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Garmin Software Version 0719.09 Cockpit Reference Guide

1. Mor 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 85 soJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 4JV oipny uadx SV3 sjueuingjsu paezey yi JU0 AEN NITE jeuonippv uonejedo jeunouqy Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Ammundatons amp Alets GARMIN 86 Caution Messages Messages Comments i Fuel timer off or out of service Electric fuel pump running manual or automatic mode Battery current over 50 A while on ground E Battery off E Flow control and shut off valve shut off x valve closed Oil chip detector on if installed X E Forward baggage door open eee USGAL for gt 30 seconds B USGAL in specified tank GPU receptacle door not closed pimedana Xx Inertial separator failure X Inertial separator extended Low fuel level sensor failure for specified tank X Generator speed is more than 103 Oil temperature below 0 C or above i 104 MEM Specified pitot heat left or right on while i X engine off MEE Specified pitot heat left or right off X i Prop deice selected and not on DETTO Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A LE o EE TE GROUND L xo Lb py pepe gt lt OPE GARMIN Annunciations amp Alerts E A E Prop deice o
2. c Press the ENT Key The message symbol now indicates the message has been opened Mark All Messages As Read 1 While viewing the Inbox on the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu 2 Turn either FMS Knob to place the cursor on Mark All New Messages As Read 3 Press the ENT Key A confirmation window is displayed 4 With cursor highlighting YES press the ENT Key The message symbols now indicate all the message have been opened Bujuuejd NEN Sd5 S2V oipny uadx 1ubi 4 Wio AeN soiINpsd01d e uepioAy puezey gt a Q zi E D Delete a Message 1 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor uoneJjedo jeunouqy 2 Turn either FMS Knob to select the desired message 3 Press the DELETE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Delete Selected Message c Press the ENT Key xipueddy sue v unuuy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 19 GARMIN itional Features Add SjuauunJjsu 1ubi4 SV3 oipny dadX Wo gt AeN S21V AEN Sd5 Puruuejd E Blank Page soinpsd0ld 92UepIOAV puezey soinjeo4 Jeuohippy uoneloedo Jeuuouqy Sue v unuuy xipueddy xopu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 80 GA
3. 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Annun Appendix Alerts NJ hd Index 38 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Procedures 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 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 10 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 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to
4. ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key nnnn FPM to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed IAS Hold in KIAS or Mach Number while the Flight Level Change aircraft is climbing descending to the Mach Hold Selected Altitude VNAV a and tracks the VNAV flight VPTH VNAV Target AFCS armed to capture the altitude Altitude Armed displayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath on approach APR s Captures and tracks the ILS glideslope Glideslope on approach Commands a preprogrammed constant Takeoff pitch attitude and wings level in preparation for takeoff Disengages the autopilot and a Go Around commands a constant preprogrammed pitch attitude and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 16 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN SSF LATERAL MODES Lateral Mode Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Limits maximum
5. Flight Planning A GARMIN CREATE A FLIGHT PLAN 30 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is moditied as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the Cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page 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 dis
6. Hazard Avoidance S ua s 2 BP 2p a e LL lt x Abnormal Operation When the phone is answered the connection is established To exit the call select the HANGUP Softkey Annun Alerts Text Messaging SMS Messages may be sent to an email address or text message capable cellular telephone Message length is limited to 160 characters including the email address The text messaging user interface is mainly through the AUX TEXT MESSAGING Page Appendix Index 12 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features Viewing the Text Messaging Page SjueuinJjsu 10613 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select SATELLITE PHONE 3 If necessary press the SMS Softkey to display the AUX TEXT MESSAGING Page Message Symbol ee m eM Viewing a Text Message When Received When viewing MFD pages other than the AUX TEXT MESSAGING Page a pop up alert will be displayed when a new text message is received Press the VIEW Softkey to view the message Pressing the IGNORE Softkey will extinguish the pop up window and leave the text message unopened Pressing the IGNR ALL Softkey will extinguish the pop window and ignore all future incoming text messages Pressing the SMS Softkey will display the AUX TEXT MESSAGING Page The pop up alerts may be enabled or disabled through the Page Menu
7. b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 22 1 2 3 4 5 6 7 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint field after the desired airway entry point If this previous 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 Turn the FMS Knob to select the desi
8. ssssssssseeeeeteee tenente 117 MFD Softkey Map 123 Loading Updated Databases 125 INDEX Index 1 IV Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING m gt n Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE oipny uadx Wwo gt AeN Press the BARO Knob CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS SJV 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 buiuue d AEN Sd5 1ubi 4 SoJnpo 20Jd SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS e2uepioAy puezey 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 SoJnjeoJ Jeuonippy uonejedo Jeuuouqv SYNCHRONIZE CDI sue v unuuy 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the lar
9. 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 Turn 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 TO waypoint of the desired leg within the departure 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 Turn 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 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sue v uoneJedo S9JnjeaJ a UEPIOAY seJnpo2o0Jd Duiuue d ACN Sd5 j4V oipny uddx SV3 sjuauinajsu unuuy Jeuuouqy jeuonippy U10 AEN xipueddy xepu 1ubi 4 1ubi 4 puezey Procedures GARMIN 4 Turn the large FMS Knob to highlight the desired a
10. 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 HSI in an arc format 120 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A amp GARMIN Appendix Level 1 Level2 Level 3 Description SjueuinJdjsu 1uDij3 BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived svi distance information ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters oipny uadx U0 AEN S 1V IN Select to display the BARO setting as inches of mercury HPA Select to display the BARO setting as hectopacals AEN Sd5 STD BARO Sets altimeter setting to standard barometric pressure Duiuue d 1461 4 SoJnpo 20Jd prn nanan pnmo n 92uepioAy puezey Select the BACK Softkey to return to the top level softkeys soinjeo4 Jeuonippy Lo 2 ps ps Ws jp e Il Jes j ekse guck mse Fe VF V3 V9 V3 V3 V3 V3 V3 V3 V3 D Select the BACK Softkey to return to the top level softkeys uonejedo Jeuuouqv sue v Junuuy Transponder Softkeys gt 5 o D E xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 121 Additional Haz
11. A flight display The MFD and PFDs are not communicating crosstalk error has occurred with each other The G1000 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs The PFD and or MFD self test has detected a service Return unit for repair problem The G1000 system should be serviced MFD1 SERVICE MFD1 needs service Return unit for repair MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software The PFD and or MFD has incorrect software mismatch communication halted installed The G1000 system should be serviced MANIFEST MFD1 software mismatch communication halted PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Contig service req d MFD1 CONFIG MFD1 config The MFD configuration settings do not match error Contig service req d backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software The MFD and PFDs have different software version mismatch Xtalk is off versions installed The G1000 system should be serviced The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 95 SoJnjeoJ 92uepioAy SoJnpo20Jd Duiuue d NEN Sd5 4JV oipny uadx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv
12. ALT 54 Altimeter setting 1 82 Altitude mode 54 Altitude volume 54 Antenna stabilization 61 Antenna tilt 59 AOPA s Airport Directory 66 Attitude amp Heading Reference System 88 Audio panel controls NAV1 NAV2 12 Barometric Altitude Minimums 3 Battery Alerts 86 Current 5 Overheat warning 85 Voltage 5 Bearing line 60 61 C Cabin pressure altitude 5 Warning 85 CDI 1 2 12 112 Cell 41 42 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index Cell mode 42 Channel Presets 68 ChartView 64 65 Code selection softkeys 12 COM 12 81 D DB Mismatch 125 DCLTR Softkey 64 Dead Reckoning 83 Declutter 82 117 125 Designated altitudes 22 Differential cabin pressure 5 Warning 85 Direct to 19 DME 11 12 Door status 10 DR mode 83 84 E Edit a flight plan 34 Enable Terrain 56 57 Engine display 5 Essential bus voltage 5 F Flap position 5 Asymmetrical deflection warning 85 Flight Director 15 Flight ID 11 Flight path marker 63 FliteCharts 64 65 Frequency Transfer 12 Fuel Alerts 85 86 Flow 5 Pressure 5 Quantity 5 Index 1 sainjee4 a UEPIOAY SoJnpa20Jd Duiuue d ACN Sd5 5JV oipny uddx SV3 sjuauinajsu Jeuonippy puezey 14 Wwo gt AeN 114 uoneJjedo Jeuuouqv sue v Junuuy Paw ao Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun
13. Duiuueld AEN Sd5 S21V oipny uadx SV3 1ubi 4 U0 AeN SoJnpo 20Jd e uepioAy puezey gt a 2 c D xipueddy sue v uoneJjedo unuuy jeunouqy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 73 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Abnormal Annun EAS AFCS GPS Nav Procedures S ou 5s 2 BB 2p e LL lt x Appendix Alerts Operation Index Additional Features 14 A GARMIN Enable Disable Incoming Text Message Pop Up Alerts 1 With the AUX TEXT MESSAGING Page displayed press the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable New Message Popups or Enable New Message Popups 3 Press the ENT Key The pop up alert will not be displayed when an incoming text message is received Reply to a Text Message While viewing the text message press the REPLY Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Reply To Message c Press the ENT Key Sending a Text Message 1 2 3 4 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Message c Press the ENT Key The TEXT MESSAGE DRAFT Window is now displayed with the cursor in
14. Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 42 5 Press the ENT Key 6 Turn the large FMS Knob to place the cursor in the STRMSCP MODE field 7 Turn the small FMS Knob to display the Cell Strike window 8 Turn either FMS Knob to select Cell or Strike Press the ENT Key 9 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of t
15. Terrain Alert Type HARD ES TAWS B Page Annunciation Aura TETES Message None TAWS System TAWS Alerting is disabled TAWS INH None MFD Terrain or Obstacle database unavailable or invalid TAWS operating None with PFD Terrain or Obstacle databases TAWS B System Test Fail database unavailable or invalid invalid software configuration system audio fault 190 00708 04 Rev A Terrain or Obstacle TAWS System Failure TAWS System Failure Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 93 SoJnjeoJ 92uepioAy SoAnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuingjsu piezeH ui W0 gt AeN ui jeuonippv uonejedo jeunouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ Ammundatons amp Alets GARMIN Alert Type P iie RN TAWS B Page Annunciation sue Annunciation Message TAWS Not Excessively degraded GPS signal Out of database coverage area TAWS Not Available Sufficient GPS signal TR None TAWS received after loss Available VOICE ALERTS Voice Alert Minimums minimums The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Airspeed Airspeed Played when the indicated airspeed
16. Turn either FMS Knob to place the cursor on Disable Iridium Transmission 3 Press the ENT Key Telephone Communication The pilot or copilot can place and answer calls on the Iridium satellite network Control and monitoring of telephone functions are accomplished through the AUX TELEPHONE Page To view the Telephone Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX TELEPHONE Page 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 69 se1npa 0Jd buiuue d ACN Sd S24V oipny uadx svi s UawIN SU JU0 AeN e uepioAy puezey mul t fet et 1 n uonejedo jeunouqy sue v unuuy xipueddy Xapu 1ubi 4 1ubi 4 jeuonippy A Additional Features GARMIN Internal External ne Phone Phone p Phone is Idle Phone is ringing Flight EAS Instruments Nav Com XPDR Audio Phone has a dial tone off hook or connected to another phone AFCS Phone dialed is busy GPS Nav Phone is dialing another phone Flight Planning Phone has failed Procedures Phone status not known Hazard Avoidance Phone is disabled T un 5 2 B2 0 LL lt x Phone is reserved for data transmission Abnormal Operation Annun Alerts Calling other phone or incoming call trom other phone Appendix Other phone is on hold Index Phones are connected 70 Garmin G1000 Cockpit Ref
17. f J 5A i 25 A i a L de nt vf GPH mr Ug Sra MAN au d FUEL FLOM TI us FUEL usn ES 6 LBS PULL RAEN HEC GPS Nav ELECTRICAL Flight Planning Procedures Hazard Avoidance sd Left Fuel Tank 4 Auxiliary Boost Pump 7 Right Fuel Line F Left Fuel Li Fuel Select Fuel Flow Dat 2 2 eft Fuel Line 5 uel Selector uel Flow Data 3 Fuel Pressure 6 Right Fuel Tanh Fuel Synoptics Page Annun Abnormal Appendix Alerts Operation Index 8 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Engine amp Airframe Systems Status of the fuel selector is indicated between the fuel tank symbols The mode automatic AUTO manual MAN or off no indication CAS message FUEL OFF generated is shown beneath the fuel selector symbol Left Fuel Switching Right Manual or Fuel Tank Fuel Tank Fuel Tank Unknown Fuel Selector Selected Selection Selected Tank Selection Off Fuel Selector Status If the auxiliary fuel boost pump is on the symbol is displayed in green The mode automatic AUTO or manual MAN is displayed next to the pump symbol If the boost pump is off the symbol is shown in light blue automatic mode or red manual mode Fuel Boost Pump Fuel Boost Pump Fuel Boost Pump On Off Auto Off Manual Auxiliary Boost Pump Status 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide fo
18. jy uonejedo SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 junuuy Jeuuouqy Jeuonippy piezeH jui xipueddy Xapu 1ubi 4 Flight Instruments Abnormal Additional Hazard Flight Planning Annun EAS Nav Com AFCS XPDR Audio GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 If two transponders are available press XPDR1 or XPDR2 to set the active transponder Otherwise proceed to step 3 3 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 4 Use the digit keys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC or COM2 MIC on the audio panel Receive Only Press the COM1 or COM2 on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 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 N
19. properly inserted Replace data card If problem PFD2 DB ERR PFD obstacle persists The G1000 system should be serviced database error exists MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle The obstacle database is present on another LRU database missing but is missing on the specitied LRU PFD2 DB ERR PFD2 obstacle database missing 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 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 97 SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 4JV oipny uadx SV3 sjueuinajsu paezey yi JU0 AEN i jeuonippv uoneJjedo jeunouqy xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ A Annunciations amp Alerts GARMIN DATABASE MESSAGE ADVISORIES CONT MFD1 DB ERR MFD1 airport E terrain database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 airport airport terrain database Ensure that the data card is properly inserted Replace data card It terrain database error exists problem persists The G1000 system should be PFD2 DB ERR PFD2 airport serviced terrain database error exists MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB
