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Garmin Software Version 0719.12 Cockpit Reference Guide

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1. nn 51 Customizing the Hazard Displays on the Navigation Map 51 STORMSCOPE Optional cccccscccssssssssscssssssssssscsssssssssscesssssssssecessssssssseesansnsssnsess 51 SiriusXM Weather Optional sss 53 Garmin Connext Weather sss 55 Traffic Systems ntt 63 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN table of Contents Terrain And Obstacle Proximity sssssssseens 65 Tertaln SVT 0 000 00 aban WI OI A E 65 Terrain Awareness amp Warning System TAWS B Display 67 Airborne Color Weather Radar 69 ADDITIONAL n Synthetic VISIOn eee ete terne inier be er ien er i Terminal Procedure Charts Airport Directory eae noster be i e s s SiriusXM Satellite Radio Entertainment Satellite Telephone amp SMS Messaging Service Maintenance Logs Auxiliary Video Optional sssseenennnnnnnn Scheduler Pilot Profiles eei tede te aate e n bent bend ABNORMAL OPERATION Reversionary Abnormal COM Operation Hazard Displays with Loss of GPS Position Unusual Attitudes senten Dead Reckonihg
2. Alert Type Ed c TAWS B Page Annunciation Surat Annunciation Message TAWS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid TAWS operating None None with PFD Terrain or Obstacle databases TAWS B System Test Fail FAWS FAIL Terrain or Obstacle database unavailable or u invalid invalid software TAMS FAIL 77 configuration system audio fault TAWS Not 0 GPS position TAMS N A Available Excessively degraded GPS u signal Out of database TAWS N A None Mo coverage area Sufficient GPS signal None None TAWS received after loss Available 112 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN VOICE ALERTS Annunciations amp Alerts Voice Alert Description 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 Incoming Call Satellite telephone is receiving a call ATC Message ew Data Link message received from ATC Traffic ayed when a Traffic Advisory TA is issued with the TIS system Traffic Not Available he aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic TAS System Test
3. WARNING Do not use the indicated data link weather product age to deter mine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age WARNING Do not rely on information from the lightning detection system display as the sole basis for hazard weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to the documentation from the lightning detection system manufacturer for detailed information about the system WARNING The system as installed in the TBM 850 900 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 system 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 system operational procedures must be learned on the ground WARNING The United States government operates the Global Positio
4. s 21 Flight Director Activation 21 Vertical Modes nnne 22 Lateral Modes usus octets ot b RE eb dd 23 GPS NAVIGATION fice a kl idet 25 Direct to Navigation sssssssseseeeeneen nnne 25 Activate a Stored Flight Plan 26 Activate a Flight Plan Leg 26 Stop Navigating a Flight 7 55 2 Vertical Navigation VNAV sssssseeennt nnne 27 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 Table of Contents GARMIN FLIGHT PLANNING ab aa a Aa 29 Weight Plannirig 3 uode uo Bhd Adana Heads edt deiude 29 Trip Plannilig teet iie tat dns 29 Create a User Waypoint Defined by Latitude amp Longitude 31 Create a User Waypoint Defined by Radials from Other Waypoints 32 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 34 Delete a User Waypoint ssssssseeeee nnn Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan Enter an Airway in a Flight Plan Creating a User Defined Hold at an Active Flight Plan Vaypoint
5. 5 Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Ahead Impact Caution ITI or or TERRAIN Caution Terrain Caution Terrain Reduced Required TERRAIN CAUTION OBsTACLE Caution Obstacle Caution Obstacle Clearance or Obstacle Caution ROC BHB a Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution or Ahead 0 i Caution Obstacle Caution Obstacle Premature Descent TERRAIN TOOLOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb OMERRAIN ME Dont sink Rate Caution or or NCR TOOLOW TERRAIN Too Low Terrain 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 111 s tin sul sub So1nje2J aoueplony s mp oold Buruue d AEN Sd5 yi oipny uadx paezey 3461 UI05 AeN jeuonippy uoneiedo Jeuuouqy 5 ia x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix n Annunciations amp Alerts A GARMIN TAWS B System Status Annunciations
6. WARNING Do not use outdated database information Databases used in the system must be updated regularly in order to ensure that the information remains current 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 Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide colli sion avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather condi tions 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A GARMIN
7. coo oon De Rn Gin Rd ed ede edad Configure Vspeed Bugs Set Barometric Radar Altimeter Minimum Descent Altitude 3 Manually Testing the Radar Altimeter KRA 405B only 3 Displaying Wind Data 4 Changing HSI Format 4 ENGINE amp AIRFRAME SYSTEMS 5 Electrical System eere et dete et tue tr tts 6 Fuel System tette iste e a ende nean 8 General Systems 3 cscs cscs se m een ee een eem etn e er alain ne 0 Cabin Pressurization sse 1 NAV COM TRANSPONDER AUDIO PANEL 3 Enter or Change Flight ID 5 75 3 ADF Tuning Optional sssseeennn tenen 3 DME Tuning Optional sse 3 Enter a Transponder Code sss 4 Selecting a COM Radio 4 Selecting 4 NAV COM Tuning 4 tita a 5 Controller Pilot Data Link Communications Optional 5 Passenger Address PA System 9 Clearance Recorder and Player 9 AUTOMATIC FLIGHT CONTROL SYSTEM
8. 39 Creating a User Defined Hold at the Aircraft Present Position 39 Removing a User Defined Hold Created at the Aircraft P POS 40 Removing a User Defined Hold Created at an Active Waypoint 40 Invert An Active Flight Plan 40 Remove a Departure Arrival Approach or Airway from a Flight Plan 41 Store a Flight Plan erre eret e eie ieri dede iles 41 Edit a Stored Flight Plan 41 Delete a Waypoint from the Flight Plan sss 42 Invert and Activate a Stored Flight 42 Copy a Flight Plan Delete a Flight Plan cere ee tenes Graphical Flight Plan Creation Export a Flight Plan to an SD Card ssss 44 PROCEDURES m Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure 46 Activate An Approach in the Active Flight Plan 4 Activate a Vector to Final Approach Fix 7 4 Activate A Missed Approach in the Active Flight Plan 48 Temperature Compensated Altitude ssssssssseeee 48 HAZARD AVOIDANCE
9. Deleting a Scheduler Message 1 Select the AU 2 Press the FM 3 Turn the large FMS Knob to highlight the name field of the scheduler X Utility Page S Knob momentarily to activate the flashing cursor message to be deleted 4 Press the CLR Key to clear the message text If the CLR Key is pressed again the message is restored 5 Press the ENT Key while the message line is cleared to clear the message text Scheduler messages appear in the Messages Window on the PFD When a scheduler message is waiting the MSG Softkey label flashes Selecting the MSG Softkey opens the Messages Window and acknowledges the scheduler message Selecting the M G Softkey again removes the Messages Window from the display and the scheduler message is deleted fro PILOT PROFILES m the message queue When the system is powered on the last selected pilot profile is shown on the MFD power up screen The system can store up to 25 profiles the currently active profile the amount of memory used and the amount of memory available are shown at the top of the AUX System Setup Page in the box labeled Pilot Profile Creating a Profil 1 Use the FMS 2 Press the FM 3 Turn the large FMS Knob to highlight CREATE in the Pilot Profile Box e Knob to select the AUX System Setup Page S Knob momentarily to activate the flashing cursor 4 Press the ENT Key A Create Profile window is displayed 5 Use the FMS Kno
10. Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees YR eee JE No data from one or both altitude sensors Smee Lam No data from one or both airspeed sensors hired eee No data from one or both heading sensors Jil OE ME No data from one or both pitch sensors 0 OE No data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Condition Sensor Window Text f Both PFDs are displaying data from the 1 Air Data Computer f Both PFDs are displaying data from the 2 Air Data Computer f Both PFDs are displaying data from the 1 Attitude amp Heading Reference System f Both PFDs are displaying data from the 2 Attitude amp Heading Reference System Both PFDs are displaying data from the 1 GPS receiver Both PFDs are displaying data from the 2 GPS receiver PFD2 is displaying data from the 1 Air Data Computer PFD1 is displaying data from the 2 Air Data Computer PFD2 is displaying data from the 1 AHRS PFD1 is displaying data from the 2 AHRS is displaying data from the 1 GPS PFD1 is displaying data from the 2 GPS 190 00708 05 Rev C Garmin G1000 Cockpit
11. Failure YD control failure AP also inoperative Roll Failure ROLL Roll axis control failure AP inoperative Pitch Failure PT CH Pitch axis control failure AP inoperative System Failure AFCS AP and MEPT are unavailable FD may still be available Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power up and preflight 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 PFT Preflight system test failed aural alert sounds at failure Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts TERRAIN SVT ALERTS PFD MFD Alert Type TERRAIN SVT MFD Aural yP Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Warning Terrain Clearance Warning RTC Terrain Imminent Terrain Impact TERRAIN Warning Terrain Warning ITI Terrain Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Warning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTTON TERRAIN Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN
