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G500/600 Cockpit Reference Guide © 2008-2015 Garmin Ltd. or its subsidiaries. All rights reserved. This manual reflects the operation of system software version 7.00, or later. Some differences in operation may be observed when comparing the information in this manual to later software versions. Garmin International, Inc., 1200 East 151st Street, Olathe, KS 66062, U.S.A. Tel: 913.397.8200 Fax: 913.397.8282 Garmin AT, Inc., 2345 Turner Road SE, Salem, OR 97302, U.S.A. Tel: 503.391.3411 Fax 503.364.2138 Garmin (Europe) Ltd., Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel. +44 (0) 870 850 1243 Fax +44 (0) 238 052 4004 Garmin Corporation, No. 68, Jangshu 2nd Road, Xizhi Dist., New Taipei City 221, Taiwan (R.O.C.) Tel: 886.02.2642.9199 Fax: 886.02.2642.9099 www.garmin.com At Garmin, we value your opinion. For comments about this guide, please e-mail: [email protected]. Except as expressly provided herein, no part of this manual may be reproduced, copied, transmitted, disseminated, downloaded or stored in any storage medium, for any purpose without the express written permission of Garmin. Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use, provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited. Garmin®, GDU™ 620 are trademarks of Garmin Ltd. or its subsidiaries. FliteCharts®, and SafeTaxi® are registered trademarks of Garmin Ltd. or its subsidiaries. These trademarks may not be used without the express permission of Garmin. NavData® is a registered trademark of Jeppesen, Inc.; SkyWatch® is a registered trademark of L-3 Avionics Systems; and SiriusXM® is a registered trademark of Sirius XM Radio, Inc.; Iridium® is a registered trademark of Iridium Communications Inc.; Canadian radar data provided by Environment Canada; United States radar data provided by NOAA; European radar data collected and provided by Meteo France. AOPA Membership Publications Inc., and its related organizations (hereinafter collectively “AOPA”) expressly disclaim all warranties, with respect to the AOPA information included in this data, express or implied, including, but not limited to, the implied warranties of merchantability and fitness for a particular purpose. The information is provided “as is” and AOPA does not warrant or make any representations regarding its accuracy, reliability, or otherwise. Under no circumstances including negligence, shall AOPA be liable for any incidental, special or consequential damages that result from the use or inability to use the software or related documentation, even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages. User agrees not to sue AOPA and, to the maximum extent allowed by law, to release and hold harmless AOPA from any causes of action, claims or losses related to any actual or alleged inaccuracies in the information. Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you. April 2015 Printed in the U.S.A. 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 accident, abuse, misuse, water, flood, fire, or other acts of nature or external causes; (iv) damage caused by service performed by anyone who is not an authorized service provider of Garmin; or (v) damage to a product that has been modified or altered without the written permission of Garmin. In addition, Garmin reserves the right to refuse warranty claims against products or services that are obtained and/or used in contravention of the laws of any country. THE WARRANTIES AND REMEDIES CONTAINED HEREIN ARE EXCLUSIVE AND IN LIEU OF ALL OTHER WARRANTIES, WHETHER EXPRESS, IMPLIED OR STATUTORY, INCLUDING ANY LIABILITY ARISING UNDER ANY WARRANTY OF MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE, STATUTORY OR OTHERWISE. THIS WARRANTY GIVES YOU SPECIFIC LEGAL RIGHTS, WHICH MAY VARY FROM STATE TO STATE. IN NO EVENT SHALL GARMIN BE LIABLE FOR ANY INCIDENTAL, SPECIAL, INDIRECT OR CONSEQUENTIAL DAMAGES, WHETHER RESULTING FROM THE USE, MISUSE OR INABILITY TO USE THE PRODUCT OR FROM DEFECTS IN THE PRODUCT. SOME STATES DO NOT ALLOW THE EXCLUSION OF INCIDENTAL OR CONSEQUENTIAL DAMAGES, SO THE ABOVE LIMITATIONS MAY NOT APPLY TO YOU. Garmin retains the exclusive right to repair or replace (with a new or newly-overhauled replacement product) the product or software or offer a full refund of the purchase price at its sole discretion. SUCH REMEDY SHALL BE YOUR SOLE AND EXCLUSIVE REMEDY FOR ANY BREACH OF WARRANTY. Online Auction Purchases: Products purchased through online auctions are not eligible for warranty coverage. Online auction confirmations are not accepted for warranty verification. To obtain warranty service, an original or copy of the sales receipt from the original retailer is required. Garmin will not replace missing components from any package purchased through an online auction. International Purchases: A separate warranty may be provided by international distributors for devices purchased outside the United States depending on the country. If applicable, this warranty is provided by the local in-country distributor and this distributor provides local service for your device. Distributor warranties are only valid in the area of intended distribution. Devices purchased in the United States or Canada must be returned to the Garmin service center in the United Kingdom, the United States, Canada, or Taiwan for service. To obtain warranty service, contact your local Garmin Authorized Service Center. For assistance in locating a Service Center near you, visit the Garmin web site at http://www.garmin.com or contact Garmin Customer Service at 866.739.5687. 190-00601-03 Rev G G500/600 Cockpit Reference Guide i WARNINGS, CAUTIONS, AND NOTES Warnings, Cautions, & Notes WARNINGS, CAUTIONS, AND NOTES ii 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 terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight. The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness warning system. Terrain data is obtained from third party sources. Garmin is not able to independently verify the accuracy of the terrain data. WARNING: The displayed minimum safe altitudes (MSAs) are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information. Always refer to current aeronautical charts for appropriate minimum clearance altitudes. WARNING: The Garmin GDU 620 has a very high degree of functional integrity. However, the pilot must recognize that providing monitoring and/ or self-test capability for all conceivable system failures is not practical. Although unlikely, it may be possible for erroneous operation to occur without a fault indication shown by the GDU 620. It is thus the responsibility of the pilot to detect such an occurrence by means of cross-checking with all redundant or correlated information available in the cockpit. WARNING: The altitude calculated by GPS receivers is geometric height above Mean Sea Level and could vary significantly 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. GPS altitude should never be used for vertical navigation. Always use pressure altitude displayed by the GDU 620 PFD or other pressure altimeters in aircraft. WARNING: Do not use outdated database information. Databases used in the G500 or G600 system must be updated regularly in order to ensure that the information remains current. Pilots using an outdated database do so entirely at their own risk. G500/600 Cockpit Reference Guide 190-00601-03 Rev G WARNINGS, CAUTIONS, AND NOTES WARNING: Do not use basemap (land and water data) information for primary navigation. Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness. WARNING: Traffic information shown on the GDU 620 Multi-Function Display is provided as an aid in visually acquiring traffic. Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic. WARNING: For safety reasons, GDU 620 operational procedures must be learned on the ground. WARNING: To reduce the risk of unsafe operation, carefully review and understand all aspects of the G500/600 Pilot’s Guide. Thoroughly practice basic operation prior to actual use. During flight operations, carefully compare indications from the G500/600 to all available navigation sources, including the information from other NAVAIDs, visual sightings, charts, etc. For safety purposes, always resolve any discrepancies before continuing navigation. WARNING: Exceeding 200 deg/second in pitch or roll may invalidate AHRS attitude provided to the GDU 620. Exceeding 450 KIAS may invalidate ADC information provided to the GDU 620. WARNING: Because of anomalies in the earth’s magnetic field, operating the G500/600 within the following areas could result in loss of reliable attitude and heading indications. North of 70° North latitude and south of 70° South latitude. An area north of 65° North latitude and between longitude 75° West and 120° West. An area north of 70° North latitude and between longitude 85° East and 114° West. An area south of 55° South latitude between longitude 120° East and 165° East. 190-00601-03 Rev G G500/600 Cockpit Reference Guide iii WARNINGS, CAUTIONS, AND NOTES WARNING: Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product. Due to time delays inherent in gathering and processing weather data for data link transmission, the weather information shown by the data link weather product may be significantly older than the indicated weather product age. WARNINGS, CAUTIONS, AND NOTES WARNING: Do not use Terrain-SVT information for primary terrain avoidance. Terrain-SVT is intended only to enhance situational awareness. WARNINGS, CAUTIONS, AND NOTES CAUTION: The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance. The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment. Portions of the Garmin GDU 620 utilize GPS as a precision electronic NAVigation AID (NAVAID). Therefore, as with all NAVAIDs, information presented by the GDU 620 can be misused or misinterpreted and therefore, become unsafe. CAUTION: The Garmin GDU 620 does not contain any user-serviceable parts. Repairs should only be made by an authorized Garmin service center. Unauthorized repairs or modifications could void both the warranty and pilot’s authority to operate this device under FAA/FCC regulations. CAUTION: The GDU 620 PFD and MFD displays use a lens coated with a special anti-reflective coating that is very sensitive to skin oils, waxes, and abrasive cleaners. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI-REFLECTIVE COATING. It is very important to clean the lens using a clean, lint-free cloth and an eyeglass lens cleaner that is specified as safe for anti-reflective coatings. iv NOTE: Do not rely solely upon data link services to provide Temporary Flight Restriction (TFR) information. Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control. NOTE: 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. NOTE: All visual depictions contained within this document, including screen images of the GDU 620 bezel and displays, are subject to change and may not reflect the most current GDU 620 system. Depictions of equipment may differ slightly from the actual equipment. G500/600 Cockpit Reference Guide 190-00601-03 Rev G WARNINGS, CAUTIONS, AND NOTES NOTE: This device complies with part 15 of the FCC Rules. Operation is subject to the following two conditions: (1) this device may not cause harmful interference, and (2) this device must accept any interference received, including interference that may cause undesired operation. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South. NOTE: This product, its packaging, and its components contain chemicals known to the State of California to cause cancer, birth defects, or reproductive harm. This notice is being provided in accordance with California’s Proposition 65. If you have any questions or would like additional information, please refer to our web site at www.garmin.com/ prop65. NOTE: Terrain-SVT is standard when the Synthetic Vision Technology™ (SVT) option is installed. The TAWS option will take precedence over TerrainSVT. NOTE: Do not use SafeTaxi, FliteCharts, or Chartview functions as the basis for ground maneuvering. SafeTaxi, FliteCharts, and Chartview functions have not been qualified to be used as an airport moving map display (AMMD). SafeTaxi, FliteCharts, and Chartview are intended to improve pilot situational awareness during ground operations and should only be used by the flight crew to orient themselves on the airport surface. 190-00601-03 Rev G G500/600 Cockpit Reference Guide v WARNINGS, CAUTIONS, AND NOTES Record of Revisions Part Number Revision 190-00601-03 A B C D E F G vi Date 6/12/08 6/1/09 Description Production release Revision reflects functionality added with SW version 3.00. Added SVT, TAWS-B, Terrain Proximity, Wind Vectors, Minimums Bug, GAD 43, and Weather Radar information. 10/26/09 Updated subscription information for FliteCharts and ChartView. 11/30/10 Added changes to reflect v4.00 and v5.00 software changes. 8/23/11 Added changes to reflect v6.00 software changes. 10/23/12 Added changes to reflect v6.11 software changes. 4/10/15 Added changes to reflect software version 7.00. G500 and G600 CRG’s are combined. G500/600 Cockpit Reference Guide 190-00601-03 Rev G TABLE OF CONTENTS Contents Warnings, Cautions, & Notes............................................................................. ii Introduction....................................................................................................... 1 Primary Flight Display (PFD).............................................................................. 2 Autopilot (AP).................................................................................................. 