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Garmin Software Version 0720.12 Cockpit Reference Guide

1. 28 Import a Flight Plan from an SD Card 29 Insert a Waypoint in the Active Flight Plan 29 Enter an Airway in a Flight Plan 30 Invert An Active Flight Plan 31 Remove a Departure Arrival Approach or Airway from a Flight Plan 31 Store a Flight Plan nennen 32 Edit a Stored Flight Plan 32 Delete a Waypoint from the Flight Plan sss 32 Invert and Activate a Stored Flight Plan 33 Copy a Flight Plan nnn Delete a Flight Graphical Flight Plan 5 Export a Flight Plan to an SD Card PROCEDURES LAL a a D R a d Load and Activate a Departure Procedure Activate A Departure Leg sss Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure 36 Activate An Approach in the Active Flight Plan 37 Activate a Vector to Final Approach Fix sss 37 Activate A Missed Approach in the Active Flight Plan 38 HAZARD AVOIDANCE nnn 39 Customizing the Hazard Displays on the Navigation 39 STORMSCOPE Optional 39 XM W
2. AEN 540 52 oipny uadx Svo syuoumasul U105 AeN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul iui TL Nav Com XPDR Audio Hazard Avoidance Additional Annun Flight Instruments Flight Planning EICAS AFCS Alerts Features Procedures GPS Nav Appendix 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 Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes TAWS is also disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 60 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Amnunciations amp Alerts ANNUNCIATIONS amp ALERTS CAS MESSAGES If t
3. Advisory Messages Advisory Messages ALTERNATOR 0 Alternator is off a Propeller is operating in Beta mode Door is ajar aircraft is on the ground MEYL Emergency bleed is on M ZMU Hr oreller is feathered UR FUEL PUMP ON 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 CaN aA Olam Generator is off Engine ignition is on MH oen system has been turned on aircraft is on the ground Mrd ica Starter engaged when Ng is less than 56 SUDA SEU 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 example Description 62 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Alerts COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is 5 200 ft f both airspeed sensors detect 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts Difference in heading sensors is gt 6 degrees Difference in pitch sensors is gt
4. 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 departure time DEP TIME field Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN FlightPlamning 6 1 8 9 10 11 12 13 NOTE The departure time on the Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Enter the departure time Press t
5. 12 13 14 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 25 oipny uddx sv l4 sjueuinasu U105 AEN 3461 52 s mp oold Duiuue d AEN Sd5 fila uonesado 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 15 16 A GARMIN Press the ENT Key Press the FMS Knob to remove the flashing cursor CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 26 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit 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 WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the
6. 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 upper 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 Turn a CRS Knob to select the desired course to from the waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOVVN 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
7. 3 Flight Director Activation 7 3 Vertical Modes asia eara a E EE och 4 Lateral Modes sse 5 7 Direct to Navigation 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight Plan 9 Vertical Navigation VNAV ssssseseeennnnnnnnnnn 9 FLIGHT PLANNING UL A ttt citi 21 Weight amp Fuel 7 5 21 e o Rn t 0000000 21 Create a New User Waypoint Defined by Latitude amp Longitude 23 Create a New User Waypoint Defined by Radials from Other Waypoints 24 Create a New User Waypoint Defined by a Radial amp Distance from Another Waypolnt rrr to eo ne et banda a etit ata 26 i 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian TbleofComtens GARMIN Delete a User 1 4 5 2 Create a New Flight Plan 5 6
8. 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 Config service req d MANIFEST GEA1 software mismatch communication halted The GEA2 configuration settings do not match those of backup configuration memory The G1000 system should be serviced The 1 GEA 71 has incorrect software installed The G1000 system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The G1000 system should be serviced 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 7 so1njeoJ 2 AEN Sd 24V oipny uadx svoli syu unysu paezey ESTE Wil jeuonippy uoneiedo Jeuuouqy EY 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 GTX 33 MESSAGE ADVISORIES A GARMIN Message Comments XPDR1 CONFIG XPDR1 config error Config service req d XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G10
9. Index Appendix Eres Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message transfer key is stuck COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote Comments 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 with other NAVS LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach 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 h
10. 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 B DISPLAY IF EQUIPPED 44 WARNING The TAWS B display shows supplemental information 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 B operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Hazara avoidance Display Terrain on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 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 3
11. iH Blue Tex Approach KDFH RNAV 17LGPs LPY RIVET iaf 253 18 8NH Small Light 176 3 3NM 2000FT Blue Tex INWOD 176 3 2NM S m t MENOL faf 176 3 9NM RW17L 176 5 3NM x p d Small White Text 99 FT 174 8NH with Altitude POLKE Restriction Bar SIUE Cross AT or ABOVE 5000 fi Facing Cross AT 2 300 ft ICI Cross AT or BELOW 3 000 ft Altitudes associated with approach procedures are auto designated This means the system will automatically use the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 19 siu uinnsul UATE 5721 oipny uadx 0105 AEN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS Procedures Appendix Alerts Operation Features Index GPS Navigation GARMIN Altitudes associated with arrival procedures are manually designated This means the system will not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated b
12. 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu iui S24V oipny uadx 5721 U10 AEN xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 Tunuuy Jeuuouqy Je
13. WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Fight Planning b Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Tum the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints
14. 190 00764 02 Rev A A GARMIN GMC 710 MESSAGE ADVISORIES Annunciations amp Alerts Message GMC CONFIG GMC Config error Config service req d Comments 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 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 MISCELLANEOUS MESSAGE ADVI SORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight p
15. 5 degrees Difference in roll sensors is gt 6 degrees Vem eee No data from one or both altitude sensors Nm eee am No data from one or both airspeed sensors No data from one or both heading sensors Ji Ee ME No data from one or both pitch sensors H Oe No data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Condition Sensor Window Text f Both PFDs are displaying data from the n e mber one Air Data Computer f Both PFDs are displaying data from the n E mber two Air Data Computer f rom the number one Attitude amp Heading Reference Both PFDs are displaying data e Both PFDs are displaying data from the number two Attitude amp Heading Reference Both PFDs are displaying data from the number one GPS receiver f rom the number two GPS receiver Both PFDs are displaying data f PFD2 is displaying data from the 1 Air Data Computer f PFD1 is displaying data from the 2 A Air Data Computer PFD2 is displaying data from the 1 AHRS F A G G i E is displayi rom the 2 PFD2 is displaying data g data rom the rom the 2 PFD