20. the TO field Enter the desired telephone number or email address Entry can be accomplished through the alphanumeric keys on the controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Enter the desired message using any combination of entry methods as described in step 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features 5 Press the ENT Key 6 Press the SEND Softkey to send the message immediately or press the SAVE Softkey to save the message in Outbox for sending at a later time Press the CANCEL Softkey to delete the message Sjueuinjijsu 1uDij3 svi Predefined Text Messages Time and effort can be saved in typing text messages that are used repeatedly by saving these messages asa predefined message oipny dadx Wwo gt AeN Create a Predefined Text Message 1 While viewing the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu 2 Turn either FMS Knob to select Edit Predefined Messages 3 Press the ENT Key The PREDEFINED MESSSAGES view is now displayed 4 Press
21. uonejedo jeuuouqv PFD Configuration Softkeys sue v Junuuy gt 5 D x Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 119 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description PFD SYN VIS PATHWAY SYN TERR HRZN HDG APTSIGNS DFLTS WIND OPIN I OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard 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
22. 2 nm aircraft position APR INACTV Approach is not The system notifies the pilot that the loaded active approach is not active Activate approach when required SLCT FREQ Select appropriate The system notifies the pilot to load the frequency for approach approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to approach the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable Bad parallel track geometry bad geometry PTK FAIL Parallel track unavailable invalid leg type PTK FAIL Parallel track unavailable IAF waypoint for parallel offset has been past IAF passed UNABLE V WPT Can t reach The current vertical waypoint can not be current vertical waypoint reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint Invalid leg type for parallel offset T2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT VNV Unavailable Unsupported The lateral flight plan contains a procedure leg type in flight plan turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the
23. ADCT airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed ADC2 AS EC ADC2 airspeed error error correction is unavailable correction is unavailable MANIFEST GDC1 software mismatch communication halted The GDC 74B has incorrect software installed MANIFEST GDC2 software The G1000 system should be serviced mismatch communication halted GCU 475 MESSAGE ADVISORIES GCU CNFG GCU Config error GCU 475 configuration settings do not match Config service req d those of backup configuration memory The G1000 system should be serviced l GCU FAIL GCU is inoperative A failure has been detected in the GCU 475 The GCU 475 is unavailable MANIFEST GCU software The GCU 475 has incorrect software installed mismatch communication halted The G1000 system should be serviced GCU KEYSTK GCU key name A key is stuck on the GCU 475 bezel Attempt Key is stuck to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORIES GMC CONFIG GMC Config error Error in the configuration of the GMC 710 Config service req d GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 109 SoJnjeoJ 92uepioAy SoAnpo20Jd Puruuejd AeN Sd5 S 4V oipny uadx SV3 sjueuinajsu
24. Battery Bus E Main Generator 5 Main Bus 8 Essential Bus a G oe Power 6 Emergency Switch Power Buses nit Door Electrical Synoptics Page Annun Abnormal Appendix Alerts Operation Index 6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Engine amp Airframe Systems Battery connection status to the main bus is indicated in green direction of current flow is indicated with an arrow next to the current readout If the battery is disconnected from the main bus the switch is closed Battery overheating is indicated in red with a BAT OVHT annunciation a CAS message is also generated Switch Open Switch Closed e Standby Generator Switch Status BAT Battery Overheat Indication 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Nn mr x D 3 mp n sue v uoneJjedo Ss9JnjeaJ e2uepioAy SoJnpa20Jd Duiuue d ACN Sd5 SD4V oipny uddx SV3 unuuy Jeuuouqy jeuonippy 14 UI0 AeEN xipueddy xepu Ll F et puezey A Engine amp Airframe Systems GARMIN FUEL SYSTEM Flight Instruments 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the FUEL Softkey to display the Fuel System Page CADIN PRESS z Es oc Se 88 x DIFF PSI u ALT SEL FT 1100 AFCS OxY PSI L FUEL OTY R USD 125 4l 100 ance AUTO A 75 t f
25. ERR PFD1 airport The airport terrain database is present on terrain database missing another LRU but is missing on the specified LRU PFD2 DB ERR PFD2 airport terrain database missing MFD1 DB ERR MFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 Safe Taxi Safe Taxi database Ensure the data card is database error exists properly inserted Replace data card If problem PFD2 DB ERR PFD2 Safe Taxi persists The G1000 system should be serviced database error exists MFD1 DB ERR MFD1 Chartview The MFD detected a failure in the ChartView database error exists database optional feature Ensure the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts The MFD detected a failure in the FliteCharts database error exists database optional feature Ensure the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport The MFD detected a failure in the Airport Directory Directory database error exists database Ensure the data card is properly inserted Replace data card If problem persists the system should be serviced 98 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN DATABASE MESSAGE ADVISORIES CONT Annunciations amp Alerts DB MISMATCH Navigati
26. FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window Hazard Avoidance Procedures Additional Features 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key 5 Once all changes have been made press the FMS Knob to remove the CUISOF Abnormal Operation Annun Alerts INVERT AND ACTIVATE A STORED FLIGHT PLAN Appendix 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 Index 34 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Flight Planning 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location SV3 SjueuinJjsu 1uDi 3 oipny uadx Wwo gt AeN 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 the FMS Knob to activate the cursor 4 T
27. Import a Flight Plan from an SD Card 21 Insert a Waypoint in the Active Flight Plan 31 Enter an Airway in a Flight Plan 32 Invert An Active Flight Plan 38 Remove a Departure Arrival Approach or Airway from a Flight Plan 33 Store a Flight Plan 33 Edit a Stored Flight Plan ssssssseenenn 34 Delete a Waypoint from the Flight Plan 34 Invert and Activate a Stored Flight Plan 34 Copy a Flight Plan eene 29 Delete a Flight Plan 35 Graphical Flight Plan Creation sss 35 Export a Flight Plan to an SD Card ssssssn 36 PROCEDURES 1 sse 37 Load and Activate a Departure Procedure sse 37 Activate A Departure Leg 3 Load An Arrival Procedure 37 Activate An Arrival Leg ssssssseeee ene 38 Load and or Activate an Approach Procedure 38 Activate An Approach in the Active Flight Plan 39 Activate a Vector to Final Approach Fix 39 Activate A Missed Approach in the Active Flight Plan 40 HAZARD AVOIDANCE sssssssennnn 41 Customizing the Hazard Displays on the Navigation Map 41 STORMSCOPE Optional 41 XM WX Satellite Weather Optional 43 Worldwide Weather ssssssseeeeenennnn 45 ECHELLE 53 Terrain And Obstacle Proximity sse 55 Ter
28. Index Hazard Avoidance 48 7 8 A GARMIN Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the GFDS Weather Data Link Page with the changed settings Restoring Default GFDS Weather Data Link Page Settings 1 2 3 4 5 Select the GFDS Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired detault s to restore all or for selection and press ENT Key Switching Between GFDS and XM WX Weather Sources 1 2 3 4 Turn the large FMS Knob on the MFD to select the MAP page group Turn the small FMS Knob to select the desired Weather Data Link Page Press the MENU Key Turn the large FMS Knob to select Display GFDS Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Legends for Displayed GFDS Weather Products 1 2 3 4 Select the GFDS Weather Data Link Page Select the LEGEND Softkey to display the legends for the displayed weather products Or a Press the MENU Key b Select Weather Legend and press the ENT Key Turn the FMS Knob to scroll through the legends if more are available than fit in the window To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A G
29. LLL Hazard Avoidance EMG Description Status Icons p e a CYCLONE WARNING The age of the displayed data is shown at the right AIREP The age of the displayed data is shown at the right PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow zi TURBULENCE The age of the displayed data is shown at the right The 21 oon altitude selection is shown at the bottom 213 ICING POTENTIAL The age of the displayed data is shown at the right BOO0FT The altitude selection is shown at the bottom WORLDWIDE WEATHER NOTE Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather Do not utilize Worldwide Weather information to penetrate hazardous weather Registering the System to Receive GFDS Weather When an account is established Garmin Flight Data services provides an Access Code which must be entered on the G1000 in order to complete the registration process 1 With the aircraft outside and having a clear view of the sky turn the large FMS Knob on the MFD to select the MAP page group 2 Turn the small FMS Knob to select the MAP WEATHER DATA LINK GFDS or XM Page If XM is displayed in the page title it will be necessary to change the datalink source to GFDS before continuing Refer to Viewing the Weather Data Link Page procedure to change the datalink source to GFDS prior to registration 3 If the system displays the Ga
30. MESSAGE ADVISORIES HDG FAULT AHRS1 A fault has occurred in the 1 GMU 44 magnetometer fault has occurred Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 A fault has occurred in the 2 GMU 44 magnetometer fault has occurred Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced mismatch communication halted The GMU 44 has incorrect software installed MANIFEST GMU2 software The G1000 system should be serviced GSR 56 MESSAGE ADVISORIES GSR1 FAIL GSR1 has failed A failure has been detected in the 1 GSR 56 The system should be serviced GDL 69A MESSAGE ADVISORIES GDL69 CONFIG GDL 69 config GDL 69 configuration settings do not match error Contig service req d those of backup configuration memory The G1000 system should be serviced 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 107 SoJnjeoJ 92uepioAy SoJnpo20Jd Duiuue d NEN Sd5 S 4V oipny uadx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uoneJjedo jeunouqy 1 E Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation A Annunciations amp Alerts GARMIN GDL 69A MESSAGE ADVISORIES CONT GDL69 FAIL GDL 69 has failed A failure has been detected
31. ONLY soiINpsd01d 1 Select the AUX SYSTEM STATUS Page on the MFD 2 Select the RA TEST Softkey The Radar Altitude window displays 50 feet and RA TEST is displayed to the left of the Radar Altitude window indicating a properly functioning system e2uepioAy puezey 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test SoJnjeoJ Jeuonippy DISPLAYING WIND DATA uonejedo Jeuuouqv 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey xipueddy sue v unuuy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 3 A Flight Instruments GARMIN CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI Annun Abnormal Additional Hazard Flight Nav Com Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Appendix Index 4 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Engine amp Airframe Systems ENGINE amp AIRFRAME SYSTEMS CABIN PRESS SjuauinJijsu ubi 3 x oS zz Do ceo 23 o COO S 4V L FUEL QTY R 122 US
32. Operation Features Avoidance Index Flight Planning 3 4 5 A GARMIN 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 USROO0 USROO1 USROO2 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 36 1 2 3 4 5 6 7 Insert the SD card into the top card slot on the MFD Press the FPL Key on the MFD 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 Socata TBM 850 190 00708 04 Rev A A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures
33. and Unsent text messages Saved messages that are meant to be sent later are stored as Drafts Each text message box may be viewed separately or together in any combination Show Inbox Messages 16 While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the INBOX Softkey Or a Press the MENU Key to display the Page Menu Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features b Turn either FMS Knob to place the cursor on Show Inbox Messages Sjueuinjijsu 1uDij3 c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Show Outbox Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the OUTBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Outbox Messages oipny uadx SV3 JUI0 AeN SJV c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window AEN Sd5 Show Draft Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the DRAFTS Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Draft Messages Puruuejd oE soiINpsd01d c Press the ENT Key The message box selected for viewing is indicated at t
34. commanded roll angle co Heading Select Captures and tracks Selected Heading Navigation GPS Arm Capture Track Navigation VOR Enroute Arm Captures and tracks selected navigation Capture Track source GPS VOR LOC Navigation LOC Arm Capture Track No Glideslope Backcourse Arm Captures and tracks a localizer signal BC Ke Capture Track for backcourse approaches Approach GPS Arm Capture Track Approach VOR Arm Capture Track Captures and tracks selected navigation APR Ke Approach ILS Arm Source GPS VOR LOC y Capture Track Glideslope Mode LOC automatically armed Commands a constant preprogrammed Takeoff constant pitch attitude and wings level in preparation for takeoff Disengages autopilot and commands Switch Go Around a preprogrammed constant pitch attitude and wings level i d di in the AFCS Status Box The low bank angle range is indicated in green along the Roll Scale of the Attitude Indicator 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 I SjueuinJjjsu 14614 SV3 oipny uadx U10 AeN AEN Sd5 S dV SJo V uoneJjedo SoJnjeoJ 92uepioAy s np 201d Puruuejd junuuy Jeuuouqy Jeuonippy paezey LTE xipueddy xepu GARMIN AFCS SjuauunJjsu 1ubi4 SV3 oipny dadx Wo gt AeN AEN Sd5 Puruuejd E Blank Page soinpsd0ld 92UepIOAV puezey s n e 4 jeuonippy uonelaedo Jeuuouqy Sue
35. 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 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 39 AEN Sd5 S241V oipny dadx SVJ sjueuinjsu Wi0 AeN yybi4 Puruuejd 1461 4 sue v uone1ado SoJnjeoJ a UEPIOAY SoJnpa20Jd Junuuy Jeuuouqy Jeuonippy puezey xipueddy xepu A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN Flight Instruments 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the go around button Nav Com GPS Nav AFCS XPDR Audio EAS Flight Planning 4 o E S 7 o ie A Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Appendix Index 40 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Hazard Avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn
36. in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software The GDL 69 has incorrect software installed mismatch communication halted The G1000 system should be serviced GWX 68 ALERT MESSAGES GWX CONFIG GWX contig error GWX 68 configuration settings do not match Config service req d 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 A failure has been detected in the GWX 68 The service Return unit for repair GWX 68 may still be usable MANIFEST GWX software The GWX 68 has incorrect software installed mismatch communication halted The G1000 system should be serviced WX ALERT Possible severe Possible severe weather detected within 10 weather ahead degrees of the aircraft heading at a range of 80 to 320 nm GDC 74B MESSAGE ADVISORIES ADC1 ALT EC ADC1 altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude ADC2 ALT EC ADC2 altitude error error correction is unavailable correction is unavailable 108 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A Index Appendix ue GARMIN Annunciations amp Alerts GDC 74B MESSAGE ADVISORIES CONT ADC1 AS EC