12. toes teo aedem edere p ape Suspected Autopilot malfunction Overpowering Autopilot Servos ssssssssen e ANNUNCIATIONS amp ALERTS CAS Messages Comparator Annunciations sssssssseee enne Reversionary Sensor Annunciations sss AFCS Alerts Terrain SVT Alerts roit a ona d a LER D o daB Terrain SVT System Status Annunciations sse 09 TAWS B Alerts s s n s n Voice Alerts MFD amp PFD Message Advisories Database Message Advisories GMA 1347D Message Advisories GIA 63W Message Advisories GEA 71 Message Advisories sss GTX 33 33D Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories sssssssseeen ne GSR 56 Message Advisories ssssssssseeenne 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 l Table of Contents GARMIN GDR 66 VHF Data link Transceiver System Messages 127 GDL 69A Message Advisories ssssssssseeene 127 GWX 68 GWX 70 Alert Messages 128 GDC 74B Message Advisories 128 GCU 475 Message Advisories s s s s s s s s nne 129 GMC 710 Message Advisories
13. PRECIP Europe 15 Infrared Satellite IR SAT E a Datalink Lightning Er DL LING 30 Continuous SIGMETs AIRMETs SIGMET SIG AIR AIRMET a oipny uddx sv siu u nnsu Yid UI0JNeN 52 Meteorological Aerodrome Report METARs 90 Continuous AEN Sd5 Duruue d Pilot Weather Report PIREPs 90 Continuous Winds Aloft WIND 2202 60 Continuous Temporary Flight Restrictions no product image 60 Continuos TFRs Terminal Aerodrome Reports z TAs no product image 60 Continuous aoueploay s mp oold paezey 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 Connext Weather Data Link Page 1 Select the Connext 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 57 saunqea4 jeuonippy suelv uoneiedo junuuy Jeuuouqy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional
14. The text messaging user interface is mainly through the AUX TEXT MESSAGING Page 82 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Additional Features Viewing the Text Messaging Page 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 Description Received text message that has not been opened Received text message that has been opened Saved text message draft not sent System is sending text message Text message has been sent System failed to send text message Predefined text message 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 83 2 Buruuejd AeN Sd5 S24V olpny
15. XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 7 8 9 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 1 2 3 4 5 6 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the EN
16. sss 129 GTS 820 Message Advisories 130 Miscellaneous Message Advisories sss 130 Flight Plan Import Export Messages 135 APPENDIX ner OO i ea etia renee 137 PFD Softkey Map tete ero ed eerta 137 MFD Softkey reete ttr t ta ite rai 143 Updating Databases 145 INDEX TEACH Anco ate Aenea ae tats Index 1 iv Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE Press the BARO Knob CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window 4 Tum the small FMS Knob clockwise to ON or counterclockwise to OFF SYNCHRONIZE CDI 1 Select t
17. 8 9 A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 1 2 Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate ce
18. Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 7 8 A GARMIN Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Connext Weather Data Link Page with the changed settings Restoring Default Connext Weather Data Link Page Settings 1 2 3 4 5 Select the Connext Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired default s to restore all or for selection and press ENT Key Switching Between Connext and SiriusXM Weather Sources 1 2 3 4 Turn the large FMS Knob on the MFD to select the MAP page group Turn the small FMS Knob to select the desired Weather Data Link Page Press the MENU Key Turn the large FMS Knob to select Display Connext Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Legends for Displayed Connext Weather Products 1 2 3 4 Select the Connext 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 Wi
19. Enable Terrain While the Terrain SVT Page is displayed select the INHIBIT Softkey Or Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Hazard avoidance 1 While the Terrain SVT Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key NOTE If Terrain SVT alerts are inhibited when the Final Approach is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS B DISPLAY o WARNING The TAWS B display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south o 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 Tum the large FMS Knob to select the Map Page Group 2 Turn the sma
20. Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair Comments The PFD and or MFD self test has detected a problem The G1000 system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced PFD1 SOFTWARE PFD1 mismatch communication halted PFD2 SOFTWARE PFD2 mismatch communication halted MFD SOFTWARE MFD mismatch communication halted The specified GDU ha
21. METAR Displays METAR flags on airport symbols shown on the Inset Map optional non Ks r r ntu amp Rs1 AHRS2 l 1 8 c vss Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN o Appendix Level 1 Level2 Level3 Description 22 SENSOR Displays softkeys for selecting the 1 and 8 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer g ADC2 Selects the 2 Air Data Computer AHRSI Selects the 1 AHRS 52 AHRS2 Selects the 2 AHRS 3n 2 S Eu nm nx FE n owe 586 rsinin ence Caron roseo 3 LA F amp n n 8 Select the BACK Softkey to return to the top level softkeys Duruue d Wil s snp old Er um DU S S S E A 77 uu gt npmsmununnun ase CCC ees ss PFD Configuration Softkeys Sue v unuuy gt s o z m x x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 139 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 1 OPTN
22. 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 850 900 190 00708 05 Rev C GARMIN ight Planning 6 7 8 9 10 11 12 13 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by
23. Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status Barometric Minimum Box Descent Altitude Box Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position 100 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN X U Abnormal operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure 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
24. Sv3 U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 154 A GARMIN A Activate a flight plan 26 Active Channel 77 Active database 148 Active Navigation Database 148 ADF 13 14 100 AHRS 107 124 126 129 139 Airport Signs 73 74 Airways 144 Air Data Computer 107 Alert messages 128 ALT 64 Altimeter setting 1 100 Altitude mode 64 Altitude volume 64 Antenna stabilization 72 Antenna tilt 70 AOPA s Airport Directory 76 ATC 15 16 17 113 Attitude amp Heading Reference System 107 Audio panel controls NAV1 NAV2 14 Barometric Altitude Minimums 3 Battery Alerts 105 Current 5 Overheat warning 105 Voltage 5 Bearing line 70 71 C Cabin pressure altitude 5 11 Warning 105 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 Index CDI 1 2 14 132 Cell 51 52 Cell mode 52 Channel Presets 78 ChartView 74 75 Code selection softkeys 14 COM 14 99 CPDLC 15 18 127 144 D Data link communication 15 DB Mismatch 145 DCLTR Softkey 74 Dead Reckoning 100 Declutter 100 137 145 Designated altitudes 28 Differential cabin pressure 5 11 Warning 105 Direct to 25 DME 13 14 Door status 10 DR mode 100 102 E Edit a flig
25. The G1000 system should be serviced PFD1 BKLT CAL INV PFD1 bklt cal lost or mismatch Return for repair PFD2 BKLT CAL INV PFD2 bklt cal lost or mismatch Return for repair MFD BKLT CAL INV MFD bklt cal lost or mismatch Return for repair The specified GDU backlight calibration cannot be found or is invalid The system should be serviced DATABASE MESSAGE ADVISORIES Message MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists Comments The MFD and or PFD detected a fault in the navigation database Attempt to reload the navigation database If problem persists the G1000 system should be serviced 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 115 so1njeoJ 2 AEN Sd S24V olpny uqax svi syu unysu paezey ESTE nubi jeuonippy uoneiedo Jeuuouqy iA 8 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix ud Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 ba
26. Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the System Status Page 19 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 To manually activate the standby navigation database 1 From the AUX SYSTEM STATUS Page select the STANDBY DB Softkey 2 A prompt similar to the following figure below is displayed select Yes to overwrite the Active Navigation Database with the Standby Navigation Database Select No to cancel Are you sure you want to activate the standby nav database now This will overwrite the active nav database on the next power cycle VES Standby Nav Database Activation Confirmation Window 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 151 sjueuinasu Yid uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld APN Sd5 2 olpny uqax jeuuouqy jeuonippy paezey wd U105 AEN su jy unuuy L Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts A Appendix 0808080880 MUG ARMIN Loading the magnetic field variation database update A copy of the current magnetic field variation database MV DB is included wi
27. Wamingstamtonsw Notes GARMIN 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 clean ers 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 coat ings CAUTION The system does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the panel and displays are subject to change and may not reflect the most current system and databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harm ful 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 comple
28. aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 24 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to fJ Key on the MFD Control Unit 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter ana 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the des 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport Ititude constraint proceed to step 5 ired altitude proceed to step 9 8 Turn the smal 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the des FMS Knob to select MSL or AGL ired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation using the PFD 1 Press the Direct to Key E on the PFD or controller 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the de