16. 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 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 GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced 74 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message Comments GIA1 SERVICE G A1 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 HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be service
17. 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 02 Rev A GARMIN 5 the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 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 activates the first leg of the approach 1
18. a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 30 1 2 3 4 5 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 If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and 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 menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Garmin G1000
19. 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure Settings 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 Enable Disable OBS Mode While Navigating with GPS 2 aaa De RD HU Rm dU ded in de ide 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 Code sees 9 Selecting a COM 9 Selecting a NAV Radio s s nennen 9 NAV COM Tuning ein ee en Re i rl ren Gr RR v Hr HR Hr 0 Digital Clearance Recorder and Player 0 Intercom System ICS Isolation sssssen 1 AUTOMATIC FLIGHT CONTROL 5
20. Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Flight Planning 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 PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the 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 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected
21. 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 of available arrivals 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 35 sjuaumasu Yid 5721 olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 unuuy jeuuouqy
22. Fuel Temperature E Temperature i l G Propeller Speed Cabin Pressure Altitude 3 Generator and and Change Rate Alternator Current Generator Speed Differential Pressure Emergency Bus g Voltages 2 G Oil Pressure Fuel Quantity Vacuum 190 00764 02 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 wh
23. Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved 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 KJ Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 39 AEN 540 S24V oipny duadx 59
24. SD card was successfully imported as a stored flight plan modified File contained user waypoints only User waypoints imported success fully No stored flight plan data was No flight plan files found to import The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified The SD card contains no flight plan data Flight plan import failed Flight plan data was not success 4 ully imported from the 50 card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system 190 00764 02 Rev A Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 67 so1njeoJ 2 AEN Sd 2 oipny uadx svoli sjuaum su paezey nubi Wil jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Appendix Index Annunciations amp Alerts A GARMIN Flight Plan Import Export Results File contained user waypoints only Description The file stored on the SD card did not c
25. active database Press the ENT Key to acknowledge the startup screen NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system display ing a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Appendix 9 If necessary press the SYNC DBS Softkey to enable database synchronization A confirmation box is displayed If Database Synchronization has been enabled prior to this step proceed to step 11 10 With YES highlighted press the ENT Key 11 The new database is copied to the SD card in bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed 12 Turn system power OFF 13 Remove the SD card from the top card slot of the MFD 14 Turn system power ON 15 Press the ENT Key to acknowledge the startup screen 16 Turn the large FMS Knob to select the AUX Page group on the MFD 17 Turn the small FMS Knob to select the System Status Page 18 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify
26. 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 Sector 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 readiust 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 02 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 Weather Alert To activate or deactivate Weather Alert select the WX ALRT Soft
27. and the copilot headset directly to the COM2 transceiver Audio is not available on the speakers In addition the following functions are no longer available NAV ILS audio speaker cockpit cockpit passengers intercom aural warning alerts on headset entertainment inputs and digital recording radio 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 37 uep ony s np 01d Buruue d AEN Sd5 52 oipny uadx 59213 5149 11 15 puezey ubi U10 AEN 3461 soJnjeoJ Jeuonippy xipueddy Suelv junuuy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EICAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established Loss of Hazard Functions with Loss of GPS Position UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glidepath e AFCS Annunciations 9 PFD Setup Menu and Vertical Deviation Flight
28. c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor 11 DELETE A USER WAYPOINT 1 Tum the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 21 sjuauimasu sub 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi 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 5 6 7 A GARMIN 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 high
29. kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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 e gt 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 oipny uadx 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 OF
30. procedure or airway 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuaumasu yp 5729 olpny uqax U105 AEN 52 2 4 AEN 540 nubi sual uonesado saunyea4 aoueplony 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 STORE A FLIGHT PLAN 1 2 3 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 7 Press the FPL Key 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 32 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate
31. slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored t is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 9
32. the correct standby navigation database cycle information is shown for each display NOTE After the navigation database is loaded or copied the top SD card may be removed Canceling Database Synchronization 1 Tum the large FMS Knob to select the AUX Page group on the MFD 2 Turn the small FMS Knob to select the System Status Page 3 Press the SYNC DBS Softkey if needed to disable automatic database synchronization 4 Acknowledge the cancellation by pressing the ENT Key The SYNC DBS Softkey on the AUX System Status Page allows enabling and disabling the automatic database synchronization feature If the SYNC DBS Softkey is pressed while a database synchronization is in progress the current synchronization process will be canceled 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 99 s m eouepioAy SoJnpa20Jd Duruue d AEN Sd5 24JV olpny uqax 59213 sjuaumasu jeuonippy 2 Wil JUI0 NEN uoneiedo Jeuuouqy Sue v unuuy pune GARMIN Appendix Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey s m d jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 100 A GARMIN A Activate a flight plan 18 Active Channel 55 Active database 97 A