37. information on Inset Map STRMSCP Displays Stormscope weather and coverage information on the Inset Map optional NEXRAD Displays NEXRAD weather and coverage m information on Inset Map optional PRECIP Displays GFDS precipitation on Inset Map optional XM LING Displays XM WX lightning information on Inset Map optional DL LTNG Displays GFDS Worldwide Weather lightning information on Inset Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optional ENT gt o T a m X U a A o d AZ m m 2 rs i nnn n Lac Le 7 E3883 368882 1L 1L ee 988 p FX FF FA 3 93 9 94x n Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Index Appendix 118 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A amp GARMIN X Appendix Level 1 Level2 Level3 Description i SENSOR Displays softkeys for selecting the 1 and d 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer m ADC2 Selects the 2 Air Data Computer AHRSI Selects the 1 AHRS 3 3 Pg AHRS2 Selects the 2 AHRS 53 Linset L___ r 3 S A nN S ODO D n nAn DNDN D swvs borrs wwo J ome ene wsrewr Berc Atunrr sto saro 3 F3 F3 nn A S Select the BACK Softkey sg to return to the top level softkeys T s n e 2uepIony paezeH jeuonippv
38. is below a given threshold for a given aircraft configuration Note this alert may be heard under normal conditions during the landing flare Traffic Played when a Traffic Advisory TA is issued with the TIS system Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued with a TAS system TAS System Test OK Played when the TAS system passes a pilot initiated self test TAS System Test Failed Played when the TAS system fails a pilot initiated self test One o clock through Played to indicate bearing of traffic from own aircraft GTS 820 only Twelve o clock or No Bearing High Low Same Played to indicate altitude of traffic relative to own aircraft GTS 820 only Altitude if within 200 feet of own altitude or Altitude not available Less than one mile Played to indicate distance of traffic from own aircraft GTS 820 only One Mile through Ten Miles or More than ten miles 94 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES DATA LOST Pilot stored data was The pilot profile data was lost System reverts lost Recheck settings to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings it desired XTALK ERROR
39. list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key S23V oipny dadx SV3 U10 AEN AEN Sd5 vu o e D e D n a UEPIOAY puezey SoJnjeoJ Jeuonippy INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan uonejedo Jeuuouqv 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 sue v unuuy 4 Turn the small FMS Knob The Waypoint Information Window is now displayed xipueddy 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 3 Additional Hazard Avoidance Abnormal Annun Flight Instruments Nav Com XPDR Audio EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed
40. mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 26 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the MFD 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 The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desire
41. 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 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 03 92uepioAy SoJnpo 0Jd Duiuue d NEN Sd5 54V oipny uddx SV3 SjueuinJjsu 1ubi 4 SoJnjeoJ Jeuonippy sue v unuuy xipueddy Xapu 614 Wi0 gt AeN puezey Abnormal Operation GARMI N Flight Instruments EAS CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Nav Com XPDR Audio Dead Reckoning Indications AFCS 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 DTK GPS Bearing Pointer Wind d
42. 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 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 125 sue v junuuy xopu xipueddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix _ GARMIN Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted System timed out prior to the database transfer completing Loading Garmin Database Updates 1 2 3 4 5 6 7 8 9 10 11 12 With system power OFF remove the MFD database card from the bottom card slot of the MFD Update the Garmin databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is pres
43. piezeH pi JU0 AEN yi jeuonippv uoneJjedo jeunouqy 1 E xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ Annunciations amp Alerts A GARMIN GMC 710 MESSAGE ADVISORIES CONT MANIFEST GMC software The GMC 710 has incorrect software installed mismatch Communication halted The G1000 system should be serviced GMC KEYSTK GMC key name Key is stuck GTS 820 MESSAGE ADVISORIES 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 GTS CONFIG GTS config error Contig service req d The GTS and GDU have incompatible configurations This alert is also set when the GTS has an invalid mode S address configured or the mode S address does not match both XPDR mode S addresses MANIFEST GTS software The GTS has incorrect software installed The mismatch communication halted G1000 system should be serviced MISCELLANEOUS MESSAGE ADVISORIES FPL WPT LOCK Flight plan waypoint is locked Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot tind the specitied waypoint and flags this message This can also occur with user
44. scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain 1 2 3 4 60 WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation Select the GAIN Softkey to activate the cursor in the GAIN field 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 Press the FMS Knob to remove the cursor Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Ground Mapping Hazard Avoidance 1 Press the MODE Softkey 2 Press the GROUND Softkey to place the radar in Ground Map Mode 3 Press the BACK Softkey 4 Press the FMS Knob to activate the cursor 5 Turn the lar
45. selected the volume can also be adjusted using the small FMS Knob 3 Select the MUTE Softkey to mute the audio Select the MUTE Softkey again to unmute the audio SiriusXM Radio volume may also be adjusted on each passenger headset 68 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features SATELLITE TELEPHONE amp SMS MESSAGING SERVICE Operation of these features in the cockpit is accomplished through the AUX TELEPHONE AUX TEXT MESSAGING AUX REPORT STATUS and AUX WI FI SETUP Pages Registering With Garmin Flight Data Services A subscriber account must be established prior to using the Iridium Satellite System Before setting up an Iridium account obtain the serial number of the Iridium Transceiver GSR1 and the System ID by viewing the AUX SYSTEM STATUS Page Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 Disable Enable Iridium Transceiver Iridium telephone may be turned on or off by performing the following steps To enable the Iridium telephone system 1 With the AUX TELEPHONE Page displayed select the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Enable Iridium Transmission 3 Press the ENT Key To disable the Iridium telephone system 1 With the AUX TELEPHONE Page displayed select the MENU Key on the MFD to display the Page Menu 2
46. the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint c Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Select the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number c Turn the large FMS Knob to highlight the LEG field d 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 NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Socata TBM 85
47. the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Predefined Message c Press the ENT Key The PREDEFINED SMS TEXT MESSAGE Window is now displayed SoJnpo20Jd Puruuejd NEN Sd5 S 21V OTE e uepioAy puezey 5 The cursor is displayed in the TITLE field Enter the desired message title Entry can be accomplished through the alphanumeric keys on the controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey 6 Press the ENT Key The cursor is now displayed in the MESSAGE field 7 Enter the desired message using any combination of entry methods as described in step 5 8 Press the ENT Key 9 Press the SAVE Softkey The new predefined message is now shown in the displayed list Pressing the CANCEL Softkey will delete the message without saving gt a Q zi E D x pu ddy sue v uoneJjedo unuuy jeunouqy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 15 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Abnormal Annun EAS AFCS GPS Nav Procedu
48. 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 Strike is less than 6 seconds old Strike is between 6 and 60 seconds old 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 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 41 AEN Sd5 S241V oipny dadx SVJ U9UINJ SU Wi0 AeN yyb14 Puruuejd oE a UePIOAY SoJnpa20Jd puezey sue v uone1odo soJnjeo unuuy Jeuuouqy jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight
49. to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Flight Planning 11 12 13 14 15 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
50. v uonejodo soJnjeo unuuy Jeuuouqy Jeuonippy xipueddy xepu Hazard Avoidance GARMI N Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or inhibit the alert on the PFD Flight Instruments Automatic Standby EAS When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode Flight Nav Com GPS Nav AFCS XPDR Audio Planning Procedures o W S lt Annun Abnormal Additional Alerts Operation Features Appendix Index 62 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Ad itional Features ADDITIONAL FEATURES Sjueuinjijsu 1uDij3 SYNTHETIC VISION SV3 WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic oipny uadx Wwo gt AeN S4V Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS infor
51. 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 identitier to reflect the new information 110 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT FPL WPT MOVE Flight plan The system has detected that a waypoint waypoint moved coordinate has changed due to a new navigation database update Verity that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan contains Verity user modified procedures procedures that have been manually edited This alert is issued only after an navigation database update Verity that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed This occurs when a stored flight plan contains Verify stored airways an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verity use of airways in stored flight plans and reload airways as needed FPLTRUNC Flight plan has been This occurs when a newly installed navigation truncated database eliminates an obsolete approach or arrival used by a stored fli
52. 0 190 00708 04 Rev A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings 7 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 8 The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 9 Theflashing 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 10 The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system 11 The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system 12 w 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 flashi
53. 000 Cockpit Reference Guide for the Socata TBM 850 RR 1 Record of Revisions GARMI N Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Table of Contents FLIGHT INSTRUMENTS sssssssssnnnnnnnnnnn Selecting the Altimeter Barometric Pressure Setting Selecting Standard Barometric Pressure Change Altimeter Barometric Pressure Setting Units Synchronizing the Altimeter Barometric Pressure Settings Synchronize CDI nennen Change Navigation Sources 0 ccccccscssessesssssssssssssesssesssessssssnesssssusesssessessessneenneeen 2 Enable Disable OBS Mode While Navigating with GPS 2 Generi UTM eona EAE E EE A EE 2 Configure Vspeed Bugs 2 Set Barometric Radar Altimeter Minimum Descent Altitude 3 Manually Testing the Radar Altimeter KRA 405B only S Displaying Wind Data ssssssssseeeeeeenenennn 3 Changing HSI Format 4 ENGINE amp AIRFRAME SYSTEMS 5 Electrical System 6 Fuel SVSIBITE soot m EURO NUR RUNI MIO UNE OEE E 8 General Systems tete 10 NAV COM TRANSPONDER AUDIO PANEL 11 Enter or Change Flight ID Optional 11 ADF Tuning Optional sssssssseeeeteeteneenes 11 DME Tuning Optional snb EDEN RMERN EUNT OTHER HU DNE PUN 11 Enter a T
54. 08 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 67 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Abnormal Annun EAS AFCS GPS Nav Procedures Avoidance S ou Ss 2 BB 2p e LL lt x Appendix Alerts Operation Index A Additional Features CG ARMIN 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 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select the SET Softkey 4 Select any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 With the XM Radio Page displayed select the VOL Softkey 2 Select the VOL Softkey to reduce volume or select the VOL Softkey to increase volume Once the VOL Softkey is
55. 90 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 99 SoJnjeoJ 92uepioAy SoAnpo20Jd Puruuejd NEN Sd5 S 4V oipny uadx SV3 sjueuinajsu piezeH yi JU0 AEN yi jeuonippv uoneJjedo jeunouqy Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LE A Annunciations amp Alerts GARMIN DATABASE MESSAGE ADVISORIES CONT DB MISMATCH Airport Terrain The PFDs and MFD have different airport terrain database mismatch database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on NAV DB UPDATED Active System has updated the active navigation navigation database updated database from the standby navigation database TERRAIN DSP PFD1 PFD2 or One of the terrain airport terrain or obstacle MFD 1 Terrain awareness display databases required for TAWS in the specified PFD unavailable or MFD is missing or invalid GMA 1347D MESSAGE ADVISORIES GMAT FAIL GMA is inoperative The audio panel self test has detected a failure GMA2 FAIL GMA2 is inoperative The audio panel is unavailable The G1000 system should be serviced GMA XTALK GMA crosstalk erro
56. ARMIN Setting Up and Customizing Weather Data for the Navigation Map Page 1 Select the Navigation Map Page 2 Press the MENU Key 3 With Map Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select the Weather Group and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON OFF range settings 7 Press the ENT Key to select an option 8 Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings GFDS Weather Data Requests The GFDS Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals if Hazard Avoidance desired and the ability to send or cancel weather data requests The window also displays the status of the GFDS data request process Requesting GFDS Weather Data Manually 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With GFDS Weather Request highlighted press the ENT Key 4 Turn the large FMS Knob to highlight the desired coverage option s and press the ENT Key to check or uncheck one of more of the following coverage selections e PRESENT POSITION Requests data based on current location e DESTINATION Requests data based on active flight plan destination if the flight plan contai
57. AV 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 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN _Nav Com XPDR Audio Panel INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob switches between volume and squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciator is lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is extinguishe
58. Alerts Index G Gain 60 Generator Current 5 Speed 5 Ground mapping 61 H Horizontal scan 60 Horizon heading 63 Inhibit 56 58 Inhibit TAWS 58 Inhibit Terrain 56 Inset Map 117 118 124 Interturbine Temperature ITT 5 Warning 85 lOl 90 92 93 Iridium 69 72 Iridium satellite network 69 J Jeppesen 65 L Lightning 41 42 M Magnetic Field Variation Database 129 130 Map panning 43 Message advisories 95 96 97 98 99 100 103 104 105 106 107 109 110 111 112 113 114 METAR 43 Minimums 94 Index 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A GARMIN MISCOMP 88 Mode S 122 Mode selection softkeys 12 Multi Function Display MFD Softkeys 123 MV DB 129 N NAV 12 NAV1 2 12 NAV2 2 12 Navigation database 21 22 NEXRAD 43 118 124 O OBS 2 Obstacles 99 100 101 Oil engine Alerts 85 Pressure 5 Temperature 5 Overspeed Protection 16 Oxygen Pressure 5 Warning 85 P Pathways 63 64 PIT 88 Predefined message 75 Propeller speed 5 R Reversionary Mode EICAS 5 Reversionary mode 81 ROC 90 92 190 00708 04 Rev A A GARMIN S SafeTaxi 64 SBAS 16 38 57 58 83 101 103 Sector scan 61 Sensor 88 SMS 69 STAB 61 Standby 59 Standby Navigation Database 127 Store Flight Plan 33 Stormscope lightning data 41 42 Strike 41 Strike mode 42 SVS 63 113 Synchronization 126 SYNC Status 128 Synthetic Vision Syst
