data Computer or other pressure altimeters in aircraft
54. nd interfaced to the G500 e 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 e 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 anon 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 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 190 01102 03 Rev G G500 Cockpit Reference Guide 37 dnhoud dVIN j LL al gt Gi m MAP 100p MAP GROUP GARMIN Viewing Terrain A NOTE Obstacles will be removed from the Terrain page when range A RNG exceeds 10 nm While viewing the Terrain page of the Map Page Group press the 360 or ARC soft keys to select the desired view TERRAIN PRO AIMITY MAP PL UUUUG ARC Y ADVISORY 360 or ARC Soft Keys L
55. neration time is displayed for Freezing Level and Winds Aloft instead of valid time 76 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN SYMBOLS Miscellaneous Symbols Symbol Description Default Aircraft Ownship High Wing Aircraft Default Map Pointer Elevation Map Pointer __ User Waypoint Parallel Track Waypoint TFR Temporary Flight Restrictions Restricted Prohibited Warning Alert Class B Airspace Class C Airspace Class D Airspace Un UJ r N 190 01102 03 Rev G G500 Cockpit Reference Guide 73 18 This page intentionally left blank G500 Cockpit Reference Guide A GARMIN 190 01102 03 Rev G A GARMIN 2009 2012 Garmin Corporation Garmin International Inc 1200 East 151 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 ORB UK Tel 44 0 870 850 1243 Fax 44 0 238 052 4004 Garmin Corporation No 68 Jangshu 2 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 01102 03 Rev G
56. o 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 December 2012 Printed in the U S A A GARMIN 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 ii consumable parts such as batteries unless product damage has occurred due to a defect in materials or workmanship iii damage caused by
57. on carefully review and understand all aspects of the G500 Pilot s Guide Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G500 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 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 south of 55 South latitude between longitude 120 East and 165 East WARNING Do not use Terrain SVT information for primary terrain avoidance Terrain SVT is intended only to enhance situational awareness 190 01102 03 Rev G G500 Cockpit Reference Guide il A WARNINGS CAUTIONS AND NOTES GARMIN Ki WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions CAU
58. radius from 3000 feet below to 3500 feet above the requesting aircraft Traffic is displayed according to TCAS symbology using four different symbols Displaying TIS Traffic While viewing the Traffic Page of the Map Page Group press the OPERATE soft key to begin displaying traffic TIS OPERATING is displayed in the upper left hand corner of the MFD A NOTE TIS is disabled when a Traffic Advisory System TAS is installed Operating MEEN L HOG UP Mode EE lt Proximity Advisory Traffic 5000 feet Advisory above and aircraft is descending 1 200 feet above and ascending Non Threat 5000 feet above and ascending TRAFFIC MAP WX AUX SENET OPERATES ERR ADVISORY Traffic Map TIS 36 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN MAP GROUP Terrain Page TERRAIN PROXIMITY OCUUUE TERRAIN SVT j OCUUUE Soft Keys Found on Terrain Page 360 ARC Garmin provides the following G500 TERRAIN 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 A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 North or 60 South A NOTE Terrain SVT is standard when the Synthetic Vision Technology SVT option is installed A NOTE TAWS alerts will be generated by the GPS TAWS unit on the PFD if an external TAWS unit is installed a
59. rt NRST or your most recently selected airport ba 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 EpL SLYVHD dNOUD Id E E E E Display Charts From Display Charts Of Display Charts From Flight Plan Nearest Airport Recent Choices 190 01102 03 Rev G G500 Cockpit Reference Guide 67 FPL GROUP GARMI H 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 SafeTaxi Optional SafeTaxi is an enhanced feature that gives greater map detail when zooming TA in on airports at close range The airport display on the map reveals runways with numbers taxiways with identifying letters numbers and airport landmarks q including ramps buildings control towers and other prominent features T2 Resolution is greater at lower map ranges When the aircraft location is within the screen boundary including within SafeTaxi ranges a