33. 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 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 select the INVERT Softkey Invert and activate stored flight plan is displayed Flight Planning 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press th
34. 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 Turn the small FMS 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 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 TFR displays TFR specific information 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian xipueddy Suelv uoneiedo sainjea4 uep ony s mp ooud buluueld AEN Sd5
35. to 29 92 in Hg 1013 hPa Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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 ON Selects Mode A transponder replies to interrogations 5 ALT Selects Mode C Altitude Reporting Mode x transponder replies to identification and Hd altitude interrogations 8 TE uoneiedo Jeuuouqy Sue unuuy gt s o 5 m E x pul 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 33 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 VFR 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 re
36. x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix poesi Annunciations amp Alerts A GARMIN 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 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 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure that the data card
37. 0 system should be serviced 78 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations 8 Alerts GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 GPS AHRS1 using backup GPS source Comments The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible 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 receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS1 GPS AHRST not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating exclusive
38. 00 system should be serviced The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced The transponder has incorrect software installed The G1000 system should be serviced GTX 33 MESSAGE ADVISORIES CONT Message Comments XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL 1 is There is no communication with the 1 GRS 77 MESSAGE ADVISORIES inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder 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 G100
39. 1 is displaying data 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 63 s mip q e2ueproAy 2 buluueld AEN Sd5 241V oipny uddx sv l3 siu u nnsul puezey ubi UI05 AEN 3461 jeuonippy uoneiedo jeuuouqv 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 AFCS ALERTS Condition Annunciation Description Pitch Failure PT CHI Pitch axis control failure Roll Failure ROLL Roll axis control failure Pitch Trim Axis If annunciated when AP is engaged a failure has occurred in Control Failure 2 RM the pitch trim system Yaw Damper Se Failure YAW YD control failure AP also inoperative System Failure AP and MET are unavailable FD may still be available Yaw Damper Failure YD control failure Elevator Mistrim Up A condition has developed causing th provide a sustained force in the nose e pitch servo to up direction Elevator Mistrim Down A condition has developed causing th provide a sustained force in the nose e pitch servo to down direction SSEERBEE Aileron Mistrim A condition has developed causing the roll servo to provide Left a sustained left force Aileron Mistrim A condition has developed caus
40. 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 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMI N Record of Revisions 190 00764 00 RevA Initial release 190 00764 01 RevA Added Synthetic Vision System and GDU 9 05 190 00764 02 Added temporary user waypoints Added import export flight plans Added CDI availability during Dead Reckoning mode Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Added GDU 10 01 m Date of Revision Affected Pages December 2010 Production release 190 00764 02 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 02 Rev A GARMIN table of contents FLIGHT INSTRUMENTS nacio it a 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29
41. 2 Press the ENT Key 10 APPROACH IN THE ACTIVE PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 37 sjuaumasu Yid 5721 oipny uddx UI0JNeN 52 AEN 540 buluueld nf s mp old uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 38 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation
42. 213 siu umn sul u102 AEN nubi buluueld nu5iu aoueploay s mp oold paezey Sue v uoneiedo SaJnjeoJ Junuuy jeuuouqy 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 40 5 6 1 8 9 A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 1 2 Press the MENU Key with the Navigation Map Page displayed 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 Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page Select t
43. 3 Selectthe TE ST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert 190 00764 02 Rev A TAS System Test Fail is heard Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 43 xipueddy suelv uoneiedo sainjea4 aueploAy SoJnpa204d Duruue d AEN Sd5 24JV olpny uqax sY213 sjuauimasu Tunuuy Jeuuouqy jeuonippy paezeH Yi U10 AEN iui 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 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
44. 40 52 suey uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 1 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 tum 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 highlight
45. 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check fly garmin com for the current database View Airport Directory Information 54 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Additional Features XM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of t
46. 52 olpny uqax sY213 sjuauimasu Tunuuy Jeuuouqy jeuonippy p EzeH Yi U10 AEN nubi x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Hazard Avoidance Procedures Alerts Operation Features Appendix Index A Hazard Avoidance GARMIN Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cyclone Warnings AIREPs PP Cell Movement City Forecast Icing Potential Freezing Levels l Turbulence PIREPS XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETs AIRMETs Winds Aloft TRAFFIC SYSTEMS NI 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 Softkey 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 cr
47. 60 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 1007 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active vvaypoint in a GPS SBAS 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 Inhibit TAWS B 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 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 AEN 540 S24V oipny uadx svo siu umnsul Tuo2 AEN iui buluueld ni aoueploay s mp oold paezey sue v uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Pla
48. 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed 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 depi
49. A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian E Warnings Gintars E Notes GARMIN 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 weather 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 equipment 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 theref
50. 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 a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 1 34 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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