59. D2 or MFD to be updated label of SD card facing left 2 Turn the system ON A prompt is displayed in the upper left corner of the display 3 Press the NO Softkey to proceed to loading the active database 4 Aprompt similar to the following is displayed Press the YES Softkey to update the active navigation database 5 After the update completes the display starts in normal mode 6 Turn the system OFF and remove the SD card from the top card slot 7 Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD 8 Apply power to the system and press the ENT Key to acknowledge the startup screen 9 Turn the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page 11 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 Loading the Jeppesen Navigation Database as the Standby Navigation Database 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 NOTE After the navigation database is loaded or copied the top SD card may be removed 127 S9JnjeaJ e2uepioAy SoJnpa20Jd Duiuue d ACN Sd5 j4V oipny uaddx SV3 sjuauinajsu Jeuonippy puezey 114 Wwo gt AeN 14 uonejedo jeuuouqv sue v junuuy xopu xipueddy Additional Hazard Fl
60. FAIL G 5T 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 51 needs A failure has been detected in glideslope service Return unit for repair receiver 1 and or receiver 2 The receiver may G S2 SERVICE G S2 needs still be available The G1000 system should be service Return unit for repair serviced when possible G S2 FAIL G S2 is inoperative GEA 71 MESSAGE ADVISORIES GEA1 CONFIG GEA1 contig error The GEA1 configuration settings do not match Contig service req d those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error The GEA2 configuration settings do not match Contig service req d those of backup configuration memory The G1000 system should be serviced MANIFEST GEAT software The 1 GEA 71 has incorrect software installed mismatch communication halted The G1000 system should be serviced MANIFEST GEA2 software The 42 GEA 71 has incorrect software installed mismatch communication halted The G1000 system should be serviced 104 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Annunciations amp Alerts GTX 33 33D MESSAGE ADVISORIES XPDR1 CONFIG XPDR1 config The transponder configuration settings do not error Contig service req d match those of backup configuratio
61. FCC regulations 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Warnings Cautions amp Notes GARMIN NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is 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 aircr
62. G 122 125 168 To aH ou AEN Sd5 OIL PSI Duiuue d 1ubi3 O G G 0000000 Oc CABIN PRESS ALT FT 4408 DIFF PSI i SoJnpa 20Jd OOO 000 OC e2uepioAy puezey se EIS Display Normal Mode EIS Display Reversionary Mode C1 Torque C CAS Display 13 Fuel Fuel F iba 2 Propeller Speed Oc T Pressure Altitude and 14 Fuel Fuel Pressure gt Change Rate 3 Generator Speed Differential Pressure 15 rud and Generator urrents 4 Interturbine Temperature 10 sd Selected Cabin Altitude 16 P and Essential Bus Voltages z Oil Pressure 11 Oxygen Pressure Fl s Aileron and x Rudder Trim and Flap 6 Oil Temperature 12 Fuel Quantity rero 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 D A Engine amp Airframe Systems GARMIN ELECTRICAL SYSTEM Flight Instruments 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the ELEC Softkey to display the Electrical System Page 5Y5 ELECTRICAL NORTH UP z E S oc Se 88 x LX pa amp sT amp v main cpu GPU LL lt oxy Ps 330 g w e L FUEL OTY R ha 1104 ti 25A uso 175 108 S LH 5 un a 128 OPH b EI oa Bus 3 BUS 2 PUS 3 BIS 4 ESS BUS BAT BUS c 2s 2c u m a N sB b ge lt b o o A a Hazard Avoidance C1 Standby Generator 4 Battery 7
63. G1000 Integrated Flight Deck Cockpit Reference Guide TBM 830 SOCATA A GARMIN Copyright 2007 2009 2011 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0719 09 or later for the Socata TBM 850 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 S040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 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 of any revision to this manual onto a hard drive or
64. 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 trom the reference waypoint Press the ENT Key The cursor is now displayed in the DIS distance field Enter the desired distance trom the reference waypoint Press the ENT Key Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 2 3 4 5 6 7 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Select the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 29 oipny uadx SV3 Sjueuinajsu WO AeN S 1V SoJnpo 0Jd Duiuue d AEN Sd5 4f1 4 2uepIony paezeH sue v uone1odo soJnjeo unuuy Jeuuouqy jeuonippy xipueddy xepu 614 Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index
65. LOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 7 Select the FLT ID Softkey GTS 820 only to enable or disable Flight ID displayed with the intruder information Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed select the MAP Softkey 3 Select the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Hazard Avoidance TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 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 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstac
66. N CDI GPS m ua Top Level PFD Softkeys Nn S O V V3 V V3 VP V 3 wz optional optional sm optional optional optional FE n kr 8S5 mx nmn onm nm SoJnpo 20Jd Select the BACK Softkey to return to the top level softkeys e uepioAy puezey Inset Map Softkeys T Level 1 Level2 Level 3 Description p INSET Displays Inset Map in PFD lower left corner 3 OFF Removes Inset Map si DCLTR 3 Selects desired amount of map detail cycles sue v junuuy 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 gt ke D x xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 117 Additional Hazard Flight Nav Com Flight Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Annun Alerts A Appendix CCC GARMIN Levell Level2 Level 3 Description Wx LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC Cycles through tratfic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain
67. Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Turn the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Turn the small FMS Knob to enter the next desired character 5 Repeat steps 3 and 4 until the desired Flight ID is entered 6 Press the ENT Key to update the Flight ID Do not perform any other G1000 functions until updating is no longer displayed ADF TUNING OPTIONAL 1 Press the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large FMS Knob to select the next desired field 4 Turn the small FMS Knob to enter the desired number 5 Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Turn the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING OPTIONAL 1 Press the ADF DME or DME Softkey 2 Turn the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauingjsu SV3 S2dV oipny uadx U10 AEN su
68. RMIN Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Reversionary mode must be entered manually in the case of PFD1 PFD2 or MFD failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display SV3 SjueuinJjsu 1uDi 3 oipny dadx Wwo gt AeN Activation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MFD 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 AEN Sd5 SJV Puruuejd oE NOTE The Socata TBM 850 Airplane Flight Manual AFM always takes precedence over the information found in this section SoJnpo 20Jd 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 e2uepioAy puezey SoJnjeoJ Jeuonippy HAZARD DISPLAYS WITH LOSS OF GPS POSITION i If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again
69. S Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor TRIP PLANNING 1 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 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 23 oipny dadx SV3 sjueuindjsu U10 AEN yyb14 S 1V SoJnpo 0Jd Duiuue d AEN Sd5 4f1 4 sue v uonejedo S9JnjeaJ e2uepioAy unuuy Jeuuouqy Jeuonippy puezey xipueddy xepu Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Procedures Planning GPS Nav EAS AFCS Appendix Alerts Operation Features Index Flight Planning 24 4 A GARMIN For Direct to planning a Select the WPTS Softkey and verity that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present Position to display P POS c Press
70. Terrain SVS operating with PFD Terrain or Obstacle databases Terrain System Test Terrain System Fail Failure Alert Type Aural Message Terrain or Obstacle database unavailable or invalid Terrain System invalid software Failure configuration system audio fault Terrain System No GPS position mA EN Excessively degraded GPS signal Out of TER WA Terrain System database coverage iuis Not Available area Sufficient GPS signal Terrain System None None i received after loss Available 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 91 SoJnjeoJ 92uepioAy SoJnpo20Jd Duiuue d NEN Sd5 4JV oipny uadx SV3 sjueuinajsu paezey yi JU0 AEN NITE jeuonippv uonejedo jeunouqy Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ A Annunciations amp Alerts _ GARMIN TAWS B ALERTS PFD MFD MED Alert Type TAWS B Page Aural Message e Pop Up Alert Annunciation Excessive Descent m PS NENNEN Pull Up Rate Warning EDR Reduced Required PULL UP TERRAIN PULL UP Terrain Terrain Pull Up Pull Terrain Clearance or Up Waring RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Terrain Impact Warning ITI Of Ahead Pull Up TERRAIN PULL UP NEM Terrai
71. While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the ADDRESS Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Address c Press the ENT Key The sorting selection is indicated at the bottom center of the list window Viewing The Content of a Text Message 1 2 3 4 5 While viewing the AUX TEXT MESSAGING Page select the desired message box Press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Press the VIEW Softkey Or Press the ENT Key Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on View Selected Message c Press the ENT Key To close the text message press the CLOSE Softkey Or a Press the MENU Key to display the Page Menu Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features b Turn either FMS Knob to place the cursor on Close Message c Press the ENT Key Mark Selected Message As Read 1 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor Sjueuinjijsu 1uDij3 svi 2 Turn either FMS Knob to select the desired message 3 Press the MRK READ Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Mark Selected Message As Read
72. a ons drin Col rporation BT Jangshu 2nd R oad t Shift Taipei County Taiwan Aur go 886 2 2642 9199 1886 2 2642 90 a f a www garmin com _ oa T 2007 2009 2011 Garmin Ltd or its subsidiaries 190 00708 04 Rev A
73. active vertical waypoint VNV Unavailable Excessive track The current track angle error exceeds the limit angle error causing the vertical deviation to go invalid VNV Unavailable Excessive The current crosstrack exceeds the limit crosstrack error causing vertical deviation to go invalid VNV Unavailable Parallel course A parallel course has been selected causing selected the vertical deviation to go invalid NON WGS84 WPT Do not use GPS The position of the selected waypoint boox for navigation to 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 The G1000 is no longer receiving data from failed the traffic system The traffic device should be serviced FAILED PATH A data path has A data path connected to the GDU or the GIA failed 63 W has failed MAG VAR WARN Large magnetic The GDU s internal model cannot determine variance Verity all course angles the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of Synthetic Vision is disabled because the aircraft available terrain region is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB Synthetic Vision is disab
74. adial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 27 oipny dadx SV3 sjueuindjsu U10 AEN yyb14 S 1V SoJnpo 20Jd Duiuue d AEN Sd5 4f1 4 sue v uoneJjedo S9JnjeaJ e2uepioAy unuuy jewuouqy Jeuonippy puezey xipueddy xepu Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 28 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD 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
75. aft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features 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 Socata TBM 850 190 00708 04 Rev A amp GARMIN Record of Revisions Change Summary 190 00708 00 Initial Release 190 00708 01 Rev A Added SVS and other GDU 9 02 parameters Rev B Clerical changes 190 00708 02 Added temporary user waypoints Added import export flight plans Added CDI availability during Dead Reckoning mode Added GDU 9 14 parameters 190 00708 03 RevA Added GDU 11 01 parameters Added GTS 820 Added AOPA Airport Directory Added database synchronization 190 00708 04 Added Profile View Added Standby Navigation Database Added new database update procedures Added Iridium Satellite Telephone amp SMS messaging Added GFDS Worldwide Weather Added WX LGND LEGEND and METAR softkeys Updated system messages Added other GDU 12 01 parameters ndn Date of Revision Affected Pages October 2011 Production release 190 00708 04 Rev A Garmin G1
76. aircraft is 53 AEN Sd5 S241V oipny dadx Sv3 sjueuingjsu Wi0D AeN HL Puruuejd oE e2uepioAy SoJnpa20Jd puezey sue v uonejedo sainjee4 unuuy Jeuuouqy Jeuonippy xipueddy xepu Abnormal Additional Annun Flight Instruments Nav Com XPDR Audio Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 94 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 TAS Optional System Self Test 1 Setthe range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST 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 TAS System Test Fail is heard Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the second rectangular page icon 3 Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the BE
77. al Operation Index Appendix LJ 102 Annunciations amp Alerts Message MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted MANIFEST GFC software mismatch communication halted MANIFEST COM software mismatch communication halted MANIFEST COM2 software mismatch communication halted MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM over temp Reducing transmitter power COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair COM1 PTT COM push to talk key is stuck COM2 PTT COM2 push to talk key is stuck Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A GARMIN GIA 63W MESSAGE ADVISORIES CONT Comments The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced Incorrect servo software is installed or gain settings are incorrect The COM1 and or COM2 has incorrect software installed The system should be serviced The NAV1 and or NAV2 has incorrect software installed The system should be serviced 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
78. ard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description ADF DME XPDR XPDRI XPDR2 STBY ON ALT GND VFR CODE 0 7 BKSP IDENT TMR REF NRST MSG Displays the ADF DME Tuning Window Displays transponder mode selection softkeys Selects the 1 transponder as active Selects the 2 transponder as active Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identitying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Message Window 122 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Appendi
79. armin G1000 Cockpit Reference Guide for the Socata TBM 850 serviced if the problem persists The PFD1 configuration module backup memory has failed The G1000 system should be The PFD1 voltage is low The G1000 system The PFD2 voltage is low The G1000 system The MFD voltage is low The G1000 system The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the G1000 system should be serviced 190 00708 04 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1basemap The MFD and or PFD detected a failure in the database error exists basemap database PFD2 DB ERR PFD2 basemap database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists If problem persists The G1000 system should be PFD2 DB ERR PFD terrain serviced database error exists MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain The terrain database is present on another LRU database missing but is missing on the specified LRU PFD2 DB ERR PFD2 terrain database missing MFD1 DB ERR MFD1 obstacle database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 obstacle obstacle database Ensure that the data card is database error exists