19 GAD 43 Attitude..........................................................................................................................................19 Heading......................................................................................................................................................20 Altitude Capture (Optional Upgrade)............................................................................................................20 Autopilot Navigation...................................................................................................................................20 GPSS...........................................................................................................................................................21 Flight Director Display..................................................................................................................................22 Vertical Speed Control.................................................................................................................................22 Autopilot Mode Annunciations.....................................................................................................................23 Additional Features......................................................................................... 24 Synthetic Vision Technology™ ......................................................................................................................24 Displaying SVT™ Terrain...............................................................................................................................25 Displaying Heading on the Horizon..............................................................................................................25 Displaying Airport Signs...............................................................................................................................25 Multi-Function Display (MFD).......................................................................... 26 Page Navigation - Moving Between Pages...................................................................................................27 Changing Settings within a Page.................................................................................................................27 Default Map Page........................................................................................................................................27 MFD Soft Key Map.......................................................................................................................................28 Map Group...................................................................................................... 29 Navigation Map 1 and Navigation Map 2 Pages...........................................................................................29 Decluttering (DCLTR) the Map Pages............................................................................................................30 Split Screen Page (Optional).........................................................................................................................34 Traffic Map Page (Optional).........................................................................................................................35 Terrain/TAWS-B Page...................................................................................................................................41 190-00601-03 Rev G G500/600 Cockpit Reference Guide vii TABLE OF CONTENTS Airspeed Tape................................................................................................................................................4 Altitude Tape.................................................................................................................................................6 Barometric Pressure.......................................................................................................................................6 Minimums Bug (Barometric or Radar Altimeter)..............................................................................................7 Altitude Bug..................................................................................................................................................9 Fast/Slow Indication......................................................................................................................................9 Wind Vectors...............................................................................................................................................10 Vertical Speed (V/S).....................................................................................................................................10 Vertical Deviation Indicator (VDI).................................................................................................................11 Temperature Display....................................................................................................................................11 DME Indication............................................................................................................................................12 Clock/Timer.................................................................................................................................................12 Attitude Indicator........................................................................................................................................12 Horizontal Situation Indicator (HSI): Aircraft Heading....................................................................................13 Adjusting the Course Pointer.......................................................................................................................14 HSI Bearing Pointers....................................................................................................................................14 Marker Beacon Annunciations......................................................................................................................16 Miscompare Annunciations..........................................................................................................................17 TABLE OF CONTENTS Terrain Pop-Up Alerts...................................................................................................................................43 WX Group........................................................................................................ 44 XM Weather Map Pages..............................................................................................................................44 Customizing the Weather Map.....................................................................................................................44 Changing Forecast Time...............................................................................................................................46 Changing Weather Altitude..........................................................................................................................46 Garmin Flight Data Services (GFDS) Map Pages............................................................................................47 FIS-B Weather Map Pages............................................................................................................................49 Customizing the Weather Map.....................................................................................................................49 Weather Radar (Optional)............................................................................... 51 Weather Radar Map Page............................................................................................................................51 Airborne Color Weather Radar.....................................................................................................................52 TABLE OF CONTENTS Aux Group....................................................................................................... 55 External Video Page (Optional).....................................................................................................................55 System Setup Page......................................................................................................................................56 XM® Information Page (Optional)................................................................................................................62 XM® Radio Page (Optional).........................................................................................................................63 Position Reporting Page...............................................................................................................................65 Iridium® Phone Page (Optional)..................................................................................................................66 System Status Page.....................................................................................................................................68 Flight Plan Group............................................................................................ 69 Active Flight Plan Page................................................................................................................................69 Viewing Your Active Flight Plan....................................................................................................................69 Waypoint Information Page.........................................................................................................................70 Charts Page (Optional)................................................................................................................................71 Chart Information........................................................................................................................................71 Selecting a Chart.........................................................................................................................................71 Selecting Other Charts.................................................................................................................................72 Viewing Charts and Panning........................................................................................................................72 Viewing Details of ChartView™ Charts........................................................................................................73 Setting Minimums.......................................................................................................................................73 Changing Day/Night View............................................................................................................................73 Viewing NOTAMs (ChartView Only)..............................................................................................................74 Alerts............................................................................................................... 75 On Screen Alerts..........................................................................................................................................75 TAWS-B Alerts.............................................................................................................................................80 Terrain-SVT™ Alerts......................................................................................................................................81 Symbols........................................................................................................... 82 Map Page Symbols......................................................................................................................................82 SafeTaxi® Symbols.......................................................................................................................................83 Traffic Symbols............................................................................................................................................83 Terrain Obstacle Symbols.............................................................................................................................85 Map Toolbar Symbols..................................................................................................................................86 XM® WX Weather Symbols and Product Age................................................................................................87 Miscellaneous Symbols................................................................................................................................88 viii G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Introduction PFD/MFD NOTE: In some models or installations, the PFD and MFD and their controls are switched to the other side. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 1 PRIMARY FLIGHT DISPLAY This reference guide covers the operation of the GDU 620 as integrated in the G500 and G600 Avionics Display Systems. The G500 and G600 Avionics Display Systems are avionics suites that combine primary flight instrumentation, navigational information, and a moving map all displayed on dual 6.5 inch color screens. The G500 and G600 systems are composed of sub-units or Line Replaceable Units (LRUs). LRUs have a modular design and can be installed directly behind the instrument panel or in a separate avionics bay if desired. This design greatly eases troubleshooting and maintenance of the G500 or G600 system. A failure or problem can be isolated to a particular LRU, which can be replaced quickly and easily. Each LRU has a particular function, or set of functions, that contributes to the system’s operation. For more details on the G500 and G600 systems, refer to the latest revision of the G500/600 Pilot’s Guide, P/N 190-00601-02. PRIMARY FLIGHT DISPLAY (PFD) Primary Flight Display (PFD) 21 1 20 19 18 17 PRIMARY FLIGHT DISPLAY 2 16 3 4 15 5 14 6 7 13 8 9 10 22 11 12 Primary Flight Display (PFD) 1 Airspeed Tape: Displays Groundspeed (GS), Airspeed Trend, Current Airspeed, and True Airspeed (TAS). Markings dependent upon installation configuration. 