51. F Softkey xipueddy Suelv uoneiedo junuuy Jeuuouqy x pul 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 00764 02 Rev A A GARMIN 4045 ENGINE INDICATION amp CREW ALERTING SYSTEM 1 CABIN PRESS Xx1000 si 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 UR 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 s m e q Jeuonippy L 0 R LA FLAPS GEN ALT VOLTS uonesiado Jeuuouqy VACUUM IN HG 5 3 EICAS Display Normal Mode EIS Display Reversionary Mode O Torque 5 Oil Temperature 9 Fuel Flow spay unuuy Interturbine CAS Display 2
52. FD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The system should be serviced The MFD and PFDs have different software versions installed The system should be serviced 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 69 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uddx 7213 sjueumasu puezey 346 u102 AEN ubiu jeuonippy uoneiedo Jeuuouqy 22 EE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN 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 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 ti
53. G1000 Integrated Flight Deck Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Copyright 2007 2009 2010 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0720 12 or later for the Piper PA 46 Meridian Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 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 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 i Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 For after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and
54. ORIES A GARMIN Message ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable Comments 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 The GDC 744 has incorrect software installed The G1000 system should be serviced GCU 476 MESSAGE ADVISORIES Message GCU CNFG GCU Config error Config 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 82 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian
55. S signal or out of None TAWS Not database coverage Available area Sufficient GPS signal None None TAWS Available database coverage area entered 66 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN MESSAGE ADVISORY ALERTS Annunciations amp 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 TN MFD FAN FAIL The cooling fan for the MFD is inoperative AV FAN FAIL The cooling fan for remote avionics has failed AURAL ALERTS Aural Alert Description Airspeed airspeed 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 The Traffic Information Service TIS has issued a Traffic Advisory alert Traffic not available The aircraft is outside the Traffic Information Service TIS coverage area not available when a TAS system is installed FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Results Flight Plan Import Export Flight plan successfully imported Description A flight plan file stored on the
56. SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data EXCEEDANCE Engine exceedance data is being logged An engine exceedance log has been captured SPD KEY DISABLED The SPD key is disabled for this model aircraft The SPD Key on GMC 710 has no function in this aircraft model 190 00764 02 Rev A 87 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian so1njeoJ 2 AEN Sd S24V oipny uadx svoli siu umn sul paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy Ins Dow x pul Flight Instruments Nav Com XPDR Audio Additional Hazard Flight Planning Abnormal EICAS AFCS GPS Nav Features Avoidance Procedures Operation Appendix Index Annunciations amp Alerts Blank Page 88 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN 190 00764 02 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 Le
57. STD BARO Softkey CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure 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 02 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
58. T KEY Copilot Passenger E Pilot Hears Annunciator Annunciator Hears Hears Selected Selected Radios Radios Aural Aural Alerts Pilot 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu sub S24V olpnyyuqax svo JUI05 AEN SH lV uonesado soJnjeoJ 2 AEN Sd junuuy jeuuouqy paezey xipueddy x pul GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila sv l4 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 02 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 o
59. anning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN 6 1 8 3 10 11 Tum the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other display PFD or MFD Apply power to the system and press the ENT Key to acknowledge the startup Screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database cycle information is shown for each display NOTE After the navigation database is loaded or copied the top SD card may be removed Loading the Jeppesen Navigation Database as the Standby Navigation Database 1 2 3 4 5 6 1 8 98 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD Verify that an SD card is inserted in the bottom slot of each display Turn the system ON A prompt screen is displayed Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the
60. ard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN GMA 1347 MESSAGE ADVISORIES CONT Message GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA config error Config service req d Comments The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The MANIFEST GMA2 software G1000 system should be serviced mismatch communication halted GMA1 SERVICE GMAT needs The audio panel self test has detected a problem in service Return unit for repair the unit Certain audio functions may still be avail GMA2 SERVICE GMA2 needs able and the audio panel may still be usable The service Return unit for repair G1000 system should be serviced when possible 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 The G A1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d
61. as been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return 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 76 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck Comments The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the G1000 system should be serviced 6 51 FAIL 6 51 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message
62. atabase Power interuption during the database loading process could result in main tenance being required to reboot the system O NOTE Garmin requests that the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to FlyGarmin com and select Aviation Data Error Report In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected diaplays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled An active synchronization has been canceled using the SYNC DBS Softkey Card Full SD card does not co
63. cient available memory or the card may have been removed prematurely 68 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments 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 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced M
64. ctions 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 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian E Wamigs Cangone amp Notes GARMIN NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE 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 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
65. ctive Navigation Database 97 ADF 9 Advisory alerts 67 AHRS 78 79 80 82 83 Aircraft alerts 61 Air Data Computer 63 Airport Signs 51 52 Airways 95 Alert messages 81 ALT 44 Altimeter setting 1 58 Altitude mode 44 Altitude volume 44 Antenna stabilization 49 Antenna tilt 47 AOPA s Airport Directory 54 AP 64 Attitude amp Heading Reference System 63 Audio panel controls NAV1 NAV2 9 Barometric Altitude Minimums 3 Barometric pressure 92 Battery Voltage 5 Bearing line 47 48 C Cabin pressure altitude 5 CDI 1 2 9 85 Cell 39 40 Cell mode 40 Index Channel Presets 56 ChartView 52 53 Clearance player 10 Clearance recorder 10 Code selection softkeys 9 COM 9 10 57 D Database synchronization 99 DCLTR Softkey 52 Dead Reckoning 59 Declutter 58 89 95 Designated altitudes 19 20 Differential cabin pressure 5 Direct to 17 DME 9 DR mode 59 60 E Edit a flight plan 32 Engine display 5 F FD 64 Flight Director 13 Flight path marker 51 FliteCharts 52 53 Frequency Transfer 10 Fuel Flow 5 Pressure 5 Quantity 5 G Gain 48 Generator Speed 5 ndex 1 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 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 Proce