60. stem see the latest revision of the G500 Pilots Guide P N 190 01102 02 Call Suppression 1 While viewing the Iridium Phone page press the small MED knob 2 Turn the large MFD knob to select the Call Suppression type of Off On or On during APR MAPR TERM 60 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN FPLGROUP Creating Entries into Phonebook 1 While viewing the Iridium Phone page of the Aux Group press the small MED 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 It 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 activa
61. t on a traditional Slip Skid Indicator Roll Scale Zero Roll Pointer Slip Skid Indicator Slip Skid Indicator 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 Current Heading Turn Rate Markings J gt gt mE Gi ebe GA J gt lt Current GPS Track Heading Trend HSI Heading Markings A NOTE If magnetic heading is lost GPS ground track will be displayed in place of heading 190 01102 03 Rev G G500 Cockpit Reference Guide 13 PRIMARY FLIGHT DISPLAY PFD GARMI H 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 A 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 z is available if an ADF source is installed TE The BRG2 sott key cycles through modes NAV2 and GPS2 if a second NAV or Ve GP
62. t reaches 150 feet above the setting for the alert 190 01102 03 Rev G G500 Cockpit Reference Guide 7 J gt ES lt TI Cc L GA J gt lt PRIMARY FLIGHT DISPLAY PFD GARMI N To set the altitude for the Minimums Bug MINIMUMS 1 While viewing the Active Flight Plan page of the FPL Group press the small MFD knob to activate the cursor 2 Turn the large MFD knob to the ALTITUDE portion of the MINIMUMS section 3 Turn the small MFD knob to enter the desired altitude Press the ENT key to confirm selection 4 When finished press the small MED 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 MNU 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 MINIMUMS SOURCE ALTITUDE gt t E A e Bn TE gt Ce lt x Ce as Radar Altimeter Value SCH Brown band represents RA MIN gt apm e ground gt 108 fe S____ Minimums Annunciations using RAD ALT for Source 8 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Altitude Bug The Altitude Bug is displayed on the Altitude Tape at the selected altitude
63. tails 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 lett of the HSI NAV STATUS Style 2 Roll Modes Autopilot Status Pitch Modes Active Mode HB JC HS AP E T ST Active Mode Armed Mode Armed Mode Autopilot Annunciations 22 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI N PRIMARY FLIGHT DISPLAY PFD Additional Features Garmin Synthetic Vision Technology Optional Synthetic Vision Technology SVT is offered as an optional feature to the G500 SVT is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots 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 WPT DIS DTK TRK e team pin 10 10 Airport HM Sign Ger ep Headin Zero Pitch Mark Line gt 2 Obstacle Tl Flight Path Marker 2 NI CDS NT j 7 Terrain un J gt Terrain lt Threat SVT Soft Keys Synthetic Vision Imagery A 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 con
64. te 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 Use 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 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 1 Press the small MFD knob and turn the large MFD knob to highlight the phone number area Press the KEYS soft key and enter the number When finished entering the number you want to call press the DIAL key 2 After completing the call press the HANG UP key mE J Gi Ad c uy gt lt m mu L G L mE J r gt 190 01102 03 Rev G G500 Cockpit Reference Guide 61 FPL GROUP GARMIN System Status Page SYSTEM STATUS MAP WX AUX DDODaNLDL 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 This page is for informational purposes and there are no items t
65. ting 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 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 ki NO LLJ le D LL un e LL be un gt un A o Ce OU Ge t V Speed References on Airspeed Tape Airspeed References A 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 50 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H 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 Wind Vector 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 Off No display of wind vectors on PFD Style1 Displays headwind and crosswind components Style2 Displays total wind direction and speed Style3 Displays total wind direction with headwind and crosswind speed components Style4 Displays total wind direction in degrees with wind speed Selecting NAV Status Styles