80. ata and pointers in the Wind Data Box on the PFD Current Track Indicator All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Flight GPS Nav Planning Procedures Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes Terrain Proximity TERRAIN SVS and TAWS are 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 Hazard Avoidance Features E o m 5 lt x Annun Appendix Alerts Index 84 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS CAS MESSAGES Warning Messages Messages Comments Engine compartment fire temperature over 200 C if installed Dissymmetry between left and right hand flaps Fuel tank selectors set to Off Fuel pressure below 10 psi Engine start ITT over 1000 C 870 C 5 s or 840 C 20 s Engine running ITT over 840 C Oilpressurebelow60psi_ Oxygen cylinder cosd Parking brake applied Torque greater than or equal to 121 4 maximum torque L ET lt ENGINE OFF LL ENGINEON L ET S S S f Rou 1 L SS p do SSS SSS AR 1 1L L1 Sf
81. 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 October 2011 190 00708 04 Rev A Printed in the U S A A GARMIN Marnings Cautions amp Notes 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 obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea L
82. card in the bottom card slot of the PFD ERR Card 2 is invalid or MFD contains invalid data EPS Service required The EPS option has been installed on an aircraft without the EPS system Software baseline and appropriate options shall be reloaded EPS S G speed sensor failed The EPS option has been installed on an aircraft without the EPS system Software baseline and appropriate options shall be reloaded CRUISE Cruise conditions met Cruise engine trend data log has been captured CRUISE II Cruise I conditions met Cruise Il engine trend data log has been captured EXCEEDANCE Engine exceedance ae An engine exceedance log has been captured data is being logged REGISTER GFDS Data services are The system is not registered with Garmin Flight inoperative register w GFDS Data Services or its current registration data 114 has failed authentication Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN nnunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Description Results Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only The file stored on the SD card did not contain a flight plan User waypoints
83. contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled checked and contains required criteria then re send the data request NO GFDS Subscription The system is not be currently subscribed to GFDS or the access code is incorrect Verify the access code Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance Reduce Request Area The GFDS weather data request area exceeds size limits Reduce weather coverage area and re send data request Request Cancelled The user has cancelled a GFDS weather data request Requested area The size of the GFDS weather data request has exceeded limits Reduce toolarge Reduce the size of the coverage area and try the weather data request again coverage area Request Failed Try The weather data request timed out Re send data request Again Transfer Preempted The GDL 59 is busy Retry request later 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 51 AEN Sd5 S241V oipny dadx Sv3 sjueuingjsu Wi0 AeN yybi4 Puruuejd oE 2uepIony SoJnpa20Jd puezey sue v uoneJjedo s9JnjeaJ unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning Hazard Avoidance Procedures EAS AFCS GPS Nav Appendix Alerts Operatio
84. d the ICS Knob controls only volume PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the INTR COM Key is enabled PA messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator flashes to indicate when play is in progress The PLAY annunciator turns off after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play If a COM input signal is detected during play of a recorded memory block play is halted 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 13 s u un su S24Y oipny uadx Sv3 WOD AEN SHaIV uonejedo SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 junuuy Jeuuouqy Jeuonippy jui xipueddy xepu 1ubi 4 puezey A Nav Com XPDR Audio Pa
85. d waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Flight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial trom the reference waypoint 12 Press the ENT Key 13 Repeat step 10 to enter the next waypoint name 14 Press the ENT Key The cursor is displayed in the RAD r
86. d before answering gt a Q zi E D uoieiado jeunouqy Disabling incoming call alerts 1 With the AUX TELEPHONE Page displayed press the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable Incoming Call Alerts sue v Junuuy 3 Press the ENT Key The voice and pop up alert will not be displayed now when an incoming call is received xipueddy xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 T A Additional Features CG ARMIN Outgoing Calls Flight Instruments Voice calls can be made from the cockpit through the Iridium Satellite Network To make a call 1 Press the TEL Key on the audio panel 2 Select the DIAL Softkey on the MFD Or While viewing the AUX TELEPHONE Page a Press the TEL Key on the audio panel b Press the MENU Key to display the Page Menu c Turn either FMS Knob to place the cursor on Dial a Phone Call d Press the ENT Key 3 Selecting the number softkeys on the MFD enter 00 country code area code phone number when calling a non satellite telephone system Enter 00 Satellite Country Code shown in the following table phone number when placing a call to another satellite telephone system 4 Press the ENT Key OK is highlighted 5 Press the ENT Key The system will begin calling the number Flight Nav Com Planning GPS Nav AFCS XPDR Audio EAS Procedures
87. dvisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria C Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS 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 small FMS Knob to select the Traffic Map Page 3 Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 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
88. e 1 AHRS is using the backup GPS path GPS source Primary GPS path has failed The G1000 system should be serviced when possible 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 105 SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 4JV oipny 4adx SV3 sjueuinajsu piezeH yi JU0 AEN yi jeuonippv uonejedo jeunouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT AHRS2 GPS AHRS2 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information AHRS2 GPS AHRS2 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information AHRS2 GPS AHRS2 not receiving backup GPS information AHRS1 GPS AHRS1 operating exclusively in no GPS mode AHRS2 GPS AHRS2 operating exclusively in no GPS mode AHRS MAG DB AHRS magnetic model database version mismatch AHRS1 SRVC AHRS1 Magnetic field model needs update AHRS2 SRVC AHRS2 Magnetic field model needs update GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass 106 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 The 2 AHRS is using the backup GPS path Primary GPS path ha
89. ed or designated as is or changed to a different altitude An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or entering a different value and pressing the ENT Key The altitude is now displayed as blue text indicating that the altitude is now designated to give vertical speed and deviation guidance Approach waypoint altitude constraints are designated in the same way as previously described for arrivals These altitudes are also displayed as blue text after being designated for use Waypoint altitude constraints may be designated up to but not including the FAE The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case the FAF altitude can be designated 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 the altitude of the Altitude is designated in determining aircraft as it passes over for use in giving vertical vertical flight path the navigation point flight path guidance guidance This altitude is provided Altitude does not match as a reference and is the published altitude not designated to be in navigation database used in determining or no published altitude vertical flight path exists g
90. em 63 T TA 94 TAF 43 TAS 54 94 105 TAWS 57 58 92 TAWS B 57 Telephone 69 71 72 74 76 Terrain 55 57 99 118 124 Terrain SVS 55 56 57 Text message 73 75 76 Text messaging 7 2 Tilt line 59 Timer 2 111 Topographical data 118 124 Torque 5 Warning 85 Traffic 41 53 123 Traffic advisory 53 Traffic Advisory 94 Traffic map page 53 54 55 Transponder 11 12 122 Trim 5 V Vertical speed guidance 22 Vertical track 94 VNV 19 82 113 Vspeed 2 W WATCH 61 Waypoint Selection Submenu 30 Index Weather Attenuated Color Highlight 61 Weather data link page 43 Weather radar 59 Wind data 120 X XM WX lightning 118 124 XM WX weather 43 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index 3 s9JnjeaJ a UEPIOAY SoJnpa20Jd Duiuue d ACN Sd5 5JV oipny uddx SV3 sjuauinajsu Jeuonippy puezey 14 Wwo gt AeN 114 uoneJjedo Jeuuouqv sue v unuuy GARMIN Index SjuauunJjsu 1ubi4 SV3 oipny dadX Wwo gt AeN S21V AEN Sd5 Puruuejd E Blank Page soinpsd0ld 92UepIOAV puezey s n e 4 jeuonippy uonelaedo Jeuuouqy Sue v unuuy UN EN 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index 4 A GARMIN E s p t o CIO m m NR d i nJ p ga 3 Garmin International Inc 00 East 151st Street LU prom E c 5 n the aS ee e Garmin
91. ent wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select 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 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 126 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded or copied the top SD card may be removed Appendix 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PF
92. erence Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN 4dditional Features Incoming Calls When viewing MFD pages other than the AUX TELEPHONE Page a pop up alert will be displayed accompanied by a ringtone heard on the selected cockpit audio The pop up alert may be inhibited at times such as during takeoff In addition to the pop up alert a ringing phone symbol will be displayed to the right of the MFD page title UDWINI SU 34fi 4 SV3 Answering an incoming call oipny uddx JUI0 AeN 1 Press the TEL Key on the audio panel 2 Select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page SJV AEN Sd5 O NOTE The Push to Talk switch is not utilized for telephone communication The microphone is active after selecting the ANSWER Softkey and stays active until the call is terminated Puruuejd oE 1 Press the TEL Key on the audio panel 2 Press the MENU Key to display the Page Menu 3 Turn either FMS Knob to place the cursor on Answer Incoming Call 4 Press the ENT Key SoJnpo 20Jd e2uepioAy puezey Selecting the IGNORE Softkey will extinguish the pop up window and leave the current call unanswered Selecting the IGNRE ALL Softkey will extinguish the pop up window for the current and all future incoming calls and leave the current call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE Page al lowing additional call information to be viewe
93. established sue v Junuuy xipueddy Loss of Hazard Functions with Loss of GPS Position xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 81 A Abnormal Operation GARMIN UNUSUAL ATTITUDES Flight Instruments 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 EAS Traffic Annunciations System Time e Glideslope Glidepath 2 e AFCSAnnunciaions PFD Setup Menu and Vertical Deviation Flight Director Windows displayed in Indicators Command Bars the lower right corner Altimeter Barometric 2 e Inset Map of the PFD Setting Temperatures Timer References e Radar Altimeter DME Information Nearest Airports Selected Altitude E Window Flight Plan e VNV Target Altitude Wind Data Messages z Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status e Barometric Minimum Box Descent Altitude Box 2 Extreme Pitch Indication cu 2t E ax Appendix Index 02 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Abnormal Operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an inval
94. evel and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Warnings Cautions amp Notes GARMIN WARNING Do not use datalink weather products e g XM WX Satellite Weat
95. ge FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF xipueddy xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Flight Instruments GARMI N CHANGE NAVIGATION SOURCES 1 2 3 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the 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 2 3 Select the OBS Softkey to select OBS Mode 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 Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 2 3 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 Turn the small FMS Knob to display the UP DOWN window T
96. ge FMS Knob to place the cursor in the TILT field 6 Adjust the antenna tilt angle by turning the small FMS Knob to position the ground returns as desired 7 Press the FMS Knob to remove the cursor 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 readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor 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 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 AEN Sd5 S241V oipny dadx SVJ U9UINJ SU Wi0D AeN yyb14 Duiuue d iui e2uepioAy SoJnpa20Jd puezey sue
97. ght plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate This occurs when the pilot attempts to activate locked flight plan a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at Arriving at waypoint xxxx where xxxx is the waypoint Xxxx waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 111 SoJnjeoJ 92uepioAy SoJnpo20Jd Duiuue d NEN Sd5 4JV oipny uadx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uonejedo jeunouqy xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ A Annunciations amp Alerts GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead Special use airspace is ahead of aircraft The less than 10 minutes aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and Special use airspace is near and ahead of the ahead aircraft position ARSPC NEAR Airspace near less Special use airspace is within 2 nm of the than
98. he Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Hazard Avoidance XM WX SATELLITE WEATHER OPTIONAL WARNING Use of XM WX Satellite Weather for hazardous weather penetration is not recommended Weather information provided by SiriusXM is approved only for weather avoidance not penetration Displaying XM WX Satellite 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 Turn the large FMS Knob to select the WPT Page Group 2 Turn 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 Turn the large FMS Knob to
99. he bottom left of the list window e uepioAy puezey Arranging Text Messages gt a Q zi E D The viewed messages may be listed according to the date time the message was sent or received the type of message read unread sent unsent etc or by message address uonejedo jeunouqy View Messages Sorted by Message Date Time While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TIME Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Date Time xipueddy sue v unuuy Xapu c Press the ENT Key The sorting selection is indicated at the bottom center of the list window 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 11 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Abnormal Annun EAS AFCS GPS Nav Procedures S ou Ss 2 BB 2p e LL lt x Appendix Alerts Operation Index Additional Features 78 A GARMIN View Messages Sorted by Message Type While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TYPE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Type c Press the ENT Key The sorting selection is indicated at the bottom center of the list window View Messages Sorted by Address
100. her or GFDS World Wide Weather for hazardous weather penetration Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear 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 Socata TBM 850 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 i