29. 12 01 parameters 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 RR 1 A Record of Revisions GARMIN Change Summary 190 00708 05 Rev A Added TBM 900 Added Maintenance Log feature Added Auxiliary Video Added CPDLC Added AC U KWIK Airport Directory Added User Defined Holding Patterns Added Landing Field Elevation enty Added temperature compensated altitude Changed GFDS Weather to Connext Weather Changed XM to SiriusXM Changed Synthetic Vision System SVS to Synthetic Vision Technology SVT Added other GDU 14 01 parameters Updated Warnings Cautions and Notes Updated CAS Messages Added a Note to Flight Instruments Clerical k zi Date of Revision Affected Pages January 2015 Production Release RR 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN table of Contents vases chica te atit 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure ssssssssee 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synchronize CD isis sich see esie e a eT HART Change Navigation Sources Enable Disable OBS Mode While Navigating with 6 5 2 Generic Timer
30. 850 900 190 00708 05 Rev C A GARMIN Hazard Avoidance Wx Product Status Icons Description 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 21000FT TURBULENCE The age of the displayed data is shown at the right The altitude selection is shown at the bottom 4m BODOFT ICING POTENTIAL The age of the displayed data is shown at the right The altitude selection is shown at the bottom GARMIN CONNEXT WEATHER NOTE Garmin Connext Weather provides information for avoiding hazardous weather Do not utilize Connext Weather information to penetrate hazardous weather Registering the System to Receive Connext Weather When an account is established Garmin Connext 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 Connext or XM Page If XM is displayed in the page title it will be necessary to change the datalink source to Connext before continuing Refer to Viewing the Weather Data Link Page procedure to change the datalink source to C
31. AUX VIDEO Page displayed press the SETUP Softkey 2 Press the BRIGHT or BRIGHT to adjust display brightness in five percent increments from 0 to 100 3 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 100 4 Press the SAT or SAT to adjust display saturationin five percent increments from 0 to 100 5 If desired return the display to the default settings by pressing the RESET Softkey 6 Press the BACK Softkey to return to the previous softkey level Display Selection Pressing the HIDE MAP Softkey removes the map and displays video on the full screen The softkey label changes to grey with black characters Pressing the HIDE MAP Softkey again restores the map view and the small video image The softkey label returns to white characters on a black background Input Selection While on the AUX VIDEO Page press the INPUT Softkey to select the video source Zoom Range Pressing the VID ZM or VID ZM Softkeys increases or decreases video display magnification between 1x and 10x The Joystick can be used to increase or decrease the range setting on the map display or zoom in and out on the video display While in the Split Screen mode pressing the MAP ACTV or VID ACTV Softkey determines which display the Joystick adjusts Pressing the softkey to display MAP ACTV allows the Joystick to control the range setting of the map display Pressing the softkey to display VID ACTV
32. Cruise l engine trend data log has been captured EXCEEDANCE Engine exceedance data is being logged An engine exceedance log has been captured REGISTER CONNEXT Data services are inoperative register w Connext The system is not registered with Garmin Connext or its current registration data has failed authentication Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User waypoints imported success fully No stored flight plan data was modified The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified o flight plan files found to import Flight plan import failed The SD card contains no flight plan data us 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 e
33. Display Reversionary Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 Sjueumasu Sue v uonejedo Sonje2J SoJnpa20Jd Buruue d AEN Sd5 yi olpny uqax junuuy jeuuouqy jeuonippy JUI0 AEN xipuaddy xe pul 3461 Wfl 2 2 x SE 2s iz 2 2 Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Engine amp Airframe Systems GARMIN ELECTRICAL SYSTEM 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the ELEC Softkey to display the Electrical System Page CABIN PRESS us ALT FT RATE FP x L FUEL OTY R usi 125 N 100 73 6 I 4 so L vi gt s OIL PSI DPH p rst ELECTRICAL enn BUS 1 BUS 2 BUSS BUS 4 655 BUS BUS OIL 5 C9009 Standby Generator Battery Battery Bus Main Generator G Main Bus Essential Bus 0 Ground Power 5 Emergency Switch Power Buses Unit Door Electrical Synoptics Page 6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C d GARMIN Engine x AlHr me 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 c
34. Flight Instruments section of the Pilots Guide for more information on situations where this might occur 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 Turn 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN __Flight instruments CONFIGURE VSPEED BUGS 1 Select the TMR REF Softkey 2 Turn the large FMS Knob to highlight the desired Vspeed 3 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 H 4 Press the ENT Key or tu
35. Guide for the Socata TBM 850 900 61 Buruue d ARN Sd5 52 olpny uqax sv siu umnnsul s snp old gt 4 s a m 5 a o saunqee4 jeuonippy Suelv uoneiedo junuuy Jeuuouqy xipuaddy x pul iui uo2 AEN nu 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 A GARMIN Cancelling a Connext Weather Data Request in Progress 1 2 3 4 5 Select the Connext Weather Data Link Page Press the MENU Key With Connext 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 Connext Weather Datalink Page Enabling Automatic Connext Data Requests 1 2 3 4 5 6 Select the Connext Weather Data Link Page Press the MENU Key With Connext 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 frequency 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
36. If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Flight Planning Or a Turn the small FMS Knob to the left Initially a flight plan wayp
37. Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old KJ Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 5 AEN Sd5 S24V oipny dadx sv4 Sjueuinsu wio gt AeN yw Duruue d Wil uep ony s mp oold paezey Sue v uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 5 6 7
38. REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate Connext Data Request Or Press the FMS Knob to return to the Connext Weather Data Link Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Hazara avoidance TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory 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 O Traffic Advisory TA dosing rate distance and vertical separation meet TA citeria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERAT
39. Reference Guide for the Socata TBM 850 900 107 saunqea4 eouepioAy s mp oold Buruue d AEN Sd5 S24JV oipny uddx svi Sjueumasu jeuonippyv uoneiedo jeuuouqv x pul iui JUI05 AEN nu paezey ka Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix z Annunciations amp Alerts A GARMIN AFCS ALERTS Alert Condition Annunciation Description Rudder Mistrim Right RUD Yaw servo providing sustained force in the indicated Rudder Mistri direction Aircraft rudder retrim after substantial pitch and ph Sium RUD power changes required Aileron Mistrim AIL Right AIL Roll servo providing sustained force in the indicated Aileron Mistrim direction AIL Elevator Mistri is 77 VELE Pitch servo providing sustained force in the indicated own 57 E NV B Misti direction May indicate a failure of the pitch trim servo or strim TELE trim system Pitch Trim Failure If AP engaged take control of the aircraft and disengage AP or stuck MEPT PT RM If AP disengaged move MEPT switches separately to Switch unstick Yaw Trim Failure If AP engaged take control of the aircraft and disengage AP or stuck MEYT Y T RM If AP disengaged move the MEYT switch to check if a stuck Switch switch is causing the annunciation Yaw Damper ae
40. Select the EXPORT Softkey The system displays the Pilot Profile Exporting Window To export the pilot profile using the current supplied name press the ENT Key with EXPORT highlighted To change the profile file name turn the large FMS Knob to highlight the SELECT FILE field then enter the new name with the large and small FMS Knobs then press the ENT Key Then press the ENT Key with EXPORT highlighted Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Additional Features 6 If the profile name to be exported is the same as an existing profile file name on the SD card the system displays an Overwrite existing file OK or CANCEL prompt Press the ENT Key to replace the profile on the SD card with the profile to be exported or turn the FMS Knob to highlight CANCEL and press the ENT Key to return to the Pilot Profile Exporting Window without exporting the profile 7 If successful the EXPORT RESULTS window displays Pilot profile export succeeded With OK highlighted press the ENT or CLR Keys or press the FMS Knob to return to the AUX System Setup Page 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 97 sjuauimasu Yid SoJnpa20Jd Duruue d APN Sd5 241V oipny uadx 3461 Tu102 AEN eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul GARMIN itional Features Add sjueuinij
41. TEXT MESSAGING AUX REPORT STATUS and AUX WI FI SETUP Pages Registering System With Garmin 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 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 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 9
42. Tum the large FMS Knob to select the Map Page Group 2 Turn the smal FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed 5 Turn the Joystick to select the desired range 6 If desired sel 190 00708 05 Rev C ect the VERTICAL Softkey for vertical scanning Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 69 xipuaddy suelv uoneiedo SaJnjeaJ uep ony 2 Duruue d AEN Sd5 24JV olpny uqax sv sjuauimnasu unuuy Jeuuouqy Jeuonippy paezey ulu U10 AEN iui x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Adjusting Antenna Tilt While viewing weather radar on the Weather Radar Page or the Navigation Map Page moving the Joystick up or down adjusts the tilt of the antenna up or down Monitor the displayed tilt value in the TILT field Wh