66. d 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 Reducing 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 COM1 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 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible COMI PTT 1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced 190 00764 02 Rev A 15 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoueplony SoJnpa204d Duruue d AEN 540 24V oipny uadx 5721 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy ii E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation
67. d Duruue d AEN Sd5 52 olpny uqax SV2l3 sjuaumasu unuuy Jeuuouqy jeuonippy paezey nuiu U105 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 Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 56 Radio volume is controlled at each passenger station Garmin G1000 C
68. 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 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 system should be serviced MFD1 DB ERR MFD1 obstacle database missing database missing PFD1 DB ERR PFD1 obstacle PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian soJnjeoJ 2 Buruuejg AEN 5649 S24V olpny uqax svoli siu umnsul paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy IBN EE
69. director Com Windows displayed in Indicators mand Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box Barometric Minimum Transponder Status Descent Altitude Box Box Extreme Pitch Indication 58 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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 ovm aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI
70. dures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts ew Appendix Index H Horizon heading 51 Horizontal scan 47 Inhibit 45 Inhibit TAVVS 45 Inset Map 89 90 ntercom isolation 11 nterturbine Temperature ITT 5 IOI 65 leppesen 53 L Lightning 39 40 90 M Map panning 41 Message advisories 69 74 76 80 82 87 MET 64 METAR 41 Minimums 67 MISCOMP 63 Mistrim 64 MKR MUTE 10 Mode 94 Mode selection softkeys 9 Multi Function Display MFD Softkeys 94 N NAV 9 10 NAV1 2 9 NAV2 2 9 ndex 2 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian A GARMIN Navigation database 19 20 68 70 73 83 84 NEXRAD 41 42 90 95 0 OBS 2 Obstacles 73 75 Oil engine Pressure 5 Temperature 5 Overspeed Protection 14 P Pathways 51 PIT 63 Propeller speed 5 R Reversionary Mode EICAS 5 6 Reversionary mode 57 ROC 65 S SafeTaxi 52 SBAS 14 36 45 59 75 76 Sector scan 48 Sensor 63 STAB 49 Standby 46 Standby Navigation Database 98 Store Flight Plan 32 Stormscope lightning data 39 40 90 Strike 39 Strike mode 40 SVS 51 86 Synchronization 96 99 Synthetic Vision System 51 190 00764 02 Rev A A GARMIN T TAF 41 TAS 43 44 78 TAWS 44 45 46 65 TAWS B 44 Terrain 44 65 73 90 95 Tilt line 47 Timer 2 83 Topographical data 90 95 Torque 5 Traffic 39 43 95 Traffic adviso
71. e Pressing the DCLTR Softkey again cycles back to the original map detail 92 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Additional Features The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal 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 AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteC
72. e radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Hazard avoidance 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 in 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 Turn 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 orleft 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 Turn 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 d
73. e Advisories GEA 71 Message Advisories GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GWX 68 Alert Messages nennen GDC 74A Message Advisories ssssssseenne GCU 476 Message Advisories GMC 710 Message Advisories s s s s s sss s s nn Miscellaneous Message Advisories ssssssss 83 APPENDIX e T 89 PFD Softkey 89 MED Softkey 5 94 Loading Updated Databases 96 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Table of Contents GARMIN Blank Page Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN Flightinstruments 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
74. e 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 4 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 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan 82 confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 33 sjuauimasu iui 5721 oipny uddx JUI0JNeN 52 2 4 AEN 540 nubi 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 A Flight Planning GARMIN GRAPHICAL FLIGHT PLAN CREATION 1 2 3 4 5 Press the FPL Key to display the
75. e 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 GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced The GMU 44 has incorrect software installed The G1000 system should be serviced 80 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN GDL 69A MESSAGE ADVISORIES Annunciations amp Alerts Message GDL69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software m
76. e map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed Appendix AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD Displays NEXRAD weather and coverage information on Navigation Map optional feature XMLING Displays XM lightning information on Navigation Map optional feature BACK 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 SUA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 95 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV olpny uqax 5213 sjuauimasu jeuonippy 2 1ubil4 Tuo2 NeN yb uoneiedo Jeuuouqy Sue v unuuy k Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EICAS AFCS GPS Nav Procedures Appendix Alerts Operation Features Index A Appendix GARMIN LOADING UPDATED DATABASES Ay CAUTION Never disconnect power to the system when loading a d
77. eather Optional sss 41 Traffic Systems esee ind niei ane t ar dts 42 Terrain Awareness amp Warning System TAWS B Display If Equipped 44 Airborne Color Weather Radar 46 ADDITIONAL FEATURES eis Synthetic Vision Terminal Procedure Charts AOPA Airport Directory XM Radio Entertainment sse ABNORMAL OPERATION 57 Reversionary Mode Abnormal COM Operation sse 57 Audio Panel Fail safe Operation sss 57 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN table of Contents Hazard Displays with Loss of GPS Position 58 Unusual Attitudes 5 5 Dead Reckoning ee idee ite e rite ie rio ie d ANNUNCIATIONS amp CAS Messages casa Comparator Annunciations sssssseee nenne Reversionary Sensor Annunciations Alerts uoce eren an te damn RU OR darent TAWS B ler m t d e ed ud s Message Advisory Alerts Aural Alerts to 00000 et Flight Plan Import Export Messages sssssennn 67 MFD amp PFD Message Advisories Database Message Advisories GMA 1347 Message Advisories GIA 63W Messag
78. ed press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 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 02 Rev A GARMIN GPS 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 ACTIVE FLIGHT PLAN 221 Large White 2277 9 Text LEMYN 220 8 0NH Large Light
79. edures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date 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 xxxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes 84 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message ARSPC NEAR Airspace near and ahead Comments 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 req
