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Garmin Software Version 0720.05 Cockpit Reference Guide

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1. Caution Messages Description z SS EIS Hydraulic pump is on Caution has 20 sec delay Oxygen system has been turned on X Left or right pitot heat has failed Displayed as warning if both fail Pitot heat is off Failure detected in stall warning system Starter engaged when Ng is more than 56 for more X than 10 sec Standby attitude battery heater failure X Surface de ice fail XIX Vacuum is low XIX Only affected side L R displayed in CAS message noted CAS messages display L R as an example Advisory Messages Inhibits Advisory Description 2 Messages zm lala in O on Oju lt AnA OEO Alternator is off BETA Propeller is operating in Beta mode DOOR AJAR Door is ajar la 430101 EMI Emergency bleed is on FEATHER Propeller is feathered Left or right fuel pump is on Inhibited if fuel pump is on for fuel autobalance when imbalance is less than 40 Ibs FUEL TEMP Fuel temperature is low ie sve 6 22M Generator is off IGNITION ON Engine ignition is on OXYGEN Oxygen system has been turned on X Mp d ee a Starter engaged when Ng is less than 56 X STBY BAT TEST OK Standby attitude battery test pass standby attitude indicator must be off Only affected side L R displayed in CAS message noted CAS messages display L R as an
2. Inhibits HE a Warning Messages Description 529332 Fuel quantity is less than 100 Ibs Generator has failed X X 3 Generator is off X gs Generator current is too high X X x Hydraulic pump is on X nterstage turbine temperature high g Low or high oil pressure X X Gas generator overspeed R Lovv or high oil temperature Left and Right Pitot Heat Fail Propeller heat failure X Propeller over or under speed Surface de ice fail X Torque is too high 9 Bus voltage is high or low 3 Windshield heater over temperature or controller malfunction Only affected side L R displayed in CAS message noted CAS messages display L R as an example Caution Messages q Inhibits a E Caution Messages Description Ee ol xs ii Giz z Propeller is operating in Beta mode X Cabin altitude is above 10 000 feet Chip detect Xt X Propeller is feathered or a failure has occurred in the feather system Fire detection system has failed x Fuel filter approaching bypass and requires maintenance X 5 Fuel imbalance is over 40 lbs X X E Fuel quantity is less than 180 Ibs 60 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts Inhibits
3. nde odi bdo di Message Advisory Alerts Aural Alerts MFD amp PFD Message Advisories Database Message Advisories GMA 1347 Message Advisories GIA 63W Message Advisories GEA 71 Message Advisories sssssssssseeee nne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories sss GWX 68 Alert Messages GDC 74B Message Advisories GCU 476 Message Advisories GMC 710 Message Advisories Miscellaneous Message Advisories ssssssss PFD Softkey MFD Softkey Map 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Table of Contents GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 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 AL
4. iui Duruue d ni aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy 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 Displaying Traffic on the Traffic Map 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 second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY WARNING The TAWS display shows supplemental in
5. Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Oil engine Pressure 5 Temperature 5 Overspeed Protection 14 P Pathvvays 49 PIT 62 Propeller speed 5 R Reversionary Mode EICAS 5 6 Reversionary mode 55 ROC 64 S SafeTaxi 50 Sector scan 46 Sensor 62 STAB 47 Standby 44 Store Flight Plan 30 Stormscope lightning data 37 38 86 Strike 37 Strike mode 38 SVS 49 83 Synthetic Vision System 49 T TAF 39 TAS 41 42 75 TAWS 42 43 44 64 65 TAVVS B 42 Terrain 42 64 70 86 91 Tilt line 45 Timer 2 80 Topographical data 86 91 190 00764 01 Rev A A GARMIN Torque 5 Traffic 37 41 91 Traffic advisory 41 Traffic map page 41 42 Transponder 9 89 90 V Vertical speed guidance 21 Vertical track 65 VNV 17 56 82 Vspeed 2 W WAAS 72 WATCH 47 Weather Attenuated Color Highlight 47 Weather data link page 39 Weather radar 44 Wind data 88 X XM lightning 86 91 XM weather 39 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index Index 3 sainjea4 aoueplony 2 Duruue d AEN Sd5 S241V olpny uqax 59213 sjuauimasu jeuonippy 2 Wil JUI0 NEN ui uoneiedo Jeuuouqy Sue v unuuy E d GARMIN Index Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld 16i Blank Page 6 2 4 aoueplony puezey soinjeod
6. WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A amp GARMIN Warnings Cautions 5 Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD vveather data should not be used for short range weather avoidance WARNING The Garmin G1000 as installed in the Piper PA 46 Meridian 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 Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures 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 equipm
7. 34 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS 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 Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN 5 the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 8 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 currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and is immediately activated 9 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob t
8. 52 2 AEN 540 nubi uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy 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 5 6 A GARMIN Select the DELETE Softkey A Delete flight plan 22 confirmation window is displayed 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 32 1 2 3 4 5 Press the FPL Key to display the Active Flight Plan Page on the MFD 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 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 Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on To change the user waypoint name follow the procedure for modifying
9. PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists PFD2 DB ERR PFD2 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced 190 00764 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 67 saunqea4 2 AEN Sd 24V oipny uadx svoli siu umnsul paezey Wil jeuonippy uoneiedo Jeuuouqy 3 PE 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 DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2
10. Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 38 3 Turn the small FMS Knob to display the Cell Strike window 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 Stormscope 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 mo
11. 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 Radio volume is controlled at each passenger station Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A 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 in the 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 e 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 2 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 w
12. Appendix Index Flight Planning A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b o d a b o d e Enter the user vvaypoint identifier facility or city Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 28 1 2 3 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 the desired airway entry point
13. BUGTE Tu102 AEN UTE aoueplony paezey s m e q jeuonippy xipueddy Suelv uoneiedo junuuy Jeuuouqy 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 cr
14. Displaying Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 49 xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S241V olpny uqax SV2l3 sjuaumnasu unuuy Jeuuouqy jeuonippy paezey nu Vuo2 AEN iui 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 A Additional features GARMIN 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 Fli