43. WGS84 waypoint Stormscope has failed The system should be serviced TRAFFIC FAIL Traffic device has failed The is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVT SVT DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVT SVT DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card Selected course for LOC2 differs from published localizer course by more than 10 degrees The SD card
44. erature compensated altitude 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed 4 Press the ENT Key CANCEL COMPENSATION is highlighted 5 Press the ENT Key The temperature compensated altitude at the FAF is cancelled 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 49 ACN Sd5 S24V oipny uadx sv4 syuauuni su u102 AEN Duruue d nubi s mp olqd aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Procedures Ssjueuinijsu fila 593 U105 AEN s24v AeN Sd5 buluueld Blank Page um aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 50 GARMIN Hazara avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the
45. has been The system cannot use this altitude in determining vertical flight path guidance 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 1 path guidance Altitude 1 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 28 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C 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 des 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enter the des ired aircraft empty weight ired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights ha
46. large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Connext Weather Data Link Page When a weather product is selected for display on the Connext Weather Data Link 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 Connext 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 56 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN H zadavoidance Expiration Weather Product Symbol Time 55 Rate Minutes Minutes Radar Precipitation 4 4 U S Canada 3
47. ony s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Display Terrain on the TERRAIN SVT Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVT 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 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVT 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 SVT Inhibit Inhibit Terrain While the Terrain SVT 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
48. seen wait for the system to finish loading before proceeding to step 5 146 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN 5 Acknowledge the Power up Page agreement by pressing the ENT Key or Appendix the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the smal FMS Knob to select the System Status Page 8 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed 9 Remove and reapply power to the system 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the smal FMS Knob to select the System Status Page 12 Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display Updating Terrain FliteCharts and ChartView Databases 1 With system power OFF remove the Supplemental Data Card from the bottom card slot of the MFD and PFD 2 Copy the updated terrain database to both Supplemental Data Cards Copy the updated FliteCharts or ChartView database to one Supplemental Data Card 3 Insert the updated Supplemental Data Cards into the bottom card slot of the MFD and PFD The Supplemental Data Card containing the FliteCharts or ChartView 4 Apply power to the sy
49. still be avail GMA2 SERVICE GMA needs able and the audio panel may still be usable The service Return unit for repair G1000 system should be serviced when practical 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 119 saunqea4 2 Buruuejd AEN 5649 24V oipny uadx sv3 syu unysu paezey nubi wi0 gt AeN nubi jeuonippy uoneiedo Jeuuouqy cA p x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES A GARMIN Message GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d Comments The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced COM1 CONFIG COM config error Config service req d COM2 CONFIG COM config error Config service req d The COM1 and or COM2 configuration settings do not match backup configuration memory The system should be serviced GIA
50. the following coverage selections PRESENT POSITION Requests data based on current location e DESTINATION Requests data based on active flight plan destination if the flight plan contains no destination dashes are displayed e FPL Requests data based on active flight plan Tum the small FMS Knob to select the desired flight plan look ahead distance option or choose REMAINING FPL to request the remainder of the flight plan e WAYPOINT Requests data based on any valid waypoint 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 59 sjuauimasu Yid AN Sd5 2 oipny uadx JUI0JNeN Duruue d Wil uep ony s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field and turn the small FMS Knob to select the desired diameter and route width of the request then press the ENT Key 6 Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Connext Data Link Page without requesting data During a Connext Data R
51. the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 2 3 4 5 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 31 sjuaumasu nubi oipny uddx UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desir
52. turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN ight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a 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 Turn the large FMS Knob to select the desired waypoint d Press the ENT Ke
53. unit for repair G S2 SERVICE G S2 needs service Return unit for repair A fault has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when practical GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error Config service req d MANIFEST GEA1 software mismatch communication halted The GEA2 configuration settings do not match those of backup configuration memory The G1000 system should be serviced The 1 GEA 71 has incorrect software installed The G1000 system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The G1000 system should be serviced 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 123 soJnjeoJ 2 AEN Sd 24V olpny uqax sv siu un sul paezey nubi jeuonippy uoneiedo Jeuuouqy ic E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts
54. uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 6 a b d a b o d a b o d A GARMIN Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired user waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 4 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 waypoin
55. 00 17 s tin su sub 5 3 S24V oipny uddx JUI05 AEN uonesado saunqea4 2 4 AEN Sd junuuy jeuuouqy feuonippv paezey Wfila x pu ddy x pul Flight Instruments Nav Com AFCS XPDR Audio EAS Flight Planning Abnormal Additional Hazard Avoidance Annun Procedures GPS Nav Appendix Alerts Operation Features Index A Nav Com XPDR Audio Panel GARMIN Viewing CPDLC Message Dialogs The status of a string of messages or dialog may be checked and past message dialogs viewed When G1000 power is cycled the list of message dialogs is deleted To view messages 1 From the MFD select the CPDLC Softkey 2 Turn the large FMS Knob to place the selection cursor over the desired message to view and press the ENT Key 3 Press the ENT Key to view the CPDLC Thread Deleting Message Dialogs While the G1000 deletes the list of message dialogs when power is turned off individual message dialogs may also be deleted manually Message dialogs considered closed may also be deleted To delete a single message dialog 1 From the MFD select the CPDLC Softkey 2 Turn the large FMS Knob to place the selection cursor over the desired message to delete 3 Select the DELETE Softkey A confirmation window appears 4 Highlight OK and press the ENT Key To delete all closed message dialogs 1 From the MFD select the CPDLC Softkey 2 Select the DEL ALL
56. 00 79 sjueuimasu Yid SoJnpa20Jd Duruue d AEN Sd5 241V olpny uqax 3461 Tu102 AEN eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy x pul Additional Features GARMIN Internal External Phone Phone 0 Flight Instruments Phone is Idle EAS Phone is ringing Phone has a dial tone off hook or connected to another phone Phone dialed is busy Nav Com XPDR Audio AFCS GPS Nav Phone is dialing another phone Flight Planning Phone has failed Procedures Phone status not known Hazard Avoidance Phone is disabled Bu 289 e EE lt Phone is reserved for data transmission Abnormal Operation Annun Alerts Appendix Other phone is on hold Index EL Calling other phone or incoming call from other phone CELELILELIIT m Phones are connected 80 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Additional 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 Answering an incoming call 1 Press the TEL Key on the audio panel 2
57. 000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far GEO LIMITS AHRS2 too far North South no magnetic compass North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 125 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax sv sjueumasu puezey ubi UI05 AeN ubi jeuonippy uoneiedo Jeuuouqy a x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operat
58. 1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN GIA 63W MESSAGE ADVISORIES CONT Annunciations amp Alerts Message MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted Comments The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect MANIFEST COM1 software mismatch comm
59. 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 Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Appendix Level 1 Level 2 Level 3 Description BRG2 ALT UNIT METERS HPA STD BARO Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifi
60. 3 Selects desired amount of map detail eycles Sue v unuuy 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 5 o z m x x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 137 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix Level 1 Level2 Level 3 Description VVX LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC Cycles through traffic 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 information on Inset Map STRMSCP Displays Stormscope weather and coverage information on the Inset Map optional NEXRAD Displays NEXRAD weather and coverage T information on Inset Map optional PRECIP Displays Connext precipitation on Inset Map optional XM LTNG Displays SiriusXM lightning information on T Inset Map optional DL LING Displays Connext Worldwide Weather lightning information on Inset Map optional
61. A GARMIN GTX 33 33D MESSAGE ADVISORIES Message XPDR1 CONFIG XPDR1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when practical XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when practical XPDR1 FAIL XPDRT is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 sys
62. Altitude Flight Level Change Maintains the current aircraft airspeed HC mna IAS Hold in KIAS or Mach Number while the i 77 FLC Key Flight Level Change aircraft is climbing descending to the Mach Hold Selected Altitude VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target disp ayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath GP on approach Captures and tracks the ILS glideslope ej Glid slope aptures and tracks the ILS glideslope GS on approach Commands a preprogrammed constant Takeoff pitch attitude and wings level in TO preparation for takeoff GA Disengages the autopilot and Switch Go Around commands a constant preprogrammed GA pitch attitude and wings level ALTS armed automati is to be captured inste ALTV armed automatically under VPTH when VNAV Target Alti Selected Altitude 22 cally when PIT VS FLC or GA active and under VPTH w ad of VNAV Target Altitude en Selected Altitude ude is to be captured instead of Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN attitude and wings level AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls win
63. C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A Wamings Cautions amp H s GARMIN NOTE If the pilot operator wants or needs to adjust the database contact Garmin Product Support to coordinate the revised DQRs NOTE Garmin requests the flight crew report any observed discrepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to FlyGarmin com and select Report An Aviation Data Error Report Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Fesorif keis Part Number Change Summary 190 00708 00 Initial Release 190 00708 01 RevA Added SVS and other GDU 9 02 parameters Rev B Clerical changes 190 00708 02 1 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
64. CAUTTON TERRAIN 1 Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRAIN 1 CAUTION ossractE Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRAIN 1 CAUTION OBSTACLE Caution Obstacle Caution 101 Obstacle TERRAIN SVT SYSTEM STATUS ANNUNCIATIONS Terrain SVT operating with PFD Terrain or Obstacle databases Alert Type rE MEDA ert RENTUR Ur Message Annunciation Annunciation rogress System Test Pass None None Terrain System y Test OK Terrain Alerting is disabled TER INH Done None MED Terrain or Obstacle database unavailable or invalid None None 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 109 sainjea4 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuauimasu 2 u u uio AeN yub jeuonippyv uoneiedo jeuuouqv ie p x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN PFD MFD Alert TERRAIN SVT Page Alert Type 0 a Aural Message Annundation Annunciation Terrain System Test Terrain System Fail Failure Terrain or Obstacle database unavaila
65. CEIVER SYSTEM MESSAGES System Message Comments CPDLC CPDLC is available Logon successful Data link is available for use CPDLC CPDLC connection lost Establish new connection Data link connection has been lost CPDLC CPDLC facility logon failed Logon failed Check pertinent entries for accuracy CPDLC CPDLC data link available Logon is still required GDR TEMP GDR over temp Reducing transmitter power The data link is ready for use but logon to the facility has not yet taken place The system has detected an over temperature condition in the GDR The transmitter operates at reduced power If the problem persists the system should be serviced GDR FAIL GDR is inoperative A fault has been detected in the GDR The system should be serviced GDR TX FAIL GDR transmitter is inoperative The system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A fault has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be servi
66. D DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established Loss of Hazard Functions with Loss of GPS Position 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 99 eoueproAy Senpa204d Buruue d ARN Sd5 S23V oipny uddx Sv3 sjueuinsu puezey ubi U105 AEN BUTLER soJnjeoJ jeuonippy xipuaddy suelv junuuy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glidepath e AFCS Annunciations 9 PFD Setup Menu and Vertical Deviation Flight Director Windows displayed in Indicators Command Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References e Radar Altimeter DME Information Nearest Airports Selected Altitude Window Flight Plan VNV Target Altitude Wind Data Messages
67. Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional Displays NEXRAD weather and coverage information on the Navigation Map optional Displays Connext precipitation on Navigation Map optional 144 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Appendix Level 1 Level 2 Description DCLIR 3 SHW CHRT CHKLIST XM LING or DL LING METAR LEGEND WX RADAR BACK UPDATING DATABASES Displays SiriusXM lightning information on the Navigation Map optional Displays Connext Worldwide Weather lightning information on the Navigation Map optional Displays METAR flags on airport symbols shown on the Navigation Map optional Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected Displays Color Weather Radar images on the Navigation Map Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active fli
68. E 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 63 AeN Sd5 S24V oipny uadx sya syu wnysu u102 AEN 10614 Duruue d Wfil4 e uepioAy SoJnpa20Jd paezey saunqea4 jeuonippy suelv uoneiedo junuuy Jeuuouqy xipuaddy x pul 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 A GARMIN Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional System Self Test 1 2 3 4 Set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey 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
69. ES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A fault has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The G1000 system should be serviced GMC KEYSTK GMC key name Key is stuck 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 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 129 saunqea4 2 AEN Sd S24V olpny uqax sv siu un sul paezey nubi Juo eN Wil jeuonippy uoneiedo Jeuuouqy ic Eu x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts GTS 820 MESSAGE ADVISORIES A GARMIN Message Comments GTS CONFIG GTS config error Config service req d MANIFEST GTS software mismatch communication halted 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 addresse
70. EXT MESSAGE Window is now displ MENU Key to display the Page Menu ayed sjuauimasu Yid SoJnpa20Jd Duruue d AEN Sd5 241V olpny uqax 3461 UI0 AeN eouepioAy paezey 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 85 s m e q jeuonippy uoneiedo Jeuuouqy Sue v unuuy xipueddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN 10 Press th
71. 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 Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key for 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 desired flight plan Select the INVERT Softkey Invert and activate stored flight plan is displayed 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Flight Planning COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the smal 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
72. G 1000 Integrated Flight Deck Cockpit Reference Guide TBM 850 amp TBM 900 GARMIN Copyright 2007 2009 2011 2014 2015 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0719 12 or later for the Socata TBM 850 900 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 Hounsdown Business Park Southampton Hampshire 040 OLR U K Ga Tel 44 0 23 8052 4000 Fax 44 0 23 8052 4004 min Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may transmitted disseminated downloaded or stored in any storage m 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 be reproduced copied edium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a sing
73. G1000 Cockpit Reference Guide for the Socata TBM 850 900 15 sjueuinasu BUT xipueddy Suelv uoneiedo sainyea4 aoueplony saunpadoid Duruue d AEN Sd5 S24JV olpny uqax unuuy Jeuuouqy jeuonippy paezey nuru uo2 AEN x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 8 GARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to selec
74. KCOS Oxygen OXY PSI Landin Field Elevation From Active Flight Plan Cabin Pressure Display The pressure in psi for the oxygen system is given as a readout below the cabin pressurization display under normal display conditions LFE Landing Field Elevation TBM 900 only The Landing Field Elevation can be set based on the destination airport in the active flight plan or entered manually When entered based on the active flight plan the elevation will be derived from the navigation database based on the destination airport System derived values appear with the destination airport identifier Manually entered values appear without the airport identifier A red X is displayed if the LFE is out of range or the data source is invalid 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 11 sjuaumasu nubi uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 2 oipny uddx junuuy jeuuouqy paezey nubi xipuaddy x pul Flight Instruments i Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index A Engine amp Airframe Systems GARMIN Setting the displayed landing field elevation to the value for the destination airport 1 Select the SYSTEM Softkey 2 Select the FMS LFE Softkey to set the LFE to the value for the destin
