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Garmin Software Version 2163.04 Cockpit Reference Guide

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1. 23 Trip Plannin gs sla tae s sl 23 Create a User Waypoint Defined by Latitude amp Longitude 25 Create a User Waypoint Defined by Radials from Other V aypoints 26 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 28 Delete a User Vlaypoint s s ss nnne Create a Flight mport a Flight Plan from an SD Card Insert a Waypoint in the Active Flight 65 31 Enter an Airway in a Flight Plan User Defined Holding Patterns Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 35 Store a Flight Plan eei ii cie tt s 35 Edit a Stored Flight Plan 36 Delete a Waypoint from the Flight Plan sss 36 Invert and Activate a Stored Flight Plan 36 Copy a Flight Plan Delete a Flight Plan rettet Graphical Flight Plan Creation Export a Flight Plan to an SD Card 38 Procedures r MURDER 39 Load and Activate a Departure Procedure sss 39 Activate A Departure Leg ssssssseeenennnnnnennes Load An Arrival Procedure Activate An
2. Suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS Procedures Appendix Alerts Operation Features Index GPS Navigation GARMIN Altitudes associated with arrival procedures are manually designated This means the system will not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to cyan Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Cyan Text Cyan Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude in the altitude of the Altitude is designat
3. 7 With DELETE highlighted press the ENT Key 8 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Importing a profile 1 2 3 Or 4 Insert the SD card containing the Pilot Profile s into the top card slot on the MFD Use the FMS Knob to select the AUX System Setup 1 Page Press the IMPORT softkey If the correct Pilot Profile file is selected with MPORT highlighted press the ENT Key If the SD card contains more than one Pilot Profile a Turn the large FMS Knob to highlight the select file field in the Pilot Profile Importing Box b Turn the small FMS Knob to display the pilot profile list and highlight the desired profile to import and press the ENT Key c With IMPORT highlighted press the ENT Key Pilot profile import succeeded is shown in the import results box Press the ENT Key The imported profile becomes the active Pilot Profile Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Exporting a profile 1 Insert the SD card for storing the Pilot Profile into the top card slot on the MFD 2 Use the FMS Knob to select the AUX System Setup 1 Page 3 Activate the desired Pilot Profile to export Only the active Pilot Profile can be exported 4 Press the EXPORT softkey 5 With EXPORT highlighted press the ENT Key 6 Pilot profile export s
4. In Transition Down and Locked Warning EIS LANDING GEAR LANDING GEAR LANDING GEAR Engine Page LANDING GEAR LANDING GEAR LANDING GEAR Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL 1 Press the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large FMS Knob to select the next desired field 4 Turn the small FMS Knob to enter the desired number 5 Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Turn the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING OPTIONAL 1 Press the ADF DME or DME Softkey 2 Turn the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection SELECTING A TRANSPONDER MODE 1 Select the XPDR Softkey to display the Transponder Mode Selection Softkeys 2 Select the desired softkey to activate the transponder mode 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu U
5. 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Press the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned press the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain WARNING Changing the gain in Weather Mode will cause 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 GAIN Softkey to activate the cursor in the GAIN field 2 Tum the small FMS 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 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 69 AEN Sd5 52 olpny uqax 5219 sjuauimasu J05 AeN sub buluueld ni uep ony s mp oold paezey spay uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Aud
6. mismatch communication halted 1 The G1000 system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The G1000 system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The G1000 system should be serviced WX ALERT Possible severe weather ahead Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 190 01842 00 Rev A A GARMIN Annunciations amp Alerts GTS 825 855 MESSAGE ADVISORIES Message GTS CONFIG GTS Config error Config service req d Comments The GTS and GDU have different copies of the GTS configuration or the Mode S address is invalid The G1000 system should be serviced GTS MANIFEST GTS software mismatch communication halted GDC 74A MESSAGE ADVISORIES The GTS has incorrect software installed The G10
7. nafter collect on of otherwise U able for any inc lity to use the software or re esentative has been advised o vely AC U KWIK Organization the AC U KWIK information included mited to the implied warranties of ormation is provided as is and esentations regarding its accuracy WIK Organizations and to the ess AC U KWIK Organizations tual or alleged inaccuracies in t in the datasets Some ju es or liability for incident al or nsee Printed in the U S ively included in this merchantability nder idental special or ated f the extent allowed ated ages he isdictions A amp GARMIN Warnings Cautions 5 Notes e 6 WARNING Do not use the terrain avoidance feature as the sole means of navigation and terrain separation The terrain avoidance feature is only to be used as and aid to terrain avoidance Garmin obtains terrain database content from third party sources and is not able to independently verify the accuracy of the terrain data WARNING Do not rely on the displayed minimum safe altitude MSAs as the sole source of obstacle and terrain avoidance information The displayed minimum safe altitudes MSAs are only advisory in nature Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING Do not use GPS derived geometric altitude for compliance with air traffic control altitude requirements in
8. 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian AEN Sd S24V oipny uddx 5219 sjuauimasu J05 AeN 364 buluueld Wil s mp oold paezey spay uoneiedo SaJnjeaJ unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 52 A GARMIN Setting Up and Customizing the Connext Weather Data Link Page 1 2 3 4 5 6 7 8 Select the Connext Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to scroll through options for each product ON OFF range settings etc Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Connext Weather Data Link Page with the changed settings Restoring Default Connext Weather Data Link Page Settings 1 2 3 4 5 Select the Connext Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired default s to restore all or for select
9. Nav Com Transponder Audio 9 7 AEO ALE 7 DME Tuning Optional cc c ccccscsssssssssessssssssssssssssssssssssssseessssvsssscessssssssseeessssnsesseess 7 Selecting A Transponder Mode 7 Enter a Transponder sees 8 Selecting a COM Radio ssssssssseeennennnnnnnnnes 8 Selecting a NAV Radio s s s s nnns 8 NAV COM Tuning sssseeenennnne nennen 8 Digital Clearance Recorder and Player 9 Intercom System ICS Isolation 9 Telephone Entertainment Audio sss 3 Automatic Flight Control System 5 Flight Director Activation 5 Vertical Modes nasa tra d a FER HE oc eo dre 6 GPS Navigation ena odii alias DAR dan one tasted 9 Direct to Navigation sssssseseeene enne nnne 9 Activate a Stored Flight Plan 20 Activate a Flight Plan Leg 20 Stop Navigating a Flight Plan 21 Vertical Navigation VNAV l l s s s s nnne 21 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Table of Contents GARMIN Flight 23 Weight amp Fuel Planning s s s s
10. Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN When zoomed in to a range of 30 nm each square block on the display represents an area of four square kilometers The following may cause abnormalities in displayed radar images Ground clutter Strobes and spurious radar data Sunstrobes when the radar antenna points directly at the sun nterference from buildings or mountains which may cause shadows Metallic dust from military aircraft which can cause alterations in radar scans Infrared Satellite Infrared Satellite IR SAT data depicts cloud top temperatures from satellite imagery Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes Displaying Cloud Tops information 1 Select the Connext Weather Data Link Page 2 Select the IR SAT Softkey To display the Infrared Satellite legend select the LEGEND Softkey when Infrared Satellite data is selected for display Data Link Lightning Lightning data shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has occurred within a two kilometer region Neither cloud to cloud nor the exact location of the lightning strike is displayed If the aircraft is also equipped with an on board lightning detection system e g L 3 WX 500 Stormscope only one lightning product may be enabled for display at a time Displaying Data L
11. Sue v unuuy xipuaddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Appendix A Index CCC GARMIN 17 Turn the small FMS Knob to select the System Status Page 18 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRS1 and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Upload
12. The G1000 system should be serviced The transponder has incorrect software installed The G1000 system should be serviced 114 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL XPDR1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder XPDR1 ADS B FAIL XPDR1 is unable to transmit ADS B messages XPDR2 ADS B FAIL XPDR2 is unable to transmit ADS B messages ADS B is inoperative The transponder may not be receiving a valid GPS position Other transponder functions may be available Service when possible GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be servic
13. iA p Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Annunciations amp Alerts A GARMIN TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS TAWS B ALERTS PFD MFD MFD PFD MFD Alert TERRAIN SVS Page Alert Type m Aural Message Annunciation Annunciation System Test in progress TER TEST one System Test pass None None E y p Test OK Terrain Alerting Inhibited TER INH None TER WA Terrain System Excessively degraded GPS signal or TER NVA Terrain System Out of database Not Available coverage area Terrain System Test Fail Terrain or Obstacle database unavailable Terrain System or invalid CTER FAIL Failure Invalid software configuration or System audio fault MED Terrain or Obstacle database unavailable or invalid None None Terrain SVS operating with PFD Terrain or Obstacle databases Index Appendix Eod Alert Type TAWS B Page Aural Message Pop Up Alert Annunciation Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Excessive Descent Rate Warning EDR 190 01842 00 Rev A A GARMIN Alert Type Reduced Required Terrain Clearance Warning RTC Imminent Terrain Impact Warning ITI Reduced Required Ob stacle Clearance Warning ROC Imminent Obstacle Impact Warning 101
14. 137 AC U KWIK 76 ADF 7 8 ADS B 132 Advisory alerts 103 AHRS 115 116 117 120 Aircraft alerts 95 Air Data Computer 97 Airport Directory 76 Airport Signs 73 74 Airways 133 Alert messages 118 Altimeter setting 1 90 Antenna stabilization 70 Antenna tilt 68 AOPA 76 AOPAs Airport Directory 76 AP 98 Attitude amp Heading Reference System 97 98 Audio panel controls NAV1 NAV2 8 Barometric Altitude Minimums 3 Barometric pressure 131 Battery Overheat warning 95 Voltage 5 Bearing line 69 70 Blue Select Mode 13 190 01842 00 Rev A Index C Cabin pressure altitude 5 CDI 1 2 8 122 Cell 45 46 Cell mode 46 Channel Presets 84 ChartView 74 75 Checklists 85 86 CLD TOP Softkey 58 Clearance player 9 Clearance recorder 9 Code selection softkeys 8 COM 8 9 89 D DB Mismatch 135 139 DCLTR Softkey 75 Dead Reckoning 91 Declutter 90 127 134 Designated altitudes 21 22 Differential cabin pressure 5 Warning 95 Direct to 19 DME 7 8 DR mode 91 92 E Edit a flight plan 36 Electronic Checklists 86 87 Electronic Stability 81 Emergency Checklist 86 Enable Terrain 65 66 ESP 81 82 F FD 98 Flap position Asymmetrical deflection warning 95 96 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index 1 uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld ARN Sd5 2 olpny uqax svo Sjueunasu jeuuouqy jeuonippy paezey wid U105 AEN 10614 Sue v unuuy xipueddy
15. 3 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 7 Press the FPL Key on the MFD then tum the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A S
16. A condition has developed causing the yaw servo to provide a Right RUD sustained force Preflight Test Performing preflight system test Upon completion of the test the aural alert will be heard Preflight system test has failed TERRAIN SVS ALERTS PFD MFD Alert Type TERRAIN SVS MFD Aural yP Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Clearance Warning RTC Imminent Terrain Impact TERRAIN Warning ITI Reduced Required Obstacle TERRAIN Clearance Warning ROC Imminent Obstacle Impact TERRAIN Warning 101 Reduced Required Terrain TERRAIN CAUTION TERRAIN Clearance Caution RTC Imminent Terain Impact TERRAIN CHUTZON TERRAIN Caution ITI Reduced Required Obstacle TERRAIN CAUTION OBSTACLE Clearance Caution ROC Imminent Obstacle Impact TERRAIN OBSTACLE Caution 101 190 01842 00 Rev A Warning Terrain Terrain Warning Terrain Terrain Warning Obstacle Obstade Warning Obstac Obstade Caution Terrain Terrain D Caution Terrain Terrain Caution Obstade Obstade Caution Obstacle Obstacle 99 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunyea4 aoueplony saunpa20Jd Fuluueld ARN Sd5 241V oipny uadx svo Sjueunasu wio gt AeN jeuonippy uoneiedo Jeuuouqy x pul iui nu paezey
17. Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 26 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the MFD to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS
18. AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey s s Jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index 4 A GARMIN Garmin Incietu Dv 3 Se MN at i 1200 East 151st Street A M TIN 7777 Olathe KS 66062 USA T u z aS p 913 397 8200 f 397 8282 lt a t i 68 scite 2nd m Shift Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 Ls K 2007 2009 2010 2014 Garmin 140 or its subsidiaries 190 01842 00 Rev A
19. Aloft Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3 000 foot increments up to 42 000 feet MSL Displaying Winds Aloft data 1 2 3 4 Select the Connext Weather Data Link Page Select the MORE WX Softkey Select the WIND Softkey Select the desired altitude level SFC surface up to 42 000 feet Select the NEXT or PREV Softkey to cycle through the altitude softkeys The WIND Softkey label changes to reflect the altitude selected To display the Winds Aloft legend select the LEGEND Softkey when Winds Aloft is selected for display PIREPs Pilot Weather Reports PIREPs describe in flight weather encountered by pilots A PIREP may contain unforecast adverse weather conditions such as low in flight visibility icing conditions wind shear turbulence and type of aircraft flown PIREPs are issued as either Routine UA or Urgent UUA Displaying PIREP text 1 2 3 4 Select the Connext Weather Data Link Page Select the MORE WX Softkey Select the PIREPS Softkey Press the RANGE Knob and pan to the desired weather report A gray circle will appear around the weather report when it is selected Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance 5 Press the ENT Key The PIREP text is first displayed in a decoded fashion then as raw text 6 Use the FMS Knob or
20. Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A 6 RecordofRevisions of Revisions GARMIN m Date of Revision Affected Pages December 2014 Production Release 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian RR 1 Record of Revisions Ss GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Tableof Contents CONTENTS Flight Instruments 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 5 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synclironize CDl eie eie n s o i o e HER Change Navigation Sources Enable Disable OBS Mode While Navigating with GPS 2 Generic TIMEN esate coon diet need dde ax am tasa an ad toad 2 Turn Individual Vspeed Bugs On or sse 2 Turn All Vspeed Bugs On or Off 3 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Engine Indication amp Crew Alerting System 5 Landing Gear Indications 5 5 6
21. FMS Knob to highlight the desired runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude c Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 1 2 40 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN 5 Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight th
22. Knob The Waypoint Information Window is now displayed 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Flight Procedures Planning GPS Nav Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Appendix Alerts Operation Features Index Flight Planning A GARMIN Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 32 1 2 3 4 5 6 7 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after
23. Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Reduced Required Ob stacle Clearance Caution ROC Imminent Obstacle Impact Caution 101 Premature Descent Alert Caution PDA Altitude Callout 500 Excessive Descent Rate Caution EDR Negative Climb Rate Cau tion NCR Annunciations amp Alerts Aural Message Terrain Terrain Pull Up Pull Up Terrain Ahead Pull Up Terrain Ahead Pull Up Obstacle Ahead Pull Up Obstacle Ahead Pull Up PFD MFD TAWS B Page Annunciation PULL UP MFD Pop Up Alert TERRAIN PULL UP RUUL 12 TERRAIN AHEAD PULL UP OBSTACLE AHEAD PULL UP PULL UP Obstade Obstacle Pull Up Pull Up Caution Terrain Caution Terrain PULL UP Terrain Ahead Terrain Ahead Caution Obstacle Cau tion Obstacle Obstacle Ahead Obstacle Ahead Too Low Terrain Five Hundred Sink Rate _ mw None None Don t Sink TEE EEEE VII TAWS B System Status Annunciations Alert Type PFD MFD Alert TAWS B Page Aural yp Annunciation Annunciation Message System Test in Proqress TAHS TEST None 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian sainqeo4 aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 sjueumasu paezey nubi u102 AEN nubi jeuonippy uon
24. Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Tum the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 65 AEN Sd5 S24V oipny duadx 59213 siu umn nsul u102 AEN Duruue d Wil uep ony s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 1 2 3 A GARMIN Or While the Terrai
25. Weather products within the selected coverage area during an initial Connext Data Request regardless of which products if any are currently enabled for display On subsequent requests previously retrieved textual data such as METARs and TAFs is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request If the system cannot complete a Connext weather data request one or more messages will appear in the request status window as shown in the following table 54 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Hazard Avoidanc e Weather Request Status Message Description Auto requests inhibited Send manual request to reset The system has disabled automatic weather data requests due to excessive errors Automatic weather data requests have stopped Send a manual weather data request to resume automatic updates Auto update retry Seconds The system will attempt another automatic weather data request after an error occurred during the previous request Timer counts down until the next automatic request occurs GFDS Comm Error 2 A communications error has occurred with the GIA The system should be serviced GFDS Comm Error 4 This occurs if multiple automatic weather data requests have recently failed or the GDL 59 or a GIA is
26. be serviced AHRS1 GPS AHRST not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed
27. hold 3 Press the MENU Key highlight Hold At Wpt and press the ENT Key The HOLD AT win dow appears with the course field highlighted sjuauimasu BU ETE 5721 oipny uddx UI0JNeN 52 4 Use the FMS Knobs to edit the entry course and press the ENT Key 5 Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key 6 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 7 Use the FMS Knobs to edit the length and press the ENT Key 8 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 9 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key 10 Press the ENT Key while LOAD is highlighted to add the hold into the flight plan 2 AEN 540 nubi Creating a user defined hold at the aircraft present position 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan VVindovv PFD 2 Press the MENU Key highlight Hold At Present Position and press the ENT Key The HOLD AT window appears with the Length mode highlighted 3 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 4 Use the FMS Knobs to edit the length and press the ENT Key 5 Use the small FMS Knob to select RIGHT or LEFT turn directi
28. is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field 24 NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings 7 flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system 8 The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 9 The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer 10 The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated
29. message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 29 sjuauimasu nubi 5721 oipny uddx UI0JNeN 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 30 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modifie
30. necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Page If the AUX SYSTEM SETUP 2 is already displayed proceed to step 4 4 Press the FMS Knob to activate the cursor 5 Tum the large FMS Knob to place the cursor in the STABILITY amp PROTECTION field 6 Turn the small FMS Knob to select ENABLE or DISABLE 7 Press the FMS Knob to remove the cursor ESP is automatically enabled on system power up Roll Engagement Roll Limit Indicators are displayed on the roll scale at 45 right and left indicating where ESP will engage As roll attitude exceeds 45 ESP will engage and the on side Roll Limit Indicator will move to 30 The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases Once engaged ESP force will be applied between 30 and 75 The force increases as roll attitude increases and decreases as roll attitude decreases The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude As roll attitude decreases ESP will disengage at 30 ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75 Pitch Engagement ESP engages at 21 nose up and 21 nose down Once ESP is engaged it will apply opposing force between 19 and 50 nose up and between 19 and 50 nose down Maximum opposing force is applied between 25 and 50 nose up and between 25 and
31. not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic WARNING Do not use SVT runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Runways are depicted at the published field elevation for the selected airport In some rare cases actual runway elevation differs significantly from the airport field elevation causing SVT runways to appear higher or lower than the actual runway Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS 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 In addition to SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 1
32. off line GFDS Comm Error 5 The Iridium or GFDS networks are not accessible Check lridium signal strength If this error persists the system should be serviced GFDS Comm Error 6 A communications error has occurred It this error persists the system should be serviced GFDS Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the data request GFDS Comm Error 8 A server error has occurred or invalid data received GFDS Login Invalid There is a problem with the GFDS registration Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 011 913 440 1135 for assistance GFDS Server Temporarily Inop The GFDS weather data server is temporarily out of service but is expected to return to service in less than 30 minutes GFDS Server Inop Invalid Coverage Area The GFDS weather data server will be out of service for at least 30 minutes The weather data request coverage area does not contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled checked and contains required criteria then re send the data request 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 55 AEN 649 S24V oipny uadx 5721 Sjueumajsul J05 AeN iui Duruue d ni eouepioAy s mp oold paezey suey uoneiedo sainjea4 Tunuuy Je
33. or LOC1 to VOR2 or LOC2 This places the cyan tuning box over the NAV2 standby frequency Select the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Select the OBS Softkey to select OBS Mode 2 Tum a CRS Knob to select the desired course to from the waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window TURN INDIVIDUAL VSPEED BUGS ON OR OFF 1 2 3 4 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN __Flight instruments TURN ALL VSPEE
34. or together NAV COM TUNING 1 2 3 Press the small tuning knob to select the desired radio for tuning A cyan box highlights the radio frequency to be tuned Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Nav Com XPDR Audio Panel DIGITAL CLEARANCE RECORDER AND PLAYER A NOTE Only the audio for the selected COM MIC Key is recorded Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation Pressing the MKR MUTE Key while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block INTERCOM SYSTEM ICS ISOLATION A NOTE In the following modes the copilot position is configured as crew NOTE In the default ICS configuration only the pilot and copilot positions can hear aircraft alerts All Intercom Mode In All Intercom mode the Pilot Copilot and Passengers hear each other and hear the aircraft audio Aircraft Audio o S PILOT COPLT PASS ICS Keys Mode Operation 190 01842 00 Rev A Garmi
35. other NAVS GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums APR ADVISORY SBAS VNAV not available Using Baro VNAV SBAS VNAV not available Check GPS sensor TRUE APR True north approach Change HDG reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 nee
36. persists the G1000 system should be serviced The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunyea4 eouepioAy saunpa20Jd Fuluueld ARN Sd5 2 oipny uadx svo Sjueunasu jeuonippy uoneiedo Jeuuouqy x pul 3 juion aeny nu paezey Eu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN Message Comments COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operat
37. service req d Comments GCU 475 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A failure has been detected in the GCU 475 The GCU 475 is unavailable The GCU 475 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The G1000 system should be serviced GMC KEYSTK GMC key name Key is stuck Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 190 01842 00 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Fligh
38. system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor PFD2 COOLING PFD2 has poor cooling Reducing power usage cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2
39. the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN cs Navigation STOP NAVIG
40. the ENT Key to scroll through the PIREP text 7 Press the FMS Knob or the CLR Key to close the PIREP text window and return to the Connext Weather Data Link Page To display the PIREP or AIREP legend select the LEGEND Softkey when PIREPs or AIREPs are selected for display The PIREP color is determined by the type routine or urgent TRAFFIC SYSTEMS o V ARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display e If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS or a Traffic Collision Avoidance System TCAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian AEN 542 52 oipny uddx 5219 sjueuimasu J05 AeN sb buluueld Wil uep ony s mp oold paezey Sue v
41. the National Airspace System NAS or internationally The primary barometric altimeter must be used for compliance With all air traffic control altitude regulations requirements instructions and clearance WARNING Do not use outdated database information Databases used in the system must be updated regularly in order to ensure that the information remains current 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 only an aid to enhance situational awareness WARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A Wamingstentane amp Notet GARMIN V ARNING Do not use data link vveather information for maneuvering in
42. the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Activates deactivates transmission of the aircrafts three dimensional position and aircraft heading for reception by ADS B systems Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN QX Appendix MFD SOFTKEY MAP optional rr TT T mn 9 puse onis A F3 V3 V3 V3 V3 A S FX sjuauimasu UATE 5721 optional optional optional r or optional optional Coo TERRAR ARW sTRSCP KERAS PALA WETAR LEGEND BACK F 1 F3 F amp Fr vx vom Press the BACK softkey to return to the top level softkeys oipny uadx U105 AEN 52 AEN 540 EY EN ES ES ES onn ES EN ES ES The DONE Softkey label changes to UNDO when the checklist item is already checked buluueld Wil MFD Softkeys i MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map e TOPO Displays topographical da
43. the option to use Split COM mode The Passengers hear each other Aircraft Audio Split COM i i OOO ICS Keys Mode Operation PILOT COPLT PASS 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Sjueuinijsu juil 52 olpny uqax 57213 wio gt AeN Suelv uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy paezey wd xipuaddy x pul Flight Instruments Nav Com AFCS XPDR Audio EICAS Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav Appendix Index A Nav Com XPDR Audio Panel GARMIN Pilot amp Copilot Isolate Mode In Pilot amp Copilot Isolate mode the Pilot and Passengers hear the aircraft audio The Copilot has the option to use Split COM mode Aircraft Audio Split COM v PILOT COPLT PASS ICS Keys Mode Operation Pilot amp Passenger Isolate Mode In Pilot amp Passenger Isolate mode the Pilot and Copilot hear the aircraft audio The Passengers hear each other Aircraft Audio v PILOT COPLT PASS ICS Keys Mode Operation Copilot amp Passenger Isolate Mode In Copilot amp Passenger Isolate mode the Pilot can hear the aircraft audio The Copilot has the option to use Split COM mode The Passengers hear each other Aircraft Audio Split COM ww PILOT COPLT PASS ICS Keys Mode Operation Garmin G1000 Cockpit Reference Guide fo
44. the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob
45. the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information SiriusXM Weather Products and Symbols Wx Product Status Icons Description US 3m CN Em NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right om ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed 12m CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed 3m XM LIGHTNING The age of the displayed data is shown at the right 2m CELL MOVEMENT The age of the displayed data is shown at the right SIGMET 2m AIRMET 5m SIGMET amp AIRMET The age of the displayed data for each is shown at the right Fus 8m CN 8m 3n mz dine iz oe METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom 48 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Hazard Avoidance Wx Product Status Icons Description 4m ae FREEZING LEVEL The age of the displayed da
46. the user defined hold defined at the Direct To waypoint Removing a user defined hold created at the aircraft present position or at a Direct To waypoint 1 Press the Direct To Key to display the DIRECT TO Window PFD or MFD 2 Press the MENU Key to display the PAGE MENU with the cursor on the Cancel Direct To NAV selection 3 Press the ENT Key The holding pattern is removed Removing a user defined hold created at an active flight plan waypoint 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the HOLD waypoint Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN 3 Press the CLR Key A Remove Holding Pattern confirmation window is displayed 4 Select OK and press the ENT Key The holding pattern is removed from Flight Planning the active flight plan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the EN
47. tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios AUDIO PANEL FAIL SAFE OPERATION If there is a failure of the Audio Panel a fail safe circuit connects the pilots headset and microphone directly to the COMI transceiver and the copilots headset directly to the COM2 transceiver Audio is not available on the speakers In addition the following functions are no longer available NAV ILS audio speaker cockpit cockpit passengers intercom aural warning alerts on headset entertainment inputs and digital recording radio 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 89 uep ony s np d01d Buruue d AEN Sd5 52 oipny uddx swold s3u u n sul puezey 34 U105 AEN ubiu saunqea4 Jeuonippy xipuaddy suelv junuuy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established Loss of Hazard Functions with Loss of GPS Position UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusu
48. uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN H Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation O Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale 62 Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick
49. waypoints These waypoints have been saved to the fully No stored flight plan data was system user waypoints No flight plans stored in the system have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed 4 Flight plan data was not successfully imported from the SD card 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 7213 sjueumasu piezeH ubi UI05 AeN 3461 jeuonippy uoneiedo Jeuuouqy ic ka x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix pod Annunciations amp Alerts A GARMIN Flight Plan Import Export Results Flight plan partially imported Description Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated The flight plan on the SD card contains more waypoints than the system can support The fl
50. 00 system should be serviced Message Comments ADC1 ALT EC ADC1 altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable ADC2 AS EC ADC2 airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable ADC1 SERVICE ADC1 needs service Return unit for repair The GDC1 should be serviced ADC2 SERVICE ADC2 needs service Return unit for repair The GDC2 should be serviced MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 Buruuejd AEN Sd 24V oipny uadx svoli siu un sul paezey Wfila Wil jeuonippy uoneiedo Jeuuouqy ic R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts GCU 476 MESSAGE ADVISORIES A GARMIN Message GCU CNFG GCU Config error Config