2 Wind Vector: Displays direction and speed of wind. 3 Heading Select Key: Press HDG and turn PFD knob to set heading bug. 4 Course Select Key: Press CRS and turn PFD knob to set the course of the selected source (VOR1, VOR2, GPS1, or GPS2). 5 Altitude Select Key: Press ALT and turn PFD knob to set altimeter bug. 6 V/S (Vertical Speed) Select Key: Press V/S and turn PFD knob to set V/S bug. 7 Barometer Select Key: Press BARO and turn PFD knob to change barometric setting. 2 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Outside Air Temperature (SAT, TAT, or ISA): Displays the current outside air temperature. 9 NAV Status Window: (NAV Style 2 Shown) Displays which GPS is selected as the Active Source, Active Waypoint (WPT), and Distance to Waypoint (DIS). NAV Style 1 (Not Shown) displays Active Source, WPT, DIS, Desired Track (DTK), and Current Track (TRK) at top of screen. 10 PFD Knob: Turn PFD knob to change bug settings, Heading Bug, Course, Altitude Bug, V/S Bug, and Barometer setting. 11 Soft Keys: Used to select available options on PFD or MFD. 12 SD Card Slots, Upper and Lower: The lower slot is used for the supplemental database card, including aviation database updates. The upper slot may be used to update the internal aviation database. 13 Soft Key Labels: Located on the bottom screen of the PFD and MFD. Selection is done by pressing the corresponding soft key. Soft keys that are available have the labels shown as white text on a black background. Soft keys that are selected have the labels shown as black text on a gray background. Soft keys that are unavailable have the labels shown as gray text on a black background. 14 Horizontal Situation Indicator (HSI): Displays the Selected Heading Box, Current Heading, Turn Rate Markings, and Heading Trend. 15 Vertical Speed Tape: Displays Vertical Speed and the Vertical Speed Bug 16 Barometric (BARO) Setting: Displays the current setting of barometric pressure. 17 Radar Altimeter Display: Displays current height above ground from the radar altimeter. Brown band in altitude tape represents the ground. 18 Fast/Slow Indicator: See your AFM for details on operation. 19 Roll Pointer and Slip/Skid Indicator: The slip/skid indicator is the bar beneath the roll pointer. The indicator moves with the roll pointer and laterally away from the pointer to indicate lateral acceleration (slip/skid). 20 Altitude Tape: Displays Current Altitude, Altitude Trend, Altitude Bug, Altitude or Radar Altimeter Minimums Bug, and BARO setting. 21 Marker Beacon: Marker Beacon Indicator 22 Clock or Timer window. 190-00601-03 Rev G G500/600 Cockpit Reference Guide PRIMARY FLIGHT DISPLAY 8 3 PRIMARY FLIGHT DISPLAY (PFD) Airspeed Tape The upper left portion of the PFD display provides Groundspeed, Airspeed Trend, Current Airspeed, and True Airspeed information. Current Airspeed is normally shown in white on the black pointer. The Trend Indicator (magenta line) indicates what the airspeed will be in six seconds, if the current acceleration is maintained. If the current acceleration will cause the airspeed to exceed Vne in six seconds, the airspeed is displayed in yellow. If the current airspeed exceeds Vne, the pointer changes to red with white text. NOTE: Airspeed tape markings are dependent upon configuration at the time of installation. Reference the AFM or POH or latest revision of the G500/600 Pilot’s Guide for more details. PRIMARY FLIGHT DISPLAY Groundspeed Mmo/ Vmo/ Vne Trend Indicator VnO Current Airspeed Vfe Vs1 Vs0 True Airspeed Airspeed Tape White triangle (See AFM/POH) Typical Airspeed Tape Markings VYSE Overspeed VMCA Overspeed Indication 4 Maximum speed with landing gear extended. Additional Reference Markings Reference Speeds G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) V-speeds (Glide, Vr, VX, and VY) default values are set during the installation process, but can be changed and turned on/off from the System Setup page on the first page of the Aux page group. When active (on), the V-speeds are displayed at their respective locations to the right of the airspeed scale. Glide Reference Marker Vr Reference Marker Vx Reference Marker Vy Reference Marker Reference Speeds Reference Marker V2 Reference Marker V1 Reference Marker Vr Reference Marker Alternate Reference Speeds 190-00601-03 Rev G G500/600 Cockpit Reference Guide 5 PRIMARY FLIGHT DISPLAY The labels for the reference markers may vary as configured during installation. PRIMARY FLIGHT DISPLAY (PFD) 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 PRIMARY FLIGHT DISPLAY 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 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Minimums Bug (Barometric or Radar Altimeter) Bug and text are cyan within 2500 ft Bug and text are white within 100 ft Bug and text are yellow when altitude reached Minimums Bug Minimums Box 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 aircraft reaches 150 feet above the setting for the alert. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 7 PRIMARY FLIGHT DISPLAY For altitude awareness, an Altitude Minimums Bug commonly 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. •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. PRIMARY FLIGHT DISPLAY (PFD) To set the altitude for the Minimums Bug: PRIMARY FLIGHT DISPLAY 1) While viewing the Active Flight Plan page of the FPL Group, press the small MFD knob to activate the cursor and turn the large MFD knob to the Source selection. 2) Turn the small MFD knob to select Off, BARO, or RAD ALT. 3) Turn the large MFD knob to the ALTITUDE portion of the MINIMUMS section. 4) Turn the small MFD knob to enter the desired altitude. Press the ENT key to confirm selection. 5) When finished, press the small MFD knob to exit the MINIMUMS box. The Minimums Bug can also be set from the Charts page of the FPL. 1) While viewing the Charts page of the FPL Group, press the MENU key and select “Set Minimums” from the Options menu. 2) Turn the small MFD knob to select Off, BARO, or RAD ALT. 3) Press the ENT key to move to enter altitude. Turn the small MFD knob to enter the desired altitude. Press the ENT key to confirm selection. Radar Altimeter Value Brown band represents the ground. Minimums Annunciations using RAD ALT for Source 8 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Altitude Bug The Altitude Bug is displayed on the Altitude Tape at the selected altitude bug setting. A portion of the Altitude Bug will be displayed at the top or bottom of the altitude tape if the selected altitude bug is off of the tape. Altitude Bug Setting 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. Within 1000 ft Within 200 ft Deviation of +/- 200ft Altitude Bug Indications Fast/Slow Indication The Fast/Slow indication from an external system may be optionally displayed on the left side of the PFD. Refer to the Airplane Flight Manual for instructions on using the Fast/Slow indications. Pointer Fast/Slow Scale Fast/Slow Scale and Pointer 190-00601-03 Rev G G500/600 Cockpit Reference Guide 9 PRIMARY FLIGHT DISPLAY Altitude Bug PRIMARY FLIGHT DISPLAY (PFD) 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. PRIMARY FLIGHT DISPLAY Wind Vector Field Wind Vector Display Vertical Speed (V/S) The Vertical Speed Tape and Vertical Speed Bug are displayed below the Altitude Tape. For aircraft with vertical speed operating limitations, red bands showing Vertical Speed Maximum and Minimum ranges will be shown on the left side of the Vertical Speed tape. Vertical Speed Maximum Vertical Speed Bug Current Vertical Speed Vertical Speed Minimum Vertical Speed Bug Setting Vertical Speed 10 G500/600 Cockpit Reference Guide Vertical Speed Warning Indication 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Vertical Deviation Indicator (VDI) The Vertical Deviation Indicator is displayed for ILS and GPS approaches with vertical guidance. The GPS approach glidepath is shown in magenta (G and indicator), while the ILS approach glideslope is shown in green (G and indicator.) Vertical Deviation Source Vertical Deviation Indicator ILS Approach Temperature Display The outside air temperature is displayed to the left of the HSI. The air data computer calculates the temperature based on temperature probe and pitot/ static inputs. The units (°C or °F) and temperature reference are selected on the AUX – SYSTEM SETUP page. The temperature reference can be selected to one of the following choices: • Static Air Temperature (SAT) – This is the calculated temperature of the stationary (static) outside air. Conceptually, this is the temperature that would be read on a thermometer floating stationary at the current location. • Total Air Temperature (TAT) – This is the calculated temperature of the outside air as it moves past the aircraft, including the rise in temperature due to air compression and friction at the current airspeed. • Difference from International Standard Atmosphere (ISA) – This is the difference between SAT and standard (ISA) temperature at the current altitude. This provides an indication of how much warmer/colder the temperature is from a “standard” atmosphere. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 11 PRIMARY FLIGHT DISPLAY GPS Approach PRIMARY FLIGHT DISPLAY (PFD) 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 Selected DME DME Hold Annunciation Set Hold for Selected DME DME Indication PRIMARY FLIGHT DISPLAY Clock/Timer The Clock/Timer function displays a clock or timer window in the lower left corner of the PFD. Show/Hide Clock Select Timer Show/Hide Timer Select Clock Start/StopTimer Reset Timer Clock and Timer Functions Attitude Indicator The standby mechanical Attitude Indicator in your aircraft is either a Ground Pointer or a Roll Pointer configuration. The GDU 620 Attitude Indicator has been configured in either a Ground Pointer or a Roll Pointer configuration to match the configuration of your aircraft’s standby Attitude Indicator. In an aircraft with an Attitude Indicator that has a Ground Pointer, the pointer above the roll scale shifts with the roll or bank angle of the aircraft to keep the Roll Scale Zero Pointer pointing towards the ground. Roll Scale Zero Pointer Roll Pointer Roll Scale Attitude Indicator with a Ground Pointer Configuration in a Left Turn In an aircraft with an Attitude Indicator that has a Sky Pointer, the pointer below the roll scale shifts with the roll or bank angle of the aircraft to keep the 12 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Roll Pointer pointing towards the sky. Roll Scale Zero Pointer Roll Pointer Roll Scale Attitude Indicator with a Sky Pointer Configuration in a Left Turn 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. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 13 PRIMARY FLIGHT DISPLAY The Slip/Skid Indicator is the bar beneath the roll pointer. The indicator moves with the roll pointer and moves laterally away from the pointer to indicate lateral acceleration. Slip/skid is indicated by the location of the bar relative to the pointer. One bar displacement from the roll pointer is equivalent to one ball displacement on a traditional Slip/Skid Indicator. PRIMARY FLIGHT DISPLAY (PFD) Current Heading Current GPS Track Turn Rate Markings Heading Trend HSI Heading Markings PRIMARY FLIGHT DISPLAY NOTE: If magnetic heading is lost, GPS ground track will be displayed in place of heading. Adjusting the Course Pointer Press the CRS key and turn the PFD knob to select a course for a VOR/ILS or OBS mode course. HSI Bearing Pointers NOTE: The Bearing Pointer for navigation source 1 (BRG1) will be an arrow with a single line. The Bearing Pointer for navigation source 2 (BRG2) will be an arrow with a double line. To toggle between the available bearing pointers, press the PFD soft key, then the BRG soft key, and then the BRG1 or BRG2 soft keys. The BRG1 soft key cycles through modes NAV1 and GPS1. Additionally, ADF is available if an ADF source is installed. The BRG2 soft key cycles through modes, NAV2 and GPS2 if a second NAV or GPS source is available. Additionally, ADF is available if an ADF source is installed. 14 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) BRG1 Pointer BRG2 Pointer Selected source for BRG 2 bearing pointer Bearing Pointers on the HSI GPS1 GPS2 VOR1 VOR2 LOC1 LOC2 CDI Source GPS Mode GPS Advisory LOI Suspend MSG LOI OCN ENR TERM APR LNAV LNAV+V LNAV/VNAV LPV LP LP +V 1.00nm 0.30nm OBS SUSP PFD HSI Annunciations 190-00601-03 Rev G G500/600 Cockpit Reference Guide 15 PRIMARY FLIGHT DISPLAY Selected source for BRG 1 bearing pointer PRIMARY FLIGHT DISPLAY (PFD) CDI Source The CDI Source on the HSI will display which navigation source is selected. Navigation sources available: GPS1, VOR1, or LOC1. Navigation sources available: GPS2, VOR2, or LOC2, if a second source is available. GPS Mode The GPS Mode annunciation on the HSI indicates the current CDI scaling of the GPS navigator. See the GPS navigator pilot’s guide for a description of each mode. PRIMARY FLIGHT DISPLAY GPS Advisory MSG: Displays when a new advisory message is displayed on the GPS navigator. LOI (Loss of Integrity): Displays when GPS integrity is lost. Suspend OBS: Displays when OBS mode is activated. SUSP: Displays when automatic waypoint sequencing on the interfaced GPS unit is suspended. Marker Beacon Annunciations Marker Beacon Location Marker Beacon Location Marker Beacons Current Beacon Icon (Standard) Icon (Blink) Inner Marker Middle Marker Outer Marker 16 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Miscompare Annunciations For complete description and conditions of miscompare annunciations, see the G500/600 Pilot’s Guide, P/N 190-00601-02. Pitch and Roll Miscompare PRIMARY FLIGHT DISPLAY Pitch Miscompare Roll Miscompare Miscompare Annunciations 190-00601-03 Rev G G500/600 Cockpit Reference Guide 17 PRIMARY FLIGHT DISPLAY (PFD) PRIMARY FLIGHT DISPLAY Switching Between Navigation Sources GPS NAVIGATOR 1 VLOC NAVIGATOR 1 GPS NAVIGATOR 2 VLOC 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 (VOR1 and VOR2, or GPS1 and GPS2). 