15. Nearest Airports Flight Plan Messages Procedures Barometric Minimum Descent Altitude Box A GARMIN The PFD declutters when the aircraft enters an unusual attitude Only the primary The following information is removed from the PFD and corresponding softkeys Glideslope Glidepath and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude 190 00764 01 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 aircrafts current estimated position A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid 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 Also
16. ON Selects Mode A transponder replies to interrogations 5 ALT Selects Mode C Altitude Reporting Mode transponder replies to identification and Hd altitude interrogations 8 TE uoneiedo Jeuuouqy Sue unuuy gt s o 3 m x x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 89 Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Index Appendix GND VER CODE IDENT TMR REF NRST ALERT MFD SOFTKEY MAP Es TRAFFIC 0 7 BKSP TOPO TERRAIN 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 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 Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window optional optional ES V 1 Select the BACK Softkey on this level to return to the top softkey level optional optional optional NEXRAD XMLTNG BACK MF
17. 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 for the MFD 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 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 30 1 2 3 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 of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Flight Planning 4 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 5 Once all changes have been made press the FMS Knob to re
18. nubi jeuonippy uoneiedo Jeuuouqy 0 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix pres Annunciations amp Alerts A GARMIN 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 preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The G1000 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 G1000 system should be serviced 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 G1000 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 setti
19. of available arrivals 190 00764 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 33 sjuaumasu Yid 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000000000 GARMIN 4 5 6 7 8 9 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 FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan 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
20. A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message 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 Comments The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 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 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 G1000 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exi
21. Comments 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 XPDRT is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder 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 serviced 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 AHRS2 GPS AHRS2 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 The 2 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 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 receivi
22. DB ERR PFD2 basemap database error exists Comments 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 PFD2 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 G1000 system should be serviced 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 G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 68 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A
23. 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 84 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 00764 01 Rev A amp GARMIN APPENDIX sjuaumasu nubi PFD SOFTKEY MAP 5721 r mu m r Er m vu m r CDI NAV1 olpny uqax uo2 AEN CDI GPS a Top Level PFD Softkeys E EY 75 NE EE EN S Duruue d Wil optional optional optional A LA F WA v n SeJnpa20Jd Select the BACK or OFF Softkey to return to the top level softkeys aoueplony paezey Inset Map Softkeys saunqee4 jeuonippy 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 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHE unuuy gt 5 3 m x x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 85 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix TRAFFIC TO
24. Jeuonippy uoneiedo jeuuouqy suay junuuy mun 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index 4 Garmin International Anc 200 East 151st Street the KS 66062 112 se cae 7 mer Hose Bull opse Road sdown Business Park 2007 2009 Garmin Ltd or its subsidiaries A GARMIN 190 00764 01 Rev A
25. Up Alert nnunciation Alert Type TAWS System Test Fail TAWS Alerting is disabled No GPS position or exces Sively degraded GPS signal TAMS N A None TAWS Not Available TAWS Available will be heard when sufficient GPS Signal is re established System Test pass TAWS System Test OK 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 MFD FAN FAIL The cooling fan for the MFD is inoperative None AV FAN FAIL The cooling fan for remote avionics has failed AURAL ALERTS Aural Alert Description Airspeed airspeed 1 Airspeed has exceeded Vmo Minimums minimums The aircraft has descended below the preset minimum descent altitude or decision altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Th e Traffic Information Service TIS has issued a Traffic Advisory alert Traffic not available Th s e aircraft is outside the Traffic Information Service TIS coverage area not available when a TAS system is installed 65 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian So1nje24 eouepioAy SoJnpa20Jd Buruue d AEN Sd5 yi oipny uddx sv l3 Sjueumansu paezey nubi
26. disposal jsp WARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East 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 It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 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 All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subjec
27. 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 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page select the CHNL Softkey 2 Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Select the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 3 xipueddy suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 52 olpny uqax 5213 sjuauimasu unuuy Jeuuouqy jeuonippy paezey Vuo2 AEN iui x pul Nav Com XPDR Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 54 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
28. example 61 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian soinjeo4 9e2uepioAy s mp old Duruue d ACN 540 241V olpny uqax SV2I3 Sjueuinijsu 2 nubi uio AeN nubi euonippv uoneiedo jJeuuouqv dd PE x pul Flight EICAS Instruments Nav Com XPDR Audio Hazard Flight Features Avoidance Procedures Planning GPS Nav AFCS Additional Abnormal Operation Index Appendix Ca Annunciations amp Alerts COMPARATOR ANNUNCIATIONS A GARMIN ALT NO COMP IAS NO COMP HDG NO COMP PIT NO COMP ROLL NO COMP Comparator Window Text Condition 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 sen sors is gt 6 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors 5 gt 6 degrees o data from one or both altitude sensors o data from one or both airspeed sensors o data from one or both heading sensors o data from one or both pitch sensors o data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS DD Sensor Window Reversio Text nary C
29. 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian amp Warnings tauuens SMotes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Change Summary 190 00764 00 RevA Initial release 190 00764 01 Added Synthetic Vision System and GDU 9 05 Revision Date of Revision Affected Pages January 2009 Production release 190 00764 01 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 00764 01 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS nacio it a 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure 5 1 Synchronize CD sic s s sonu nui s s sun sudu 1 Change Navigation Sources s s s s s s s s s siss s issss n 2 E
30. operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed MANIFEST GDL software mismatch communication halted A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced The GDL 69 has incorrect software installed The G1000 system should be serviced 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 77 saunqea4 2 AEN Sd S24V olpny uqax svoli siu umnsul paezey nubi Juo ney Wil jeuonippy uoneiedo Jeuuouqy Ins E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix bres Annunciations amp Alerts GWX 68 ALERT MESSAGES A GARMIN Message GWX CONFIG GWX config error Config service req d Comments GWX 68 configuration settings do not match t
31. 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 Tum 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 activate Direct to Navigation using the PFD 1 Press the Direct to Key Z 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 to place the cursor over the ALT altitude field 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu sub 5721 olpny uqax 0105 AEN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR A
32. 1 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Code selection softkeys 9 COM 9 10 55 Crew Alerting System CAS Inhibits 59 D DCLTR Softkey 50 Dead Reckoning 57 Declutter 56 85 91 Designated altitudes 20 21 Differential cabin pressure 5 Direct to 17 DME 9 DR mode 57 58 E Edit a flight plan 30 Engine display 5 F Flight Director 13 Flight path marker 49 FliteCharts 50 51 Frequency Transfer 10 Fuel Flow 5 Pressure 5 Quantity 5 G Gain 46 Generator Speed 5 H Horizon heading 49 Horizontal scan 46 Index Index 1 sainjea4 aoueplony 2 Duruue d AEN Sd5 S241V olpny uqax 59213 sjuauimasu jeuonippy 2 Wil JUI0 NEN ui uoneiedo Jeuuouqy Sue v unuuy mk LEON Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts l Appendix index Inhibit 44 Inhibit TAWS 44 Inset Map 85 86 Intercom isolation 11 Interturbine Temperature ITT 5 IOI 64 J Jeppesen 51 L Lightning 37 38 86 M Map panning 39 Message advisories 66 71 73 77 79 83 METAR 39 Minimums 65 MISCOMP 62 MKR MUTE 10 Mode S 90 Mode selection softkeys 9 Multi Function Display MFD Softkeys 90 N NACO 51 NAV 9 10 NAV1 2 9 NAV2 2 9 Navigation database 19 21 NEXRAD 39 40 86 91 0 OBS 2 Obstacles 70 72 Index 2
33. 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 13 sjuaumasu UATE 5721 oipny uadx wio gt AeN ARN Sd5 52 sue v uoneiedo sainjea4 aoueplony 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey 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 AFCS armed to capture the altitude Selected Altitude displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn Fr Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn rpm to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed Hi nna IAS Hold in IAS or Mach while the aircraft is at FLC Key Flight Level Change dimbing descending to the Selected Mach Hold Altitude FLC M nmn VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i R Altitude Armed disp ayed in the VNAV Target Alti
34. 3 x4 n m mn m Ern tere ezn oa fersen J L JL L de L sss 1 EY V3 V3 A NUH nnn m o UM 5721 oipny uddx U105 AeN 52 AEN 540 Duruue d 1ubil4 PFD Configuration Softkeys SoJnpa20Jd PFD Displays second level softkeys for additional PFD configurations DFLTS Resets PFD to default settings including changing units to standard eouepioAy paezey SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features saunyea4 yeuonippyv PATHVVAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan uoneiedo Jeuuouqy SYN TERR Enables synthetic terrain depiction HRZN Displays compass heading along the HDG Zero Pitch line APT Displays position markers for airports SIGNS within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Suey unuuy gt 5 3 a x x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 87 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 BRG2 ALT UNIT STD BARO 88 OPTN I OPTN 2 OPTN 3 OFF METERS IN HPA A GARMIN Displays softke
35. AFCS NOTE If the attitude 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 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 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 Pitch Hold default PIT APR Key Approach VOR Glidepath GP LOC Glideslope GS 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 activates flight director
36. AN 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 MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select 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 190 00764 01 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 29 sjuauimasu sub 5721 olpny 4uqax UI0JNeN 52 2 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy 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 A GARMIN 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 MED it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK
37. ATE A FLIGHT PLAN LEG 18 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 00764 01 Rev A GARMIN Ps Navigation STOP NAVIGATING 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 2217 11 70 Large White 22U 90 220 8 0NM 9900 Large Light E k Blue Text Poprooch KDFH RNAV 17LePs LPY 18 8N Small Light 33 Blue Tex d Small Light MENOL faf 39 70 RH17 53 8 pus NOE Small White Text 990FT 0 8 with Altitude POLKE Restri
38. D Softkeys Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN CAS CAS V MAP TRAFFIC TOPO TERRAIN AIRWAYS STRMSCP NEXRAD XM LING BACK DCLTR 3 SHW CHRT CHKLIST Appendix Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alert ing System Display to warrant scrolling Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map 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 Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and S
39. G S2 is inoperative 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 A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 190 00764 01 Rev A 73 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 7219 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy IBN PE 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 GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments 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 GEA1 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 Con
40. G1000 Integrated Flight Deck Cockpit Reference Guide for the Piper PA 46 Meridian System Software 0720 05 or later A GARMIN Copyright 2007 2009 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0720 05 or later for the Piper PA 46 manual to earlier or later software versions Meridian Some differences in operation may be observed when comparing the information in this Garmin International Inc 1200 Fast 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Southampton Tel 44 0870 8 5040 9RB U K 501241 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Fax 4410870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Web Site Address www garmin com ssly provided herein no part of this manua in any storage medium Except as expre disseminated downloaded or stored written permiss manual and of commercial dis not be used wit NavData is a of L 3 Commu Honeywell an January 2009 ion of Garmin Garmin hereby grants any revision to this manual onto a hard drive o be viewed for personal use provided that such electronic or p must contain the complete te
41. GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Tum 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 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Nav Com XPDR Audio Panel INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPIT Key on either audio panel to select those isolated from hearing the Nav Com radios and music PILOT KEY COPLT KEY Copilot Passenger E Pilot Hears Annunciator Annunciator Hears Hears Selected Selected Radios Radios Aural Aural Alerts Pilo
42. If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN 4 Turn the small FMS Knob one click clockwise and select 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 Flight Planning menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position 5 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 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted 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 ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PL
43. Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 4 Select 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 Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARS or SIGMETs 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 39 AEN 640 S24V oipny uddx svn Tuo2 AEN nubi buluueld ni aoueploay s mp oold paezey Suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Alerts Operation Features Appendix Index Hazard Avoidance GARMIN information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a
44. MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version 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 GMA 1347 MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced 70 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts GMA 1347 MESSAGE ADVISORIES CONT Message MANIFEST GMA1 software mismatch communication halted o MANIFEST GMA2 software Comments The audio
45. NDER AUDIO PANEL ENTER A TRANSPONDER CODE 1 Select the XPDR Softkey to display the transponder mode selection softkeys 2 Select the CODE Softkey to display the transponder code selection softkeys for digit entry 3 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 COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu iui S24V oipny uadx 5721 wio gt AeN xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 Tunuuy Jeuuouqy Jeuonippy paezey nu x pul Nav Com AFCS XPDR Audio EICAS Abnormal Additional Hazard Annun Flight Instruments Flight Planning
46. PO TERRAIN STRMSCP NEXRAD XM LING A GARMIN 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 NEXRAD weather and coverage information on Inset Map optional feature Displays XM lightning information on Inset Map optional feature SENSOR 86 Caer Lanrs1 8Rs2 l 8 c mse ADCI ADC2 AHRS1 AHRS2 Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers Selects the 1 Air Data Computer Selects the 2 Air Data Computer Selects the 1 AHRS Selects the 2 AHRS Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A N Appendix e GARM mn 77 77 mu r sjuauimasu nubi Wn ET Tree Terr n BS n 4 a sl es AA 7 PRG2NAN Select the BACK Softkey to return to the top level softkeys BAGH GPS BAGH ADF BRGI OFF L IL TL TL L beers cc vse l FU V3 VA VA Vx v HNH 7 og l Lom om oes or l ll l pack L msc FE V3 V3 V3 V3 V3 V
47. T Loss of GPS navigation Insufficient satellites Comments Loss of GPS navigation due to insufficient satellites 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 Change HDG reference to TRUE TRUE APR True north approach Vertical guidance generated by WAAS is unavailable use LNAV only minimums 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 service Return NAV1 needs unit for repair NAV2 SERVICE service Return NAV2 needs unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FAIL G S1 is inoperative G S2 FAIL
48. T UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting 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 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian xipueddy Suelv uoneiedo sainjea4 aoueplony s mp ooud buluueld AEN Sd5 S24JV olpny uqax Sy2l junuuy Jeuuouqy Jeuonippy paezey 346 u102 AEN 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 light blue tuning box over the NAV1 standby frequency in the up
49. TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cloud Top Cell Movement City Forecast Freezing Levels Cyclone Warnings m S gm METARs Surface Analysis SIGMETs AIRMETs Winds Aloft TRAFFIC SYSTEMS WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic e If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Soltkey is displayed Ifa Traffic Advisory System TAS is configured a STANDBY OPERATE TEST and ALT MODE Softkey is displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS only not available with TIS intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale 40 Traffic Symbol Description Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Traffic Informati on Service TIS Hazard Avoidance NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is no
50. UA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax 5213 sjuauimasu jeuonippy 2 1ubil4 Tuo2 NeN 1i uoneiedo Jeuuouqy Sue v unuuy k GARMIN Appendix Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld 16i Blank Page 6 2 4 aoueplony puezey s m d jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy xe pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 92 A GARMIN A Activate a flight plan 18 Active Channel 53 ADF 9 Advisory alerts 65 AHRS 75 76 77 79 Aircraft alerts 59 Air Data Computer 62 Airport Signs 49 50 Airways 91 Alert messages 78 ALT 42 Altimeter setting 1 56 Altitude mode 42 Altitude volume 42 Antenna stabilization 47 Antenna tilt 45 Attitude amp Heading Reference System 62 Audio panel controls NAV1 NAV2 9 Barometric Altitude Minimums 3 Barometric pressure 88 Battery Voltage 5 Bearing line 45 46 C Cabin pressure altitude 5 CDI 1 2 9 81 Cell 37 38 Cell mode 38 Channel Presets 54 ChartView 50 51 Clearance player 10 Clearance recorder 10 190 00764 0
51. a user waypoint Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 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 active 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
52. an Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 00764 01 Rev A A GARMIN 4045 ENGINE INDICATION amp CREW ALERTING SYSTEM 1 CABIN PRESS 1000 zi dmn s 3 2 a TORQUE LB FT 820 LB FT 820 oFF 2 tH 10000 zs DIFF PSI E 400 3 6 FUEL QTY gt L LBS a 600 in PROP 7 RPM 2000 400 300 9 200 4 100 E a NG z RPH 65 0 Z RPM 570 570 OIL PSI buluueld nubi FFLOH PPH 275 OIL PSI 118 y FUEL TEMP C 5 12 ELECTRICAL OIL TEMP C 68 OIL TEMP 7 s 6 y AMPS Y CABIN PRESS 5 ar CREW ALERT SYSTEM VOLTS GENERATOR OFF ALTERNATOR OFF 9 31 VACUUM IN HG ALT FT 18888 DIFF PSI FUEL QTY 570 HS 57g FFLOW PPH FUEL TEMP C 2 RUDDER TRIM s m e q Jeuonippy L 0 R LA FLAPS GEN ALT VOLTS uonesiado Jeuuouqy VACUUM INHG 5 3 EICAS Display Normal Mode EIS Display Reversionary Mode O Torque 5 Oil Temperature 9 Fuel Flow spay unuuy Interturbine CAS Display 2 Fuel Temperature E Temperature i l G Propeller Speed Cabin Pressure Altitude 3 Generator and and Change Rate Alternator Current Generator Spe
53. art on ground ESI e Aircraft on ground GROUND Takeoff TOPI Aircraft in air AIR anding LOPI Alerts affected by an inhibit are not displayed while the inhibit is enabled If an alert is displayed prior to the activation of an inhibit affecting it the alert continues to be displayed normally until the condition causing the alert ceases to exist 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 If a GEA or GIA fails all CAS messages depending on sensors associated with that LRU are automatically inhibited Inhibits cannot be activated by invalid sensor data Warnings Messages Warning Messages Inhibits a Description Supsa ternator has failed X X ternator is off X ternator current is too high X X eed over temperature in altitude above 12 000 feet ifferential cabin pressure is high oor is ajar X Engine fire A flap system failure has occurred imbalance is over 125 Ibs Fuel pressure is low X X 59 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sainjea4 2 Duruue d AEN Sd5 S24JV olpny uqax sY213 sjuauimasu 2 nubi JUI05 NEN RETE jeuonippy uoneiedo Jeuuouqy il PE x pul Annunciations amp Alerts GARMIN
54. ation Data 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOVV 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 43 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian AEN Sd5 S24V oipny uadx svn Tuo2 AEN iui Duruue d ni s mp oold paezey Suelv uoneiedo s m junuuy Jewuouqy 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 Inhibit TAWS While the TAWS B Page is displayed select 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 select the INHIBIT Softkey 1 2 3 Or 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 44 WARNING Begin trans
55. ble to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic
56. ce should be serviced STRMSCP FAIL Stormscope has failed Stormscope has failed The G1000 system should be serviced 82 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message FAILED PATH A data path has failed Comments A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles SVS SVS DISABLED Out of available terrain region 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 Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS 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 SCHEDULER message Message criteria entered by the user 83 190 00764 01 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 Ins Dow x pul Flight