75. MFD Softkeys ir Level 1 Level 2 Description pE SYSTEM Enables the Synoptics Page softkeys 8 or CAS Scroll up or down Displayed only when a ii CAS T sufficient number of items are displayed in E and the Crew Alerting System Display to warrant ae CAS scrolling s ELEC Selects the Electrical Synoptics Page FUEL Selects the Fuel Synoptics Page d GEN Selects the General Synoptics Page si x 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 143 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 Description CPDLC LOGON LOGOFF NEW DELETE DEL ALL BACK TRAFFIC PROFILE TOPO TERRAIN AIRWAYS STRMSCP NEXRAD or PRECIP When available accesses CPDLC softkeys Displays Logon screen for the CPDLC system Displays Logoff screen for the CPDLC system Accesses New CPDLC message screen Delete selected CPDLC message Delete all CPDLC messages Returns display to previous softkey level Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays removes Profile View on Navigation Map Page Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map
76. OK ayed when the TAS system passes a pilot initiated self test TAS System Test Failed ayed when the TAS system fails a pilot initiated self test One o dock through Twelve o dock or No Bearing High Low Same Altitude if within 200 feet of own altitude or Altitude not available P 1 Played when a Traffic Advisory TA is issued with a TAS system P P P ayed to indicate bearing of traffic from own aircraft GTS 820 only Played to indicate altitude of traffic relative to own aircraft GTS 820 only Less than one mile One Mile through Ten Miles or More than ten miles Played to indicate distance of traffic from own aircraft GTS 820 only MFD amp PFD MESSAGE ADVISORIES Message lost Recheck settings Comments DATA LOST Pilot stored data was The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display The MFD and PFDs are not communicating crosstalk error has occurred with each other The G1000 system should be serviced 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 113 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx Sv3 sjueumasu piezeH ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy p x pul
77. OM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 80 08 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO REGION WORLDWIDE WORLDWIDE CYCLE 1211 1212 EFFECTIVE 26 AUG 2012 18 N0U 2012 EXPIRES 23 SEP 2612 15 DEL 2812 NO WILL BE ASSUMED IN 21 SECONDS 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 149 s mip q e uepioAy s mp o d Duruue d AEN Sd5 241V oipny uddx Sv3 SjueuinJjsu jeuonippy puezey Wil wio AeN Yid uoneiedo Jeuuouqy sue v unuuy ES Reed GARMIN 5 After the navigation database files are copied to the bottom SD card the display will appear as shown in the following figure INITIALIZING SYSTEM DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 80 88 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO WORLDWIDE WORLDWIDE 1211 1212 25 806 2012 18 N U 2812 23 SEP 2812 15 DEL 2812 NO WILL BE ASSUMED IN 18 SECONDS UPDATING STANDBY NAVIGATION DATABASE PLEASE WAIT UPDATED STANDBY NAVIGATION DATABASE SUCCESSFULLY PRESS ANY KEY TO CONTINUE CONTINUING IN 9 SECONDS 6 Asinstructed on the display press any key to continue The display will now appear as shown in the following fi
78. Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Flight Planning IMPORT A FLIGHT PLAN FROM AN SD CARD 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the 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 exist
79. Select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page A 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 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 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 viewed before answering 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 3 Press the ENT Key The voice and pop up alert will not be displayed now when an incoming call is received 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 81 saunpa20dd Buruuejd AeN Sd5 S24V oipny uadx sva s u u nnsul nubi Tu102 AEN 346 aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Nav Com XPDR Audio Haz
80. Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 71 sjuauimasu UATE SoJnpa20Jd Duruue d AEN Sd5 241V oipny uadx 3461 Tu102 AEN eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 6 GARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Acti
81. Softkey A confirmation window appears 3 Highlight OK and press the ENT Key Disconnecting from the CPDLC System After successfully initiating a CPDLC session the LOGOFF Softkey becomes available To Log off the CPDLC System 1 From the MFD select the CPDLC Softkey 2 Select the LOGOFF Softkey Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C amp GARMIN Nav Com XPDR Audio Panel Enabling Disabling Data Mode It may be desirable to disable Data Mode on the GDR 66 VHF Data Link Transceiver or conversely to enable it To disable data mode on the GDR 66 1 From the MFD select the CPDLC Softkey 2 Press the Menu Key to display the page menu 3 Turn the small FMS Knob to highlight Disable Data Mode and press the ENT Key To enable data mode on the GDR 66 1 From the MFD select the CPDLC Softkey 2 Press the Menu Key to display the page menu 3 Turn the small FMS Knob to highlight Enable Data Mode and press the ENT Key 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
82. T Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Procedures 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 optional RAD ALT or TEMP COMP 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 Press the ENT Key If BARO RAD ALT or OFF was selected step 8 proceed to step 11 If TEMP COMP was selected in step 8 the cursor moves to the TEMP AT field Turn the small FMS Knob to enter the temperature at the destination airport The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value 11 Press the ENT Key LOAD or ACTIVATE is now displayed wit
83. URE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the 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 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 45 sjuauimasu UATE 5 3 olpny uqax 0105 AEN 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com
84. Viewing the Maintenance Logs Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select MAINTENANCE LOG The AUX MAINTENANCE LOGS Page is now displayed AUXILIARY VIDEO OPTIONAL There are four modes of operation of the auxiliary video display Full Screen Full Screen with Digital Zoom Split Screen with Map and Split Screen with Map and Digital Zoom Displaying auxiliary video 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select VIDEO and display the AUX VIDEO Page The video display softkeys shown below appear on the AUX VIDEO Page Control of the AUX VIDEO Page can also be accessed through the Page Menu Selecting video menu options 1 While viewing the AUX VIDEO Page press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key Once the ENT key is pressed on any option the page menu closes and returns to the AUX VIDEO Page Video Setup Video brightness contrast and saturation may be adjusted be selecting the setup function While viewing the setup function softkeys after 45 seconds of softkey inactivity the system reverts to the AUX VIDEO Page softkeys 90 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN _ Additional Features Adjusting the video settings 1 With the
85. allows the Joystick to control the zoom setting of the video display When zooming in on the video display a Zoom Window will appear in the upper right of the display A box within this window indicates the portion of the display currently being viewed The currently displayed portion of the full display may be adjusted by using Joystick 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 91 sjueuinasu Yid Son pa20Jd Duruue d AEN Sd5 241V olpny uqax fij Tu102 AEN 2 s m e q xipuaddy Suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN SCHEDULER The Scheduler feature can be used to enter and display reminder messages e g Hot Section Inspection or Phase 1 Maintenance Check in the Messages Window on the PFD Messages can be set to display based on a specific date and time event once the message timer reaches zero one time default setting or recurrently whenever the message timer reaches zero periodic Message timers set to periodic alerting automatically reset to the original timer value once the message is displayed When power is cycled all messages are retained until deleted and message ti
86. ard Avoidance Abnormal Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Procedures Additional Features Appendix Alerts Operation Index Additional Features A GARMIN Outgoing Calls 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 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 country code area code phone number when calling a non satellite telephone system Enter Satellite Country Code shown in the following table phone number when placing a call to another satellite telephone system Satellite System Country Code Inmarsat 870 ICO 8810 or 8811 Ellipso 8812 or 8813 lridium 8816 or 8817 Globalstar 8818 or 8819 4 Press the ENT Key OK is highlighted 5 Press the ENT Key The system will begin calling the number When the phone is answered the connection is established To exit the call select the HANGUP Softkey 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
87. ation airport in the current flight plan Manually setting the displayed landing field elevation 1 Select the SYSTEM Softkey 2 Select the MAN LFE Softkey 3 Use the 250 and 25 FT softkeys to set the desired elevation 4 Toconfirm the new LFE value select the ACCEPT Softkey If the ACCEPT Softkey is not selected the value will flash briefly and return to the previous setting Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN NAV COM TRANSPONDER AUDIO PANEL ENTER OR CHANGE Nav Com XPDR Audio Panel FLIGHT ID OPTIONAL 1 Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Tum the smal FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Tum the smal 5 Repeat steps 6 Press the ENT Key to update the Flight ID Do not perform any other FMS Knob to enter the next desired character 3 and 4 until the desired Flight ID is entered 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 smal 5 Repeat steps FMS Knob to enter the desired number 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 P