18 NOTE: Verify the navigation source by the indication on the HSI. NOTE: The selected navigator is the source for all PFD and MFD functions, except for bearing pointers and external TAWS PFD annunciations. G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Autopilot (AP) The G500/600 is able to interface to certain autopilot systems to provide the functions described in this section. Please refer to your particular Airplane Flight Manual and autopilot documentation for specific information and operating instructions. GAD 43 Attitude If the GAD 43 Adapter is providing attitude to the autopilot, test the disconnect mechanism prior to each flight in the following manner: 1) Allow all avionics to complete power up and begin normal operation. 2) Engage the autopilot while on the ground. NOTE: If the AP TEST soft key is held for longer than one second, the test will not run. CAUTION: Do not use the autopilot if the AP TEST key fails to disconnect the autopilot. Autopilot Disconnect When the GDU 620 attitude monitors have detected an AHRS malfunction, or the inability to actively monitor the AHRS, a “Check Attitude” annunciation will be displayed on the PFD and the autopilot will automatically disconnect. NOTE: Only appears with the installation of an optional GAD 43 Adapter. Check Attitude Annunciation 190-00601-03 Rev G G500/600 Cockpit Reference Guide 19 PRIMARY FLIGHT DISPLAY 3) Press and release the AP TEST soft key and verify that the autopilot disconnects normally. PRIMARY FLIGHT DISPLAY (PFD) Heading PRIMARY FLIGHT DISPLAY The GDU 620 heading bug may be used in conjunction with the “Heading” mode of supported autopilots. When the autopilot is in “heading” mode and the heading bug is adjusted in the normal manner, and the autopilot will turn to and maintain the selected heading. Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot heading mode. Selected Heading Box on HSI Altitude Capture (Optional Upgrade) Adjust the altitude bug in the normal manner when using the altitude capture interface. Some autopilot installations support arming and disarming of the selected altitude using the ALT key on the PFD. The PFD knob window will indicate when this function is available. The selected altitude may be alternately armed or disarmed by pressing and holding the ALT key on the PFD bezel. Arm/Disarm Altitude Bug Autopilot Navigation The GDU 620 acts as a switching source between the installed navigation sources (e.g. GPS/VLOC 1-2). The navigation source that is displayed on the HSI is sent to the autopilot. Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot navigation functions. 1) Set your navigation source and HSI to the desired course. 2) Engage your autopilot in navigation mode. 3) Control your autopilot navigation through the navigation source and the HSI. 20 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) GPSS The GDU 620 will send the GPSS commands from the displayed GPS source to the autopilot. For example, if GPS 1 is displayed on the HSI, the GPSS commands from GPS 1 will be sent to the autopilot. Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the autopilot’s GPSS function. NOTE: GPSS commands are not sent to the autopilot when a VLOC source is displayed on the HSI. 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. GPSS OFF GPSS ON GPSS Mode Control When GPSS mode is on, the heading bug on the HSI changes to a hollow outline and a crossed-out heading bug appears in the PFD Knob Mode Indicator, indicating that the autopilot is not coupled to the heading bug. The bug is still controllable and may still be used by the pilot for reference. GPSS is annunciated in the lower left portion of the PFD. The GPSS mode annunciation depends on the location of the NAV STATUS information, as shown in the following figure. NAV Status Style 2 NAV Status Style 1 GPSS Mode Annunciations 190-00601-03 Rev G G500/600 Cockpit Reference Guide 21 PRIMARY FLIGHT DISPLAY 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. PRIMARY FLIGHT DISPLAY (PFD) Flight Director Display PRIMARY FLIGHT DISPLAY Flight director commands are presented as a single cue flight director on the PFD. SVT Off SVT On Flight Director Bars Showing Aircraft Pitch Vertical Speed Control The GDU 620 vertical speed bug may be used to control vertical speed with certain autopilots. Refer to the Airplane Flight Manual and autopilot system documentation for instructions on how to use the vertical speed mode, if available. Adjust the vertical speed bug in the normal manner when using the vertical speed mode interface. Some autopilot installations support engaging/disengaging the vertical speed mode using the VS key on the PFD. The vertical speed mode may be alternately engaged or disengaged by pressing and holding the VS key on the PFD bezel. Engage/Disengage VS Bug 22 G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) Autopilot Mode Annunciations Some autopilots support mode annunciations located at the top of the PFD. Refer to the Airplane Flight Manual and autopilot system documentation for details on the autopilot mode annunciations. When autopilot annunciations are displayed at the top of the PFD, the Nav Status information will be located to the left of the HSI (NAV STATUS Style 2). Roll Modes Autopilot Status Pitch Modes Active Mode Armed Mode Active Mode Armed Mode 190-00601-03 Rev G G500/600 Cockpit Reference Guide PRIMARY FLIGHT DISPLAY Autopilot Annunciations 23 PRIMARY FLIGHT DISPLAY (PFD) Additional Features Synthetic Vision Technology™ Synthetic Vision Technology (SVT) is offered as a feature to the G500/600. SVT is primarily comprised of a computer-generated forward-looking, attitude aligned view of the topography immediately in front of the aircraft from the pilot’s perspective. SVT information is shown on the PFD. SVT offers a three-dimensional view of terrain and obstacles. Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red. PRIMARY FLIGHT DISPLAY Airport Sign Zero-Pitch Line Horizon Heading Mark Obstacle Flight Path Marker SVT Terrain Terrain Threat SVT Soft Keys Synthetic Vision Imagery 24 NOTE: SVT will become disabled if the databases necessary to display SVT are unavailable (generating a GDU DB ERR or SVT DISABLED alert) or AHRS or GPS data is unavailable. SVT may be restored once the fail conditions are removed by following the steps in “Displaying SVT Terrain.” G500/600 Cockpit Reference Guide 190-00601-03 Rev G PRIMARY FLIGHT DISPLAY (PFD) The following features are part of the Synthetic Vision Technology. For more details refer to the G500/600 Pilot’s Guide, Rev. G or later. •Flight Path Marker •Horizon Heading Marks •Terrain/Obstacle Display and Alerting •Three-dimensional Traffic •Wind Vectors •Airport Signs •Runway Display •Water •Zero-Pitch Line •Altitude Minimums Bug NOTE: SVT may be deactivated under certain conditions, such as loss of heading. Once the condition is resolved SVT may restart automatically, otherwise, to reactivate SVT, press the PFD soft key followed by the SYN VIS soft key, then the SYN TERR soft key. NOTE: SVT features are not a substitute for standard course and altitude deviation information using the CDI, VSI, and VDI. Displaying SVT™ Terrain 1) Press the PFD soft key. 2) Press the SYN VIS soft key. 3) Press the SYN TERR soft key. 4) Press the BACK soft key to return to the previous page. Displaying Heading on the Horizon 1) 2) 3) 4) 5) Press the PFD soft key. Press the SYN VIS soft key. If 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) 2) 3) 4) Press the PFD soft key. Press the SYN VIS soft key. If not already enabled, press the SYN TERR soft key. Press the APTSIGNS soft key. 5) Press the BACK soft key to return to the previous page. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 25 PRIMARY FLIGHT DISPLAY MULTI-FUNCTION DISPLAY (MFD) Multi-Function Display (MFD) MULTI-FUNCTION DISPLAY 7 6 5 4 2 1 3 Multi-Function Display (MFD) NOTE: In some models or installations, the PFD and MFD and their controls are switched to the other side. 1 Soft Keys 2 Large MFD knob: Use to move between page groups. 3 Small MFD knob: Use to move within page groups. 4 Enter: Validates or confirms a menu selection or data entry. 5 Clear: Erases information, cancels entries, or removes page menus. Pressing and holding the CLR key displays the first page of the Map Group. 6 Menu: Displays configuration items for each page of the page groups. 7 Range Select: Changes the range on the map pages. Up arrow zooms out, down arrow zooms in. Also aids in scrolling up and down text pages. 26 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MULTI-FUNCTION DISPLAY (MFD) Page Navigation - Moving Between Pages Page Group Turn Large MFD knob Page Turn Small MFD knob 1) Turn the large MFD knob to move between page groups. 2) Turn the small MFD knob to change pages within the page group. NOTE: Page Group and Page are shown at the bottom of the MFD. 1) Press the MENU key and make the necessary adjustments with the large MFD knob and small MFD knobs. 2) Press the small MFD knob to activate editing. 3) Turn the large MFD knob to select the desired item. 4) Turn the small MFD knob to change the highlighted value. 5) Press ENT to accept displayed value or press the small MFD knob to cancel selection or exit the editing mode. Default Map Page Press and hold the CLR key to return to the first page of the MAP group. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 27 MULTI-FUNCTION DISPLAY Changing Settings within a Page 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. MAP Navigation Map 2 Split Screen Navigation Map 1 Declutter Map Traffic Topo Terrain Declutter Map Traffic Topo Terrain Traffic* Terrain Declutter View 360 Map Arc Traffic Inhibit Topo Terrain * Softkeys depend on configuration MULTI-FUNCTION DISPLAY WX Weather Map 1 Legend FCST Time (XM) WX Alt Dn WX Alt Up Weather Map 2 Legend FCST Time (XM) WX Alt Dn WX Alt Up AUX External Video System Setup XM Info Lock Default Unit RA Test Dflt Spd Video 1 Video 2 Setup XM Radio System Status DB ACTV DB SYNC LRU Active Fpl Info Category CAT CAT + ALL Channel CH CH + DIR CH AUX 28 Weather Radar Weather Map 3 Mode Legend Control FCST Time (XM) Horizon WX Alt Dn Vertical WX Alt Up Back Volume Mute Vol Vol + Presets PS1 PS2 ... PS15 (continued) Position Reporting Iridium Phone Dial Answer Hang Up Vol Keys 1234 5678 90*# Send FPL Wpt Info Charts INFO/MAP NOTAM Rwy/Freq Detail APT DIR Select WX/NOTAM Header Plan Profile Minimums G500/600 Cockpit Reference Guide ALERTS TRND/ACK CAPTURE BACK 190-00601-03 Rev G MAP GROUP Map Group Navigation Map 1 and Navigation Map 2 Pages Soft Keys Found on Navigation Map Pages 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). 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 1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group, while the map pointer is active, move the map pointer to highlight a waypoint. 2) Press ENT to display information about the highlighted waypoint. 3) Press the INFO soft key (if available) to view more information about the highlighted waypoint. 4) Press the WX soft key (if available) to view TAF and METAR information. Press the small MFD knob again to return to the map. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 29 MAP GROUP: NAV PAGES Moving the Map Pointer Around the Map (Panning) MAP GROUP Decluttering (DCLTR) the Map Pages MAP GROUP: SETUP OPTIONS There are four levels of decluttering, DCLTR, DCLTR-1, DCLTR-2, and DCLTR-3. DCLTR shows the most detail while DCLTR-3 removes most detail. While viewing Navigation Map 1 or Navigation Map 2 page of the Map Page Group, press the DCLTR soft key. Each successive press of the DCLTR soft key will toggle through the declutter levels. Turning on Map Overlays While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group, press the MAP soft key. Select the Traffic, TOPO, or Terrain overlays by pressing the appropriate soft key. Measuring Distances 1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group, press MENU. 2) Turn the large MFD knob or the small MFD knob to highlight “Measure Bearing/Distance” and then press ENT. 3) Turn the large or small MFD knobs to move the map pointer. The distance, bearing, and coordinates are displayed at the top of the screen. Distance, Bearing and Coordinates Display Measuring Map Pointer 4) Press ENT to reset the distance and bearing values. 5) Press the small MFD knob to stop measuring. 30 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP Customizing Maps 1) While viewing Navigation Map 1 or Navigation Map 2 of the Map Page Group, press the MENU key. MAP GROUP: SETUP OPTIONS Map Setup Option Menu 2) Press the ENT key to enter the setup page. The selected group will be flashing. 3) Turn the small MFD knob to activate the drop down menu and to move within available groups (Map, Weather, Traffic, or Aviation). Available Groups 4) Press the ENT key to select the group and set your preferences. 5) Turn the large MFD knob to move between fields. 6) Turn the small MFD knob to display available options. Press the ENT key to select your preference and move to the next option. 7) When completed with setting preferences, press the small MFD knob to return to the Navigation Map 1 page. 8) Repeat the above steps to set preferences for the remaining groups. NOTE: In the Map Options Setup section, the selected range is defined as the map range below which the display feature will be visible. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 31 MAP GROUP MAP GROUP: SETUP OPTIONS Map Setup Options Group MAP Selections •Orientation (North Up, Track Up, DTK up, HDG up) •North Up At (Off to 500 NM) •Auto Zoom (On or Off) •Land Data (On or Off) •Track Vector Length (Off to 20 mins) •Wind Vector (On or Off) •Enhanced Range Ring (On or Off) •Topo Data (On or Off) •Topo Scale (On or Off) •TERRAIN Data (On or Off) •Obstacle Viewing Range (Off to 15 NM) •Power Line Viewing Range (Off to 15 NM) •Lat/Lon Viewing Range (Off to 500 NM) •Selected Alt Range Arc (On or Off) •NEXRAD Data Viewing Range (Off to 500 NM) •NEXRAD Cell Movement (On or Off) WEATHER •NEXRAD Legend (On or Off) •NEXRAD Source (US or Canada) •XM Lightning Viewing Range (Off to 500 NM) TRAFFIC •Traffic Mode (Off, All Traffic, TA/PA, TA Only) •SafeTaxi Viewing Range (Range: Off to 2.5 NM) •RWY Extension Range (Range: Off to 2.5 NM) •INT/NDB Viewing Range (Range: Off to 15 NM) •VOR Viewing Range (Range: Off to 150 NM) •Class B/TMA (Range: Off to 500 NM) •Class C/TCA (Range: Off to 150 NM) •Class D (Range: Off to 150 NM) AVIATION •Restricted (Range: Off to 150 NM) •MOA (Military) (Range: Off to 150 NM) •Other/Adiz (Range: Off to 150 NM) •TFR (Range: Off to 500 NM) •Airways (Off, All, LO Only, HI Only) •Smart Airspace (On or Off) •Show Airspaces (All, Below 18000ft - Below 3000ft) •Airspace Labels (On or Off) 32 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP 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. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 33 MAP GROUP: SETUP OPTIONS SafeTaxi® (Optional) SafeTaxi is an enhanced feature that gives greater map detail when zooming in on airports at close range. The airport display on the map reveals runways with numbers, taxiways with identifying letters/numbers, and airport landmarks including ramps, buildings, control towers, and other prominent features. Resolution is greater at lower map ranges. When the aircraft location is within the screen boundary, including within SafeTaxi ranges, an airplane symbol is shown on the navigation map views for enhanced positional awareness. This database is updated on a 56-day cycle. MAP GROUP Split Screen Page (Optional) Soft Keys Found on Split Screen Page MAP GROUP: SPLIT SCREEN PAGE External Video is an optional function that displays video provided by an externally mounted video source on the aircraft. 1) While viewing the Map function, turn the small MFD knob to the third page of the map group. Current Video Source Display of External Video Source Map Display 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. 34 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP Traffic Map Page (Optional) Soft Keys Found on Traffic Map Page OPERATE STANDBY MOTION ALT MODE DESELECT STANDBY ABSOLUTE RELATIVE OFF DURATION BACK BELOW NORMAL ABOVE UNRSTD Traffic Display When a traffic alert is generated by an interfaced traffic system, the PFD will display a traffic annunciator and the MFD will have a pop-up screen displaying the detected traffic, if not viewing the Traffic page. To remove the pop-up, press the CLR key. Press the ENT key to go to the traffic page. The traffic pop-up window will be removed when the traffic alert is no longer active. Traffic Annunciation Traffic Traffic Pop-Up PFD Traffic Display 190-00601-03 Rev G MFD Traffic Pop-Up Window G500/600 Cockpit Reference Guide 35 MAP GROUP: TRAFFIC PAGE OPR/STBY MAP GROUP Displaying and Operating Traffic Advisory Systems (TAS) Operating Mode Range Ring Non-Threat Traffic Traffic Advisory, Off Scale Aircraft is Out of Range, 1200 ft Above and Climbing MAP GROUP: TRAFFIC PAGE Ownship Symbol Proximity Advisory, Aircraft is 5000 ft Above and Descending Traffic Advisory, 1200 ft Above and Climbing Non-Bearing Traffic (System is Unable to Determine Bearing), Aircraft Distance is 8.0 NM, 1100 ft Above and Descending Traffic Map - TAS NOTE: Depending on your traffic configuration, the OPERATE and STANDBY soft keys may not be available. Traffic Mode Field Altitude Mode Field 36 NOTE: Some traffic systems will not enter standby mode while airborne. G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP Press the ALT MODE soft key to change what traffic is displayed. Pressing the BELOW, NORMAL, ABOVE or UNRSTD soft keys will determine what traffic is displayed. The selection is shown in the altitude mode field. The values below define what each altitude mode displays, relative to the altitude of the aircraft. Soft Key BELOW NORMAL ABOVE UNRSTD Description Displays traffic from -9900 to +2700 ft Displays traffic from -2700 to +2700 ft Displays traffic from -2700 to +9900 ft All traffic is displayed (unrestricted) from +/-9900 ft 1) While viewing the Traffic Map Page of the Map Page Group, press the MENU key and select Test Mode from the menu. 2) Verify that a traffic message is shown next to the altitude tape on the PFD and that the traffic pop-up is displayed on the MFD. After a few seconds, test mode is exited automatically by the traffic system. Traffic Annunciation Traffic Annunciation on PFD 190-00601-03 Rev G G500/600 Cockpit Reference Guide 37 MAP GROUP: TRAFFIC PAGE TAS Test Mode (On Ground) MAP GROUP MAP GROUP: TRAFFIC PAGE TIS Traffic The Traffic Map Page is configured to show surrounding TIS traffic data in relation to the aircraft’s current position and altitude, without clutter from the basemap. Aircraft orientation on this map is always heading up unless there is no valid heading. TIS receives traffic information from ground stations, and is updated every five seconds. The GDU 620 displays up to eight traffic targets within a 7.5-NM radius, from 3000 feet below to 3500 feet above the requesting aircraft. Displaying TIS Traffic While viewing the Traffic Page of the Map Page Group press the OPERATE soft key to begin displaying traffic. “TIS OPER” is displayed in the upper left hand corner of the MFD. NOTE: TIS is disabled when a Traffic Advisory System (TAS) is installed. Operating Mode Traffic Advisory, Aircraft is 1200 feet above, climbing, and moving in the direction of the line Proximity Advisory, Aircraft is 3000 feet above, descending, and moving in the direction of the line 38 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP ADS-B Traffic (Optional) The ADS-B traffic page provides an enhanced display of traffic from a compatible ADS-B In system. Available ADS-B traffic features may include individual target selection and other details, such as type, direction, groundspeed, and motion. ADS-B and TCAS Status and Altitude Filter Selected Traffic Info Traffic Motion Vector Basic Directional Traffic, 4000 ft Below and Climbing Ownship Icon Range Rings Turn Cursor Knob for Next Target Selected Vector Motion and Duration NOTE: ADS-B targets will be shown as the filled-in icon when they are within 6NM laterally and 1200 ft vertically of the ownship; otherwise, they are shown as the hollow icons. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 39 MAP GROUP: TRAFFIC PAGE Map Orientation Range Ring Radius MAP GROUP ADS-B Target Selection Traffic targets displayed on the dedicated traffic page may be selected in order to obtain additional information about a traffic target. 1) Press the small MFD knob to start target selection. 2) Turn the small or large MFD knobs to step through selection of the available targets. MAP GROUP: TRAFFIC PAGE 3) Press the small MFD knob to stop target selection. Press the DESELECT key to stop selection and/or clear target selection. ADS-B Status ADS-B Status displays the current status of traffic application: Off, Surface, Airborne, Fail, Test, or N/A. TAS/TCAS/TCAD Status This shows the current operating mode/status of an interfaced TAS/TCAS/ TCAD system: STBY, GND, APR, OPER, or FAIL. ADS-B Motion Vector When Absolute Motion Vectors are selected, the vectors extending from the traffic targets depict the target reported track and speed over the ground. When Relative Motion Vectors are selected, the vectors extending from the traffic targets display how the traffic target is moving relative to your aircraft. These vectors are calculated using the traffic target’s track and ground speed and your aircraft’s track and ground speed. These two values are combined to depict where the traffic target is moving purely with respect to your aircraft and give a forecast of where the traffic target will be, relative to your aircraft, in the near future. 40 NOTE: Absolute motion vectors are the same color as the traffic target. Relative motion vectors are yellow for TAs and otherwise are green. The annunciation on the bottom of the dedicated traffic page indicates which vector type is selected and their length. NOTE: Relative motion vectors are not available on the ground. G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP Terrain/TAWS-B Page (Optional) Soft Keys Found on Terrain/TAWS-B Page 360 ARC INHIBIT Garmin provides the following Terrain/TAWS selections, based upon your system configuration. WARNING: Do not use Terrain-SVT information for primary terrain avoidance. Terrain-SVT is intended only to enhance situational awareness. NOTE: Terrain data is not displayed when the aircraft latitude is greater than 75° North or 60° South. NOTE: Terrain-SVT is standard when the Synthetic Vision Technology (SVT) option is installed. The TAWS option will take precedence over Terrain-SVT. NOTE: TAWS alerts will be generated by the GPS TAWS unit on the PFD if an external TAWS unit is installed and interfaced to the G500/600. •TERRAIN-PROXIMITY - is a non-TSO-C151b certified terrain awareness system. Do not confuse Terrain Proximity with TAWS. TAWS is TSOC151b certified and Terrain Proximity is not. Terrain Proximity does not provide warning annunciations or voice alerts, it only provides color indications on map displays when terrain and obstacles are within a certain altitude threshold from the aircraft. •TERRAIN-SVT - refers to a subset of Class B TAWS that meets the terrain alerting requirements outlined in Section 7.b of AC 23-26. Terrain-SVT is a non-TSO-C151b certified terrain awareness system. Do not confuse Terrain-SVT with TAWS. TAWS is TSO-C151b certified and TerrainSVT is not. Terrain-SVT is a subset of Class B TAWS that provides a 190-00601-03 Rev G G500/600 Cockpit Reference Guide 41 MAP GROUP: TERRAIN/TAWS-B PAGE VIEW MAP GROUP MAP GROUP: TERRAIN/TAWS-B PAGE Class B TAWS FLTA functionality, including visual alerting and aural alerting. Terrain-SVT is provided with the Synthetic Vision functionality and not marketed separately. Garmin Terrain-SVT is available in GDU 620 v3.00 or later, with SVT enabled. •TAWS-B - is an optional feature developed that meets the terrain alerting and ground proximity requirements for Class B TAWS system as defined in TSO-C151b. Viewing Terrain NOTE: Obstacles/Wires will be removed from the Terrain/TAWS page when range (RNG) exceeds 10 NM. While viewing the Terrain/TAWS-B page of the Map Page Group, press the VIEW soft key and then press the 360 or ARC soft keys to select the desired view. 360 or ARC Soft Keys Pressing the INHIBIT soft key, deactivates the PDA/FLTA aural and visual alerts. See AFMS for guidance on inhibiting TAWS. Inhibit Soft Key Press MENU for selections to hide or show Aviation Data Overlay on the Terrain page. NOTE: Installations with a valid external TAWS-B source will not display the INHIBIT key. Aviation Data Overlay 42 G500/600 Cockpit Reference Guide 190-00601-03 Rev G MAP GROUP Terrain Pop-Up Alerts TAWS-B Pop-Up Alert on MFD TERRAIN-SVT™ Pop-Up Alert TERRAIN-SVT alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Refer to the Alerts section of this guide for more information on alerts, both visual and aural. When an alert is issued, annunciations appear on the PFD and MFD (TAWS page only). If the TERRAINSVT 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. TAWS-B Pop-Up Alert TAWS-B alerts typically employ a CAUTION or a WARNING alert severity level, or both. When an alert is issued, visual annunciations are displayed and aural alerts are simultaneously issued. Refer to the Alerts section of this guide for more information on alerts, both visual and aural. When an alert is issued, annunciations appear on the PFD and MFD (TAWS page only). If the TAWS-B Page is not displayed at the time, a pop-up alert appears on the MFD. To acknowledge the pop-up alert and return to the currently viewed page, press the CLR key. To acknowledge the pop-up alert and go to the TAWS-B page, press the ENT key. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 43 MAP GROUP: TERRAIN/TAWS-B PAGE TERRAIN-SVT Pop-Up Alert on MFD WX GROUP WX Group WX GROUP: XM WEATHER PAGES XM Weather Map Pages Soft Keys Found on XM Weather Map Pages LEGEND FCST TIME WX Alt Dn WX Alt Up NOTE: The preferences set on XM Weather Map pages are unique to each page. Customizing the Weather Map 1) While viewing any of the XM Weather Map pages in the WX Page Group, press the MENU key to display the page menu. Press ENT. 2) Turn the small MFD knob to select Weather Setup 1 or Weather Setup 2 and press ENT. 3) Turn the large MFD knob to select desired item to change. Turn the small MFD knob to set the preference of the weather feature option. 4) Press ENT to confirm your selection. 5) To return to the XM Weather Map page, press the small MFD knob. 44 G500/600 Cockpit Reference Guide 190-00601-03 Rev G WX GROUP XM Weather Items WX Page Menu - Weather Setup Adjustment Map Orientation NEXRAD Data Viewing Range NEXRAD Legend Source Echo Top Data Viewing Range Cloud Top Data Viewing Range Lightning Data Viewing Range Cell Mov Data Viewing Range SIG/AIR Viewing Range PIREPS Data Viewing Range METAR Data Viewing Range Surface Data Viewing Range Frz Lvl Data Viewing Range Wnds Aloft Data Viewing Range County Data Viewing Range TFR Data Viewing Range AIREPS Data Viewing rnage Icing Data Viewing Range Turbulence Data Viewing Range Cyclone Data Viewing Range North Up, Track Up Off, 10 NM to 500 NM On/Off US, Canada Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 50 NM to 500 NM WX GROUP: XM WEATHER PAGES Menu Item NOTE: Due to similarities in color schemes, it is not possible to display NEXRAD Data and Echo Top Data at the same time. NOTE: Due to similarities in color schemes, it is not possible to display Echo Top Data and Cloud Top Data at the same time. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 45 WX GROUP WX GROUP: XM WEATHER PAGES 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. 