101. herefore 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 successtully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 115 SoJnjeoJ 92uepioAy soJnpo20Jd Puruuejd AeN Sd5 4JV oipny 4adx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uoneJjedo jeunouqy 122 E xepu GARMIN Annunciations amp Alerts SjuauunJjsu 1ubi4 SV3 oipny dadx Wwo gt AeN S23V AEN Sd5 Puruuejd E Blank Page soinpsd0ld 92UepIOAV puezey s n e 4 jeuonippy uoiesado jeuuouqy OA xipueddy xopu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 116 GARMI N LLL Appendix APPENDIX SjueuinJjsu 1uDi 3 PFD SOFTKEY MAP nnn D S D Y v 4 D svi CDI NAV1 CDI NAV2 oipny uadx Wwo gt Ae
102. iable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed 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
103. id 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 NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable
104. ight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix FCCC GARMIN 128 1 2 3 4 5 7 8 3 10 11 12 13 14 15 16 17 18 19 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD Verity that an SD card is inserted in the bottom slot of each PFD and the MFD Turn the system ON A prompt is displayed Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD After the navigation database files are copied to the bottom SD card press any key to continue as instructed Again press any key to continue as instructed on the display Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting 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 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed Turn system power OFF Rem
105. ight Nav Com Flight Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Annun Alerts Index Appendix Level 2 Description 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 the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional NEXRAD Displays NEXRAD weather and coverage information on Hr the Navigation Map optional PRECIP Displays GFDS precipitation on Navigation Map optional XM LING Displays XM WX lightning information on the or Navigation Map optional DLLING Displays GFDS Worldwide Weather lightning information on the Navigation Map optional METAR Displays METAR flags on airport symbols shown on the Navigation Map optional LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected BACK Returns to top level softkeys Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Appendix Level 1 Level 2 Description DCLTR 3 SHW CHRT CHKLIST Selec
106. imported success only user waypoints These waypoints have been saved to the fully No stored flight plan data was system user waypoints No flight plans stored in the system modified have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD 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 File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun The flight plan on the SD card contains more waypoints than cated the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way The flight plan on the SD card contains one or more waypoints points locked 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 The flight plan file on the SD card contains user waypoints loaded The quantity of stored user waypoints has exceeded system Capacity t
107. io Page SV3 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select XM Radio 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled oipny uddx JUI0 AeN SJV 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 AEN Sd5 Puruuejd oE 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 SoJnpo 20Jd e uepioAy puezey mul t fet et 1 n jeuonippy Select an Available Channel within the Selected Category uoneJjedo jeunouqy 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go down through the list in the Channel Box or move up 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 xipueddy sue v unuuy Xapu 190 007
108. jsu oipny dadx Wwo gt AeN 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 KIXD KDFW Puruuejd 1461 4 KARLA 221 11 7NM 13000FT g Large White COVIE 221 9 NM 12400FT inn 2 LEMYN 220 80NM A Large Light i f Blue Text 5 Approach KDFW RNAV 17LGPs LPY RIVET iaf 259 18 8NM ges Small Light z DRAAK 176 3 3MM Blue Text 3 INWOD 176 3 2NM Small Light MENOL faf 176 3 9MM oh a 7 RW17L map 176 5 3NM 3 zx Small White Text POLKE Restriction Bar uonejedo jeunouqy sue v junuuy SIS Cross AT or ABOVE 5000 ft FAS Cross AT 2 300 fi xipueddy ins Cross AT or BELOW 3 000 fi Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 21 1ubi 4 peas is puezey jeuonippv Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation GARMI N Since altitudes loaded with an arrival procedure are published only for turbojet aircraft the altitudes are displayed as white text indicating that the altitudes are displayed for reference only An arrival waypoint altitude may be us
109. le Location Terrain Obstacle above or within 100 below current aircraft altitude I I Terrain Obstacle between 100 and 1000 below current aircraft altitude Black Terrain Obstacle is more than 1000 below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map TERRAIN SVS option is installed and the TAWS option has not been installed 75 degrees north or 60 degrees south 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 NOTE Terrain SVS is only available when the Synthetic Vision System SVS A NOTE Terrain data is not displayed when the aircraft latitude is greater than AEN Sd S24V oipny 4adx svi sjueuimsu Wi0 gt AeN Duiuue d iui e2uepioAy SoJnpa20Jd puezey SoJnjeoJ jeuonippy sue v uonejedo junuuy jewuouqy xipueddy xopu 1ubi 4 Abnormal Additional Annun Flight Instruments Nav Com XPDR Audio Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 56 Display Terrain on the TERRAIN SVS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired select the VIEW Softkey to access the ARC a
110. led because a terrain resolution too low database of sufficient resolution 9 arc second or better is not currently installed 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 113 SoJnjeoJ 92uepioAy soJnpo20Jd Duiuue d NEN Sd5 4JV oipny 4adx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uoneJjedo jeunouqy 122 E xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ A Annunciations amp Alerts GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments CHEDULER message Message criteria entered by the user CHECK CRS Database course for Selected course for LOC1 differs from published LOC1 LOC ID is CRS localizer course by more than 10 degrees CHECK CRS Database course for Selected course for LOC2 differs trom published LOC2 LOC ID is CRSJ localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD The SD card was removed from the top card 1 REM Card 1 was removed slot of the PFD or MFD The SD card needs to Reinsert card be reinserted PFD1 PFD2 or MFD1 CARD The SD card was removed from the bottom 2 REM Card 2 was removed card slot of the PFD or MFD The SD card Reinsert card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid MFD contains invalid data The SD
111. matic request occurs GFDS Comm Error 2 A communications error has occurred with the GDL59 or GIA The G1000 should be serviced 50 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Hazard Avoidance Weather Request Description Status Message GFDS Comm Error 4 This occurs if multiple automatic weather data requests have recently failed or the GDL 59 or a GIA is off line GFDS Comm Error 5 This can occur if the GDL 59 is off line or not configured or the Iridium or GFDS networks are not accessible Check Iridium signal strength If this error persists the G1000 should be serviced GFDS Comm Error 6 A communications error has occurred It this error persists the G1000 should be serviced GFDS Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the data request GFDS Comm Error 8 A server error has occurred or invalid data received GFDS Login Invalid There is a problem with the GFDS registration Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance GFDS Server The GFDS weather data server is temporarily out of service but is expected Temporarily Inop to return to service in less than 30 minutes GFDS Server Inop The GFDS weather data server will be out of service for at least 30 minutes Invalid Coverage Area The weather data request coverage area does not
112. mation 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 e Three dimensional Traffic e Airport Signs e Runway Display buruue d AEN Sd5 E SoJnpo 20Jd e2uepioAy puezey mul t fet et 1 n jeuonippy uoneJjedo jeunouqy 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 x pu ddy sue v unuuy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 63 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Abnormal Annun EAS AFCS GPS Nav Procedures S ua 5s 2 BB E a e LL lt x Appendix Alerts Operation Index Additional Features A GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 2 3 4 5 Press
113. mp PFD Message Advisories ssssssseeeeeee 95 Database Message Advisories cccccccsssesssessessesseessscssecsessesssessussssessesseeseessessean 96 GMA 1347D Message Advisories sssssssssee 100 GIA 63W Message Advisories ssssssseeeeeeeee 101 GEA 71 Message AdVISOFIGS 0 0 cccccccccsssessssssessscsesssesssessesssesssesssesseessessseaseesneeseeseen 104 GTX 33 33D Message Advisories sssssssssseee 105 GRS 77 Message Advisories sssssssseeeeeeee 105 GMU 44 Message Advisories sssssssseeeeeeeee 107 GSR 56 Message Advisories ssssssssseeeeeee 107 GDL 69A Message Advisories sssssssssseeeeeee 107 GWX 68 Alert Messages etre rrt bat oe btt eet tu ueb bad 108 GDC 74B Message Advisories sssssssseeeeneeeee 108 GCU 475 Message Advisories ssssssssseseeeeeee 109 GMC 710 Message Advisories ssssssseseeeeee 109 GTS 820 Message Advisories sssssssseseeeeeee 110 Miscellaneous Message Advisories sssssssee 110 Flight Plan Import Export Messages 115 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 il Table of Contents GARMIN APPENDIX sssennnnnnnntnnnnnnttttnnnnnntttttnnnnnnttttns 117 PFD Softkey Map
114. n Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 58 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude I I Black Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key Garmin G1000 Cock
115. n Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Up Obstacle Clearance or Pull Up Waming ROC Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 0 I Obstacle Obstacle Pull Up Pull Up CAUTION TERRAIN or Reduced Required Caution Terrain Caution Terrain Clearance Terrain Caution RTC or Terrain Ahead Terrain Ahead n Imminent Terrain TERRAIN AHEAD Terrain Ahead Terrain Ahead Impact Caution ITI or or CAUTION TERRAIN Caution Terrain Caution Terrain CAUTION OBSTACLE SOT OBSTACLE AHEAD Reduced Required Caution Obstacle Caution Obstacle Clearance Obstacle or Obstacle Ahead Obstacle Ahead Caution ROC 92 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN PFD MFD Alert Type TAWS B Page Annunciation Imminent Obstacle Impact Caution IOI Premature Descent Alert Caution PDA Altitude Callout II 500 H Excessive Descent Rate Caution EDR Negative Climb Rate Caution NCR TAWS B System Status Annunciations Pop Up Alert Annunciations amp Alerts Aural Message Obstacle Ahead Obstade Ahead or Caution Obstacle Caution Obstacle Too Low Terrain Five Hundred Sink Rate Don t Sink or Too Low
116. n Features Index Hazard Avoidance GARMI N Cancelling a GFDS Weather Data Request in Progress 1 2 3 4 5 Select the GFDS Weather Data Link Page Press the MENU Key With GFDS Data Request highlighted press the ENT Key Turn the large FMS Knob to select CANCEL REQ and press the ENT Key The request status box indicates Request Cancelled Press the FMS Knob to return to the GFDS Weather Datalink Page Enabling Automatic GFDS Data Requests 1 2 3 4 5 6 52 Select the GFDS Weather Data Link Page Press the MENU Key With GFDS Weather Request highlighted press the ENT Key Choose the desired weather coverage options Turn the large FMS Knob to select the UPDATE RATE setting Then turn the small FMS Knob to highlight the desired automatic update trequency OFF 5 Min 10 Min 15 Min 20 Min 25 Min 30 Min 45 Min or 60 Min then press the ENT Key The SEND REQ button is highlighted and a countdown timer is displayed in the REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate GFDS Data Request Or Press the FMS Knob to return to the GFDS Weather Data Link Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN TRAFFIC SYSTEMS Hazard Avoidance e If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic A
117. n air 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 Navigation VOR Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT Pitch Hold default PIT Approach Glidepath GP Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 15 Sjueuinijsu 1uDij3 SV3 oipny dadx U0 AEN AEN Sd5 S 1V SjJo V uonejedo SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd junuuy Jeuuouqy Jeuonippy piezeH iui xipueddy xepu Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun GPS Nav AFCS EAS Procedures Appendix Alerts Operation Features Index A AFS aL GARMIN VERTICAL MODES 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 pea RING displayed in the Selected Altitude
118. n memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config The transponder configuration settings do not error Contig service req d match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software The transponder has incorrect software installed mismatch communication halted The G1000 system should be serviced MANIFEST GTX2 software The transponder has incorrect software installed mismatch communication halted The G1000 system should be serviced XPDR1 SRVC XPDR1 needs The 1 transponder should be serviced when service Return unit for repair possible XPDR2 SRVC XPDR2 needs The 2 transponder should be serviced when service Return unit for repair possible XPDR1 FAIL XPDR1 is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES AHRS1 TAS AHRS1 not receiving The 1 AHRS is not receiving true airspeed from valid airspeed 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 The 2 AHRS is not receiving true airspeed from valid airspeed the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup Th
119. n to adjust the tilt of the antenna up or down Monitor 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 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 AEN Sd5 S 4V Duiuue d iui e2uepioAy SoJnpa20Jd puezey sue v uonejedo soJnjeaJ unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 2 3 Press the MENU Key Turn the large FMS Knob to select Show Bearing Line 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
120. n while engine off Rear cargo door open Stall warning heat on while engine off Stall warning heat off X Starter generator running Vacuum pressure less than 3 75inHg X X Only affected side L R or L R displayed in CAS message applicable messages listed here display L R for example HOM Inhibits prevent certain CAS messages from being displayed during the following conditions Engine off e Aircraft in air AIR Engine on Landing Operation Phase Inhibit LOPI e Aircraft on ground Ground e Takeoff Operation Phase Inhibit TOPI 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 87 SoJnjeoJ 92uepioAy SoJnpo 0Jd Duiuue d AEN Sd5 SAV oipny uddx SV3 SjueuinJjsu pezeH 614 U05 AeEN jeuonippv uonejodo jeunouqy Xapu 1ubi 4 Flight Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Additional Abnormal Operation Ammundatons amp Alets GARMIN COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is gt 200 ft If both airspeed sensors detect 35 knots this is inhibited If either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts If either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts Difference in heading sensors is gt 6 deg
121. nd 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Hazard Avoidance 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key A NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the cu
122. nel GARMIN Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block Flight Instruments EAS Nav Com 2 5 2 ce e a x Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS Appendix Index 14 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN AFCS AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis A 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 Control Pressed Roll Hold default ROL Pitch Hold default PIT CWS Button GA Switch Modes Selected Roll Hold default ROL Pitch Hold default PIT Roll Hold default ROL Pitch Hold default PIT Takeoff on ground TO Takeoff on ground TO Go Around in air GA Go Around i
123. nformation presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Socata TBM 850 Airplane Flight Manual 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Marnings Cautions amp Notes 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 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 rel