80. een flight path guidance Altitude has been etrieved from the retrieved from the navigation database navigation database or has been entered by and is provided as a the pilot and matches reference a published altitude in the navigation database 20 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN FLIGHT PLANNING WEIGHT amp FUEL PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters 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 all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cur
81. eld With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER 24 1 2 3 4 5 6 7 8 9 WAYPOINTS Turn the large FMS Knob on the Control Unit 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 WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A GARMIN ight Planning 10 The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS K
82. harts 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 3 2 Buruuejd AeN Sd5 S24V oipny uadx svola siu u nnsul Wfl Tu102 AEN 346 aoueplony paezey s n ze 4 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
83. he ENT Key vvhen finished Departure time may be entered in local or UTC time depending upon system settings The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 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 CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Ke
84. he MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 2 Select the Stormscope Page 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 02 Rev A A GARMIN 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 weather 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 Turn
85. he XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY 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 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 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 55 x pu ddy su jy uoneiedo sainjea4 aoueplony SoJnpa204
86. hlighted GPS Navigation 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MS 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 E on the PFD or controller 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob counterclockwise to place the cursor over the ALI altitude field 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimasu sub 5721 olpny uqax 0105 AEN ACN 5
87. ie Ahead Pull Up Obstacle Ahead Pull Up PULL UP Obstade Obstacle Pull Up Pull Up Caution Terrain Caution Terrain LE m E e nnl Terrain Ahead Terrain Ahead Caution Obstacle Cau tion Obstacle Obstacle Ahead Obstacle Ahead Five FweHundred Sink Rate None None 65 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian soJnjeoJ 2 AEN Sd S24V oipny uadx svoli siu umn su paezey u102 NEN jeuonippy uoneiedo Jeuuouqy is 14 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix zz Annunciations amp Alerts A GARMIN TAWS B System Status Annunciations PFD MFD Alert TAWS B Page Aural Alert Type s s Annunciation Annunciation Message rogress TANS System System Test Pass None None Test OK TAWS B System Test TAWS System Fail TAMS FAIL Failure Terrain or Obstade database unavailable or invalid TAWS System invalid software TAMS FAIL Failure configuration system audio fault MFD Terrain or Obstacle database unavailable or invalid P None None System operating with PFD Terrain or Obstacle databases TAWS Not No GPS position Available Excessively degraded GP
88. ing the roll servo to provide Right a sustained right force Rudder Mistrim A condition has developed causing the yaw servo to Left provide a sustained force Rudder Mistrim A condition has developed causing the yaw servo to provide a Right sustained force Preflight Test test the aural alert will be heard Performing preflight system test Upon completion of the Preflight system test has failed 64 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN TAWS B ALERTS Alert Type Excessive Descent Rate Warning EDR Reduced Required Terrain Clearance Warning RTC Imminent Terrain Impact Warning ITI Reduced Required Ob stade Clearance Warning ROC Imminent Obstade Impact Warning 101 Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Reduced Required Ob stade Clearance Caution ROC Imminent Obstade Impact Caution 101 Premature Descent Alert Caution PDA Altitude Callout 500 Excessive Descent Rate Caution EDR Negative Climb Rate Cau tion NCR 190 00764 02 Rev A Annunciations amp Alerts MFD Pop Up Alert Aural Message PULL UP Pull Up TERRAIN PULL UP muunI PULP PFD MFD TAWS B Page Annunciation PULL UP Terrain Terrain Pull Up Pull Up Terrain Ahead Pull Up Terrain Ahead Pull Up Obstac
89. ion on Inset Map optional feature Displays XM lightning information on Inset Map optional feature SENSOR 90 qsm ni Lanrs1 AHRS2 l 8 c mse ADCI ADC2 AHRSI 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 41 Air Data Computer Selects the 42 Air Data Computer Selects the 1 AHRS Selects the 22 AHRS Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Appendix sjuauimasu nubi r m r 4 5721 Select the BACK Softkey to return to the top level softkeys oipny uddx U105 AeN 52 NEN Sd5 Wila s mp 01d PFD Configuration Softkeys PFD Displays second level softkeys for additional PFD configurations DFLTS Resets PFD to default settings including changing units to standard aoueplony 2 saunqea4 jeuonippy SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction uoneiedo Jeuuouqy su jy unuuy HRZN HDG Displays compass heading along the Zero Pitch line gt 5 3 m x APTSIGNS Displays position markers for airports within approxi
90. is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 72 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments The PFDs and MFD have different navigation database versions or types Americas European etc installed Crossfill is off Install correct navigation database version or type in all displays DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or types Americas European etc installed Install correct standby navigation database version or type in all displays DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or types installed Install correct
91. ismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced GWX 68 ALERT MESSAGES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The G1000 system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The G1000 system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian so1njeoJ 2 Buruuejd AEN 5649 2 olpny uqax svoli siu umnsul paezey nubi u102 NEN Wil jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix bres Annunciations amp Alerts GDC 74A MESSAGE ADVIS
92. isplayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 4 AEN Sd5 S 24V oipny uddx 5213 sjuaumasu Tuo2 AEN sub Duruue d nf aoueploay s mp oold paezey Suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EICAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Adjusting Gain WARNING Changing the gain in Weather Mode will cause precipitation 48 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
93. ite Advisory information no immediate action required When a new red CAS warning message appears it flashes inversely red on white in conjunction 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 02 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Sjueunasu 3f BS BO a3 o sH ly uoneiado SoJnjeaJ eouepioAy 2 Fuluueld AEN 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
94. iteria Traffic Advisory Off Scale Traffic Symbol Description 4 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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 not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Turn 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 6 Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert 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
95. 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 GARMIN 4 5 6 1 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 36 1 2 3 4 5 6 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight
96. key Activating and deactivating will also enable or inhibit the alert on the PFD 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 49 AEN Sd5 52 oipny uddx 5219 sjuaumasu J05 AeN 364 Duruue d Wil aoueploay s mp oold paezey suelv uoneiedo s m unuuy Jeuuouqy Jeuonippy xipueddy x pul A GARMIN Hazard Avoidance Ssjueuinijsu fila svold oipny uadx U105 AEN s24v AeN Sd5 Duruue d Blank Page 6 2 4 2 saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 50 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 f
97. lank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN nearest recent user or airway waypoints Flight Planning 5 Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key 6 Repeat step numbers 4 and 5 to enter each additional flight plan waypoint 7 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 IMPORT A FLIGHT PLAN FROM AN SD CARD 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Select the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a lis
98. lans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 83 soJnjeoJ 2 Bujuuejd AEN Sd S24V oipny uadx svoli siu umnsul paezey JU05JAEN nubi jeuonippy uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Verify user modified procedures DB CHANGE Database changed Comments This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date Verify user modified procedures DB CHANGE Database changed This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date Verify user modified procedures DB CHANGE Database changed This occurs when a stored flight plan contains proc
99. le for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you December 2010 190 00764 02 Rev A Printed in the U S A amp GARMIN Warnings Cautions 5 Notes eo 60 6 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 able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obs
100. lighted press the ENT Key CREATE A NEW FLIGHT PLAN 28 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the Cursor Creating a stored flight plan 1 2 3 4 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a b
101. 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 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 02 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 02 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 f Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is hig
102. ly in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 19 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 s d oipny uadx 7213 sjueumasu puezey BITTE UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass Comments 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 softwar
103. mately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm x pul 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 21 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix WIND DME BRGI HSI FRMT BRG2 ALT UNIT STD BARO 92 OPTN I OPTN 2 OPTN3 OFF 360 HSI ARC HSI METERS IN HPA A GARMIN Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed Wind direction arrow with direction and speed Information not displayed Select to display the DME information window Cycles the Bearing 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HST in an arc format Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets barometric pressure
104. mes The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced 70 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 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
105. nning EICAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Enable TAWS B 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 46 WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page 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 Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which th
106. nnn 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 Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath GP on approach Captures and vede te lbs diae n 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 02 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
107. nobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Tum the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 11
108. ntain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Loading Garmin Database Updates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 96 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN 4X 97 Appendix 3 4 5 6 1 8 9 10 11 12 13 Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Make sure the SYNC DBS Softkey is in the enabled state Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select
109. o return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry 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 structur
110. ockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 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 PFD2 By pressing the DISPLAY BACKUP Button on the right audio panel NOTE The Piper PA 46 Meridian Pilot s Operating Handbook POH always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios AUDIO PANEL FAIL SAFE OPERATION If there is a failure of the Audio Panel a fail safe circuit connects the pilot s headset and microphone directly to the COMI transceiver
111. of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries WATCH FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc Honeywell and Bendix King are registered trademarks of Honeywell International Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fitness for a particular purpose The information is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances induding negligence shall AOPA be liab
112. ontain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way points locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have suffi
113. ore 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 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A 4 GARMIN Warnings Cautions amp Notes 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 disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of
114. orward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 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 GARMIN 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey t
115. plies 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 MFD Softkeys Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN CAS CAS V DCLTR 3 SHW CHRT CHKLIST 190 00764 02 Rev A 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 TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on th
116. plony SoJnpa204d Duiuue d AEN 540 S24V oipny uadx 5721 Sjueumasu puezey ubi 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 a Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message VNV Unavailable Excessive crosstrack error Comments 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 xxxx The position of the selected waypoint xxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint TRAFFIC FAIL Traffic device has failed The system is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU GSD 41 or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic co
117. re 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 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 13 sjuaumasu nubi 5721 oipny uadx u102 AEN ARN Sd5 52 sue v uoneiedo sainjea4 aoueplony 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey xipueddy 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 dimb 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