57. cedure s s s s 34 Activate An Approach in the Active Flight Plan 35 Activate a Vector to Final Approach Fix sss 35 Activate A Missed Approach in the Active Flight Plan 35 HAZARD AVOIDANCE tidie 37 Customizing the Hazard Displays on the Navigation 37 STORMSCOPE Optional 37 XM Weather 39 Traffic Systems nnne 40 Terrain Awareness amp Warning System TAWS Display 42 Airborne Color Weather Radar 44 ADDITIONAL FEATURES 55 trattati tnter 49 Synthetic Visloil a orien meae sans neris 49 Terminal Procedure Charts sse 50 XM Radio Entertainment ABNORMAL OPERATION Reversionary Abnormal COM Operation Hazard Displays with Loss of GPS Position 55 Unusual Attitudes eub tta ctc tct tcn br 56 TUT O 57 i Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN table of Contents ANNUNCIATIONS amp ALERTS CAS USES Ret leds d dide Comparator Annunciations ssssssseeee enn Reversionary Sensor Annunciations AFCS Alerts oue SD TAWS Alerts
58. ction Bar SIUE Cross AT or ABOVE 5 000 fi Facts Cross AT 2 300 fi inn 131 Cross AT or BELOW 3 000 ft 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian siu uinnsu fila 5721 oipny uadx 010 AEN spay uoneiedo s m SoJnpa20Jd Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nuru xipuaddy x pul Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Appendix Index GPS Navigation GARMIN 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 FAFE Note these altitudes are displayed as small light blue text 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 light blue 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
59. d force in the indicated direction Aileron Mistrim Left Elevator Mistri 2 i i i JELE Pitch servo providing sustained force in the indicated Elevator Mistri direction May indicate a failure of the pitch trim servo or T TELE trim system Pitch Trim Failure PTRM If AP engaged take control of the aircraft and disengage AP or 75 If AP disengaged move MEPT switches separately to unstick wi 517 YD control failure AP also inoperative Roll Failure Roll axis control failure AP inoperative Pitch Failure Pitch axis control failure AP inoperative System Failure FAVS OSH and MEPT are unavailable FD may still be available Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power up and Preflight Test preflight system tests as this may cause the preflight system test to fail or never to start if servos fail their power up tests Power must be cycled to the servos to remedy the situation PFT Preflight system test failed aural alert sounds at failure 190 00764 01 Rev A 63 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 aoueplony SoJnpa204d Duruue d AEN 540 S2JV oipny uadx Svol3 sjueumasu puezey ubi U105 AEN ubiu jeuonippy uoneiedo Jeuuouqy Ea x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal O
60. de 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 display Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Wenn Avoidant XM WEATHER OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove vveather data from the Navigation Map Page 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 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS
61. ducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating 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 COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR 2 remote transfer 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 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 LOI GPS integrity lost Crosscheck with other NAVS n Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian GPS integrity is insufficient for the current phase of flight 190 00764 01 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message GPS NAV LOS
62. e The system cannot use this altitude in determining vertical flight path guidance 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian siu uin su sub 5721 oipny uadx 0105 AEN suelv uoneiedo SaJnjeoJ SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy paezey nu xipueddy x pul GARMIN GPS Navigation Sjueuinijsu fila 5721 U105 AEN S2dV Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jewuouqy suay unuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 22 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 first rectangular page icon 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty 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 a
63. e identifier for each additional flight plan waypoint 8 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 Using the PFD 1 2 3 4 5 6 7 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active 27 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu iui 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com Flight EICAS Instruments XPDR Audio AFCS Flight Procedures Planning GPS Nav Hazard Features Avoidance Additional Abnormal Operation
64. eN Sd5 Duruue d Blank Page 6 2 4 2 saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 48 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 not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic 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
65. ed Differential Pressure Emergency Bus g Voltages 2 G Oil Pressure Fuel Quantity Vacuum 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EICAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A EcAS 00880 GARMIN CREW ALERTING SYSTEM CAS NOTE Refer to the Annunciations and Alerts section for specific CAS messages NOTE Refer to the Pilot s Operating Handbook POH for emergency procedures ELECTRICAL OIL TEMP C AMPS CAS Window CAS Display EZ piy GENERATOR OFF 2 9 ALTERNATOR OFF VACUUI LJ M IN HG y 0 R RUDDER TRIM L o TENT THR REF KRST Normal Mode Reversionary Mode CAS Message Displays Message Prioritization NOTE Red warning messages cannot be scrolled through and remain at the top of the CAS display The scroll bar changes to yellow if more than ten caution messages exist to be scrolled through Warning red Immediate crew awareness and action required Master Warning triggered Caution yellow Immediate crew awareness and possible future corrective action required Master Caution triggered Advisory white Advisory information no immediate action required When a new red CAS warning message appears it flashes inversely red on white in conjuncti
66. emperature PE 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 self test has detected a problem in the unit The G1000 system should be serviced 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunyea4 ARN SdD 2 oipny uadx paezey 346 u102 AEN jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix m Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message Comments 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 WAAS 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 COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Re
67. ent Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Piper PA 46 Meridian Pilot s Operating Handbook Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 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 The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian amp Warnings tauvens Notes GARMIN WARNING Lamp s inside this product may 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
68. etry invalid leg type PTK FAIL Parallel track unavailable Invalid leg type for parallel offset past IAF PTK FAIL Parallel track unavailable 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 vertical 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 Doox The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic devi
69. ezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy Ins p x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation 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 aviation 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 aviation database update Verify that the user modified procedures in stored f