3) Exit and return to the map page by pressing either the LEGEND soft key, ENT key, or the small MFD knob. Mini-Legend Changing Forecast Time 1) When the Surface Data products (Surface Analysis and City Forecasts) are displayed, the time period for these forecasts can be changed with the FCST TIME soft key. 2) Press the FCST TIME soft key to cycle through the age of the information in 12 hour increments from CURRENT to 48 HR. Changing Weather Altitude 1) When Winds Aloft, Turbulence, or Icing products are displayed, the altitude for these forecasts can be selected with the WX Alt Up/Dn soft keys. 2) Press the WX Alt Dn or WX Alt Up soft keys to cycle through the available forecast periods as shown on the right side of the weather page. 46 G500/600 Cockpit Reference Guide 190-00601-03 Rev G WX GROUP Garmin Flight Data Services (GFDS) 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 G500/600 Pilot’s Guide, P/N 190-00601-02. After registering you are able to display GFDS data: 1) While viewing any one of the three pages of the WX Group, press the MENU button. 2) Highlight GFDS Data Request and press the ENT button to display the GFDS DATA REQUEST page. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 47 WX GROUP: GFDS PAGES Soft Key Found on GFDS Weather Map Pages WX GROUP Coverage Area Distances: Remaining FPL, Next 50 NM Next 500 NM Coverage Area Width of Coverage: 50 NM - 500 NM WX GROUP: GFDS PAGES Update Rate: Off - 60 Minutes Cancel Manual Request Manual Request Status of Request GFDS Data Request Page Configuring GFDS Data Request Page 1) Turn the large MFD knob to the Coverage box. Press ENT to select or deselect the coverage areas. Selected coverage areas are denoted by a green check mark. 2) Turn the large MFD knob to the Auto Request box and press ENT to change the update rate to either OFF or ON. 3) Turn the large MFD knob to the Manual Request box and press ENT to either send request or cancel current request. 4) Press the small MFD knob to return to the GFDS page. 48 G500/600 Cockpit Reference Guide 190-00601-03 Rev G WX GROUP FIS-B Weather Map Pages LEGEND FCST TIME WX Alt Dn WX Alt Up NOTE: The preferences set on FIS-B Weather Map pages are unique to each page. Customizing the Weather Map 1) While viewing any of the FIS-B Weather Map pages in the FIS-B Page Group, press the MENU key to display the page menu. 2) Turn the small MFD knob to select Weather Setup and press ENT. 3) Turn the large MFD knob to select the desired item to change. Turn the small MFD knob to set the preference of the weather feature option. 4) Press ENT to confirm your selection. 5) To return to the FIS-B Weather Map page, press the small MFD knob. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 49 WX GROUP: FIS-B WEATHER PAGES Soft Keys Found on FIS-B Weather Map Pages WX GROUP FIS-B Weather Items WX GROUP: FIS-B WEATHER PAGES WX Page Menu - Weather Setup 50 Menu Item Adjustment Map Orientation NEXRAD Data Viewing Range NEXRAD Legend Source SIG/AIR Viewing Range PIREPS Data Viewing Range METAR Data Viewing Range Wnds Aloft Data Viewing Range TFR Data Viewing Range North Up, Track Up Off, 10 NM to 500 NM On/Off CONUS, Regional, Combined Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM Off, 10 NM to 500 NM G500/600 Cockpit Reference Guide 190-00601-03 Rev G WX GROUP Weather Radar (Optional) Weather Radar Map Page Soft Keys Found on Weather Radar Map Page Operating Mode Weather Alert (GWX only) Control Window Precipitation Scale Weather Radar 190-00601-03 Rev F G600 Cockpit Reference Guide 51 WX GROUP: WEATHER RADAR Operating Mode WX GROUP Airborne Color Weather Radar WX GROUP: WEATHER RADAR WARNING: Begin transmitting only when it is safe to do so. If transmitting on the ground is necessary, ensure that no personnel or objects are within the minimum safe distance from the radar antenna. For Garmin GWX radars, the minimum safe distance may be up to 14 feet. For 3rd-party radars, refer to the radar pilot’s guide or other manufacturer documentation to determine the minimum safe dis-tance. CAUTION: In Standby Mode, the antenna is parked at the center line. It is always recommended to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly. Displaying Weather on the Weather Radar Page 1) Turn the large MFD knob to select the last page of the WX Page Group. 2) Press the MODE soft key. 3) If the aircraft is on the ground, press the STANDBY soft key to initiate the warm-up period. After the warm-up is complete, the radar enters Standby Mode. After the aircraft is airborne, press the WEATHER soft key. OR If the aircraft is already airborne, press the WEATHER or GROUND soft key. The warm-up period is initiated, after which the radar begins transmitting. The horizontal scan is initially displayed. Press the BACK soft key, then the VERTICAL soft key to scan vertically. 4) Press the RNG keys to select the desired range. Adjusting Antenna Tilt 1) Press and turn the small MFD knob to 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. 52 G600 Cockpit Reference Guide 190-00601-03 Rev F WX 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°. 1) Press the CONTROL soft key. 2) Press the BRG soft key. Sector Scan (GWX Radars Only) 1) Press the small MFD knob and turn the large MFD knob to move to the SECTOR SCAN field. 2) Turn the small MFD knob to select FULL, 60°, 40°, or 20° scan. 3) If desired, readjust the Bearing Line to change the center of the Sector Scan. Turn the large MFD knob to move cursor to the BEARING field and turn the small MFD knob to adjust the line. Adjusting Gain WARNING: Changing the gain in Weather Mode (Garmin GWX units only) causes precipitation intensity to be displayed as a color not representative of the true intensity. Remember to return the gain setting to “Calibrated” for viewing the actual intensity of precipitation. 1) Press the small MFD knob and turn the large MFD knob to move to the GAIN field. 2) Turn the small MFD knob to adjust the gain for the desirable level. The gain setting is visible in the gain field as a movable horizontal bar in a flashing box. The line pointer is a reference depicting the calibrated position. 3) Press the ENT key to remove the cursor. 4) To restore the gain to the calibrated position, press the GAIN CAL soft key. 190-00601-03 Rev F G600 Cockpit Reference Guide 53 WX GROUP: WEATHER RADAR 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: WX GROUP Antenna Stabilization 1) To activate or deactivate the antenna stabilization, press the CONTROL soft key. WX GROUP: WEATHER RADAR 2) Press the STAB ON soft key to activate antenna stabilization or press the STAB OFF soft key to deactivate. The current stabilization condition is shown in the upper right of the weather radar display. Weather Attenuated Color Highlight (WATCH™) (GWX Weather Radar only) WATCH (Weather Attenuated Color Highlight) which helps identify possible “shadowing” effects of short-range cell activity – identifying areas where radar return signals are weakened, or attenuated, by intense precipitation (or large areas of lesser precipitation) and may not fully reflect the “storm behind the storm”. To activate the WATCH feature, press the CONTROL soft key. Press the WATCH soft key. Press the WATCH soft key again to deactivate. Automatic Standby When the weather radar system is in the Weather or Ground Map Mode, upon landing the system automatically switches to Standby Mode. Altitude Compensated Tilt (ACT) - GWX 70 only Altitude Compensated Tilt (ACT) automatically adjusts the tilt to compensate for altitude changes as you climb or descend. Turbulence Detection - GWX 70 only (optional) Turbulence Detection activates a feature that detects and displays severe turbulence. Turbulence Detection is inactive at ranges greater that 160 NM. This optional feature requires a separate enablement. See your dealer for details. If Turbulence Detection is enabled and available, Turbulence Detection will be reported as Inactive in any of the following conditions: • Scan orientation is not Horizontal • Scan range is greater than 160 NM • Radar mode is not Weather Ground Clutter Suppression (GCS) - GWX 70 only (optional) Ground Clutter Suppression reduces the amount of returns as a result of highly reflective objects on the ground, such as buildings or cities, while maintaining the intensity and size of weather returns. his optional feature requires a separate enablement. See your dealer for details. 54 G600 Cockpit Reference Guide 190-00601-03 Rev F AUX GROUP Aux Group External Video Page (Optional) Soft Key Found on External Video Page 1) While viewing the External Video Page of the Aux Page Group, press the desired video soft key (VIDEO 1, VIDEO 2, or FULL). 2) Press the SETUP soft key. The BRIGHTNESS in the CURRENT box will flash. Turn the small MFD knob to change the brightness of the video output. 3) Turn the large MFD knob to CONTRAST and turn the small MFD knob to change the contrast level of the video output. 4) Turn the large MFD knob to SATURATION and turn the small MFD knob to change the saturation level of the video output. 5) Press the small MFD knob to exit out of the setup mode. Setting the Zoom Level of the Video Output 1) While viewing the External Video Page of the Aux Page Group, press the small MFD knob. 2) Press the RNG (Range) keys to zoom in and out. The range of the zoom feature is 1x up to 10x. 3) Press the small MFD knob to exit. Setup Soft Key Video Soft Keys 190-00601-03 Rev G Full Soft Key G500/600 Cockpit Reference Guide 55 AUX GROUP: SYSTEM SETUP PAGE Setting Brightness, Contrast, and Saturation Levels The following steps can be applied to either Video 1 or Video 2. AUX GROUP System Setup Page Soft Keys Found on System Setup Page AUX GROUP: 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. Setting Airspeed References 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob. Turn the large MFD knob to move to the desired field in the AIRSPEEDS box. 2) Turn the small MFD knob to change the speeds and to also turn the speeds ON or OFF. When the speeds are turned ON they are shown near the bottom of the Airspeed Tape if airspeed is zero. V Speed References on Airspeed Tape 56 Airspeed References 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. G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP Selecting Wind Vector Styles 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob and turn the large MFD knob to move to the field in the PFD OPTIONS box. 2) Turn the small MFD knob to select the styles available for displaying wind vectors. Each style shows direction and velocity of the wind. Style 2 Style 3 Style 4 Style 1 Displays headwind and crosswind components Style 2 Displays total wind direction and speed. Style 3 Displays total wind direction with headwind and crosswind speed components. Style 4 Displays total wind direction in degrees with wind speed. Selecting NAV Status Styles When selected, Nav Status information is displayed on the PFD either on the top of the display (Style 1) or to the left of the HSI (Style 2). 1) While viewing the System Setup page of the AUX page group, press the small MFD knob to activate the cursor. 2) Turn the large MFD knob to highlight the desired NAV Status value. 3) Turn the small MFD knob to select the style and press ENT. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 57 AUX GROUP: SYSTEM SETUP PAGE Style 1 AUX GROUP Selecting Temperature Reference 1) While viewing the System Setup page of the AUX page group, press the small MFD knob to activate the cursor. Turn the large MFD knob to highlight the desired Temp Reference value. AUX GROUP: SYSTEM SETUP PAGE 2) Turn the small MFD knob to select the Temp Reference type and press ENT. Figure 3-44 Outside Air Temperature Selection Synchronization (For Dual Installations Only) NOTE: The SYNCHRONIZATION option will only be available if a second GDU 620 is installed. 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob and turn the large MFD knob to move to the desired field in the SYNCHRONIZATION box. 2) Turn the small MFD knob to turn ON or OFF synchronization of the CDI. Turn the large MFD knob to move to the BARO setting. Turn the small MFD knob to turn the synchronization of the barometer ON or OFF. Turn the small MFD knob to turn the synchronization of databases ON or OFF. 3) Press ENT to move to the DATE/TIME box or press the small MFD knob to exit the editing mode. Synchronization Option 58 G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP Setting Time Format 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob. Turn the large MFD knob to the desired field in the DATE/TIME box. The only items that are able to be modified is the TIME FORMAT and TIME OFFSET. The date and time are coordinated with the GPS. 2) Turn the small MFD knob to display your choices of LOCAL 12hr, LOCAL 24hr, and UTC (Universal Time, Coordinated). Turn the small MFD knob to the desired format and press ENT to confirm your selection. Setting Time Offset 2) Use the small MFD knob and large MFD knob to edit the time offset. 