118. rence Guide for the Piper PA 46 Meridian SaJnjeoJ 2 buluueld AEN Sd5 S24JV olpny uqax 5213 sjueuimasu 2 Wil uio AeN 1i jeuonippy uoneiedo Jeuuouqy Dow x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Additional Abnormal Operation Index Appendix m Annunciations GARMIN Caution Messages Description Caution Messages Propeller is operating in Beta mode BV PE Cabin altitude is above 10 000 feet LU hip detect MH op cller is feathered or a failure has occurred in the feather system LE Fire detection system has failed EEUU ee filter approaching bypass and requires maintenance Feel imbalance is over 40 Ibs Hu quantity is less than 180 Ibs BOSTON Hycraulic pump is on Caution has 20 sec delay DEBIT Oxygen system has been turned on aircraft is in the air BUSA et or right pitot heat has failed Displayed as warning if both fail BOM NRO Piot heat is off MZ P opeller heat failure aircraft is on the ground BEES Failure detected in stall warning system VUE Starter engaged when Ng is more than 56 for more than 10 sec M a VR Standby attitude battery heater failure Bud Surface de ice fail ETT Vacuum is low Only affected side L R displayed in CAS message noted CAS messages display L R as an example
119. ry 43 Traffic map page 43 44 Transponder 9 93 94 V Vertical speed guidance 20 Vertical track 67 VNV 17 58 85 86 Vspeed 2 W WATCHG 49 Waypoint Selection Submenu 28 Weather Attenuated Color Highlight 49 Weather data link page 41 Weather radar 46 Wind data 92 X XM lightning 90 95 XM weather 41 190 00764 02 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 ka LEON GARMIN index Sjueuinijsu fila 5721 oipny uadx U105 AEN s24v AeN Sd5 buluueld Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay junuuy mun 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Index 4 A GARMIN Garmin International Anc 200 East 151st Street the KS 66062 112 Mila 7 mer Hose Bull opse Road sdown Business Park 2007 2009 2010 Garmin Ltd or its subsidiaries 190 00764 02 Rev A
120. sor 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 Turn the large FMS Knob to select the AUX page group 2 Turn 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian Flight Planning 21 oipny uddx Sy2l3 sjueuinasu U105 AEN ubiu 52 2 AEN 540 nubi uoneiado 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 22 4 For a b o d A GARMIN Direct to planning Select the 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
121. t of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 29 sjuauimasu sub 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 nubi sual uoneiado saunyea4 aoueplony yunuuy 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 5 A GARMIN Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or a Turn the small FMS Knob to the left Initially
122. tacle 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 74A 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 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 190 00764 02 Rev
123. terrain database version or type in all displays DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database installed Install correct obstacle database in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347 MESSAGE ADVISORIES Message Comments GMA2 FAIL GMA2 is inoperative GMA XTALK GMA crosstalk error has occurred GMAT FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced An error has occurred in transferring data between the two GMAs The G1000 system should be serviced 190 00764 02 Rev A 73 Garmin 61000 Cockpit Reference Guide for the Piper PA 46 Meridian saunqea4 2 Buruuejd AEN 5649 2 olpny uqax svoli syu unysu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy 3 EE x pul Haz
124. the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen Navigation Database as the Active Navigation Database 1 2 3 4 5 NOTE Loading the Jeppesen navigation database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or MFD to be updated label of SD card facing left Turn the system ON A prompt similar to the following is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database After the update completes the display starts in normal mode 97 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian SaJnjeoJ e uepioAy SoJnpa204d Duruue d AEN Sd5 S241V oipny uddx sY213 sjuauimasu jeuonippy 2 Juil Tuo2 NeN iui uoneiedo Jeuuouqy Sue v unuuy DR Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Pl
125. ther than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis AFCS NOTE If the 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 befo
126. uired 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 CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next 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 190 00764 02 Rev A 85 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian s m p q aoue
127. uonippy paezey nu x pul Nav Com AFCS XPDR Audio EICAS Abnormal Additional Hazard Annun Flight Instruments Flight Planning 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 02 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 COPL
128. urse angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region 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 f message Message criteria entered by the user COURSE SEL Current track will not intercept selected course The aircraft is flying away from the selected course and will not intercept CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees 86 Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 190 00764 02 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card Comments The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The
129. vel 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 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian 89 Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EICAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix TRAFFIC TOPO 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 informat
130. wo 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 Description ternator has failed Warnings Messages ternator is off ternator current is too high Warning Messages A eed over temperature CABINALT 12000 altitude above 12 000 feet ifferential cabin pressure is high MU Door is ajar aircraft is in the air ocv nn BETTE A flap system failure has occurred imbalance is over 125 Ibs 0101101 pressure is low MH Fue quantity is less than 100 lbs Bea eer Generator has failed 2351011111 Generator is off MEHRAB Generator curent is too high MELUM Hydraulic pump is on HERE ierstage turbine temperature high OILPRESSURE o or high oil pressure NGOVERSPEED generator overspeed BUNULA Low or high oil temperature BEL Left and Right Pitot Heat Fail Propeller heat failure aircraft is in the air ovo EM over or under speed Surface de ice fail vv oo is too high Bus voltage is high or low HUR in si eli heater over temperature or controller malfunction 190 00764 02 Rev A Garmin G1000 Cockpit Refe
131. y 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 pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude in the altitude of the Altitude is designated determining vertical aircraft as it passes for use in giving flight path guidance over the navigation vertical flight path point This altitude guidance Altitude is provided as a does not match the reference and is not published altitude in designated to be used navigation database or in determining vertical no published altitude flight path guidance exists Small Text Altitude is not Altitude is designated The system cannot designated to be used for use in giving vertical use this altitude in in determining vertical flight path guidance determining vertical flight path guidance Altitude has b
132. y when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 2 3 Turn the large FMS Knob on the Control Unit 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 23 190 00764 02 Rev A Garmin G1000 Cockpit Reference Guide for the Piper PA 46 Meridian sjuauimnasu nubi 5721 oipny uddx UI0JNeN 52 2 4 AEN 540 Juil sual uoneiado SoJnjeaJ 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 4 5 6 7 8 9 A GARMIN Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE fi

Garmin Software Version 0720.12 Cockpit Reference Guide

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