70. fig 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 GTX 33 MESSAGE ADVISORIES The 2 GEA 71 has incorrect software installed The G1000 system should be serviced 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 The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced 74 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts GTX 33 MESSAGE ADVISORIES CONT Message XPDR1 SRVC XPDR1 needs service Return unit for repair
71. formation only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 42 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Hazard avoidance 3 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 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 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 below aircraft altitude Enable Disable Avi
72. ft to display a list of flight plan waypoints This list is populated only when there is an active flight plan 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 waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or 25 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu yp 5721 oipny uddx UI0JNeN 52 s mp oold Duiuue d AEN Sd5 fila uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey 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 7 8 9 10 A GARMIN 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 After pressing the ENT Key the cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key The cursor i
73. he VVPTS Softkey and verify that the starting vvaypoint 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 Or Fo a b d 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 Or For a b o d flight plan leg planning Select 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 will be 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 depart
74. hich the 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 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 BOOO0d Loss of Hazard Functions with Loss of GPS Position 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 55 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sY213 sjuaumasu 2 nf JUI05 AEN iui soinjeo4 Jeuonippy xipuaddy Suelv junuuy x pul Nav Com XPDR Audio Hazard Avoidance Additional Flight Instruments Flight Planning EICAS AFCS Procedures GPS Nav Features Annun Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES functions are displayed in these situations are disabled when the aircraft experiences unusual attitudes 56 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Extreme Pitch Indication System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References
75. hose 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 GDC 74B MESSAGE ADVISORIES Message Comments ADC1 ALT EC ADCI 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 2 airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted 78 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian The GDC 74B has incorrect software installed The G1000 system should be serviced 190 00764 01 Rev A A GARMIN GCU 476 MESSAGE ADVISORIES Annunciations amp Alerts Message GCU CNFG GCU Config error Config
76. i Wfil4 Nav Com XPDR Audio Hazard Avoidance Additional Flight Instruments Flight Planning EICAS AFCS Procedures GPS Nav Features Annun 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 Track Bug All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 58 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN ANNUNCIATIONS amp ALERTS CAS MESSAGES Display Inhibits Annunciations amp Alerts Inhibits prevent certain CAS messages from being displayed during the following conditions Engine off on ground ESDI Engine st
77. light 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 aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 80 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed aviation 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
78. ll 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 second rectangular page icon 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 23 oipny uddx Sy2l3 sjueuinasu U105 AEN ubiu 52 2 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy 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 24 4 For a b o d A GARMIN Direct to planning Select t
79. m XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain 3 WARNING Changing the gain in Weather Mode will cause precipitation 46 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 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn 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 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 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 Sec
80. mitting 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 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Hazara avoidance Or If the aircraft is already airborne select 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 5 Turn the Joystick to select the desired range 6 If desired select 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 Moni tor the displayed tilt value i
81. move the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the sma 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 desired flight plan 5 Select 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 stora ge location COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Tum the sma 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 5 Select the COPY Softkey A Copy to flight plan 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 for the MFD 2 Tum the sma 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu nubi 5721 oipny uddx UI0JNeN
82. n the TILT field 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 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 feld 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 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 Select 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 AEN Sd5 52 oipny uddx 5219 sjuaumasu J05 AeN sb buluueld Wila s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Co
83. nable Disable OBS Mode While Navigating with GPS 2 aaa De RD BR dU dad 2 Configure Vspeed Bugs Individually sss 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 Crew Alerting System CAS 6 NAV COM TRANSPONDER AUDIO PANEL 9 Enter a Transponder sss 9 Selecting a COM Radio 9 Selecting a NAV Radio s s nennen 9 NAV COM Tuning ein ee en i rl ren Gr RR 0 Digital Clearance Recorder and Player 0 Intercom System ICS Isolation sssssen 1 AUTOMATIC FLIGHT CONTROL 5 3 Flight Director Activation 7 3 Vertical Modes asia eara a E EE och 4 Lateral Modes sse 5 GPS NAVIGATION retineo teilte bd 770090 906 7 Direct to Navigation ssssssseseeenen nnne 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight Plan sssssennnn 9 Vertical Navigation VNAV cccccccssssssssssssssss
84. navigation APR Key Approach ILS Arm 1 Source GPS VOR LOC Capture Track Glideslope Mode automatically armed sauna Disengages autopilot and commands GA GA constant pitch angle and wings level Switch No annunciation 7 in the AFCS Status Box The acceptable bank angle range is indicated in green along the Ro 190 00764 01 Rev A Sca le of the Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sv l3 sjuounasu oipny uddx U105 AeN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 buluueld Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul iui TL paezey GARMIN AFCS Ssjueuinijsu fila 5721 oipny uadx U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 16 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 EE 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
85. ng any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced 190 00764 01 Rev A 75 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 AEN Sd S24V olpny uqax svoli siu umnsul paezey nubi u102 NEN Wil jeuonippy uoneiedo Jeuuouqy ud 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 GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 GPS AHRS1 not receiving backup GPS information Comments 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 versio
86. ngs do not match backup configuration memory The G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The G1000 system should be serviced 66 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the 61000 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 G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G1000 system should be serviced