51. 2 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 49 AEN 549 S24V oipny uadx 5721 u102 AEN Yubilu Duruue d Wil s mp oold paezey uonesado soJnjeoJ junuuy jeuuouqy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Weather data is provided when the pilot initiates either a manual or automatic Connext data request on the Connext Weather Data Link Page on the MFD No weather data is displayed until the first Connext Weather Data Request is made Registering with Garmin Flight Data Services A subscriber account must be established prior to receiving Connext Weather products Contact Garmin Flight Data Services at https fly garmin com fly garmin support applications satelliteservices or by calling 1 866 739 5687 in the United States or 011 913 440 1135 After a subscriber account has been established the system must be registered for data link features such as reporting services or Connext Weather Registration is accomplished by entering the required access code This process is only performed when initially setting up the system for Connext services 1 With the aircraft outside and having a clear view of the sky turn the large FMS Knob
52. 20 miles WARNING Lamp s inside this product contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian A Wamings Cautions Motes GARMIN WARNING Do not use a QFE altimeter setting with this system System functions will not operate properly with a QFE altime
53. 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 2 3 With the Navigation Map displayed press the MAP Softkey Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Terrain and obstacles may be displayed in the Profile View by selecting the PROFILE Softkey TERRAIN SVS OPTIONAL 64 NOTE Terrain SVS is only available when the Synthetic Vision Technology SVT option is installed and the TAWS B option has not been installed NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazara avoidance Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360
54. 50 nose down 82 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Additional Features The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft There are no indications marking the pitch ESP engage and disengage limits in these nose up nose down conditions High Airspeed Protection Exceeding Vmo will result in ESP applying force to raise the nose of the aircraft When the high airspeed condition is remedied ESP force is no longer applied SIRIUSXM SATELLITE RADIO The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Sof
55. 90 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian n Seanpeooid Buluueld AEN Sd 523 oipny uadx svolti syuaumasu U105 AeN eouepioAy paezey s n ze 4 jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipuaddy x pul iui nuru Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry anothe
56. ANNUNCIATIONS Reversionary Condition un 2 o Text Both PFDs are displaying data from the n cu mber one Air Data Computer f Both PFDs are displaying data from the n c mber two Air Data Computer f Both PFDs are displaying data from the n System e mber one Attitude amp Heading Reference f Both PFDs are displaying data from the n System mber two Attitude amp Heading Reference f Both PFDs are displaying data from the number one GPS receiver 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 97 sainjea4 2 buluueld AEN Sd5 24V olpny uqax sv l sjuauimasu 2 Wil uio AeN nubi euonippv uoneiedo jJeuuouqy iie E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN Reversionary Condition Sensor Window Text Both PFDs are displaying data from the number two GPS receiver USINGADC1 PFD2 is displaying data from the 1 Air Data Computer UsNGADC2 PFD1 is displaying data from the 2 Air Data Computer USING AHRS1 PFD2 is displaying dat
57. ATE 52 oipny uadx 5721 U10 AEN sualy uonesado saunqea4 2 4 AEN Sd junuuy jeuuouqy feuonippv paezey Wfila x pu ddy x pul Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audio EICAS GPS Nav Procedures Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 2 3 Select the XPDR Softkey to display the transponder mode selection softkeys Select the CODE Softkey to display the transponder code selection softkeys for digit entry Use the digit keys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC or COM2 MIC on the audio panel Receive Only Press the COM1 or COM2 on the audio panel SELECTING A NAV RADIO 1 2 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 Press the NAV1 NAV2 or AUX Key on the audio panel to select or deselect the navigation radio audio source Pressing the AUX Key selects and deselects the ADF and DME All radio keys can be selected individually
58. ATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN 227 11 7N Large White COVIE 220 90N d LEMYN 220 ETE ae Large Cyan Approach KDFW RNAV 17LGPS LPV on 259 13 9NH Small Cyan 1 176 33w 2000FT Text INWOD 1767 3 2MM Small Cyan MENOL faf 176 39 Subdued Text ae ee m Small White Text 930FT 17 08 with Altitude POLKE Restriction Bar SIUE Cross AT or ABOVE 5 000 fi Fac Cross AT 2 300 ft 161610 Cross AT or BELOW 3 000 ft Altitudes associated with approach procedures are auto designated This means the system will automatically use the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small cyan text 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 21 svol4 wp olpny uqax uo2 AEN
59. Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts TEN Appendix Index Flight Director 15 Flight path marker 73 FliteCharts 74 75 Frequency Transfer 8 Fuel Alerts 95 96 Flow 5 Pressure 5 Quantity 5 G Gain 69 70 Generator Speed 5 H Horizon heading 73 Horizontal scan 69 Inhibit 65 67 Inhibit TAWS 67 Inhibit Terrain 65 Inset Map 127 128 134 Intercom isolation 9 Interturbine Temperature ITT 5 Warning 95 IOI 99 100 101 J Jeppesen 75 L Level Mode 81 Lightning 45 46 128 Index 2 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN M Magnetic Field Variation Database 140 Map panning 48 Message advisories 105 107 110 115 117 119 120 121 MET 98 METAR 47 134 Minimums 103 MISCOMP 97 Mistrim 98 99 MKR MUTE 9 Mode 132 Mode selection softkeys 7 8 Multi Function Display MFD Softkeys 133 N NAV 8 NAV1 2 8 NAV2 2 8 Navigation database 21 22 104 107 109 110 NEXRAD 47 128 133 134 NEXRAD Softkey 57 0 OBS 2 Obstacles 110 111 Oil engine Alerts 95 Pressure 5 Temperature 5 Overspeed Protection 16 Oxygen warning 95 P Pathvvays 73 74 PIREP 60 190 01842 00 Rev A A GARMIN PIT 97 Power up Page 85 Profile View 47 Propeller speed 5 R Register 50 Reversionary Mode EICAS 5
60. Arrival Leg Load and or Activate an Approach Procedure 40 Activate An Approach in the Active Flight Plan 42 Activate a Vector to Final Approach Fix s s si s s s 4 Activate A Missed Approach in the Active Flight Plan 42 Temperature Compensated Altitude ssssssseee 42 Hazard Avoidance 45 Customizing the Hazard Displays on the Navigation 45 STORMSCOPE Optional cccccccccssssssssscssssssssssscsssssssssecesssssssssscessssssessecesansssssnsess SiriusXM Weather Optional sss Connext Weather Optional s s s s S ss Traffic Systems Terrain And Obstacle Proximity Terrain SVS Optional Terrain Awareness amp Warning System TAWS B Display Optional 66 Airborne Color Weather Radar 68 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN table of Contents Additional 6 s s ooo 73 Synthetic VISIOn dee We He e OR e 73 Terminal Procedure Charts ssssseennn 74 Ai
61. C U KWIK and expressly disclai in this data exp merchantabilit AC U eliability or otherwise Licen maximum extent allowed by from any cause of action clai information arising out of Ga do not allow the limitation o its re m all warrant ess or implie ied including but not lim y representation ns or exclusions may not ated organizations herea y and fitness for a particular pu KWIK Organizations do not warrant or ma ons Inc and i warranties with The infor s regardin negligence sha result from the urpose AOPA be li use or inabi horized repr ees not to armless AOPA fro curacies in the inf ied warranties 0 orm app f ter collecti to not li pose The in e any rep ies with respect d including but See agrees not to s aw to release and hold harm ms or losses related to any ac rmin s use of the information exclusion of implied warranti consequential damages so th December 2014 190 01842 00 Rev A ts related organizations herei espect to the AOPA informati ted to the implied warranties mation is provided as is and AOPA does not g its accuracy reliability or sue AOPA and to the maximum m any causes of action claims or losses re ation Some jurisdictions do not allow the iability for incidental or consequential dam y to you f ue AC U K e above limitations or exclusions may not apply to lice f
62. COMPENSATION is highlighted 5 Press the ENT Key The temperature compensated altitude at the FAF is cancelled 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 43 sjuauimasu nubi 5721 oipny uddx UI0JNeN 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Procedures Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v ARN Sd5 buluueld Blank Page um aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 44 GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved f
63. D BUGS ON OR OFF mal ED gt m a g 2 o 2 2 a 1 Select the TMR REF Softkey 2 Press the MENU Key 3 Turn the FMS Knob to highlight the desired option 4 Press the ENT Key Select the TMR REF Softkey to remove the window 5219 SET BAROMETRIC MINIMUM DESCENT ALTITUDE olpny uqax 0105 AEN 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO TEMP COMP field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or TEMP COMP Selecting TEMP COMP will allow the system to use an altitude compensated for temperature 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey 2 buluueld AEN Sd5 241V 1ubil4 eouepioAy paezey DISPLAYING WIND DATA 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS AFCS Procedures GPS Nav Appendix Alerts Operation Features Index F
64. ETAR and TAF text 4 Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text METAR text must be completely scrolled through before scrolling NGE Knob and pan to the desired airport through the TAF text 5 Press the FMS Knob or the CLR Key to return to the Connext Weather Data Link Page Or 1 Select the Weather Information Page a Turn the b Select the WX Softkey to select the Weather Information Page 190 01842 00 Rev A large FMS Knob to select the Waypoint Page Group Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 59 AEN Sd5 S 24V oipny uddx 5219 sjuauimasu Tuo2 AEN sub Duruue d aoueploay s mp oold paezey SH lV uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 60 2 3 4 A GARMIN Press the FMS Knob to display the cursor Use the FMS Knob to enter the desired airport and press the ENT Key Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text Note that the METAR text must be completely scrolled through before scrolling through the TAF text To display the METAR legend on the Connext Weather Data Link Page select the LEGEND Softkey when METARs are selected for display Winds
65. FD1 Airport Directory database error exists The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 multiple database errors exists database errors exists PFD1 DB ERR PFD1 multiple The MFD and or PFD detected a failure in more than one database If problem persists the system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFDs and MFD have different navigation database versions or types Americas European etc installed Crossfill is off Install correct navigation database version or type in all displays DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or types Americas European etc installed Install correct standby navigation database version or type in all displays DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or types installed Install correct terrain database version or type in all displays 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 7213 Sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy ic pm x pul Hazard Flight Nav Com Fligh
66. G1000 Integrated Flight Deck Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Copyright 2014 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 2163 04 or later for the Piper PA 46 Meridian Some differences in operation may be observed when comparing the information in thi s manu Garmin International Inc Tel 913 397 8200 al to earlier or later software versions 1200 East 151st Street Olathe Kansas 66062 U S A Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Fax 503 364 2138 Tel 5 03 391 3411 5040 LR U K ES andi Web Except transm othe or p el 44 0 23 8052 4000 Garmin Corporation No 68 Jangsh el 886 02 2642 9199 or after hours emergency aircraft o n electronic storage m notice and provided furthe revisi Site Address www garmin com as expressly provided herei itted disseminated without the express writt inted copy of this manual or on hereto is strictly p Fax 913 397 8282 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton Hampshire Fax 44 0 23 8052 4004 downloaded or stored in any st en permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to edium to be viewed for personal use prov evision must conta
67. Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN ight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a
68. M Card 1 was removed Reinsert card The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data EXCEEDANCE Engine exceedance data is being logged An engine exceedance log has been captured SPD KEY DISABLED The SPD key is disabled for this model aircraft The SPD Key on GMC 710 has no function in this aircraft model REGISTER GFDS Data services are inoperative register w GFDS The system is not registered with Garmin Flight Data Services or it s current registration data has failed authentication Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments TRN AUD FAIL Trn Awareness audio source unavailable The audio source for terrain awareness is offline Check GIA1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req d Ter
69. N Qo U 6 Appendix IN Select to display the BARO setting as 2 inches of mercury 28 HPA Select to display the BARO setting as hectopacals R STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa olpny uqax UI05 AEN 52 SENSOR PFD OBS CDI DME ITMR REF D ODO D D AEN Sd5 Select the BACK Softkey to return to the top level softkeys buluueld Wila 1 2 3 4 5 6 7 IDENT BKSP BACK MSG F3 FV F3 V3 EN EN ES mnm onm nm 74 SeJnpa20Jd Transponder Softkeys H z XPDR Displays transponder mode selection 22 softkeys 2 STBY Selects Standby Mode transponder does not reply to any interrogations F 5 ON Selects Mode A transponder replies to 88 interrogations ALT Selects Mode C Altitude Reporting Mode 5 transponder replies to identification and altitude interrogations gt 5 m x x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix GND VER CODE IDENT ADS B TX IDENT TMR REF NRST ALERT 132 0 7 BKSP A GARMIN Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters
70. NREST unrestricted Softkey The selection is displayed in the Altitude Mode field 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 5 Press the MUTE Softkey to mute TAS voice alerts Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed press the MAP Softkey 3 Press the TRAFFIC Softkey Traffic is now displayed on the map 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 63 AEN 540 52 oipny uddx svn Sjueumajsul Tuo2 AEN iui Duruue d aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Displaying Terrain and Obstacles on the Terrain Proximity Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Terrain Proximity Page If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the
71. P config error Config service req d ESP is not configured properly The system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s p 2 Buruuejd AEN 5649 24V oipny uadx svoli syu unysu paezey nubi wi0 gt AeN nubi jeuonippy uoneiedo Jeuuouqy ps Eu x pul Flight Instruments Nav Com XPDR Audio Additional Hazard Flight Planning Abnormal EICAS AFCS GPS Nav Features Avoidance Procedures Operation Appendix Index Annunciations amp Alerts Blank Page 126 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 01842 00 Rev A amp GARMIN U hu Appendix APPENDIX sjuauimasu UATE PFD SOFTKEY MAP 5721 r mu m r FE m 75 m rs CDI NAV1 olpny uqax uo2 AEN CDI GPS Top Level PFD Softkeys E optional 77 OD D HU HU HU Hu D n Duruue d Wil optional optional optional PREGP DL LING optional or y n Nu 2 Select the BACK or OFF Softkey gt to return to the top level softkeys Sz ES m z Inset Map Softkeys ae go os 5 INSET Displays Inset Map in PFD lower left corner 2 2 OFF Removes Inset Map EH DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutter
72. Page 8 Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display 9 Remove power from the system Loading the Jeppesen Navigation Database as the Active Navigation Database The Jeppesen Navigation Database that is loaded to internal memory as the active database will be used by the system NOTE Loading the Jeppesen Navigation Database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow A NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or MFD to be updated label of SD card facing left 2 Turn the system ON A prompt is displayed in the upper left corner of the display DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO WORLDWIDE WORLDWIDE 1284 12805 09 RPR 2814 07 MAY 2814 7 MAY 2814 04 1UN 2814 NO WILL BE ASSUMED IN 21 SECONDS 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide
73. Reference Guide for the Piper PA 46 Meridian Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix WIND DME BRGI HSI FRMT BRG2 ALT UNIT A GARMIN HRZN HDG Displays compass heading along the APTSIGNS OPTN I OPTN 2 OPTN3 OFF 360 HSI ARC HSI METERS Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed Wind direction arrow with direction and speed Information not displayed Select to display the DME information window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMI
74. Request Cancelled 5 Press the FMS Knob to return to the Connext Weather Data Link Page Enabling Automatic Connext Data Requests 1 2 3 4 Select the Connext Weather Data Link Page Press the MENU Key With GFDS Weather Request highlighted press the ENT Key Choose the desired weather coverage options 56 5 Turn the large FMS Knob to select the UPDATE RATE setting Then turn the small FMS Knob to highlight the desired automatic update frequency OFF 5 Min 10 Min 15 Min 20 Min 25 Min 30 Min 45 Min or 60 Min then press the ENT Key Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance 6 The SEND REQ button is highlighted and a countdown timer is displayed in the REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate Connext Data Request Or Press the FMS Knob to return to the Connext Weather Data Link Page Connext Weather Products Precipitation Precipitation data is not real time The lapsed time between collection processing and dissemination of radar images can be significant and may not reflect the current radar synopsis Due to the inherent delays and the relative age of the data it should be used for long range planning purposes only NOTE Precipitation data cannot be displayed on the Navigation Map Page at the same time as terrain Display
75. Reversionary mode 89 ROC 99 100 101 S SafeTaxi 74 SBAS 16 40 66 67 91 Scheduler 77 Sector scan 70 Secure Digital SD card 85 Sensor 97 SiriusXM weather 47 STAB 70 Standby 68 Standby Navigation Database 138 Store Flight Plan 35 Stormscope lightning data 45 46 128 Strike 45 Strike mode 46 SVS 73 Synchronization 135 SYNC Status 139 Synthetic vision SVT 124 Synthetic Vision System 73 System ID 50 T TA 103 TAF 47 59 190 01842 00 Rev A Index TAS 63 103 115 TAWS 66 67 68 101 TAWS B 66 Telephone 13 Terrain 64 66 101 110 128 133 Terrain SVS 64 65 66 Tilt line 68 69 Timer 2 121 Topographical data 128 133 Torque 5 Traffic 45 62 133 Traffic advisory 62 Traffic Advisory 103 Traffic map page 62 63 64 Transponder 7 8 131 132 V Vertical speed guidance 22 Vertical track 103 VNV 19 90 123 W WAAS 111 WATCH 70 Waypoint Selection Submenu 30 Weather Attenuated Color Highlight 70 Weather data link page 47 Weather radar 68 Wind data 130 Winds Aloft 60 WIND Softkey 60 X XM lightning 128 134 XM Radio 83 84 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index 3 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax sY213 sjuauimasu jeuonippy 2 nubi Tuo2 NeN qb uoneiedo Jeuuouqy Sue v unuuy 1821 GARMIN Index Sjueuinijsu fila 5721 Tu102 AEN s24v
76. T Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 35 sjuauimasu BUT 5721 olpny uqax 0105 AEN 52 2 4 AEN 540 nubi aoueplony paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning GARMI N 2
77. TORED FLIGHT PLAN 1 2 36 Press the FPL Key on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Press the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied Flight Planning 5 Press the COPY Softkey A Copy to flight plan 22 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Press the DELETE Softkey A Delete flight plan 4 confirmation window is displaye
78. The G1000 system should be serviced MANIFEST GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments AHRS1 SERVICE AHRS1 needs service Return unit for repair A failure has been detected in the 1 AHRS The system should be serviced AHRS2 SERVICE AHRS2 needs service Return unit for repair A failure has been detected in the 2 AHRS The system should be serviced AHRS1 CONFIG AHRS1 config error Config service req d AHRS configuration settings do not match those of backup configuration memory The system should be serviced AHRS2 CONFIG AHRS2 config error Config service req d AHRS configuration settings do not match those of backup configuration memory The system should be serviced AHRS1 CAL AHRS1 calibration version error Srvc req d The 1 AHRS calibration version error The system should be serviced AHRS2 CAL AHRS2 calibration version error Srvc req d The 2 AHRS calibration version error The system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as inv
79. Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor 11 12 13 14 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 21 sjuaumasu sub 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 28 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD to select the WPT page group Turn
80. VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments database error exists MFD1 DB ERR MFD1 navigation PFD1 DB ERR PFD1 navigation database error exists database error exists PFD2 DB ERR PFD2 navigation The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR 2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s n e 4 aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 Sjueumasu paezey wi0 gt A
81. a based on active flight plan destination if the flight plan contains no destination dashes are displayed FPL Requests data based on active flight plan Turn the small FMS Knob to select the desired flight plan look ahead distance option or choose REMAINING FPL to request the remainder of the flight plan WAYPOINT Requests data based on any valid waypoint 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field and turn the small FMS Knob to select the desired diameter and route width of the request then press the ENT Key 6 Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Connext Data Link Page without requesting data During a Connext Data Request the Request Status box initially displays Contacting GFDS Once a connection is established the Request Status Box displays Receiving Wx Data Time Remaining with an estimated data transfer time either minutes or seconds If desired the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength The system retrieves all available Connext
82. a from the 1 AHRS USING AHRS2_ PFD1 is displaying data from the 2 AHRS USING GPS1 PFD2 is displaying data from the 1 GPS USING GPS2_ PFD1 is displaying data from the 2 GPS AFCS ALERTS Condition Annunciation Description Pitch Failure PT CHI Pitch axis control failure Roll Failure ROLL Roll axis control failure Pitch Trim Axis If annunciated when AP is engaged a failure has occurred in Control Failure PT RM the pitch trim system Yaw Damper Failure YAW YD control failure AP also inoperative System Failure AFCS AP and MEPT are unavailable FD may still be available Elevator Mistrim TELE A condition has developed causing the pitch servo to Up provide a sustained force in the nose up direction Elevator Mistrim JELE A condition has developed causing the pitch servo to Down provide a sustained force in the nose down direction Aileron Mistrim A condition has developed causing the roll servo to provide Left AIL a sustained left force Aileron Mistrim A condition has developed causing the roll servo to provide Right AIL a sustained right force 98 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Condition Annunciation Description Rudder Mistrim A condition has developed causing the yaw servo to Left RUD provide a sustained force Rudder Mistrim
83. airspeed is provided by the system 11 The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system 12 The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD 13 The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 25 sjuauimasu wp 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance
84. al attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glidepath e AFCS Annunciations 9 PFD Setup Menu and Vertical Deviation Flight director Com Windows displayed in Indicators mand Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box Barometric Minimum Transponder Status Descent Altitude Box Box Extreme Pitch Indication 30 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Abnormal operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircraft s current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an inv
85. alid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software MANIFEST GMU2 software mismatch communication halted mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 AEN Sd 24V olpny uqax svoli siu un sul paezey nubi Wil jeuonippy uoneiedo Jeuuouqy 5 R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations amp Alerts GDL 69A MESSAGE ADVISORIES A GARMIN Message GDL69 CONFIG GDL 69 config Comments GDL 69 configuration settings do not match error Config service req d those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software The GDL 69 has incorrect software installed
86. alid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a posi
87. altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Timer Expired Countdown timer on the PFD has reached zero Traffic The Traffic Information Service TIS has issued a Traffic Advisory alert TIS not available The aircraft is outside the TIS coverage area not available with TAS nstalled Traffic Traffic ayed when first Traffic Advisory TA is issued with an optional TAS P System Traffic for each subsequent TA TAS System Test Passed Played when the optional TAS system passes a pilot initiated self test TAS System Test Fail Played when the optional TAS system fails a pilot initiated self test TCAS One System Test Played when the optional TCAS system passes a pilot initiated self Passed test TCAS One System Test Played when the optional TCAS system fails a pilot initiated self test Fail FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others modified Flight Plan Import Export Description Results Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only The file stored on the SD card did not contain a flight plan User waypoints imported success only user
88. amp Alerts A GARMIN Caution Messages Description Chip detected An error was reported by the CAPS interface A fault was detected on the CAPS interface Propeller is fe athered or a failure has occurred in the feather system Fire detection system has failed Fuel filter approaching bypass and requires maintenance Fuel imba ance is over 40 Ibs Fuel quan tity is less than 180 Ibs A compon ent f the gear system has failed Hydra Oxygen systen 0 ulic pump is on Caution has 15 sec delay n has been tumed on Left pi tot heat has failed ight pitot heat has failed tot heat is off R Pi P opeller heat failu e ailure detected in stall warning system F Starter engaged when Ng is more than 56 for more than 10 sec Surface de ice fai Advisory Messages Bavsony Description DVABZ The 1 cooling fan for remote avionics has failed DVPAT VEZ YMEE The 2 cooling fan for remote avionics has failed BETA Propeller is operating in Beta mode DOOR AJAR Cabin door is not closed lias XU Emergency bleed is on FEATHER Propeller is feathered Shown when on ground or when NP lt 1350 L FUEL PUMP ON Le t fuel pump is on Inhibited if fuel pump is on for fuel autobalance when imbalance lt 40 Ibs R FUEL PUMP ON Right fuel pump is on Inhibited if fuel pump is on for fuel autobalance when imbal
89. ance 40 Ibs FUEL TEMP Fuel temperature is low Lene EU M Engine ignition is on ML RA EZ MEME The cooling fan for the MFD has failed 96 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Annuneiations amp Alerts Advisory Messages OXYGEN Oxygen system has been turned on Y RB The cooling fan for PFD1 has failed YA ETYM The cooling fan for PFD2 has failed EIAS ME Stall heater is on MAYO IO Starter engaged when Ng is less than 56 Description COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is gt 200 ft f both airspeed sensors detect lt 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts Difference in heading sensors is gt 6 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees PY eee No data from one or both altitude sensors NSM eee am No data from one or both airspeed sensors No data from one or both heading sensors Ji OE ME No data from one or both pitch sensors ORENK No data from one or both roll sensors REVERSIONARY SENSOR
90. ata card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists PFD1 DB ERR P
91. card in the system 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sainjea4 aoueplony saunpadold Duruue d AEN Sd5 S24JV oipny uddx sv l4 sjuauimasu jeuonippy paezey nubi Tuo2 NeN nubi uoneiedo Jeuuouqy Sue v unuuy EA Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix 5 GARMIN 2 3 4 5 6 1 8 9 10 11 12 Update the basemap SafeTaxi airport terrain obstacle and or airport directory databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen If a Verifying message is seen wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select t
92. ced GMAT SERVICE GMAT needs Service Return unit for repair The audio panel self test has detected a problem in the unit Certain audio functions may still be avail able and the audio panel may still be usable The G1000 system should be serviced when possible GIA 63W MESSAGE ADVISORIES Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The G A1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 temperature is too high If problem
93. chronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Updating Basemap SafeTaxi Obstacle and Airport Directory Databases These databases may be copied to one Supplemental Data Card then automatically synchronized to other
94. clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS or Traffic Collision Avoidance System TCAS1 Optional System Self Test 1 Set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test will take approximately eight seconds to complete When completed successfully traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed see Annuciations amp Alerts section If the self test fails the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page OPERATING is displayed in the Traffic Mode field 3 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or U
95. ct the Checklist Page Select the EMERGCY Softkey Turn the FMS Knob to select the desired emergency checklist and press the ENT Key Press the ENT Key or select the CHECK Softkey to check the selected emergency checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Additional Features 5 When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window and GO TO NEXT CHECKLIST is highlighted If GO TO NEXT CHECKLIST is selected prior to checking all the checklist items CHECKLIST NOT FINISHED will be displayed in yellow text 6 Press the ENT Key to advance to the next checklist 7 Select the RETURN Softkey to return to the previous checklist 8 Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 87 2 Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul 1614 Tu102 AEN yw 6114 aoueplony paezey xipuaddy Suelv uoneiedo sa
96. ctive ACTIVATE A DEPARTURE LEG 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure Procedures 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 39 sjuauimasu UATE 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000000 GARMIN 4 5 6 7 8 9 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large
97. cycle information is shown for each display Loading the Jeppesen Navigation Database as the Standby Navigation Database The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD card prior to its effective date The Jeppesen Navigation Database is available from Jeppesen seven days prior to its effective date 1 2 NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD Verify that an SD card is inserted in the bottom slot of each PFD and the MFD Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN 008 ndex 3 Turn the system ON A prompt is displayed D YOU WANT T UPDATE THE STANDBY NAVIGATION DATABASE N THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO WORLDWIDE WORLDWIDE 1284 1285 09 RPR 2814 07 MAY 2814 7 MAY 2814 04 1UN 2814 NO WILL BE ASSUMED IN 21 SECONDS 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card press any key to verify as instructed 6 After database veri
98. d 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the MFD to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 37 sjuauimasu Yid 5721 oipny uddx UI0JNeN 52 2 Bujuuejd AEN Sd5 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N 3 4 5 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USROOO USR001 5 002 and so on To change the user waypoi
99. d as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Press the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Flight Planning IMPORT A FLIGHT PLAN FROM AN SD CARD NOTE See the Annunciations amp Alerts section for flight plan import message descri
100. dditionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy SUSPECTED AUTOPILOT MALFUNCTION NOTE Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure If an autopilot failure or trim failure is suspected to have occurred perform the following steps 1 Firmly grasp the control wheel 2 Press and hold the AP DISC Switch The autopilot will disconnect and power is removed from the trim motor Power is also removed from all primary servo motors and engaged solenoids Note the visual and aural alerting indicating autopilot disconnect 92 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Abnormal operation 3 Retrim the aircraft as needed Substantial trim adjustment may be needed 4 Pull the appropriate circuit breaker s to electrically isolate the servo and solenoid components 5 Release the AP DISC Switch sjueuinasu wp 5721 OVERPOWERING AUTOPILOT SERVOS In the context of this discussion overpowering refers to any pressure or force applied to the pitch controls when the autopilot is engaged A small amount of pressure or force on the pitch controls can cause the autopilot automatic trim to run to an out of trim condition Therefore any application of
101. displays are subject to change and may not reflect the most current system and databases Depictions of equipment may differ slightly from the actual equipment 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A amp GARMIN ____ Waring Cautions k Notes 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 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 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the fo
102. ds of a 20 second interval the autopilot is automatically engaged with the flight director in Level Mode bringing the aircraft into level flight An aural Engaging Autopilot alert is played and the flight director mode annunciation will indicate LVL for vertical and lateral modes 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Buluueld AEN 540 52 oipny uadx sol sjuauinysu U102 AEN aoueplony paezey s n ze 4 jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipueddy x pul iui nuru Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features GARMIN The pilot can interrupt ESP by pressing and holding either the Control Wheel Steer ing CWS or Autopilot Disconnect AP YD DISC TRIM INTRPT switch Upon re leasing the CWS or AP YD DISC TRIM INTRPT switch ESP force will again be ap plied provided aircraft attitude and or airspeed are within their respective engagement limits ESP can also be overridden by overpowering the servos mechanical torque limit ESP can be enabled or disabled on the AUX SYSTEM SETUP 2 Page on the MFD To enable or disable ESP 1 Tum the large FMS Knob to select the AUX Page Group 2 Turn the small FMS Knob to select the System Setup Page 3 If
103. ds service Return unit for repair NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted NAV1 and or NAV2 software mismatch The system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunyea4 aoueplony 2 4 ARN 540 2 oipny uadx svo Sjueunasu jeuonippy uoneiedo Jeuuouqy x pul iui U105 AeN nu 2 ies EE Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN Message Comments G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G S1 needs s
104. dures must be learned on the ground WARNING 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 system utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the system can be misused or misinterpreted and therefore become unsafe Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A amp GARMIN Cautions Notes WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the Pilot s Guide documentation and the Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the system 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 Do not use the system to attempt to penetrate a thunderstorm The illustrations in this guide are only examples Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding any thunderstorm identified as severe of giving intense radar echo by at least
105. e 1 Use the FMS Knob to select the AUX System Setup 1 Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight RENAME in the Pilot Profile Box 4 Press the ENT Key 5 In the Rename Profile window turn the FMS Knob to select the profile to rename 6 Press the ENT Key 7 Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 79 Son pa20Jd Duruue d APN Sd5 241V oipny uadx 3461 UI0 AeN eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 80 A GARMIN 8 With RENAME highlighted press the ENT Key 9 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Deleting a profile 1 Use the FMS Knob to select the AUX System Setup 1 Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Tum the large FMS Knob to highlight DELETE in the Pilot Profile Box 4 Press the ENT Key 5 In the Delete Profile window turn the FMS Knob to select the profile to delete 6 Press the ENT Key
106. e desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO or TEMP COMP 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure Press the ENT Key If BARO or OFF was selected step 8 proceed to step 11 If TEMP COMP was selected in step 8 the cursor moves to the TEMP AT field Turn the small FMS Knob to enter the temperature at the destination airport The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value UJ 10 s mp old 11 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currentl
107. e settings 7 Press the ENT Key to select an option 8 Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings Connext Weather Data Requests Hazard Avoidance The Connext Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals if desired and the ability to send or cancel weather data requests The window also displays the status of the Connext data request process Requesting Connext Weather Data Manually 1 Select the Connext Weather Data Link Page 2 Press the MENU Key 3 With GFDS Weather Request highlighted press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 53 AEN Sd5 S 24V oipny uddx 5219 sjueuimasu Tuo2 AEN sub buluueld nubi aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 4 Turn the large FMS Knob to highlight the desired coverage option s and press the ENT Key to check or uncheck one of more of the following coverage selections e PRESENT POSITION Requests data based on current location DESTINATION Requests dat
108. eN nubi jeuonippy uoneiedo Jeuuouqy ic ka x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN Message Comments MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing database missing PFD2 DB ERR PFD2 obstacle The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace d
109. ed AHRS2 TAS AHRS2 not receiving airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 AEN Sd S24V oipny uadx svoli syu unysu paezey Wfila u102 NEN Wil euonippv uoneiedo Jeuuouqy ie Eu x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN Message Comments AHRS1 GPS AHRST not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should
110. ed 1 determining vertical aircraft as it passes for use in giving flight path guidance over the navigation vertical flight path point This altitude guidance Altitude is provided as a does not match the reference and is not published altitude in designated to be used navigation database or in determining vertical 1 no published altitude flight path guidance exists Small Text Altitude is not Altitude is designated The system cannot designated to be used for use in giving vertical use this altitude in in determining vertical flight path guidance determining vertical flight path guidance Altitude has been flight path guidance Altitude has been etrieved from the retrieved from the navigation database navigation database or has been entered by and is provided as a the pilot and matches reference a published altitude in the navigation database 22 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN FLIGHT PLANNING WEIGHT amp FUEL PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters Flight Planning The Weight Fuel Exceedances Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the WEIGHT PLANNING page 1 Select the EMPTY WT Softkey to place the cursor in the Basic Emp
111. eded 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V oipny uadx 7219 Sjueumasu puezey ubi UI05 AeN ubiu uoneiedo Jeuuouqy ic R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN Message Comments FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace withi
112. eiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix od Amundatons amp Alerts TAWS System System Test Pass None None Test OK TAWS B System Test Fail Terrain or Obstacle database unavailable TAWS System or invalid Failure invalid software configuration system audio fault MFD Terrain or Obstacle database unavailable or invalid R None None System operating with PFD Terrain or Obstacle databases TAWS Not No GPS position TAWS N A Available Excessively degraded GPS signal or out of TAWS Not database coverage LTAWS N A Available area MESSAGE ADVISORY ALERTS Alerts Window Message Audio Alert PFD1 FAN FAIL The cooling fan for PFD1 is inoperative PFD2 FAN FAIL The cooling fan for PFD2 is inoperative R one MFD FAN FAIL The cooling fan for the MFD is inoperative AV FAN FAIL The cooling fan for remote avionics has failed AURAL ALERTS Aural Alert Description Airspeed Airspeed has exceeded VMO 102 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Minimums Minimums The aircraft has descended below the preset minimum descent altitude or decision
113. ertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation boox The position of the selected waypoint xxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint TRAFFIC FAIL Traffic device has failed STRMSCP FAIL Stormscope has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced Stormscope has failed The G1000 system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoueplon
114. ervice Return unit for repair G S2 SERVICE G S2 needs Service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The G1000 system should be serviced GTX 33 33D ES MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d MANIFEST GTX1 software mismatch communication halted The transponder configuration settings do not match those of backup configuration memory
115. es 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 most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian D xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax 5921 sjuauimasu junuuy Jeuuouq
116. fication is complete press any key to continue as instructed on the display 7 Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting 8 Press the ENT Key to acknowledge the startup screen 9 Turn the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page 11 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle 12 Turn system power OFF 13 Remove the SD card from the top card slot of the MFD 14 Turn system power ON 15 Press the ENT Key to acknowledge the startup screen 16 Turn the large FMS Knob to select the AUX Page group on the MFD 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian uonesado s n e 4 eouepioAy s mp oold Buruue d AEN Sd5 yi oipny uddx sv l3 siu u nnsu jeuuouqy jeuonippy paezey T TR wio gt AeN 1614
117. file Box Press the ENT Key A Create Profile window is displayed Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key Pilot profile names cannot begin with a blank as the first letter Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Additional Features 6 In the next field use the small FMS Knob to select the desired settings upon which to base the new profile Profiles can be created based on Garmin factory defaults default profile settings initially based on Garmin factory defaults unless edited by the pilot or current system settings 7 Press the ENT Key 8 With CREATE highlighted press the ENT Key to create the profile SjueuinJjsu 346 5721 Or Use the large FMS Knob to select CREATE and ACTIVATE and press the ENT Key to activate the new profile 9 To cancel the process select CANCEL with the large FMS Knob and press the ENT Key Selecting an active profile 1 Use the FMS Knob to select the AUX System Setup Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Tum the large FMS Knob to highlight the active profile field in the Pilot Profile Box 4 Turn the small FMS Knob to display the pilot profile list and highlight the desired profil 5 Press the ENT Key The system loads and displays the system settings for e the selected profile Renaming a profil
118. for the Piper PA 46 Meridian s mip q e uepioAy SaJnpa20Jd Duruue d AEN Sd5 241V oipny uddx sv l3 siu uinnsul jeuonippy piezeg nubi Tuo2 NeN Yid uoneiedo Jeuuouqy Sue v unuuy eed Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN 3 4 Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL QUERWRITE THE ACTIVE NAVIGATION DATABASE FROM TO WORLDWIDE WORLDWIDE 1204 1285 09 RPR 2014 7 MAY 2014 7 MAY 2014 04 2014 NO WILL BE ASSUMED IN 8 SECONDS 9 10 11 After the update completes the display starts in normal mode Turn the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD Apply power to the system and press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database
119. ge Advisories 5 GMU 44 Message Advisories 7 GDL 69A Message Advisories sss 8 GWX 68 Alert Messages 8 ii 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Table of Contents GARMIN GTS 825 855 Message Advisories sssssssseee 119 GDC 74A Message Advisories sssssssssenne 119 GCU 476 Message Advisories sssssssseeeene 120 GMC 710 Message Advisories 120 Miscellaneous Message Advisories sssssse 121 ADBEDUDO 27 PFD Softkey 2 21 LEA AET nnne 33 Loading Updated Databases 34 dT PEN Index 1 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Select the PFD Softkey to display the second level softkeys 2 Select the STD BARO Softkey CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure sett
120. he AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display Updating Terrain Airport Terrain FliteCharts and ChartView Databases The Terrain and Airport Terrain databases must be copied to both Supplemental Data Cards The FliteCharts or ChartView databases should be copied to the MFD Supplemental Data Card only 1 2 3 4 With system power OFF remove the Supplemental Data Card from the bottom card slot of the MFD and PFD Update the terrain airport terrain and or FliteCharts or ChartView databases on the appropriate Supplemental Data Cards Insert the updated Supplemental Data Cards into the bottom card slot of the MFD and PFD Apply power to the system check that the databases are initialized and displayed on the power up screen A Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN o 600X0X Appendix 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Tum the small FMS Knob to select the System Status
121. he approach waypoints are displayed in slanted text HABUK iaf 021 5 7NM HABUK iaf 021 5 7NM 22788rFT FALUR 261 4 7NH FALUR 91 4 7NM 8418Fr CEGIX faf 51 5 9NH CEGIX fuf SSH 5 SNM 27529FT RW35R map 5 1NH RW35R map d r 5 11NM 6368FT r 5NM 6368FT 6368FT 348 5NM 5355FT MOGAL mahp MOGAL mahp 97121 HOLD 8 2211 HOLD 38 6 0NH L Altitudes Displayed Without Altitudes Dis Ded With Temperature Compensation ompensation 4 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Enabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Procedures 4 Use the small FMS Knob to select the temperature at the lt airport gt The compensated altitude is computed as the temperature is selected 5 Press the ENT Key ACTIVATE COMPENSATION is highlighted 6 Press the ENT Key The compensated altitudes for the approach are shown in the flight plan Disabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed 4 Press the ENT Key CANCEL
122. ight plan was imported with as many waypoints as possible Some waypoints not loaded Way points locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely PILOT PROFILE IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results No pil
123. in the complete text of this copyright that any unauthorized commercia ohibited distribut u 2nd Road Shiir Taipei County Taiwan Fax 886 02 2642 9099 n ground AOG technical support for Garmin panel mount tegrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 n no part of this manual may be reproduced copied orage medium for any purpose this manual onto a hard drive or ided that such electronic ion of this manual or any Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries WATCH ta cn NavData is a registered trademark of Jeppesen Inc St of L 3 Communications Honeywell and Bendix King are registered trademarks of Honeywell International Inc iteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin ormscope is a registered trademark iriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AOPA Membership Publicati AOPA expressly disclaim al data express or imp and fitness for a pa warrant or make an no circumstances in consequential dama ticular p cluding ges that documentation even if AOPA or an AOPA aut uch damages User ag possibility of s by law to release and hold h to any actual or alleged inac limitation or exclusion of impl so the above limitatio A