124. ng cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature 13 w CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tur the large FMS Knob on the MFD Control Unit to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 25 oipny 4adx sV3 sjueuingsu 34fi 4 Wi0 gt AeN S4V SoJnpo 20Jd Duiuue d AEN Sd5 4f1 4 2uepIony paezeH s y uone1odo soJnjeo unuuy Jeuuouqy jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check
125. ns no destination dashes displayed e FPL Requests data based on active flight plan Turn the small 190 00708 04 Rev A FMS Knob to select the desired flight plan look ahead distance Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 n are AEN Sd5 S241V oipny dadx SVJ U9UINJ SU Wi0 AeN yyb14 Puruuejd oE a UEPIOAY SoJnpa20Jd puezey sue v uonejodo soJnjeo unuuy Jeuuouqy Jeuonippy xipueddy Xapu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N option or choose REMAINING FPL to request the remainder of the flight plan e WAYPOINT Requests data based on any valid waypoint 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field and turn the small FMS Knob to select the desired diameter and route width of the request then press the ENT Key 6 Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the GFDS Data Link Page without requesting data During a GFDS Data Request the Request Status box initially displays Contacting GFDS Once a connection is established the Request Status Box displays Receiving Wx Data Time Remaining with an estimated data tran
126. ntifier location etc Press the ENT Key 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 Turn the large FMS Knob to place the cursor over the ALT altitude field GPS Navigation SV3 Sjueuinijsu 1uDi 3 oipny dadx Wwo gt AeN AEN Sd5 S dV sue v uoneJjedo S9JnjeaJ 92uepioAy SoJnpa20Jd Duiuue d unuuy Jeuuouqy jeuonippy p1ezeH i xipueddy xepu Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EAS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation 7 8 3 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to ac
127. o display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway uonejedo Jeuuouqv STORE A FLIGHT PLAN sue v unuuy 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan xipueddy xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 33 Flight Planning GARMI N EDIT A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Select the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location Flight Instruments EAS Nav Com XPDR Audio 6 Enter the changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page AFCS DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor GPS Nav c a uS a 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 c Turn the large
128. on The PFDs and MFD have different navigation database mismatch Xtalk is off database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Standby The PFDs and MFD have different standby Navigation database mismatch navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database The PFDs and MFD have different terrain mismatch database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle The PFDs and MFD have different obstacle database mismatch database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 1
129. ot press the AP DISC Switch during servo power up and preflight system tests as this may cause the preflight Preflight Test system test to fail or never to start if servos fail their power up tests Power must be cycled to the servos to remedy the situation Preflight system test failed aural alert sounds at failure TERRAIN SVS ALERTS PFD MFD TERRAIN SVS MFD Aural Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Warning Terrain Clearance Warning RTC Terrain Imminent Terrain Impact DATA WARNING TERRAIN Warning Terrain Warning ITI Terrain Reduced Required Obstacle AI Warning Obstacle Clearance Warning ROC Obstacle Alert Type Imminent Obstacle Impact TERRAIN WARNING OBSTACLE Warning Obstacle Warning lOl Obstacle Reduced Required Terrain Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact Caution Terrain Caution ITI Terrain Reduced Required Obstacle Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact Caution Obstacle Caution IOl Obstacle 90 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN 0 Annunciations amp Alerts TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS PFD MFD Alert TERRAIN SVS Page Annunciation Annunciation rogress Terrain System Terrain Alerting is MFD Terrain or Obstacle database unavailable or invalid None None
130. 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 SateTaxi 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 SiriusXM is a trademark of SiriusXM Satellite Radio 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 including negligence shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has
131. ove the SD card from the top card slot of the MFD Turn system power ON 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 standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Appendix Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRSI and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor i
132. pit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Hazard Avoidance AIRBORNE COLOR WEATHER RADAR WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna 4 CAUTION In Standby Mode the antenna is parked at the center line It is always 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 Sjueuinijsu 614 SV3 oipny uadx Wwo gt AeN causing damage to the radar assembly Displaying Weather on the Weather Radar Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 Ifthe 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 the radar will begin transmitting The horizontal scan is initially displayed 5 Turn the Joystick to select the desired range 6 If desired select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or dow
133. plays 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 identitier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN FPightPlanning IMPORT A FLIGHT PLAN FROM AN SD CARD Sjueuinijsu 1uDi 3 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the MFD 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
134. r An error has occurred in transferring data has occurred between the two GMAs The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced GMA2 CONFIG GMA2 contig error Contig service req d MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The MANIFEST GMA 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 100 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN nnunciations amp Alerts GIA 63W MESSAGE ADVISORIES GIA1 CONFIG GIA1 config error Contig service req d GIA2 CONFIG GIA2 config error Contig service req d GIA1 CONFIG GIA1 audio contig error Contig service req d GIA2 CONFIG GIA2 audio config error Contig service req d COM1 CONFIG COM config error Contig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system
135. r the Socata TBM 850 9 sjuauinajsu E solv uoneJjedo SoJnjeoJ 92uepioAy SoJnpo 0Jd Duiuue d ACN Sd5 SAV oipny uaddx junuuy Jeuuouqy Jeuonippy 614 Wi0 gt AeN xipueddy xepu 1ubi 4 puezey Flight Instruments Nav Com Abnormal Additional Hazard Flight Planning Annun 2 3 lt cc ea A gt AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Engine amp Airframe Systems GARMIN GENERAL SYSTEMS 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the GEN Softkey to display the Fuel System Page The General Synoptics Page aircraft diagram displays open doors in red CAS messages also generated Statuses of propeller stall sensor heater pitot probe and windshield heat are also indicated on the diagram White indicates that heat is off propeller and windshield Light blue indicates heat has been selected windshield Green indicates heat is on e Yellow indicates heat has failed propeller pitot tube and stall sensor CABIN PRESS TRK SYSTEM GENERAL ALT FT RATE FPH 1000 OXY PSI w NUT L FUEL QTY R USG 122 OIL PSI ELECTRICAL AMPS ul EE OIL C eee c FUEL General Synoptics Page 10 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR Audio Panel ENTER OR CHANGE FLIGHT ID OPTIONAL 1
136. ra SS 55 Terrain Awareness amp Warning System TAWS B Display 57 Airborne Color Weather Radar 59 I Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMIN Table of Contents ADDITIONAL FEATURES sss 63 Synthetic Vision nennen 63 Terminal Procedure Charts ssssssseeeennnn 64 AOPA Airport Directory sssssseeeeeeen tente 66 SiriusXM Satellite Radio Entertainment ssss 67 Satellite Telephone amp SMS Messaging Service 69 ABNORMAL OPERATION 81 Reversionary Mode sssssseeeeeenen eren 81 Abnormal COM Operation sse 81 Hazard Displays with Loss of GPS Position 81 Unusual Attitudes 82 Dead Reckoning 83 ANNUNCIATIONS amp ALERTS 85 CAS INS SA CS s 85 Comparator Annunciations sssssssseeeee eene 88 Reversionary Sensor Annunciations sssssseeeeeeee 88 PS ce lg Cee ee ee E eee 89 Terrain SVS ATGDESS ccc concevcnnsrtoeonscomuuecamanseonnaeonnieeannannsemonmoeuyanenmuannbaien 90 Terrain SVS System Status Annunciations sss 91 TAW S B AITTE 92 Voce 94 MFD a
137. ransponder Code 12 Selecting a COM Radio css cers resrccestcococaseromaaeaeomsenuan EODD NEUE 12 Selecting a NAV Radio 12 NAV COM Tuning eis EMIUIERIUISISEDUNNSEIUE CBE RUBIEEUBUATEREUNUANERURURUERRURUARE HERI RERUM 12 lucu e 13 Passenger Address PA System 13 Clearance Recorder and Player ssssssse 13 AUTOMATIC FLIGHT CONTROL SYSTEM 15 Flight Director Activation sssssssseeeennenn 15 Vertical Modes eter odi mede tem dein dU HT d UE 16 Lateral MOSS coo entr EM MU GU NE M EEEEE 17 GPS NAVIGATION nois Den eR ERmU CHEM DM MU DU LN MUS 19 Direct to Navigation 19 Activate a Stored Flight Plan 20 Activate a Flight Plan Leg sssssssseeeeeeennn 20 Stop Navigating a Flight Plan 21 Vertical Navigation VNAV ssssssseeeeeeen eene 21 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Table of Contents GARMIN FLIGHT PLANNING ssssnn 23 Weight Planning tentent 23 Trip Planning 23 Create a User Waypoint Defined by Latitude amp Longitude 25 Create a User Waypoint Defined by Radials from Other Waypoints 26 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 28 Delete a User Waypoint sssssssssseeeeeeneenn 29 Create a Flight PAI m m 30
138. red airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN _ Sst Planning INVERT AN ACTIVE FLIGHT PLAN UDUWINI SU 34fi 4 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 oipny uadx Sv3 JUI0 AeN S 1V 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor AEN Sd5 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 c 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 ag D ts a UEPIOAY SoJnpa20Jd puezey SoJnjeoJ Jeuonippy 3 Press the CLR Key t
139. rees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees AVG eee fm No data from one or both altitude sensors PSOE No data from one or both airspeed sensors TPLCM ORG 0 No data from one or both heading sensors rM No data trom one or both pitch sensors SUM LOEO MM No data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Condition Sensor Window Text Both PFDs are displaying data from the number one Air Data Computer Both PFDs are displaying data from the number two Air Data Computer Both PFDs are displaying data from the number one Attitude amp Heading Reference System Both PFDs are displaying data from the number two Attitude amp Heading Reference System Both PFDs are displaying data from the number one GPS receiver Both PFDs are displaying data from the number two GPS receiver Index PFD2 is displaying data from the 1 Air Data Computer PFD1 is displaying data from the 2 Air Data Computer PFD2 is displaying data trom the 1 AHRS Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A 88 A GARMIN Reversionary Sensor Window Text AFCS ALERTS PFD1 is displaying data from the 2 AHRS PFD2 is displaying data from the 1 GPS PFD1 is displaying data from the 2 GPS Alert Condition Annunciation Description Rudder Mistrim Right Rudder Mistrim Left Aileron Mistrim Right Yaw
140. res S ou 5s 2 BB 2p e LL lt x Appendix Alerts Operation Index A Additional Features CG ARMIN 10 Press the MENU Key to display the Page Menu 11 Turn either FMS Knob to place the cursor on Stop Editing Predetined Message 12 Press the ENT Key Send a Predefined Text Message 1 2 3 4 6 7 8 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the alphanumeric keys on the controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Press the PREDEFD Softkey The PREDEFINED MESSAGE MENU Window is displayed Press the ENT Key The predefined message text is inserted into the message field If desired the message can be edited by using the FMS Knobs Press the ENT Key Press the SEND Softkey to transmit the message Text Message Boxes Received text messages reside in the Inbox as Read or Unread messages The Outbox contains Sent
141. rmin Flight Data Service Registration window proceed to step 7 Otherwise press the MENU Key The Page Menu window is now displayed 5 Turn the large FMS Knob to select Register With GFDS in the menu list 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 45 AEN Sd5 S241V oipny duadx SV3 sjueuinjsu Wi0 AeN yyb14 Puruuejd oE 2uepIony SoJnpa20Jd puezey sue v uonejodo soJnjeoJ unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com Flight GPS Nav AFCS XPDR Audio EAS Instruments Flight Planning Hazard Avoidance Procedures Annun Abnormal Additional Alerts Operation Features Appendix Index Hazard Avoidance GARMI N 6 Press the ENT Key The Garmin Flight Data Service Registration window is now displayed 7 Enter the access code provided by Garmin Flight Data Services in the ACCESS CODE field 8 Press the ENT Key REGISTER will now be highlighted 9 Press the ENT Key The system will contact Garmin Flight Data Services System registration is complete when REGISTERED is displayed in the STATUS field Accessing GFDS Worldwide Weather Products Weather data is provided when the pilot initiates either a manual or automatic GFDS data request on the GFDS Weather Data Link Page on the MFD No weather data is displayed until the first GFDS Weather Data Request is made 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob
142. rrent aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY WARNING The TAWS B display shows supplemental information only It should not be used for navigation A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Turn 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 360 Softkey to return to the 360 default display 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 37 AEN Sd5 S241V oipny dadx SVJ U9UINJ SU Wi0 AeN yyb14 Puruuejd oE a UePIOAY SoJnpa20Jd puezey sue v uonejedo soJnjeaJ unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annu
143. rrival 5 Press the ENT Key A list of transitions is displayed for the selected arrival 6 Turn either FMS Knob to select the desired transition 7 Press the ENT Key A list of runways may be displayed for the selected arrival 8 Turn the large FMS Knob to highlight the desired runway 9 Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan Nav Com Flight XPDR Audio EAS Instruments AFCS ACTIVATE AN ARRIVAL LEG GPS Nav 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key Flight Planning 4 o E S 7 o ie A Hazard Avoidance LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 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 Additional Features Abnormal Operation 1 Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH 3 Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach
144. rt PIREPs Temporary Flight Restrictions TFRs Terminal Aerodrome Reports TAFs Hazard Avoidance Expiration Time Minutes Refresh Rate Minutes Europe 15 UO Continuous Nn lt c Uo Continuous Continuous Continuous Continuous no product image Continuous Continuous i pma no product image The composite precipitation image is updated every 3 minutes but individual radar sites may take between 3 and 10 minutes to provide new data Setting Up and Customizing the GFDS Weather Data Link Page 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With Weather Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON OFF range settings etc 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 U S Canada 3 AeN Sd5 S241V oipny duadx Sv3 sjueuinajsu Wi0 AeN yyb14 Duiuue d 1461 4 a UEPIOAY SoJnpa20Jd pyezeH sue v uone1odo soJnjeo unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features
145. rt in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen terminal 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 Ihe FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function buiuue d AEN Sd5 S24V oipny uadx svi sjueuinaj