66. to either OFF or ON Turn the large MFD knob to the Manual Request box and press ENT to either send request or cancel current request Press the small MFD knob to return to the GFDS page G500 Cockpit Reference Guide 190 01102 03 Rev G GARMIN Weather Radar Optional Weather Radar Map Page WEATHER RADAR MAP WX AUX FPL Soft Keys Found on Weather Radar Map Page oF e STAB ON BRG Operating Stabilization WEATHER Mode On Off Weather CS Lnd es Alert E GWX only Radar Beam Scan Line SES TILT UP 13 25 SE BEARING L 0 Control SECTOR SCAN FULL Window GAIN CAL M WEATHER RADAR MAP WX AUX FPL OOO RON HORIZONTE ALERTS Weather Radar 190 01102 03 Rev G G500 Cockpit Reference Guide 45 cc t el x e cc LLJ E et LL A gt Ge o 2S WX GROUP GARMIN Airborne Color Weather Radar WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna 4 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 k
67. tom 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 Horizontal Situation Indicator HSI Displays the Selected Heading Box Current Heading Turn Rate Markings and Heading Trend Vertical Speed Tape Displays Vertical Speed and the Vertical Speed Bug Barometric BARO Setting Displays the current setting of barometric pressure Radar Altimeter Display Displays current height above ground from the radar altimeter Brown band in altitude tape represents the ground J gt ES mE Cc L mr z GA J gt lt Fast Slow Indicator See your AFM for details on operation 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 Altitude Tape Displays Current Altitude Altitude Trend Altitude Bug Altitude Minimums Bug and BARO setting 00000 00000000 Marker Beacon Marker Beacon Indicator 190 01102 03 Rev G G500 Cockpit Reference Guide 3 gt et E A e Bn el LL gt Ce E Ce PRIMARY FLIGHT DISPLAY
68. und 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 on GFDS and how to register see the latest revision of the G500 Pilot s Guide P N 190 01102 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 MNU button PAGE MENU Display XM Weather Register With GFDS Weather Setup Weather Legend Press the MFD knob to return to base page 2 Highlight GFDS Data Request and press the ENT button to display the GFDS DATA REQUEST page 190 01102 03 Rev G G500 Cockpit Reference Guide 43 HS UU Coverage GARMIN GFDS DATA REQUEST Coverage Area H PRESENT POSITION Distances X MEL Remaining FPL FLIGHT PLAN Next 50 NM EEN Next 500 NM DIAMETER RTE WIDTH Width of Coverage 50 NM 500 NM Update Rate UPDATE RATE Off 60 Minutes MANUAL REQUEST SEND REQ CANCEL REQ Cancel Manual Request Next auto update 4 Minutes Status of Request Press the MFD knob to return to base page GFDS Data Request Page Configuring GFDS Data Request Page 1 44 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 Turn the large MFD knob to the Auto Request box and press ENT to change the update rate
69. v G G500 Cockpit Reference Guide 55 AUXGROUP GARMIN XM Information Page Optional AM INFORMATION MAP WX AUX FPL III Soft Key Found on XM Information Page While viewing the XM Information page of 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 Subscription information is available at http Avww garmin com xm AUDIO RADIO ID L CD5 8J ID 2GKT6 HJ SIGNAL STRONG SIGNAL STRONG SERVICE CLASS WEATHER PRODUCTS B AIRMET E FRZ LYL m SIGMET m CITY il LING B SFC m CLD TOP METAR E TAF im COUNTY i NEXRAD WIER O CYCLONE m RADAR CVRG WIND im ECHO TOP E SCIT When activation has been completed press the LOCK softkey to lock the activation XM INFORMATION MAP WX AUX FPL 00W00 00 LOCK I ALERTS XM Information Page 56 G500 Cockpit Reference Guide 190 01102 03 Rev G GARMI H AUX GROUP XM Radio Page Optional EREE SERERE Soft Keys Found on XM Radio Page ALL Selecting a Channel l 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 Press ENT to make the highlighted channel the Active Channel Press the small MFD knob to end editing Press CHNL and then the CH or CH soft keys to increment up or down one
70. wing 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 Usethe 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 Easter gt c E G sed jo c BE un un ell LL S un mi c J 0 I Gi m mm 190 01102 03 Rev G G500 Cockpit Reference Guide 53 AUX GROUP GARMIN MFD Display Units A 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 A NOTE The corresponding GNS must
71. y referred to as the Minimums Bug 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 e 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 Bug and text Bug and text are Bug and text are dre yellow when cyan within 2500 ft white within 100 ft altitude reached Minimums yy Bug Minimums Box BARO MIN 2000 Pd Minimums Annunciations using BARO for Source Alerting is inhibited while the aircraft is on the ground and also if a value has been set for altitude alerting until the aircraf

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