124. ing GRS1 Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS1 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN 00 8 ndex 2 When the upload is complete the prompt for the next GRS upload is displayed as seen in the following figure GRS2 MY DB Update Available Update from 2005 to 2010 FA OK or CANCEL GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use Uploading GRS2 Mag Var Database STARTING UPLOAD 6 0 Uploading Database to GRS2 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 AEN Sd5 24V oipny uadx svoli sjuaum su Jeuonippy paezey ni U105JNeN 146114 uoneiedo Jeuuouqy Sue v unuuy lz GARMIN Index Sjueuinijsu fila 5721 Tu102 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey s s Jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 142 A GARMIN A Access code 50 Activate a flight plan 20 Active Channel 83 Active database 138 Active Navigation Database
125. ing Precipitation Weather Information 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the Connext Weather Data Link Page 2 Select the PRECIP Softkey Radar data shown represents lowest level base reflectivity of radar returns The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the Connext Weather Data Link Page For the Precipitation legend select the LEGEND Softkey when Precipitation is selected for display Precipitation Limitations Radar images may have certain limitations Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics wet hail vs rain For example it is not possible to distinguish between wet snow wet hail and rain 2 Radar base reflectivity is sampled at the minimum antenna elevation angle An individual radar site cannot depict high altitude storms at close ranges It has no information about storms directly over the site 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 57 uonesado s n e 4 aoueploay s mp oold Buruue d AEN Sd5 yi olpnyygqax sv l3 Sjueumasu junuuy jeuuouqy jeuonippy xipueddy x pul iui JUI0JNeN nu paezey Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight
126. ing at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 1 and or COM2 may still be usable The G1000 system should be serviced when possible COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 CONFIG COM1 configuration error COM2 CONFIG COM2 configuration error COM1 and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST COM1 software MANIFEST COM2 software mismatch communication halted mismatch communication halted COM1 and or COM2 software mismatch The system should be serviced LOI GPS integrity lost Crosscheck with
127. ing in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF SYNCHRONIZE CDI 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian uonesado saunqea4 2 Buruuejg AEN 5649 S24V oipny uadx sv junuuy jeuuouqy jeuonippy paezey ESTE JU05JAEN xipueddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1 2 3 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the cyan tuning box over the NAV1 standby frequency in the upper left corner of the PFD Select the CDI Softkey again to change from VOR1
128. inished to remove the Chart Setup Menu AIRPORT DIRECTORY The Aircraft Owners and Pilots Association AOPA and optional AC U KWIK Airport Directory add enhanced airport information when viewing airports on the WPT Airport Information Page Both Airport Directories are available for downloading at flygarmin com However copy only one of the databases to the Supplemental Data Card The system cannot recognize both databases simultaneously 76 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN View Airport Directory Information While viewing the WPT Airport Information Page if necessary press the INFO 1 Softkey to change the softkey label to display INFO 2 Airport information is displayed on the right half of the display SCHEDULER Additional Features The Scheduler feature can be used to enter and display reminder messages e g Oil Change Switch fuel tanks or Altimeter Transponder Check in the Messages Window on the PFD Messages can be set to display based on a specific date and time event once the message timer reaches zero one time default setting or recurrently whenever the message timer reaches zero periodic Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed When power is cycled all messages are retained until deleted and message timer countdown is resumed Scheduler messages appear in the Ale
129. injea4 unuuy Jeuuouqy Jeuonippy x pul GARMIN itional Features Add Sjueuinijsu fila svold olpny uddX U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s l Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 88 GARMIN Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE If the system detects an MFD failure reversionary mode is entered automatically Reversionary mode must be entered manually inthe case ofa PFD failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Manual activation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MED By pressing the DISPLAY BACKUP Button on the left or the right audio panel PFD2 By pressing the DISPLAY BACKUP Button on the right audio panel NOTE The Piper PA 46 Meridian Pilot s Operating Handbook POH always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the
130. ink Lightning information 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the Connext Weather Data Link Page 2 Select the DL LTNG Softkey To display the Data Link Lightning legend on the Connext Weather Data Link Page select the LEGEND Softkey when Data Link Lightning is selected for display 58 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN SIGMETs and A IRMETs Hazard Avoidance The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the Connext data request Displaying SIGMETs and AIRMETs 1 Select the Co nnext Weather Data Link Page 2 select the SIG AIR Softkey 3 To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon 4 Press the ENT key To display the SIGMET and AIRMET legend select the LEGEND Softkey when SIGMETs and AIRME Ts are selected for display METARs and TAFs NOTE METAR information is only displayed within the installed navigation database service area METAR and TAF text are displayed on the WPT Weather Information Page TAF information is displayed in its raw form when it is available Displaying METAR and TAF text 1 On the Connext Weather Data Link Page select the METAR Softkey 2 Press the RA 3 Press the ENT Key The Weather Information Page is shown with M
131. io Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 3 4 A GARMIN Press the FMS Knob to remove the cursor Press the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Ground Mapping 1 2 3 Press the MODE Softkey Press the GROUND Softkey to place the radar in Ground Map Mode Press the BACK Softkey Sector Scan 1 2 3 4 5 6 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan Press the FMS Knob to display the cursor Turn the large FMS Knob to place the cursor in the SECTOR SCAN field Turn the small FMS Knob to select FULL 60 40 or 20 scan If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan Press the FMS Knob to remove the cursor Antenna Stabilization 1 2 To activate or deactivate the antenna stabilization press the MODE Softkey Press the STAB ON Softkey to activate antenna stabilization or press the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activa
132. ion and press ENT Key Switching Between Connext and SiriusXM Weather Sources 1 2 3 4 Turn the large FMS Knob on the MFD to select the MAP page group Turn the small FMS Knob to select the desired Weather Data Link Page Press the MENU Key Turn the large FMS Knob to select Display Connext Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Legends for Displayed Connext Weather Products 1 2 Select the Connext Weather Data Link Page Select the LEGEND Softkey to display the legends for the displayed weather products Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Or a Press the MENU Key b Select Weather Legend and press the ENT Key 3 Turn the FMS Knob to scroll through the legends if more are available than fit in the window 4 To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Setting Up and Customizing Weather Data for the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select the Weather Group and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON OFF rang
133. itional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 7 8 9 A GARMIN Press the ENT Key again or use the large FMS Knob to move the cursor to the next field For periodic and one time message use the FMS Knob to enter the timer value HH MM SS from which to countdown and press the ENT Key For event based messages a Use the FMS Knob to enter the desired date DD MM YY and press the ENT Key b Press the ENT Key again or use the large FMS Knob to move the cursor to the next field c Use the FMS Knob to enter the desired time HH MM and press the ENT Key 10 Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message Deleting a scheduler message 1 2 3 4 5 Select the AUX Utility Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight the name field of the scheduler message to be deleted Press the CLR Key to clear the message text If the CLR Key is pressed again the message is restored Press the ENT Key while the message line is cleared to clear the message text PILOT PROFILES Creating a profile 78 1 2 3 4 5 Use the FMS Knob to select the AUX System Setup Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight CREATE in the Pilot Pro
134. ivates flight director 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 15 svol4 Sjueumajsul sub olpny uqax U10 AeN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude Captures the Selected Altitude ALTS Armed Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn r Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn Fem to the Selected Altitude Maintains the current aircraft Flight Level Change airspeed while the aircraft is dimbing FLC Key FLC nnnkr descending to the Selected Altitude Vertical Path Captures and tracks decent legs of an VNV Tracking active vertical profile Key VNV Target Altitude Captures the Vertical Navigation VNV n ALTV Capture Target Altitude Glidepath Captures and tracks the SBAS glidepath GP on approach Ca
135. level softkeys Sensor Softkeys Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN 000 Appendix ADCI Selects the 1 Air Data Computer Zl ADC2 Selects the 2 Air Data Computer E AHRSI Selects the 1 AHRS AHRS2 Selects the 2 AHRS r 75 NN ES S oipny uddx U105 AeN n 7 m r 52 Select the BACK Softkey to return to the top level softkeys AEN Sd5 l l J 366 nsi FARC Hs l l l amp c vse L IL LL eres L L Tac F3 V3 A F3 FS PS 98 98 08 08 098 n9 L ICom J ome omes L or L L L L Lsee L iss E V3 IY 7 EM S HNH 75 n onm PATHWAY SYN TERR HRZN HDG APTSIGNS BACK MSG E V3 V3 V3 F3 7 EN nn n nm om Duruue d nubi SeJnpa20Jd aoueplony paezey saunqee4 jeuonippy PFD Configuration Softkeys or PFD Displays second level softkeys for a8 additional PFD configurations sa DFLTS Resets PFD to default settings including su jy unuuy changing units to standard SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features gt 5 3s o x PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction x pul 190 01842 00 Rev A Garmin 61000 Cockpit
136. light Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 01842 00 Rev A A GARMIN 1045 ENGINE INDICATION amp CREW ALERTING SYSTEM X snnn 400 DIFF PSI CABIN PRESS ALT FT 8000 g DIFF PSI 26 FUEL QTY LBS 500 RUD E PPH 310 TRIM 5 FUEL C wj AMPS GEN 130 ea By ALT 40 B VOLTS 28 0 VACUUM IN HG 56 FLAPS 15 LANDING GEA 0 EICAS Display Normal Mode EIS Display Reversionary Mode Torque Fuel Quantity 3 Generator and Alternator Currents Interstage Turbine Fuel Flow Voltages Temperature 0 Propeller Speed Fuel Temperature 5 Vacuum Generator Speed Cabin Pressure Altitude Rudder Trim FUEL QTY LBS 600 508 408 and Change Rate Oil Pressure 1 Differential Pressure 77 Flap Position 5 Oil Temperature 2 Destination Elevation 17 Gear osition 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian sjueumasu spay uoneiedo s m p q SoJnpa20Jd buluueld AEN 540 24V olpny uqax junuuy jeuuouqy feuonippv xipueddy x pul 10614 Wfl paezey Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Appendix Index EICAS LANDING GEAR INDICATIONS A GARMIN Position Up amp Locked
137. n 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm APR INACTV Approach is not active Special use airspace is within 2 nm of the aircraft position The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach SLCT NAV Select NAV on CD for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Message Comments PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next v
138. n G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu UATE 52 oipny uadx 5219 U105 AEN xipuaddy Suelv uoneiedo saunjea4 aoueplony 2 Duruue d AEN Sd5 junuuy Jeuuouqy Jeuonippy paezey ubi x pul Nav Com AFCS XPDR Audio EICAS Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning Procedures GPS Nav Appendix Alerts Operation Features Index A Nav Com XPDR Audio Panel GARMIN Pilot Isolate Mode In Pilot Isolate mode the Pilot Copilot and Passengers hear the aircraft audio The Copilot and Passengers also hear each other Aircraft Audio b PILOT COPLT PASS ICS Keys Mode Operation Passenger Crevv Isolate Mode n Passenger Crew Isolate mode the Pilot and Copilot hear the aircraft audio and each other The Passengers hear each other Aircraft Audio bh d d PILOT COPLT PASS ICS Keys Mode Operation Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Nav Com XPDR Audio Panel Copilot Isolate Mode In Copilot Isolate mode the Pilot and Passengers hear the aircraft audio and each other The Copilot has the option to use Split COM mode Split COM Aircraft Audio n v PILOT COPLT PASS ICS Keys Mode Operation All Isolate Mode In All Isolate mode the Pilot hears the aircraft audio The Copilot has
139. n GPS a titude Indicator d Navigation VOR mode maximum limited to the Low Bank mode value if it is engaged roll command limit will be evel mode can only become activated as a 7 of Electronic Stability and Protection ESP Refer to the Additional Features section for a detailed discussion of the optional ESP feature Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 With the MFD selected on the controller press the Direct to EZ Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted GPS Navigation 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to acti
140. n SVS Page is displayed press the MENU Key Turn the small FMS Knob to select Enable Terrain Press the ENT Key NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY OPTIONAL 66 WARNING Do not use the terrain avoidance feature as the sole means of navigation and terrain separation The terrain avoidance feature is only to be used as and aid to terrain avoidance Garmin obtains terrain database content from third party sources and is not able to independently verify the accuracy of the terrain data NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS B operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 2 Turn the large FMS Knob to select the Map Page Group Turn the
141. nding on sensors associated with that LRU are automatically inhibited Inhibits cannot be activated by invalid sensor data Warnings Messages Warning Messages Description Alternator has failed Bleed over temperature Cabin altitude above 12 000 feet Landing gear not down and locked Cabin door is not closed Engine fire A flap system failure has occurred Fuel imbalance is over 125 Ibs Fuel pressure is low Fuel quantity is less than 100 Ibs A component of the gear system has failed Generator has failed Hydraulic pump is on Both left and right pitot heat have failed Propeller heat failure Surface de ice fai Underspeed protection active Windshield heater over temperature or controller malfunction Caution Messages Caution Messages Description Propeller is operating in Beta mode Cabin altitude is above 10 000 feet Landing gear not down and locked 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 95 sainjea4 2 Duruue d AEN Sd5 S24JV olpny uqax sY213 sjueuimasu 2 Wil uio AeN Yid jeuonippy uoneiedo Jeuuouqv E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations
142. near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions 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 WARNING Do not rely on information from the lightning detection system display as the sole basis for hazard weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to the documentation from the lightning detection system manufacturer for detailed information about the system WARNING The Garmin system as installed in this aircraft 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 WARNING Do not use the system until carefully reviewing and gaining a thorough understanding of all aspects of the system s Pilot s Guide documentation and the Airplane Flight Manual Do not attempt to learn system operational procedures while the aircraft is in the air For safety reasons system operational proce
143. nt name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 7 38 NOTE See the Annunciations amp Alerts section for flight plan export message descriptions Insert the SD card into the top card slot on the MFD Press the FPL Key to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Press the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is a