146. s displayed as shown in the following figure Uploading GRS1 Mag Var Database STARTING UPLOAD B E Uploading Database to GRS1 2 When the upload is complete the prompt for the next GRS upload is displayed as seen in the following figure 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 129 soJnjeaJ e uepioAy SoJnpa20Jg Duiuue d ACN Sd5 jJV oipny uadx svi sjueuingjsu jeuonippy p1ezeH ufi UI0 AEN ui uoneJjedo Jeuuouqv sue v unuuy xopu xipueddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix CTC GARMIN 130 GRS2 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use Uploading GRSZ Mag Var Database STARTING UPLOAD nisi Uploading Database to GRS2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN A Activate a flight plan 20 Active Channel 67 Active database 127 Active Navigation Database 126 ADF 11 12 82 AHRS 88 89 105 106 107 109 119 129 Airport Signs 63 64 Airways 124 Air Data Computer 88 Alert messages 108
147. s failed The G1000 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS intormation Check AFMS limitations The G1000 system should be serviced The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced The 2 AHRS is not receiving backup GPS information The G1000 system should be serviced The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced The 2 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced The 1 AHRS and 2 AHRS magnetic model database versions do not match The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid 190 00708 04 Rev A A GARMIN Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES CONT MANIFEST GRS1 software The 1 AHRS has incorrect software installed mismatch communication halted The G1000 system should be serviced MANIFEST GRS2 software The 2 AHRS has incorrect software installed mismatch communication halted The G1000 system should be serviced GMU 44
148. 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 WX Satellite 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 SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 43 AEN Sd5 S241V oipny dadx SVJ U9UINI SU Wi0 AeN yyb14 Duiuue d iui e2uepioAy SoJnpa20Jd puezey sue v uoneJjedo S9JnjeaJ unuuy Jeuuouqy Jeuonippy xipueddy xepu Nav Com Flight GPS Nav AFCS XPDR Audio EAS Instruments Flight Planning Hazard Avoidance Procedures Annun Abnormal Additional Alerts Operation Features Appendix Index Hazard Avoidance GARMI N 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 displa
149. servo providing sustained force in the indicated direction Aircraft rudder retrim after substantial pitch and power changes required Aileron Mistrim Lett Elevator Mistrim Down Roll servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure or stuck MEPT Switch Yaw Trim Failure or stuck MEYT Switch Yaw Damper Failure Roll Failure Pitch Failure System Failure 190 00708 04 Rev A Pitch servo providing sustained force in the indicated direction May indicate a failure of the pitch trim servo or trim system If AP engaged take control of the aircraft and disengage AP If AP disengaged move MEPT switches separately to unstick If AP engaged take control of the aircraft and disengage AP RM TRM If AP disengaged move the MEYT switch to check if a stuck switch is causing the annunciation H OL ui eem 8m AFCS Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 89 Annunciations amp Alerts SoJnjeoJ 92uepioAy SoJnpo 0Jd Duiuue d ACN Sd5 SAV oipny uddx SV3 SjueuinJjsu pezeH 614 U0 AeN jeuonippv uonejedo jeunouqy x pul 4f1 4 Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ Ammundatons amp Alets GARMIN Her Condition Performing preflight system test aural alert sounds at completion Do n
150. sfer time either minutes or seconds If desired the GFDS Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background GFDS Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength The system retrieves all available Worldwide Weather products within the selected coverage area during an initial GFDS Data Request regardless of which products Gf any are currently enabled for display On subsequent requests previously retrieved textual data such as METARs and TAFS is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request If the system cannot complete a GFDS weather data request one or more messages will appear in the request status window as indicated in the following table Weather Request Description Status Message Auto requests inhibited The system has disabled automatic weather data requests due to Send manual request excessive errors Automatic weather data requests have stopped Send a to reset manual weather data request to resume automatic updates Auto update retry The system will attempt another automatic weather data request after an Seconds error occurred during the previous request Timer counts down until the next auto
151. should be serviced The system has detected a failure in COM1 and or COM2 COM and or COM2 may still be usable The G1000 system should be serviced when possible 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 00708 04 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT COM1 RMT XFR COM1 remote The COM and or COM2 transfer switch is stuck transter key is stuck in the enabled or pressed position Press the COM2 RMT XFR CON remote transfer switch again to cycle its operation It transfer key is stuck the problem persists the G1000 system should be serviced LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase with other NAVS of flight GPS NAV LOST Loss of GPS Loss of GPS navigation due to insufficient navigation Insufficient satellites satellites a NAY pe Loss of GPS navigation due to GPS failure navigation GPS fail POSAT AET Ge Abort approach due to loss of GPS navigation navigation Abort approach APR DWNGRADE Approach Vertical guidance generated by SBAS is downgraded unavailable use LNAV only minimums TRUE APR True north approach Displayed after passing the first waypoint of a Change HDG reference to TRUE true north approach
152. should be serviced The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced The COM1 and or COM2 configuration settings do not match backup configuration memory The ndn EUIS UE config system should be serviced error Contig service req d GIA1 COOLING GIA1 The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature temperature too low GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted A GIA mismatch has been detected where only HW MISMATCH GIA hardware one is SBAS capable mismatch GIA2 communication halted The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 101 s n e j 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 S 4V oipny YddX SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uoneJjedo jeunouqy 12 p xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnorm
153. splay 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 66 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 intormation is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features SIRIUSXM SATELLITE RADIO ENTERTAINMENT SjueuinjJjsu 4614 The XM Radio Page provides information and control of the audio entertainment features of the SirtusXM Satellite Radio Selecting the XM Rad
154. su ui JU0 AEN ui SoJnpo 20Jd a UEPIOAY puezey gt a Q zi E D 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 x pu ddy sue v uoneJjedo unuuy jeunouqy Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 65 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Abnormal Annun EAS AFCS GPS Nav Procedures Avoidance S ou 5s 2 BB 2p e LL lt x Appendix Alerts Operation Index A Additional Features CG ARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to di
155. the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the HRZN HDG Softkey Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 2 3 4 5 Press the PFD Softkey Press the SYN VIS Softkey If not already enabled press the SYN TERR Softkey Press the APTSIGNS Softkey 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 64 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Additional Features 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 airpo
156. tivate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option trom 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 Socata TBM 850 190 00708 04 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 SV3 sjuauing
157. to select the GFDS Weather Data Link Page When a weather product is selected for display on the GFDS Weather Data Link Page a box containing a symbol for the product and its age in minutes are shown in the upper right If weather data has not been requested N A is shown next to the product symbol instead of age The age of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time Weather products are updated continuously or refreshed at specific intervals defined in the Refresh Rate column in the following table If for any reason a weather product is not refreshed within the defined Expiration Time intervals the data is considered expired and is removed from the display The age of the expired product is replaced by dashes If more than half of the expiration time has elapsed the color of the product age readout changes to yellow The refresh rate represents the interval at which the GFDS servers make available the most current known weather data It does not necessarily represent the rate at which new content is received from weather sources 46 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN Weather Product Radar Precipitation PRECIP Infrared Satellite IR SAT Datalink Lightning DL LING SIGMETs AIRMETs SIG AIR Meteorological Aerodrome Report METARs Winds Aloft WIND Pilot Weather Repo
158. ts 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 LOADING UPDATED DATABASES tenance being required to reboot the system SYSTEM STATUS Page In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system 4 CAUTION Never disconnect power to the system when loading a database Power interuption during the database loading process could result in main A NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX 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 SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH ui JU05 AEN i jeuonippv uoneJjedo jeuuouqv followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs
159. uidance Small Text Altitude is not Altitude is designated for The system cannot designated to be used use in giving vertical flight use this altitude in in determining vertical path guidance Altitude determining vertical flight path guidance has been retrieved from flight path guidance Altitude has been the navigation database retrieved from the or has been entered by navigation database the pilot and matches a and is provided as a published altitude in the reference navigation database 22 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A A GARMIN WEIGHT PLANNING Flight Planning FLIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters The Weight Planning 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 Turn the large FM
160. uonejedo jeunouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor Should be serviced cooling Reducing power usage PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck CNFG MODULE PFD1 configuration module is inoperative PFD1 VOLTAGE PFD1 has low A GARMIN The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced voltage Reducing power usage should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage should be serviced DATABASE MESSAGE ADVISORIES MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists 96 G
161. urn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 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 1 2 3 Select the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 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 Toremove the window press the CLR Key or the TMR REF Softkey m gt n SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE oipny uadx Wwo gt AeN 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 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 AEN Sd5 S dV Puruuejd oE MANUALLY TESTING THE RADAR ALTIMETER KRA 405B
162. urn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key S 1V AEN Sd5 ag D 5 Cs 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 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 SoJnjeoJ a UEPIOAY SoJnpa20Jd Jeuonippy puezey uonejedo Jeuuouqv sue v unuuy GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan xipueddy xepu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 35 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts
163. v unuuy xipueddy xopu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 2 3 4 5 6 7 8 9 Press the Direct to fff Key on the MFD Control Unit Enter the waypoint identifier Press the ENT Key to confirm the identifier The Activate field is highlighted If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 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 9 Turn the small FMS Knob to select MSL or AGL 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 2 3 4 5 6 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 19 Press the Direct to Key E on the PFD or controller Turn the large FMS Knob to place the cursor in the desired selection field Turn the small FMS Knob to begin selecting the desired ide
164. when the nav angle is set to AUTO Mi ips pid B O Loss of GPS navigation due to position error navigation Position error GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair 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 GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 103 SoJnjeoJ 92uepioAy SoJnpo20Jd Duiuue d NEN Sd5 4JV oipny 4adx SV3 sjueuinajsu paezey yi JU0 AEN yi jeuonippv uonejedo jeunouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LJ A Annunciations amp Alerts GARMIN GIA 63W MESSAGE ADVISORIES CONT NAV1 RMT XFR NAV1 remote The remote NAV1 and or NAV2 transfer switch transfer key is stuck is stuck in the enabled or pressed state NAV2 RMT XFR NAV2 remote Press the transfer switch again to cycle its transfer key is stuck operation If the problem persists the G1000 system should be serviced G S1
165. x MFD SOFTKEY MAP optional optional SjueuinJjsu 1uDi 3 A Vu DCLTR 1 SV3 ry DCLTR 2 gt lt v zZ ERES Select the BACK Softkey onthislevel 3 2 optional optional to return to the top softkey level Bo 5 3 PRECIP DL LTNG es PRECIP DL cro S optional Or Or optional optional oe FI FC C3 3 UN CA S 1V AEN Sd5 sverev oes Jp we J JE se J 9c Jp ses JL ee Fir ckCu 95x son n n oss n n PA F MFD Softkeys E Levell Level 2 Description 3 SYSTEM Enables the Synoptics Page softkeys ELEC Selects the Electrical Synoptics Page e uepioAy puezey FUEL Selects the Fuel Synoptics Page GEN Selects the General Synoptics Page SoJnjeoJ Jeuonippy CAS Displays the up and down scrolling softkeys CAS 1 Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling uoneJjedo Jeuuouqv CAS 4 Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling sue v junuuy MAP Enables second level Navigation Map softkeys gt ke D x TRAFFIC Displays traffic information on Navigation Map PROFILE Displays removes Profile View on Navigation Map Page Xapu 190 00708 04 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 123 A GARMIN Additional Hazard Fl
166. y the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols cou Description Status Icons P us C1 NEXRAD Available for the US and Canada The age of the displayed data CN TT for each is shown at the right 5 ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed 12 CLOUD TOP The age of the displayed data is shown at the right Not T displayed when ECHO TOP is displayed i an XM LIGHTNING The age of the displayed data is shown at the right 4 3 CELL MOVEMENT The age of the displayed data is shown at the right zT Eu 1 SIGMET amp AIRMET The age of the displayed data for each is shown at the AIRMET 5m lliyi i SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom T us Tiny METAR Available for the US and Canada The age of the displayed data for CN Em US sf WINDS ALOFT Available for the US and Canada The age of the displayed NN Pa data for each is shown at the right The altitude selection is shown at the 3000FT bottom COUNTY WARNING The age of the displayed data is shown at the right 44 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 04 Rev A GARMI N LLL

Garmin Software Version 0719.09 Cockpit Reference Guide

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