3) Press ENT to confirm your selection. Press the small MFD knob to exit the editing mode. To convert UTC to local time, a time offset must be chosen. See the table below to determine the time offset. Time Zone Atlantic Eastern Central Mountain Pacific Alaskan Hawaiian Standard Local Time Offset -4 hours -5 hours -6 hours -7 hours -8 hours -9 hours -10 hours 190-00601-03 Rev G Daylight Saving Time Offset -3 hours -4 hours -5 hours -6 hours -7 hours -8 hours -9 hours G500/600 Cockpit Reference Guide 59 AUX GROUP: SYSTEM SETUP PAGE 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. AUX GROUP AUX GROUP: SYSTEM SETUP PAGE MFD Display Units NOTE: At any time during the setting of your preferences, pressing the DFLT UNIT soft key will restore the settings for brightness, synchronization, time format, time offset and display units to the initial settings. NOTE: The corresponding GPS navigator must also be set to match the selection chosen (distance, speed, NAV angle, pressure, and temperature units) on the GDU 620. Setting Distance and Speed Units 1) Press the small MFD knob and turn the large MFD knob to move to the MFD DISPLAY UNITS box. 2) Turn the small MFD knob to display your choices of IMPERIAL, METRIC, and NAUTICAL units for distance and speed displayed on MFD. Press ENT to confirm your selection. Press the small MFD knob to exit editing mode. Setting Altitude and Vertical Speed Units 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob and turn the large MFD knob to move to the desired field of the MFD DISPLAY UNITS box. 2) Turn the small MFD knob to display your choices of FEET or METRIC units for altitude and vertical speed. Press ENT to confirm your selection. Press the small MFD knob to exit editing mode. Setting Nav Angle 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob and turn the large MFD knob to move to 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 of the SYSTEM DISPLAY UNITS box. 60 G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP 2) Turn the small MFD knob to display your choices of INCHES(in) or HECTOPASCALS (hpa) for your barometric pressure units. Press ENT to confirm your selection and move to the next preference or press the small MFD knob to exit editing mode. Setting Temperature Units 1) While viewing the System Setup Page of the Aux Page Group, press the small MFD knob and turn the large MFD knob to move to the desired field of the SYSTEM DISPLAY UNITS box. Data Link 1) Press the small MFD knob and turn the large MFD knob to move to the Data Link box. 2) Turn the small MFD knob to display your choices of the available WX/TFR Source. Press ENT to confirm your selection. Press the small MFD knob to exit editing mode. Radar Altimeter Test NOTE: Not all radar altimeters have the test function. Press the RA TEST soft key (if available) to activate the radar altimeter test. An RA TEST annunciation will be displayed on the PFD. For more information on the Radar Altimeter and its settings, see the latest revision of the G500/600 Pilot’s Guide, P/N 190-00601-02. RA TEST Annunciation on PFD If the unit fails the self-test, the RA FAIL annunciation will appear on the PFD. RA FAIL Annunciation on PFD 190-00601-03 Rev G G500/600 Cockpit Reference Guide 61 AUX GROUP: SYSTEM SETUP PAGE 2) Turn the small MFD knob to display your choices of CELSIUS(°C) or FAHRENHEIT(°F) for the temperature. Press ENT to confirm your selection and press the small MFD knob to exit editing mode. AUX GROUP XM® Information Page (Optional) Soft Key Found on XM Information Page AUX GROUP: XM RADIO PAGE While viewing the Aux Group, turn the small MFD knob to display the XM Information screen. This page contains the Data Radio and Audio Radio IDs. The only option on this page is to LOCK in your information once your subscription has been activated. XM Information Page 62 G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP XM® Radio Page (Optional) Soft Keys Found on XM Radio Page TO 1) While viewing the XM Radio page of the Aux Page Group, press the small MFD knob and then turn the small MFD knob to highlight the desired channel. 2) Press ENT to make the highlighted channel the Active Channel. 3) Press the small MFD knob to end editing. 4) Press CHNL and then the CH+ or CH- soft keys to increment up or down one channel at a time in the active category. 5) Press CHNL and then the DIR CH soft key to directly select a channel in the active channel field. Turn the small MFD knob and large MFD knob to select desired channel. 6) Press ENT to save the selection or press the small MFD knob to cancel selection. Selecting a Channel within a Category 1) Press CATGRY to highlight the category window. 2) Press CAT+ or CAT- to cycle through the different categories or turn the small MFD knob to the category and press ENT. 3) Turn the small MFD knob to move to the desired channel. 4) Press ENT to make that channel the active channel. 5) Press the small MFD to end editing. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 63 AUX GROUP: XM RADIO PAGE Selecting a Channel AUX GROUP Volume While viewing the XM Radio page of the Aux Group, press the VOL soft key. Press the VOL+ or VOL- soft keys or turn the small MFD knob to increase or decrease radio volume. Press the small MFD knob when done adjusting. To mute the radio, press the MUTE soft key. To restore the radio volume, press MUTE again or the VOL+ or VOL- soft keys. AUX GROUP: XM RADIO PAGE Storing a Preset Channel While viewing the XM Radio page, you may set a preset for the Active Channel. Press the PRESETS soft key. Press and hold a preset soft key, such as PS1 until it blinks. You are able to preset up to 15 channels. Recalling a Preset Channel While viewing the XM Radio page, press the PRESETS soft key and press the preset soft key for the desired stored channel, such as PS1. To move to the next group of presets, press the MORE soft key. 64 G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP Position Reporting Page Soft Key Found on Position Reporting Page Position Reporting Status The Status window shows the time until the next data transmission and the status of the reporting system. Settings Window 1) While viewing the Position Reporting page, press the small MFD knob. 2) Turn the large MFD knob to change the report type to either AFF (Automatic Flight Following) or Standard. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 65 AUX GROUP: POSITION REPORTING Position Reporting Page AUX GROUP Iridium® Phone Page (Optional) Soft Keys Found on Iridium Phone Page AUX GROUP: IRIDIUM PHONE Status Window Name and Phone Number Field Phonebook Catalog Icon Volume Level Iridium Phone Page For detailed use of the Iridium Phone system, see the latest revision of the G500/600 Pilot’s Guide, P/N 190-00601-02. Call Suppression 1) While viewing the Iridium Phone page, press the small MFD knob. 2) Turn the large MFD knob to select the Call Suppression type of Off, On, or On During APR/MAPR/TERM. The last setting will suppress call during approaches, missed approaches, or during terminal procedures. 66 G500/600 Cockpit Reference Guide 190-00601-03 Rev G AUX GROUP Creating Entries into Phonebook 1) While viewing the Iridium Phone page of the Aux Group, press the small MFD knob to activate the cursor. 2) Turn the large MFD knob to highlight the phonebook catalog icon. Turn the small MFD knob to display phonebook. 3) If the name already exists, it will be displayed in the drop down menu. If you are adding a new entry, highlight, (New Entry). Press ENT. 4) Turn the small MFD knob to enter each letter of the name. Press ENT. Deleting Entries into Phonebook 1) Press the small MFD knob to activate the cursor and then turn the large MFD knob to select the Phone Book Catalog icon. 2) Turn the small MFD knob to display the contents of the Phone Book Catalog and highlight the desired entry. Press ENT to select the catalog entry. 3) Turn the large MFD knob to highlight the DELETE key. Press ENT to delete the catalog entry. Press the small MFD knob again to cancel the selection cursor. Editing a Phone Book Catalog Entry 1) Press the small MFD knob to activate the cursor and then turn the large MFD knob to select the Phone Book Catalog icon. 2) Turn the small MFD knob to display the contents of the Phone Book Catalog and highlight the desired entry. Press ENT to select the catalog entry. 3) 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 1) While viewing the Iridium Phone page, enter a phone number using the KEYS soft key, rotary knobs, or select one from the Phone Book catalog. 2) Press the DIAL key. 3) After completing the call, press the HANG UP key. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 67 AUX GROUP: IRIDIUM PHONE 5) Turn the large MFD knob to move to enter the phone number. Turn the small MFD to enter each number. Press ENT. AUX GROUP System Status Page AUX GROUP: SYSTEM STATUS PAGE Soft Keys Found on System Status Page The System Status page of the AUX Page group shows the status, serial number, and version of LRUs as well as the effectivity information. There are no menu options. In the LRU Status column, a green check means the unit is present and operating properly, while a red X indicates an absence or failure. System Status 1) While viewing the System Status page of the Aux Page Group, press the DB ACTV soft key and turn the small MFD knob to view the list of the databases loaded into the GDU 620. Press the small MFD knob to exit. 2) Press the DB SYNC soft key synchronize databases with a second LRU. Press the small MFD knob to exit. 3) Press the LRU soft key and turn the small MFD knob to scroll through the status, serial number, and version of each LRU. Press the small MFD knob to exit. 68 G500/600 Cockpit Reference Guide 190-00601-03 Rev G FPL GROUP Flight Plan Group Active Flight Plan Page Soft Keys Found on Active Flight Plan Page Viewing Your Active Flight Plan Active Flight Plan Page 1) While viewing the Active Flight Plan page of the FPL Page Group, press the small MFD knob and then turn the large MFD knob to highlight waypoints in the flight plan. 2) Press the INFO soft key to view information about the highlighted waypoint. 3) Press the small MFD knob to return to the Active Flight Plan page. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 69 FPL GROUP: ACTIVE FLIGHT PLAN The active flight plan (as received from the active GPS unit) is shown on the first page of the Flight Plan page group. No changes to the flight plan can be made from the GDU 620. All flight plan changes must be made from the GPS unit. FPL GROUP Waypoint Information Page Soft Keys Found on Waypoint Information Page FPL GROUP: WAYPOINT INFO PAGE WX/NOTAM Facility Identifier Facility Name Facility Location Facility Type Bearing & Distance to Wpt from Present Position Map Region Lat/Lon Map Window Map Orientation Wpt Weather Info Soft Key Airport Directory Soft Key Info/Map Soft Key Rwy/Freq Soft Key Waypoint Information Page 1) While viewing the Waypoint Information page of the FPL Page Group, press the small MFD knob and then turn the small MFD knobs to enter or select the waypoint. You can also turn the small MFD knob counterclockwise to obtain drop down menus for FPL, Nearest, and Recent. 2) Press the RWY/FREQ soft key to view runway and frequency information about the waypoint. 3) Press the APT DIR soft key (if available) to view the airport directory information such as facility hours, noise abatement, pattern, etc. Press the small MFD knob and turn to scroll down the page (if available). 4) Press the WX or WX/NOTAM soft key (if available) to view METARs, TAFs, or NOTAMs for the waypoint. 70 G500/600 Cockpit Reference Guide 190-00601-03 Rev G FPL GROUP Charts Page (Optional) Soft Keys Found on Charts Page Chart Information ChartView™ (Optional with Enablement Card) ChartView resembles the paper version of Jeppesen terminal procedures charts. The charts are displayed in full color with high resolution. The MFD depiction shows the aircraft position on the moving map in the plan view of approach charts and on airport diagrams. ChartView requires an enablement card. The ChartView database is updated on a 14-day cycle. ChartView is disabled 70 days after the expiration date and is no longer available for viewing upon reaching the disable date. Selecting a Chart 1) While viewing the Charts page of the FPL Page Group, press the SELECT soft key to change the airport or chart. 2) Turn the small and large MFD knobs to select the airport identifier and press ENT to accept the selected airport. 3) Turn the large MFD knob to select the desired chart. 4) Press ENT to display the desired chart. NOTE: The chart for the selected destination airport or approach is automatically loaded. If no flight plan is entered, the chart page will default to the nearest airport. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 71 FPL GROUP: CHARTS PAGE 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. FPL GROUP Selecting Other Charts You are able to choose other charts to display based on your flight plan (FPL), charts of the nearest airport (NRST) or recently selected airports (RECENT). 1) While viewing the Charts page of the FPL Page Group, press the SELECT soft key. 2) Turn the small MFD knob counterclockwise. 3) Turn the small MFD knob to show FPL, NRST, or RECENT. FPL GROUP: CHARTS PAGE 4) Turn the large MFD knob to highlight the desired airport, then press ENT. Display Charts From Flight Plan Display Charts Of Nearest Airport Display Charts From Recent Choices Viewing Charts and Panning 1) While viewing the Charts page of the FPL Page Group, press the RNG (Range) keys to zoom in and 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. 72 G500/600 Cockpit Reference Guide 190-00601-03 Rev G FPL GROUP Viewing Details of ChartView™ Charts 1) While viewing the Charts page of the FPL Page Group, press the DETAIL soft key. 2) Press the HEADER, PLAN, PROFILE, or MINIMUMS soft keys to view detailed sections for the chart for those topics. Setting Minimums Changing Day/Night View 1) While viewing the Charts page of the FPL Page Group, press the MENU key to display the Options menu. 2) Turn the small MFD knob to Chart Setup. Press ENT. The Color Scheme option will be highlighted. 3) Turn the small MFD knob to select Day - Auto - Night. Press the small MFD knob to save the selected value and return to the Charts page. 4) If “Auto” is selected, turn the large MFD knob to highlight the Display Level Brightness value. Turn the small MFD knob to 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. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 73 FPL GROUP: CHARTS PAGE 1) While viewing the Charts page of the FPL Page Group, press the MENU key to display the Options menu and press ENT. 2) Turn the small MFD knob to select the source, BARO or RAD ALT. Press the ENT key. 3) Turn the small MFD knob to select the altitude. Press ENT to set the altitude. FPL GROUP Viewing NOTAMs (ChartView Only) FPL GROUP: CHARTS PAGE In the event there is an active NOTAM (Notice to Airmen) for a particular chart, the NOTAM soft key will be available. To view the information press the NOTAM soft key. Charts Page 74 G500/600 Cockpit Reference Guide 190-00601-03 Rev G ALERTS Alerts Contact your Garmin dealer for service if any of the following alerts appear. Refer to the Airplane Flight Manual and ADAS+ ETM documentation in the event that Engine Trend Monitor (ETM) alerts are displayed. On Screen Alerts Alert 190-00601-03 Rev G G500/600 Cockpit Reference Guide ALERTS Description ADC Altitude Error Correction is unavailable. ADC1 ALT EC GDC is reporting that altitude correction is unavailable. AHRS 1 or AHRS 2 is not receiving any GPS information. AHRS1 GPS AHRS 1 or AHRS 2 is operating exclusively in no-GPS mode. AHRS 1 or AHRS 2 is using the backup GPS information. AHRS1 or AHRS 2 magnetic field model needs update. This AHRS1/2 SRVC appears on the ground only. AHRS1/2 TAS AHRS1 or AHRS 2 is not receiving true airspeed from ADC. ALT KEY INOP The ALT key is disabled. ALT NO COMP No data from on or more altitude sensors. ARINC 429 CONFIG ARINC 429 configuration error. ARINC 708 CONFIG ARINC 708 configuration error. AUD NOT AVAIL Audio system is not available. AUD SYS FAIL Audio system has failed. CAL LOST Registry reports that the GDU 620 has lost calibration data. CNFG MISMATCH GDU 1-2 airframe configuration settings disagree. CNFG MODULE Failure of configuration module. 75 ALERTS Alert Description • GDL 88 ADS-B Failure. Unable to transmit ADS-B messages. • GDL 88 ADS-B fault. • ADS-B fault: UAT receiver. • ADS-B fault: 1090 receiver. • GDL 88 needs service. • GDL 88 ADS-B is not transmitting position. Check GPS devices. DATALINK • GDL 88 control panel input fault. Check transponder mode. • GDL 88 ADS-B fault. Pressure altitude source inoperative. • GDL 88 external traffic system inoperative or connection lost. • GDL 88 configuration module needs service. ALERTS • GDL 88 is inoperative or connection to GDU is lost. • GDL 88 CSA failure. • GDL 88 external traffic system has a low battery. • GDL 88 external traffic system in standby for more than 60 seconds. DATA LOST Pilot stored data was lost. Recheck data and settings. DB ERR Database found on top card. DB SYNC COMPLETE Database sync complete. DB SYNC DISABLED No database card found to receive databases. DB SYNC ERROR Not enough space to receive one or more databases. DIAG MODE System is in Diagnostic Mode. DSCRT CONFIG Discrete output configuration error. ENG SENSOR UNIT • Configuration error. Communication with sensors is halted. 1/2 • Communication with sensors lost. FAN 1/2 FAIL ETM CAPTURE ETM EXCEED 76 Cooling fan #1 or #2 has failed. ADAS+ engine trend monitor is recording trend data. ADAS+ engine trend monitor is reporting an exceedence or advisory condition. G500/600 Cockpit Reference Guide 190-00601-03 Rev G ALERTS Alert ETM FAULT Description ADAS+ engine trend monitor is reporting a system fault. • Cooling fan 1/2 has failed. • Unit may operate at extreme temperatures FAN 1/2 FAIL • Extended operation at high temperatures is not recommended as damage to the GDU may occur. • PFD/MFD coloration may be incorrect. GAD 43E CONFIG GATE MODE GDL 69 190-00601-03 Rev G G500/600 Cockpit Reference Guide ALERTS GAD 43 • Backlight may dim to reduce power and heat. Gyro Emulation Type Mismatch Fault Yaw Rate Scale Factor Mismatch Fault GDU AHRS Monitor Fault Pitch Deviation Fault Roll Deviation Fault Yaw Rate Deviation Fault AHRS A429 Attitude Timeout Fault AHRS A429 Attitude Invalid Fault AHRS Pitch Out of Range Fault AHRS Attitude Invalid Fault AHRS A429 Heading Timeout Fault AHRS A429 Heading Invalid Fault Reference Timeout Fault Application SCI Integrity Fault Configuration Integrity Fault AC Reference Lost Calibration Integrity Fault Unit Fault Power Supply Fault GAD 43 communication lost. GAD 43e configuration error. Communication halted. Automated testing is on. GDL 69/69A has failed. 77 ALERTS Alert GEO LIMITS GPS1/2 FAIL GPS(1/2) PPS FAIL GSR FAIL GWX CONFIG GWX SERVICE HDG FAULT HDG LOST HTAWS IAS NO COMP ALERTS <LRU> CONFIG <LRU> COOLING <LRU> DB ERR <LRU> KEYSTK <LRU> SERVICE <LRU> VOLTAGE MANIFEST NAV1/2 FAIL NO RADAR DATA PIT NO COMP PREV EXCEED RADAR CONTROLS DISAGREE REGISTER GFDS ROL NO COMP RS-232 CONFIG RS-485 CONFIG 78 Description AHRS too far North/South, no magnetic compass. No GPS1 or GPS2 data is available. The PPS signal has not been received in more than 5 seconds. The GSR 56 has failed. GWX configuration error. Configuration service required. GWX need service. Return unit for repair. AHRS 1 magnetometer fault has occurred. HDG features disabled or defaulted to GPS1 TRK. • External HTAWS not available. Internal TERRAIN-HSVT alerting enabled. • External HTAWS configuration mismatch. No data from one or more airspeed sensors. Error in configuration of specific LRU, where <LRU> denotes specific LRU. Specific LRU has poor cooling, reducing power usage. Database for specific LRU is corrupt. <LRU> <KEY> is stuck. Specific LRU needs service. <LRU> has low voltage reducing power usage. GDU has received product data for an LRU that should have a manifest entry, but is not in the manifest. No navigation receiver #1 or #2 data. No data is being sent to the GDU. No data from one or more pitch attitude sensors. ADAS+ engine trend monitor is reporting a previous exceedence. Data does not match for 15 seconds or more. Data services are inoperative. GFDS is not registered. No data from one or more roll attitude sensors. RS-232 configuration error. RS-485 configuration error. G500/600 Cockpit Reference Guide 190-00601-03 Rev G ALERTS Alert SIMULATOR STORMSCOPE SVT DISABLED SW MISMATCH TAWS TDB TERRAIN DSP TRAFFIC CONFIG TRAFFIC FAIL Description Sim Mode is active. Do not use for navigation. Stormscope® either reports a failure or has timed out. Out of available terrain region. Terrain DB resolution too low. GDU software version strings to no match. Xtalk is off. • External TAWS not available. Internal TERRAIN-SVT alerting enabled. • External TAWS configuration mismatch. Airframe does not support terrain database. Terrain awareness unavailable. (For configurations using TAWS-B or TERRAIN-SVT). ADS-B traffic data does not match configuration. • Traffic device has failed. 190-00601-03 Rev G G500/600 Cockpit Reference Guide ALERTS • Traffic data will no longer be displayed. TRAFFIC STDBY Traffic device is in standby mode while airborne. TRK LOST GPS1 TRK lost. HSI defaulted to GPS2 TRK. TRK TRAFFIC Heading lost. Traffic is now based on track. WX ALERT Possible severe weather ahead. WX RADAR Weather radar has failed. WX RDR SERVICE Weather radar needs service. WXR INPUT FAULT Weather radar is not receiving one or more inputs. 79 ALERTS TAWS-B Alerts Alert Type PFD/MFD Alert Annunciation Excessive Descent Rate Warning (EDR-W) FLTA Terrain Warning (RTC-W, ITI-W) “Pull Up” “Terrain Ahead, Pull Up; Terrain Ahead, Pull Up”* or “Terrain, Terrain; Pull Up, Pull Up” “Obstacle Ahead, Pull Up; Obstacle Ahead, Pull Up”* or “Obstacle, Obstacle; Pull Up, Pull Up” “Wire Ahead, Pull Up; Wire Ahead, Pull Up”* or "Wire, Wire, Pull Up, Pull Up" “Terrain Ahead; Terrain Ahead”* or “Caution, Terrain; Caution, Terrain” “Obstacle Ahead; Obstacle Ahead”* or “Caution, Obstacle; Caution, Obstacle” "Wire Ahead; Wire Ahead" or “Caution, Wire; Caution Wire” “Too Low, Terrain” FLTA Obstacle Warning (ROC-W, IOI-W) FLTA Wire Warning (ILI-W, RLC-W) ALERTS FLTA Terrain Caution (RTC-C, ITI-C) FLTA Obstacle Caution (ROC-C, IOI-C) FLTA Wire Caution (ILI-C, RLC-C) Premature Descent Alert Caution (PDA) Voice Callout (VCO-500) Excessive Descent Rate Caution (EDR-C) Negative Climb Rate Caution (NCR-C) Aural Message None “Five-Hundred” “Sink Rate” “Don’t Sink”* or “Too Low, Terrain” * Alerts with multiple messages are configurable at installation and are installationdependent. Alerts for the default configuration are indicated with asterisks. \ 80 G500/600 Cockpit Reference Guide 190-00601-03 Rev G ALERTS Terrain-SVT™ Alerts Alert Type GPS signal re-established Terrain System Test Successful Terrain System Test in Progress PFD/MFD Alert Annunciation None None Aural Message “Terrain System Available” “Terrain System test OK” None Terrain Alerting is disabled None No GPS position Excessively degraded GPS signal Terrain SVT System Test Fail “Terrain System Not Available” Alert Type 190-00601-03 Rev G PFD/MFD Alert Annunciation Aural Message ALERTS FLTA Terrain Caution (RTC-C, ITI-C) FLTA Terrain Caution (RLC-C, ILI-C) FLTA Terrain Warning (RTC-W, ITI-W) FLTA Terrain Warning (RLC-W, ILI-W) FLTA Obstacle Caution (ROC-C, IOI-C) FLTA Obstacle Warning (ROC-W, IOI-W) “Terrain System Failure” “Caution, Terrain, Terrain” “Caution, Wire, Wire” “Warning, Terrain, Terrain” “Warning, Wire, Wire” “Caution, Obstacle, Obstacle” “Warning, Obstacle, Obstacle” G500/600 Cockpit Reference Guide 81 SYMBOLS Symbols Map Page Symbols Symbol Description Unknown Airport Non-towered, Non-serviced Airport Towered, Non-serviced Airport Non-towered, Serviced Airport Towered, Serviced Airport Soft Surface, Serviced Airport Soft Surface, Non-serviced Airport SYMBOLS Private Airport Heliport Intersection LOM (compass locator at outer marker) NDB (Non-directional Radio Beacon) VOR VOR/DME ILS/DME or DME-only VORTAC TACAN 82 G500/600 Cockpit Reference Guide 190-00601-03 Rev G SYMBOLS SafeTaxi® Symbols Symbol Description Helipad Airport Beacon Under Construction Zones Designated Water Areas Traffic Symbols Description SYMBOLS TAS Symbol Other Traffic Proximity Advisory (PA) Traffic Advisory (TA) Traffic Advisory Off Scale TAS/TCAS Traffic Symbols TIS Symbol Description Proximate Traffic (other than TA traffic) Traffic Advisory (TA) Traffic Advisory Off Scale TIS Traffic Symbols 190-00601-03 Rev G G500/600 Cockpit Reference Guide 83 SYMBOLS Symbol , , Description Basic Non-Directional Traffic (White in Air, Brown on Ground) Basic Directional Traffic (White in Air, Brown on Ground) Basic Off-scale Selected Traffic Proximate Non-Directional Traffic Proximate Directional Traffic Proximate Off-scale Selected Traffic Non-Directional Alerted Traffic SYMBOLS Off-Scale Non-Directional Alerted Traffic Directional Alerted Traffic Off-Scale Directional Alerted Traffic Non-Directional Surface Vehicle Directional Surface Vehicle ADS-B Traffic Symbols 84 G500/600 Cockpit Reference Guide 190-00601-03 Rev G SYMBOLS Terrain Obstacle Symbols Unlighted Obstacle (Height is less than 1000 ft AGL) Lighted Obstacle (Height is less than 1000 ft AGL) Unlighted Obstacle (Height is greater than 1000 ft AGL) Lighted Obstacle (Height is greater than 1000 ft AGL) Tower Windmill Grouped Obstacles Power Line The “*” notes grouped obstacles. Projected Flight Path 100 ft Threshold Threat Location Unlighted Obstacle Terrain above or within 100 ft below the aircraft altitude (Red) 1000 ft Terrain between 100 ft and 1000 ft below the aircraft altitude (Yellow) Terrain more than 1000 ft below the aircraft altitude (Black) Terrain Altitude/Color Correlation 190-00601-03 Rev G G500/600 Cockpit Reference Guide 85 SYMBOLS NOTE: Obstacles will be removed from the Terrain/TAWS page when range (RNG) exceeds 10 nm. SYMBOLS Map Toolbar Symbols Symbol Description Terrain Proximity Enabled and Available Indicator Terrain Proximity Enabled and Not Available Indicator Point Obstacle Enabled and Available Indicator Point Obstacle Enabled and Not Available Indicator Wire Obstacles Enabled and Available Indicator Wire Obstacles Enabled and Not Available Indicator StormScope SYMBOLS StormScope Enabled and Not Available Indicator Traffic Enabled and Available Indicator Traffic Enabled and Not Available Indicator 86 G500/600 Cockpit Reference Guide 190-00601-03 Rev G SYMBOLS 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. The product label in the legend will turn yellow at half the expiration time and grey when expired. Expired products will not be shown on the display. Weather Product 30 30 60 30 30 60 90 90 60 120 90 60 90 60 90 90 180 60 SYMBOLS NEXRAD (NEXRAD and Echo Top are Mutually Exclusive) Echo Top (Cloud Top and Echo Top Mutually Exclusive) (NEXRAD and Echo Top Mutually Exclusive) Cloud Top (Cloud Top and Echo Top Mutually Exclusive) XM Lightning Cell Movement SIGMETs / AIRMETs METARs City Forecast Surface Analysis Freezing Levels Winds Aloft County Warnings PIREPS TFRs AIREPS Icing Turbulence Cyclone Warnings Expiration Time (Minutes) NOTE: Product age is not displayed for individual reports of AIRMETs, SIGMETs, City Forecasts, County Warnings, Cell Movement and TFRs. Product generation time is displayed for Freezing Level and Winds Aloft instead of valid time. 190-00601-03 Rev G G500/600 Cockpit Reference Guide 87 SYMBOLS Miscellaneous Symbols Symbol Description Low Wing Prop High Wing Prop Jet Piston Rotorcraft Turbine Rotorcraft Default Map Cursor Measuring Cursor SYMBOLS MFD Wind Vector (w/ valid GPS solution) Parallel Track Waypoint Restricted/Prohibited/Warning/Alert TFR (Temporary Flight Restrictions) MOA ( ( ( ) ) ) Class B Airspace (De-Emphasized Smart Airspace) Class C Airspace (De-Emphasized Smart Airspace) Class D Airspace (De-Emphasized Smart Airspace) Airspace Altitude Label (Upper/Lower Limits) User Waypoint 88 G500/600 Cockpit Reference Guide 190-00601-03 Rev G © 2009-2015 Garmin Corporation Garmin International, Inc. 1200 East 151st Street, Olathe, Kansas 66062, U.S.A. Tel. 913/397.8200 or 866.739.5687 Fax 913/397.8282 Garmin AT, Inc. 2345 Turner Rd., SE, Salem, Oregon 97302, U.S.A. Tel. 503/581.8101 or 800/525.6726 Fax. 503/364.2138 Garmin (Europe) Ltd. Liberty House, Bulls Copse Road, Hounsdown Business Park, Southampton, SO40 9RB, U.K. Tel. +44 (0) 870 850 1243 Fax +44 (0) 238 052 4004 Garmin Corporation No. 68, Jangshu 2nd Road, Xizhi Dist., New Taipei City 221, Taiwan (R.O.C) Tel. 886/2.2642.9199 Fax 886/2.2642.9099 Garmin Singapore Pte., Ltd. 46 East Coast Road #05-06 Eastgate Singapore 428766 Tel. (65) 63480378 Fax (65) 63480278 www.garmin.com Part Number 190-00601-03 Rev. G
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