144. o select MUS1 or MUS2 and select the crew positions to receive the music audio Selecting any key other than PILOT COPLT PASS MUS MUS2 or will cancel Blue Select Mode Pressing the small knob will also cancel Blue Select Mode After approximately ten seconds with no input the Blue Select Mode will automatically cancel Enabling Disabling Muting Press and hold the MUS1 MUS2 or ec Key for two seconds to switch muting on and off The aural message Mute Music on Reception Enabled Disabled or Mute Tel and Jack on Reception Enabled Disabled is heard 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Sjueunasu 52 oipny uadx 5721 U10 AEN Suelv uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui nu A Nav Com XPDR Audio Panel GARMIN Flight EICAS Instruments Nav Com 25 x x o x GPS Nav AFCS Flight Planning Blank Page Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Procedures Appendix Index Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis AFCS NOTE If the at
145. on and press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 33 aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Flight Procedures Planning GPS Nav Additional Hazard Avoidance Abnormal Annun Flight Instruments EICAS AFCS Appendix Alerts Operation Features Index Flight Planning GARMI N 34 6 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key 7 Press the ENT Key while ACTIVATE is highlighted to immediately activate the hold Creating a User Defined Hold at a Direct To Waypoint 1 Press a Direct to Key and set up the Direct To waypoint as desired but select HOLD instead of ACTIVATE when finished 2 Use the FMS Knobs to edit the entry course and press the ENT Key 3 Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key 4 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 5 Use the FMS Knobs to edit the length and press the ENT Key 6 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 7 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key 8 Press the ENT Key while ACTIVATE is highlighted to activate the Direct To with
146. on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX SYSTEM STATUS Note the System ID number in the AIRFRAME field 3 Turn the large FMS Knob to select the MAP Page group 4 Tum the small FMS Knob to select the MAP WEATHER DATA LINK CNXT Page 5 Press the MENU Key If necessary select Display GFDS Weather 6 Press ENT Key The GARMIN FLIGHT DATA SERVICE REGISTRATION Window is now displayed 7 Press the MENU Key The Page Menu window is now displayed 8 Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field 9 Press the ENT Key REGISTER will now be highlighted 10 Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field Accessing Connext Weather Products 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Connext Weather Data Link Page When a weather product is selected for display on the Connext Weather Data Link 90 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance Page a box containing a symbol for the product and its age in minutes are shown in the upper right If weather data has not been requested N A is shown next to the product symbol instead of age The age of the weather product is based on the time difference between when the data was assembled
147. on the ground and the current GPS time Weather products are updated continuously or refreshed at specific intervals defined in the Refresh Rate column in the following table If for any reason a weather product is not refreshed within the defined Expiration Time intervals the data is considered expired and is removed from the display The age of the expired product is replaced by dashes If more than half of the expiration time has elapsed the color of the product age readout changes to yellow The refresh rate represents the interval at which the GFDS servers make available the most current known weather data It does not necessarily represent the rate at which new content is received from weather sources Expiration Weather Product Symbol Time 5 Rate Minutes Minutes Radar Precipitation E T U S Canada 3 PRECIP Europe 15 Infrared Satellite afi IR SAT E Data Link Lightning Eh DL LING 30 Continuous SIGMETS AIRMETs SIGMET R SIG AIR AIRMET 2 Meteorological Aerodrome Report METARs 90 Continuous Pilot Weather Report Winds Aloft WIND 2202 60 Continuous PIREP 90 Continuous Temporary Flight Restrictions no product image 60 TFRs 7 no product image 60 Continuous The composite precipitation image is updated every 3 minutes but individual radar sites may take between 3 and 10 minutes to provide new data
148. or weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old KJ Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LTNG 2 Tum the large FMS Knob to select STRMSCP MODE 3 Turn the small FMS Knob to display the Cell Strike window 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 ACN Sd5 S24V oipny duadx 59213 5349 0115 nubi Duruue d Wil s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 46 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormsco
149. ot profile plan files found to import Description Displayed if the SD card does not have one or more valid pilot profile filenames Overwrite existing profile Displayed if the profile name matches the name of existing profile Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Annunciations amp Alerts Flight Plan Import Export Description Results Profile name invalid Enter a Displayed if the profile name is invalid different profile name All available pilot profiles in use Displayed if the maximum number for pilot profiles has Delete a profile before importing been reached another Pilot profile import failed Displayed if the importing operation fails for any other reason Pilot profile import succeeded Displayed if the importing operation succeeds Overwrite existing file Displayed if the filename matches the name of an existing file on the SD card Pilot profile export failed Displayed if the export operation fails Pilot profile export succeeded Displayed if the export operation succeeds MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with prefer
150. ount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists LOADING UPDATED DATABASES Database information is obtained from third party sources Inaccuracies in the data may be discovered from time to time Garmin communicates this information by issu ing a Database Alert These notifications are available on http fly garmin com Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to http fly garmin com and select Aviation Data Error Report 134 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system A NOTE When loading database updates the DB Mismatch message will be displayed until database syn
151. pe Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Tum the large FMS Knob until the Map Page group is selected 2 Tum the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data from the dis
152. play Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN y Neen Avaidanes SIRIUSXM WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions Displaying SiriusXM on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD and or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page 3 Winds Aloft can be displayed in the Profile View by selecting the PROFILE Softkey Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Switching Between SiriusXM and Connext Weather Sources 1 Tum the large FMS Knob on the MFD to select the MAP page group 2 Tum the small FMS Knob to select the desired Weather Data Link Page 3 Press the MENU Key 4 Turn the large FMS Knob to select Display XM Weather or Display Connext Weather and press the ENT Key Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Gro
153. pressure or force to the controls should be avoided when the autopilot is engaged Overpowering the autopilot during flight will cause the autopilots automatic trim to run resulting in an out of trim condition or cause the trim to hit the stop if the action is prolonged In this case larger than anticipated control forces are required after the autopilot is disengaged The following steps should be added to the preflight check 1 Check for proper autopilot operation and ensure the autopilot can be overpowered oipny uddx UI0JNeN 52 ARN Sd5 Wil s mp 01d 2 Note the forces required to overpower the autopilot servo clutches paezey s E 2 E 5 2 jeuonippy xipuaddy suelv junuuy x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 93 Annun Additional Hazard Flight Nav Com Flight Appendix Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Index Blank Page 94 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN ANNUNCIATIONS amp ALERTS CAS MESSAGES Annunciations amp Alerts If two alert levels of the same message are active simultaneously e g DOOR AJAR warning and DOOR AJAR advisory only the higher alert level is displayed Ifa GEA or GIA fails all CAS messages depe
154. ptions 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the MFD to display the Active Flight Plan Page 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Press the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again press the IMPORT SoJnpa20Jd AEN 540 nubi svo sjuounasu U105 AEN 346 olpny uqax 52 Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If required press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint 4 Turn the small FMS
155. ptures and tracks the ILS glideslope ej Glid slope aptures and tracks the ILS glideslope GS on approach Go Around Commands a constant pitch attitude GA and wings level TO GA Commands a constant pitch angle switch Takeoff and wings level on the ground in TO preparation for takeoff 16 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN AFCS Vertical Mode Description Control Annunciation Level ALTS armed automatically when PIT VS FLC or GA active and under VPTH wh is to be captured instead of VNAV Target Altitude Autopilot engages and commands pitch angle necessary to establish zero vertical FPM LVL en Selected Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Tevel mode can only become activated as a of Electronic Stability and Protection ESP Refer to the Additional Features section for a detailed discussion of the optional ESP feature LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll attitude Roll Hold or rolls the wings level depending on default ROL the commanded bank angle Limits the maximum commanded roll BANK 5 Low Bank angle Key Heading Select Captures and tracks the Selected HDG HDG Heading Key Navigation GPS GPS Navigation VOR 777 Cap
156. r source of charts on board the aircraft SafeTaxi SafeTaxi gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing n Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Additional Features Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal procedur
157. r the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Nav Com XPDR Audio Panel TELEPHONE ENTERTAINMENT AUDIO The telephone entertainment ZH Key controls a telephone or entertainment device connected to the rear of the audio panel or to the Front Panel Jack The MUSI and MUS2 Key controls the Entertainment Music audio input The Front Panel Jack can be used as an entertainment input or a telephone input in which case it disables the rear telephone interface The Front Panel Jack is a 3 5 mm stereo jack that is compatible with popular portable entertainment devices such as MP3s CD players and cell phones The headphone outputs of the entertainment devices can be plugged into the Front Panel Jack or the MUSI or MUS2 external jacks The music MUSI MUS2 and telephone entertainment audio are distributed using the Blue Select Mode The Blue Select Mode is entered by pressing the small knob when the volume control cursor flashing white annunciator is not active If the volume control cursor is active press the small knob twice The first press will cancel the volume control cursor the second will activate Blue Select Mode The annunciator over the Key will be flashing blue Any combination of the annunciators over the PILOT COPLT and PASS buttons may be blue Select the desired button to turn the blue annunciator on or off to distribute the telephone entertainment audio to selected crew passenger positions Turn the large knob t
158. rain audio alerts are not configured properly The system should be serviced HOLD EXPIRED Holding EFC time expired Expect Further Clearance EFC time has expired for the User Defined Hold BARO MISMATCH Correct baro mismatch for VNAV guidance Altimeter setting is not the same on PFD1 and PFD2 Synchronize settings for VNAV guidance TERRAIN DISABLED Terrain Awareness DB resolution too low TAWS is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed GDU ZOOM LIMITED Map zoom has been automatically limited Increases in map range are automatically limited at gt 68 degrees 35 minutes north or south a gt CURSOR LIMITED Map panning limit has been reached AV AFT FAN FAIL The cooling fan for remote avionics has failed Map cursor panning is limited to lt 89 degrees north or south The cooling fan for the aft remote avionics has failed CPCS CONFIG ERROR Unexpected config strapping GAE 43 FAILURE Using controller cabin information ESP OFF ESP selected off Electronic Stability and Protection has been disabled on the SYSTEM SETUP 2 page ESP FAIL ESP is inoperative The ESP function has failed and is inoperative The system should be serviced ESP DEGRADE ESP IAS mode is inoperative IAS mode of ESP is inoperative The system should be serviced ESP CONFIG ES
159. red settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 sanpa20Jg Buruuejd AEN 5649 24V oipny uddx svoli sjuaum su paezey nubi Wil jeuonippy uoneiedo Jeuuouqy ic Eu x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN Message Comments MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The
160. rm of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication if the air or on the ground Go to FlyGarmin com and select Aviation Data Error Report NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft NOTE The pilot operator must have access to Garmin and Jeppesen database alerts and consider their impact on the intended aircraft operation The database alerts can be viewed at www flygarmin com by selecting Aviation Database Alerts 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A Wamings Cautions amp Notes GARMIN NOTE The pilot operator must review and be familiar with Garmin s database exclusion list as discussed in SAIB CE 14 04 to determine what data may be incomplete The database exclusion list can be viewed at www flygarmin com by selecting Database Exclusions List NOTE The FAA has asked Garmin to remind pilots who fly with Garmin database dependent avionics of the following t is the pilot s responsibility to remain familiar with all FAA regulatory and advisory guidance and info
161. rmal Annun Flight Instruments EICAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint For flight plan leg planning a b o d Press the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM
162. rmation related to the use of databases in the National Airspace System Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements DQRs by virtue of a Type 2 Letter of Authorization LOA from the FAA A copy of the Type 2 LOA is available for each database and can be viewed at http fly garmin com by selecting Type 2 LOA Status Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance but does not constitute authorization to fly any and all terminal procedures that may be presented by the system It is the pilot s responsibility to operate in accordance with established AFM S and regulatory guidance or limitations as applicable to the pilot the aircraft and installed equipment NOTE If the pilot operator wants or needs to adjust the database contact Garmin Product Support to coordinate the revised DQRs NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to FlyGarmin com and select Report An Aviation Data Error Report Garmin G1000
163. rport Directory Scheduler ae Pilot Profiles edet eedem t be b ta bat n d d Electronic Stability Protection ESP SiriusXM Satellite Radio Electronic Checklists rettet cete e mte Abnormal Operation Reversionary Mode Abnormal COM Operation Audio Panel Fail safe Operation Hazard Displays with Loss of GPS Position 90 Unusual Attitudes Dead Reckoning sssssseeeeennnn nennen Suspected Autopilot Malfunction sssssss 92 Overpowering Autopilot Servos ssssssee nnn 93 Annunciations amp Alerts CAS Messads ain ie diat m a PB RE HE Ge Comparator Annunciations Reversionary Sensor Annunciations AFCS Alerts Terrain SVS Alerts Terrain SVS System Status Annunciations TAWS B Alerts es Message Advisory Alerts Aural Alerts coda brad amr o E UTER Ge a DE Flight Plan Import Export Messages Pilot Profile Import Export Messages MFD amp PFD Message Advisories ssssssssene Database Message Advisories GMA 350 Message Advisories GIA 63W Message Advisories ssssssssseen 1 GEA 71 Message Advisories 4 GTX 33 33D ES Message Advisories ssssssssse 4 GRS 77 Messa