87. ns 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 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 76 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations amp Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid 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
88. o highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 35 sjuauimasu Yid 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d Wil s mp old uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul GARMIN Procedures Ssjueuinijsu fila svold oipny uadx U105 AEN S2dV AeN Sd5 Duruue d Blank Page s mp oold aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 36 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 P
89. of aircraft The aircraft will penetrate the airspace within 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 Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CD for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 190 00764 01 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 7219 sjueumasu puezey 346 wio gt AeN ubiu jeuonippy uoneiedo Jeuuouqy PE 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 A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message bad geometry PTK FAIL Parallel track unavailable Comments Bad parallel track geom
90. on with the Master Warning Indicator Pressing the Master Warning Indicator acknowledges all flashing red messages extinguishing the master warning lights and stops warning message flashing Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN 00 8 EA When a new yellow caution message appears on the CAS display it appears as black text on a yellow background Pressing the Master Caution Indicator acknowledges all unacknowledged yellow messages extinguishing the master caution light The caution message is displayed as yellow text on black after it is acknowledged Messages are displayed until the issue is corrected Once acknowledged CAS warning messages are shown in red text and are displayed until the issue is corrected 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Sjueunasu 3f BS BO EI o Suelv uoneiado SoJnjeaJ eouepioAy 2 Fuluueld ARN Sd5 2 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul nubi nu GARMIN EICAS Ssjueuinijsu fila oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPO
91. ondition Both PFDs are displayin g data from then mber one Air Data Computer Both PFDs are displayin g data from the number two Air Data Computer Both PFDs are displayin System g data from the number one Attitude amp Heading Reference Both PFDs are displayin System g data from the number two Attitude amp Heading Reference Both PFDs are displayin g data from the number one GPS receiver Both PFDs are displayin g data from the number two GPS receiver PFD2 is displaying data f rom the 1 Air Data Computer PFD1 is displaying data f rom the 2 Air Data Computer PFD2 is displaying data from the 1 AHRS PFD1 is displaying data from the 42 AHRS PFD2 is displaying data from the 41 GPS PFD1 is displaying data r rom the 2 GPS Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN Annunciations amp Alerts AFCS ALERTS Alert Condition Annunciation Description Rudder Mistri Right 7 RUD Yaw servo providing sustained force in the indicated Rudder Mistrim direction Aircraft rudder retrim after substantial pitch and Left RUD power changes required Aileron Mistrim gt a Roh Roll servo providing sustaine
92. or the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Flight instruments 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey zu g 2 o 2 a 5721 TURN ALL VSPEED BUGS ON OR OFF 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 olpny uqax 0105 AEN 52 SET BAROMETRIC MINIMUM DESCENT ALTITUDE AEN Sd5 1 Select the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 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 aoueplony SoJnpa204d Duruue d puezey ubi so1njeoJ jeuonippy 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 xipueddy Suelv uoneiedo junuuy Jeuuouqy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridi
93. ossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu XM RADIO ENTERTAINMENT 52 The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Additional Features 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 Softkey 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 Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move
94. panel has incorrect software installed The G1000 system should be serviced G mismatch communication halted GMA1 SERVICE GMAT needs f sjuauimasu Yid 5721 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 service Return unit for repair u GMA2 SERVICE GMA2 needs service Return unit for repair GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIAT over The GIA1 and or GIA2 temperature is too high 57 If problem persists the 61000 system should be j GIA2 COOLING GIA2 over pri p serviced t
95. per left corner of the PFD Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue 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 Tum 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 CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 Select the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin G1000 Cockpit Reference Guide f
96. peration Index Appendix m Annunciations 8 Alerts TAWS ALERTS Alert Type Excessive Descent Rate Warning EDR Reduced Required Terrain Clearance Warning RTC Imminent Terrain Impact Warning ITI Reduced Required Ob stacle Clearance Warning ROC Imminent Obstacle Impact Warning 101 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 64 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Aural Message Pull Up PFD MFD TAWS B Page Annunciation PULL UP MFD Pop Up Alert Terrain Terrain Pull Up Pull Up Terrain Ahead Pull Up Terrain Ahead Pull Up Obstacle Ahead Pull Up Obstacle Ahead Pull Up PULL UP Obstacle Obstacle Pull Up Pull Up Caution Terrain Caution Terrain Terrain Ahead Terrain Ahead Caution Obstacle Cau tion Obstacle Obstacle Ahead Obstacle Ahead m gal None Five Hundred PULL UP PULL UP l PULL UP None Don t Sink Noe 190 00764 01 Rev A A GARMIN Annunciations amp Alerts TAWS System Status Annunciations PFD MFD MED TAWS B Page Aural Message A PEN Pop
97. 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 20 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN GPS Navigation the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance entered by the pilot Altitude is designated for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no published altitude exists White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot use this altitude in determining vertical flight path guidance Small Text Altitude is not designated to be used in determining vertical flight path guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude is designated for use in giving vertical flight path guidance Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation databas
98. ress 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 for 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 Strike is between 6 and 60 seconds old E 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 LING 2 Tum the large FMS Knob to select STRMSCP MODE 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 37 AEN 540 S24V oipny uadx svo siu umnsul Tuo2 AEN iui Duruue d nf aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio
99. s now displayed in the DIS distance field Enter the desired distance from the reference waypoint Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 2 3 4 5 6 7 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Select the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN 26 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Fight Planning Using the MFD 1 Press the FPL Key 2 Tum the small FMS Knob to display the Flight Plan Catalog Page 3 Select the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter th
100. 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 190 00764 01 Rev A 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 79 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 AEN Sd 2 olpny uqax svoli syu unysu pa