164. rts Window on the PFD When a scheduler message is waiting the MSG Softkey flashes an Advisory Pressing the MSG Softkey opens the Alerts Window and acknowledges the scheduler message The softkey label no longer flashes after pressing the softkey Pressing the MSG Softkey again removes the Alerts Window from the display and the scheduler message is deleted from the message queue Entering a scheduler message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight the first empty scheduler message naming field 4 Usethe FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key 5 Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type 6 Turn the small FMS Knob to select the message type Event Message issued at the specified date time One time Message issued when the message timer reaches zero default setting e Periodic Message issued each time the message timer reaches zero 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 7 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx 5723 syu wnysu Tu102 AEN yw 6114 aoueplony paezey s n ze jeuonippy xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Add
165. s Appendix Alerts Operation Index Additional Features 86 6 7 8 9 A GARMIN Press the ENT Key or select the CHECK Softkey to check the selected checklist item The line item turns green and a checkmark is placed in the associated box The next line item is automatically selected for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or select the UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window and GO TO NEXT CHECKLIST is highlighted If 60 TO NEXT CHECKLIST is selected prior to checking all the checklist items CHECKLIST NOT FINISHED will be displayed in yellow text Press the ENT Key If GO TO NEXT CHECKLIST is displayed when pressing the ENT Key the next checklist in the group will be displayed If EXIT CHECKLISTS is displayed when pressing the ENT Key the system Will exit the Checklist Page Select the EXIT Softkey to exit the Checklist Page and return to the page last viewed When returning to the Checklist Page after selecting the EXIT Softkey the system will return to the last select checklist item Immediately Accessing Emergency Procedures 1 2 3 4 From any page on the MFD select the CHKLIST Softkey or turn the large FMS Knob to sele
166. s land and SUA data DCLTR 3 Removes everything except the active flight plan Sue v unuuy gt 5 3s o x x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix WX LGND TRAFFIC TOPO TERRAIN STRMSCP NEXRAD A GARMIN Displays icon and age on the Inset Map for the selected weather products optional Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map Displays terrain information on Inset Map Select to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft Displays XM NEXRAD weather and coverage on Inset Map optional or Displays Worldwide Weather precipitation on Inset Map optional Displays XM lightning information on Inset Map optional feature Displays Worldwide Weather lightning information on Inset Map optional o 9 g z m x U g E 5 m 4 E 2 m 7 z 2 o 4 2 7 o Le amp Rs1 HRs2 l 8 c vse SENSOR Select the BACK Softkey to return to the top
167. s the INHIBIT Softkey Or 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 07 AEN Sd5 S24V oipny duadx 59213 siu umn nsul u102 AEN Duruue d Wil e uepioAy s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key AIRBORNE COLOR WEATHER RADAR WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea 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 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Press the MODE Softkey If the aircraft is on the ground press the STANDBY Softkey to initiate the one min
168. small FMS Knob to select the TAWS B Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 1007 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS B alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key Enable TAWS While the TAWS B Page is displayed pres
169. t Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN Message Comments DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database installed Install correct obstacle database in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 350 MESSAGE ADVISORIES Message Comments GMA1 CONFIG GMAT config error Config service req d GMAT FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The G1000 system should be servi
170. t plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or Update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as ne
171. t the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 With the XM Radio Page displayed press the VOL Softkey 2 Press the VOL Softkey to reduce volume or press the VOL Softkey to increase volume Once the VOL Softkey is pressed the volume can also be adjusted using the small FMS Knob Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Radio volume may also be adjusted at each passenger station 3 Press the MUTE Softkey to mute the audio Press the MUTE Softkey again to unmute the audio Mute SiriusXM audio 1 Select the XM Radio Page 2 Press the MUTE Softkey to mute the audio Press the MUTE softkey again to unmute the audio ELECTRONIC CHECKLISTS The system accesses the checklists from an SD card inser
172. ta e g coastlines HE terrain rivers lakes and elevation scale on ES Navigation Map TERRAIN Displays terrain information on Navigation Map uoneiedo Jeuuouqy AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature Sue v unuuy gt 5 o a x x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN NEXRAD Displays XM NEXRAD weather and coverage on Inset Map optional or Or Displays Worldwide Weather precipitation on Inset Map PRECIP optional XMLING Displays XM lightning information on Inset Map optional feature or Displays Worldwide Weather lightning information on DLLING Inset Map optional METAR Displays METAR flags on airport symbols shown on the Navigation Map optional LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected BACK Returns to top level softkeys DCLIR 3 Selects desired am
173. ta is shown at the right us 8m CN 12m 3000FT WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right CYCLONE WARNING The age of the displayed data is shown at the right AIREP The age of the displayed data is shown at the right 21000FT PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow TURBULENCE The age of the displayed data is shown at the right The altitude selection is shown at the bottom 4m 6000FT ICING POTENTIAL The age of the displayed data is shown at the right The altitude selection is shown at the bottom CONNEXT WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions 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 190 0184
174. te or deactivate the WATCH feature press the WATCH Softkey This feature is only available in the Horizontal Scan Mode 70 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance Weather Alert To activate or deactivate Weather Alert press the WX ALRT Softkey Activating and deactivating also enables or inhibits the alert on the PFD sjuauimnasu sub 5721 Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode olpny uqax U105 AEN 52 Buruuejd ARN Sd5 Wil SeJnpa20Jd gt 4 S a m 5 fal o Sue v uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 01842 00 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Hazard Avoidance Ssjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld 1i Blank Page 6 2 4 eouepioAy 2 s m d Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 72 GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational aware ness only and may
175. ted into the card slot If the SD card contains an invalid checklist file or no checklist the Power up Page messages display Checklist File Invalid or Checklist File N A not available and the CHKLIST Softkey is not available The following colors are used for checklist items e Cyan Items not selected or checked Yellow Caution notes White Item is selected Red Warning notes Green Item has been checked Gray General notes Accessing and Navigating Checklists 1 From any page on the MFD select the CHKLIST Softkey or turn the large FMS Knob to select the Checklist Page 2 Turn the large FMS Knob to select the GROUP field 3 Turn the small FMS Knob to select the desired procedure and press the ENT Key 4 Turn the large FMS Knob to select the CHECKLIST field 5 Turn the small FMS Knob to select the desired checklist and press the ENT Key The selected checklist item is indicated with white text surrounded by a white box 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Additional Features 85 s mp oo4d Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul Tu102 AEN UTE eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedure
176. ter setting Use only a QNH altimeter setting for height above mean sea level or the standard pressure setting as applicable CAUTION The 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 Itis 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 CAUTION The system 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 the pilot s authority to operate this device under FAA FCC regulations NOTE When using Stormscope there are several atmospheric phenomena in addition to nearby thunderstorm that can cause isolated discharge points in the strike display mode However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleaned NOTE Do not rely 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 All visual depictions contained within this document including screen images of the panel and
177. the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN USER DEFINED HOLDING PATTERNS A holding pattern can be defined at any active flight plan waypoint or at the aircraft present position Creating a user defined hold at an active flight plan waypoint Flight Planning 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the waypoint for the
178. tion Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sepeooid uluueld AEN 549 52 oipny uadx 5721 syuoumasul uo2 AEN 2 saunyea4 yeuonippyv Sue v unuuy xipuaddy x pul iui n l Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation GARMI N CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD e Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes TAWS is also disabled A
179. titude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT TO GA Switch Go Around GA Go Around GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS FLC Key Roll Hold default ROL Flight Level Change FLC VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS NAV Key Navigation VOR Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT GPS APR Key Approach VOR Pitch Hold default PIT LOC HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director The selected navigation receiver must have a valid LOC signal before BC Key press act
180. tkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 83 x pu ddy su jy uoneiedo sainjea4 aoueplony s mp ooud buluueld AEN Sd5 S24JV olpny uqax SV2l3 sjueuimasu junuuy Jeuuouqy Jeuonippy paezey ubi wo gt AeN 3461 x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 84 A GARMIN Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page select the CHNL Softkey Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly selec
181. to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A A GARMIN Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 The
182. tures and tracks the selected NAV VOR navigation source GPS VOR LOC Key Navigation LOC Capture Track LOC No Glideslope Backcourse Capture Captures and tracks a localizer signal BC Key BC Track for backcourse approaches 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian svola sjuouinasu olpny uqax ARN Sd5 So4V suelv uoneiedo sainjea4 aoueplony 2 buluueld Junuuy jeuuouqy jeuonippy xipuaddy x pul iui nu wo gt AeN paezey Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS Lateral Mode Description Control Annunciation Approach GPS GPS Approach VOR VAPP Capture Track Captures and tracks the selected APR Ke Approach LOC navigation source GPS VOR LOC y Capture Track LOC Glideslope Mode automatically armed Commands a constant pitch angle and wings level in the air TO GA m Commands a constant pitch angle Switch Takeoff and wings level on the ground in TO preparation for takeoff ia Autopilot engages and commands IL wings level No annunciation in the AFCS Status Box The acceptable bank angle range is indicated in green along the Roll Scale of the A The Heading Navigatio
183. ty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enter the desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor TRIP PLANNING 1 Tum the large FMS Knob to select the AUX page group 2 Tum the small FMS Knob to select the first rectangular page icon 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 23 olpny uqax sv l4 sjueuinasu U105 AEN BUTLER 52 2 4 AEN 540 nubi eouepioAy paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abno
184. ucceeded is shown in the export results box Press the ENT Key to exit the Pilot Profile Exporting Box ELECTRONIC STABILITY PROTECTION ESP Electronic Stability and Protection ESP is an optional feature that is intended to discourage the exceedance of attitude and established airspeed parameters This feature will only function when the aircraft is above 200 feet AGL and the autopilot is not en gaged ESP engages when the aircraft exceeds one or more conditions pitch roll low air speed and Vmo beyond the normal flight parameters Enhanced stability for each condition is provided by applying a force to the appropriate control surface to return the aircraft to the normal flight envelope This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep at titude or high airspeed As the aircraft deviates further from the normal attitude and or airspeed the force increases up to an established maximum to encourage control movement in the di rection necessary to return to the normal attitude and or airspeed range Except in the case of high airspeed when maximum force is reached force remains constant up to the maximum engagement limit Above the maximum engagement limit forces are no longer applied There is no maximum engagement related to a high airspeed condition When ESP has been engaged for more than ten seconds cumulative not necessarily consecutive secon
185. up 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Press the available softkeys to select the desired SiriusXM Weather product 4 Press the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 AEN 640 52 olpny adX sv l4 Sjueumajsul JU05 AeN iui Duruue d Wil aoueploay s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Map Panning Information Weather Data Link Page 1 2 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display
186. ute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne press the WEATHER Softkey Or If the aircraft is already airborne press the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired press the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Monitor the displayed tilt value in the TILT feld When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 68 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 01842 00 Rev A GARMIN Hazard avoidance 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Bearing Line
187. uuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Weather Request Description Status Message No GFDS Subscription 1 The system is not be currently subscribed to GFDS or the access code is incorrect Verify the access code Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 011 913 440 1135 for assistance Reduce Request Area The GFDS weather data request area exceeds size limits Reduce weather coverage area and re send data request Request Cancelled The user has cancelled a GFDS weather data request Requested area too large Reduce coverage area The size of the GFDS weather data request has exceeded limits Reduce the size of the coverage area and try the weather data request again Request Failed Try Again The weather data request timed out Re send data request Transfer Preempted The data link is busy Retry request later Cancelling a Connext Weather Data Request in Progress 1 2 3 4 Select the Connext Weather Data Link Page Press the MENU Key With GFDS Data Request highlighted press the ENT Key Turn the large FMS Knob to select CANCEL REQ and press the ENT Key The request status box indicates
188. vate Direct to Navigation using the PFD 1 Press the Direct to Key E on the PFD or controller 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob counterclockwise to place the cursor over the ALT altitude field 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu Yid 5721 oipny uddx UI0JNeN ACN 540 S24V Suelv uoneiedo sainjea4 aoueplony 2 buluueld unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in
189. y Jeuonippy paezey ubi wo gt AeN ubiu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when f
190. y SoJnpa204d Duruue d AEN 540 S24V olpny uqax 7213 Sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN Message Comments MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SCHEDULER f message Message criteria entered by the user SVT SVT DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVT SVT DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD 1 RE
191. y active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 13 Press the ENT Key 12 190 01842 00 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian suey uonejedo so1mea4 e ueptony Buluueld AEN SdD 52 olpny yqax svoli Sjuoumasu unuuy jJeuuouqv Jeuonippy paezey yu 0105 AEN 4613 xipuaddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the go around button TEMPERATURE COMPENSATED ALTITUDE When temperature compensated altitude is enabled for the loaded approach the altitudes associated with t

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