101. sssssssssssssssessssssssseessssssssneessssnssseeesasn 9 FLIGHT PLANNING nn 23 Weight amp Fuel Planning sssssseeeenennnnnnnnn 23 Trip Planrilng nro te reo e Ra are re E HUE 23 Create a New User Waypoint ssssssee nnn 25 Delete a User Waypoint ssssssseeen nnn 26 Create a New Flight Plan sss 26 Insert a Waypoint in the Active Flight Plan sss 28 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian TbleofCoens GARMIN Enter an Airway in a Flight Plan 28 Invert An Active Flight Plan 29 Remove a Departure Arrival Approach or Airway from a Flight Plan 29 Store a Flight Plan 30 Edit a Stored Flight Plan 30 Delete a Waypoint from the Flight Plan sss 30 Invert and Activate a Stored Flight 31 Copy a Flight eee eee 31 Delete a Flight Plan 31 Graphical Flight Plan 5 32 PROCEDURES a ted tic utn bed ducat 33 Load and Activate a Departure Procedure sss 33 Activate A Departure Leg ssssssseeeenennnnnennns 33 Load An Arrival Procedure 33 Activate An Arrival Leg 34 Load and or Activate an Approach Pro
102. sts The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays 190 00764 01 Rev A 69 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix ee Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Aviation database type mismatch Xtalk is off Comments The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays The PFDs and
103. t Alerts Pilot Copilot Copilot Passengers Passengers Music Music Selected Radios Selected Aural Copilot ON Radios Aural Alerts Passengers Alerts Pilot Copilot Music Passengers Music Selected Radios Aural Alerts Pilot Copilot Passengers Music Selected Radios Aural Alerts Pilot Passengers Music Selected Selected Radios Aural radios Alerts Pilot Aural Passengers Alerts Music Copilot Selected Selected Radios Radios Aural Passengers Aural Alerts Pilot Alerts Pilot Music 77 Copilot 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu sub S24V olpnyyuqax svo JUI05 AEN sualy uonesado saunqea4 uepjoay seinpe2oJd Buruuejd AEN 5649 junuuy jeuuouqy paezey xipueddy x pul GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila svold oipny uadx UI0 AeEN S2dV AeN Sd5 Duruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 12 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
104. t 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 sma 3 Select the OPERATE Softkey to begin displaying traffic OPERATING is FMS Knob to select the Traffic Map Page displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is 5 Rotate the Joystick clockwise to display a larger area or rotate counter displayed in the Traffic Mode field clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System Self Test System TAS Optional 1 Setthe range to 2 6 nm 2 Select the STANDBY Softkey 3 Selectthe TE 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test ST Softkey OK is heard If the self test fails the system reverts to Standby Mode and a voice alert 190 00764 01 Rev A TAS System Test Fail is heard Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian AEN 540 S24V oipny uddx svn
105. t to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A amp GARMIN Sing Cautions amp 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 The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features
106. teCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that 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 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 90 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Additional Features The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen
107. terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of 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 National Aeronautical Charting Office NACO 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 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 2 Buluueld AeN Sd5 S24V oipny uadx svola siu u nnsul
108. the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS 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 is 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 WAAS Mode due to the lack of satellite measurements needed to determine a position 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 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 37 s np 20ad ujuuejd AEN 540 52 oipny uadx Svo syuoumasul U105 AeN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul iu
109. tor Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A GARMIN Hazara avoidance Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select 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 activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode 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 190 00764 01 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 AEN Sd5 52 oipny uddx 5219 sjuaumasu J05 AeN sb buluueld Wila aoueploay s mp oold paezey suelv uoneiedo s m unuuy Jeuuouqy Jeuonippy xipueddy x pul GARMIN Hazard Avoidance Ssjueuinijsu fila 5721 oipny uadx U105 AEN s24v A
110. tude ALTV window Glidepath Captures and tracks the WAAS GP glidepath on approach Captoresand tede thelb diae S Glideslope aptures and tracks the ILS glideslope GS on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA Switch and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured inste ad of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle HDG Heading Select Captures and tracks Selected Heading Key HDG Navigation GPS GPS Arm Capture Track Navigation VOR Enroute Arm Captures and tracks selected navigation NAV VOR Capture Track source GPS VOR LOC Key Navigation LOC Arm Capture Track LOC No Glideslope Backcourse Arm Captures and tracks a localizer signal BC Ke BC Capture Track for backcourse approaches y Approach GPS GPS Arm Capture Track Approach VOR VAPP Arm Capture Track 1 Captures and tracks selected
111. udio 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 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 ACTIV
112. ure time DEP TIME field 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 00764 01 Rev A GARMIN ight Planning 6 7 8 9 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed field Enter a calibrated airspeed Press the ENT Key when finished CREATE A NEW USER WAYPOINT 1 2 3 4 5 6 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select 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 REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Use one of the following methods to enter the reference waypoint a Turn the small FMS Knob to the le
113. xt of this copyright notice and p tribution of this manual or any revision heret Garmin and G10009 are registered trademarks of Garmin FliteCharts and SafeTaxi are trademarks of Garmin hout the express permission of Garmin registered trademark of Jeppesen In nications and XM is a 190 00764 01 egistered trademar d Bendix King are registered trademarks of Honeywell International Inc Fax 886 permissi Rev A 102 2642 9099 may be reproduced copied transmitted for any purpose without the express on to download a single copy of this r other electronic storage medium to inted copy of this manual or revision ovided further that any unauthorized is strictly prohibited Ltd or its subsidiaries WATCH Ltd or its subsidiaries These trademarks may C Stormscope is a registered trademark of XM Satellite Radio Inc Printed in the U S A amp Warnings Cantans amp Notes GARMIN WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not a
114. ys 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 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 Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 01 Rev A A GARMIN 7 Appendix nnnnn n nnn un sjuauimasu sub XPDR1 XPDR2 STBY ON ALT GND VFR CODE IDENT BACK MSG Fr VY F3 5 HEM Select the BACK Softkey to return to the top level softkeys 5721 LT TT T Ts L s L 5 L 7 ekse T back L veo EF V3 A 3 7 HU n o n 73 n5 oipny uddx U105 AeN Select the BACK Softkey to return to the top level softkeys Transponder Softkeys o XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does 59 not reply to any interrogations

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