88. aximum torque TBM 850 only t TBM 900 only Caution Messages Messages Comments The Autopilot is ON while the Yaw Damper is OFF O uel timer off or out of service ESSESSE I Electric fuel pump running manual or automatic mode BATAMP O Battery current over 50 A while on ground sor Better of BEES MI Flow control and shut off valve shut off valve closed DEBT oil chip detector on if installed 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 sainjea4 2 Duruue d AEN Sd5 52 olpny uqax sv sjuauimasu 2 ni uio AeN yb jeuonippy uoneiedo jJeuuouqv iic E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Appendix Index Amundatons amp Alerts GARMIN Messages Comments Back up pressurization mode Cabin altitude target forced to 9800 ft CPDLC DISABLED CPDLC data mode is disabled FRONT CARGO DOOR Forward baggage door open FUELIMBALANCE Fuel tanks imbalanced by more than 15 USGAL for gt 30 seconds Fuel quantity less than or equal to 9 1 USGAL in specified tank GPU receptacle door not closed IGNTON O Ignition exciter running INERTSEP FAIL Inertial separator failure INERTSEPON Inertial separator extended Low fuel level sensor fa
89. b to enter a profile name up to 16 characters long and press the ENT Key Pilot profile names cannot begin with a blank as the first letter 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 93 sjueuinasu Yid SoJnpa20Jd Duruue d AEN Sd5 241V oipny uaddx 346 Tu102 AEN aoueplony paezey xipuaddy Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 6 7 8 9 A GARMIN In the next field use the small FMS Knob to select the desired settings upon which to base the new profile Profiles can be created based on Garmin factory defaults default profile settings initially based on Garmin factory defaults unless edited by the pilot or current system settings Press the ENT Key With CREATE highlighted press the ENT Key to create the profile Or Use the large FMS Knob to select CREATE and ACTIVATE and press the ENT Key to activate the new profile To cancel the process select CANCEL with the large FMS Knob and press the ENT Key 10 Press the FMS Knob to deactivate the cursor Selecting an Active Profile 1 2 3 4 5 6 Use the FMS Knob to select the AUX System Setup Page Press the FMS Knob momentari
90. ble or invalid TER FAIL Terrain System invalid software Failure configuration system audio fault No GPS position TER WA ertain SEU ot Available Excessively degraded GPS signal Out of TER N A None errain System database coverage ot Available area Sufficient GPS signal None None Terrain System received after loss Available TAWS B ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Pull Terrain Clearance or Up Warning RTC gi Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Terrain Impact Warning or Ahead Pull Up iiy MR Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Up Obstacle Clearance or Pull Up ere 4 Obstacle Ahead Pull Up Obstacle Ahead Pull Up 110 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts PFD MFD MFD Alert Type TAWS B Page Aural Message k r Pop Up Alert Annunciation mminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up o Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain
91. bstacles 118 119 120 Oil engine Alerts 105 Pressure 5 Temperature 5 Overspeed Protection 22 Oxygen Pressure 5 11 Warning 105 P Pathvvays 73 74 PIT 107 Predefined message 85 Propeller speed 5 190 00708 05 Rev C A GARMIN R Response Request 17 Reversionary Mode EICAS 5 Reversionary mode 99 ROC 109 110 111 S SafeTaxi amp 74 SBAS 22 46 67 68 101 120 122 Scheduler 92 SD Card 37 44 95 96 97 133 134 135 146 148 149 150 151 Sector scan 71 Sensor 107 SiriusXM lightning 138 145 SiriusXM Weather 53 SMS 79 STAB 72 Standby 69 Standby Navigation Database 149 151 Store Flight Plan 41 Stormscope lightning data 51 52 Strike 51 Strike mode 52 Supplemental Data Card 146 147 SVT 73 133 Synchronization 146 Synthetic Vision System 73 T TA 113 TAF 53 TAS 64 113 124 TAWS 67 68 110 TAWS B 67 Telephone 79 81 82 84 86 Terrain 65 67 118 138 144 190 00708 05 Rev C Index Terrain SVT 65 66 67 Text message 83 85 86 Text messaging 82 Tiltline 70 Timer 2 130 Topographical data 138 144 Torque 5 Warning 105 Traffic 51 63 144 Traffic advisory 63 Traffic Advisory 113 Traffic map page 63 64 65 Transponder 13 14 142 Trim 5 V Vertical speed guidance 28 Vertical track 113 Video settings 91 VNV 25 100 132 133 Vspeed 3 W WATCHG 72 Waypoint Selection Submenu 36 Weather Attenuated Color Highlight 72 Weather data link pag
92. ced 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 127 saunqea4 uepjoay seinpa2o0Jd Buruuejd AEN 5649 24V oipny uadx svi syu unysu paezey ETSI wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy 5 ER x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix od Annunciations amp Alerts A GARMIN GWX 68 GWX 70 ALERT MESSAGES Message GWX CONFIG GWX config error Config service req d Comments GWX 68 70 configuration settings do not match those of the GDU configuration The G1000 system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 70 or the GWX 68 70 is reporting a fault The GWX 68 70 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair A fault has been detected in the GWX 68 70 The GWX 68 70 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 70 has incorrect software installed The G1000 system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm GDC 74B MESSAGE ADVISORIES Message Comments ADC1 ALT EC ADCI altitude error co
93. 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 The selected Display Pane depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 00708 05 Rev C Garmin
94. d Send a manual weather data request to resume automatic updates Auto update retry Seconds The system will attempt another automatic weather data request after an error occurred during the previous request Timer counts down until the next automatic request occurs Connext Comm Error 2 Connext Comm Error 4 A communications error has occurred with the GDL59 or GIA The G1000 should be serviced This occurs if multiple automatic weather data requests have recently failed or the GDL 59 or a GIA is off line 60 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Hazard Avoidance Weather Request Status Message Description Connext Comm Error 151 This can occur if the GDL 59 is off line or not configured or the Iridium or Connext networks are not accessible Check Iridium signal strength If this error persists the G1000 should be serviced Connext Comm Error 6 A communications error has occurred It this error persists the G1000 should be serviced Connext Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the data request Connext Comm Error 8 A server error has occurred or invalid data received Connext Login Invalid There is a problem with the Connext registration Contact Garmin at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assista
95. d press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 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 aoueplony paezey saunyea4 jeuonippy uoneiedo Jeuuouqy 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 xipuaddy suelv junuuy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 41 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 5 6 7 A GARMIN Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key of the MFD and turn the small
96. d within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC or COM2 MIC on the audio panel Receive Only Press the COM1 or COM2 on the audio panel SELECTING A NAV RADIO 1 2 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 Press the NAV1 NAV2 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 NAV COM TUNING 1 2 3 Press the small tuning knob to select the desired radio for tuning A cyan box highlights the radio frequency to be tuned Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C 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 d
97. derstorms 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 Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed WARNING Do not use a QFE altimeter setting with this system System functions will not operate properly with a QFE altimeter setting Use only a QNH altimeter setting for height above mean sea level or the standard pressure setting as applicable 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A
98. dress 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 Press the ENT Key The sorting selection is indicated at the bottom center of the list window 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 87 s tin sul sub s inp o4d buluueld APN Sd5 241V olpny uqax 3461 Tu102 AEN aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 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 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 p
99. e 53 Weather radar 69 Wind data 140 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 Index 3 sjuaumasu BUT so1njeoJ 2 Buruuejg AEN 5649 2 oipny uadx Jeuonippy paezey ni uo2 AEN uoneiedo Jeuuouqy Sue v unuuy gg EN GARMIN Index Ssjueuinijsu fila 593 U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 Index 4 A GARMIN Pss Garmin Internati onal Inc 1200 East 151st Street Olathe KS 66062 USA ES 397 8200 f 913 307 8282 Aviation Sup Garmin Corporation 68 Jangshu 2nd Road Shiir Taipei County Taiwan _ p 886 2 2642 9199 f 886 2 2642 9099 0 2007 2009 2011 2014 2015 Garmin Ltd or its subsidiaries 190 00708 05 Rev
100. e MENU Key to display the Page Menu 11 Turn either FMS Knob to place the cursor on Stop Editing Predefined 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 and Unsent text messages Saved messages that are meant to be sent later are stored as Drafts Each text message box may b
101. e 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 10 Turn the small 11 Press the Display Database Selection Softkey to show active navigation FMS Knob to select the AUX Page group on the MFD FMS Knob to select the System Status Page 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 The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD card prior to its effective date The Jeppesen Navigation Database is available from Jeppesen seven days prior to its effective date NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of each PFD and the MFD 3 Turn the system ON A prompt similar to the following is displayed DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTT
102. e limitations o AC U KWIK and its relate expressly disclaim all war anti and fitness for a Organizations do not warrant oth allowed by action claim out of Garm lim 5 January 2015 erwise Licensee agrees not to s aw to release and hold ha s or losses related to any act in s use of the information i itation or exclusion of implied warrant the above limitations or exclusions may not apply to licensee rpose y representation eglige result ser ag d wa es wi or ma 190 00708 05 Rev C s regard nce sha f ranties o s may not app eanyr m Ua n ies 0 ees not to d harmless AOPA fro mited inform epresentations regardin ue AC U KWIK Organizati ess AC U KWIK Organi or alleged inacc the datasets Some jur S related organizations herei espect to the AOPA informati ted to the implied warranties ng its accuracy reliability or f na on of ter collectively included in this merchantability mation is provided as is and AOPA does not otherwise Under m any causes of action claim form iabi r y to you d organizations hereafter collectively AC U KWIK O th respect to the AC U KWIK information in data express or implied including but not li particular purpose The to the implied warranties ation is p ons a r liability for incidenta Pri AOPA be liable for any inci rom the use o
103. e the center point of the Sector Scan 2 Press the FM 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field S Knob to display the cursor 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 6 Press the FM 190 00708 05 Rev C Scan S Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 71 xipuaddy sue v uoneiedo sainjea4 uep ony 2 Duruue d AEN Sd5 S24JV unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or
104. e viewed separately or together in any combination Show Inbox Messages 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 850 900 190 00708 05 Rev C GARMIN Additional Features b Turn either FMS Knob to place the cursor on Show Inbox Messages 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 Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window 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 Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Arranging Text Messages 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 ad
105. ecorded block 20 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT Takeoff on ground TO Takeoff on ground TO Go Around in air GA Go Around in 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 NAV Key Navigation VOR Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT GPS Pitch Hold default PIT APR Key Approach VOR Glidepath GP LOC Glideslope GS HDG Key Heading Selec
106. ector 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 1f the boost pump is off the symbol is shown in cyan 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 9 sjuaumasu Yid sual uone1edo So1nje2J s mp oold Buruue d AEN 540 yi oipny uddx unuuy jeuuouqy jeuonippy paezey bii U105 AEN xipuaddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine amp Airframe Systems GENERAL SYSTEMS A GARMIN 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 wi
107. ed the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 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
108. edures in stored flight plans are correct and up to date Verify stored airways DB CHANGE Database changed This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft posit
109. egrees 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 Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 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 SVT NOTE Terrain SVT is only available when the Synthetic Vision Technology SVT option is installed and the TAWS option has not been installed NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 65 AEN 540 S24V oipny dadx Sv3 s u umn sul u02 AEN nubi Duruue d Wil uep
110. en scanning vertically on the Weather Radar Page a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing While viewing weather radar on the Weather Radar Page or the Navigation Map Page moving the Joystick right or left adjusts the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be 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 70 Garmin G1000 Cockpit Reference Guide for t
111. equest the Request Status box initially displays Contacting Connext Once a connection is established the Request Status Box displays Receiving Wx Data Time Remaining with an estimated data transfer time either minutes or seconds If desired the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength The system retrieves all available Worldwide Weather products within the selected coverage area during an initial Connext Data Request regardless of which products if any are currently enabled for display On subsequent requests previously retrieved textual data such as METARs and TAFS is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request If the system cannot complete a Connext weather data request one or more mes sages will appear in the request status window as indicated in the following table Weather Request Status Message Description Auto requests inhibited Send manual request to reset The system has disabled automatic weather data requests due to excessive errors Automatic weather data requests have stoppe
112. er and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets altimeter setting to standard barometric pressure n nnn n Select the BACK Softkey to return to the top level softkeys 1 2 3 4 5 6 7 IDENT BKSP BACK MSG Select the BACK Softkey to return to the top level softkeys Transponder Softkeys 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 141 SoJnjeaJ e uepioAy s mp o d Duruue d AEN Sd5 241V oipny uddx Sv3 SjueuinJjsu piezeH U10 AEN jeuonippy uoneiedo Jeuuouqy Sue v unuuy gt s o z m x x pul iui nu 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 ADF DME XPDR IDENT TMR REF NRST MSG XPDRI XPDI2 STBY ON ALT GND VER CODE 0 7 BKSP 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 Selec
113. er is also removed from all primary servo motors and engaged solenoids Note the visual and aural alerting indicating autopilot disconnect 3 Retrim the aircraft as needed Substantial trim adjustment may be needed 4 Pull the appropriate circuit breaker s to electrically isolate the servo and solenoid components 5 Release the AP DISC Switch 102 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C E GARMIN Abnormal Operation OVERPOWERING AUTOPILOT SERVOS In the context of this discussion overpowering refers to any pressure or force applied to the pitch controls when the autopilot is engaged A small amount of pressure or force on the pitch controls can cause the autopilot automatic trim to run to an out of trim condition Therefore any application of pressure or force to the controls should be avoided when the autopilot is engaged Overpowering the autopilot during flight will cause the autopilots automatic trim to run resulting in an out of trim condition or cause the trim to hit the stop if the action is prolonged In this case larger than anticipated control forces are required after the autopilot is disengaged The following steps should be added to the preflight check 1 Check for proper autopilot operation and ensure the autopilot can be overpowered 2 Note the forces required to overpower the autopilot servo clutches 190 00708 05 Rev C Garmin G1000 Cockpit Refere
114. eselect 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 extinguished the ICS Knob controls only volume CONTROLLER PILOT DATA LINK COMMUNICATIONS OPTIONAL The CPDLC Controller Pilot Data Link Communications system provides data link communication between the aircraft and an Air Traffic Control facility Communication is normally in the form of text message elements that resemble phraseology used in voice communications with ATC Generally messages are closed with an acknowledgement or acceptance When a message is acknowledged the connection with the ATC facility is not terminated but kept active for future communication Communication hand off to the next ATC facility is usually performed automatically but may also be accomplished manually by the pilot Connecting to the CPDLC System A flight plan must be filed prior to logging on to t
115. ey The holding pattern is removed from the active flight plan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern INVERT AN ACTIVE FLIGHT PLAN 1 2 3 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN ight Planning 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 s tin su UATE REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 5 3 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints olpny uqax Wi0 gt AeN 52 AEN 540 gt e SeJnpa20Jd 3 Press the CLR Key to display a confirmation window 4 With OK highlighte
116. file Box Knob to select the AUX System Setup Page S Knob momentarily to activate the flashing cursor 4 Press the ENT Key 5 In the Delete Profile window turn the FMS Knob to select the profile to delete 6 Press the ENT Key 7 With DELETE 8 To cancel the process use the large FMS Knob to select CANCEL and highlighted press the ENT Key press the ENT Key 9 Press the FM S Knob to deactivate the cursor Importing a Profile from an SD Card 1 Insert an SD card containing the pilot profile s into the top card slot on the MFD 2 Turn the FMS Knob to select the AUX System Setup Page 3 Select the IM 190 00708 05 Rev C PORT Softkey Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 95 s anp 201d Buluueld AEN 540 S24V oipny uadx sva siu umnsul Wil swop AeN Yid eouepioAy paezey xipuaddy Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 4 5 6 7 8 A GARMIN The system displays the Pilot Profile Importing Window with IMPORT highlighted To change the selected profile to be imported from the SD card shown as SELECT FILE turn the large FMS Knob to highlight the profile file name
117. flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan 4 confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the smal 3 Press the FM 4 Turn the large FMS Knob to highlight the flight plan to be deleted FMS Knob to select the Flight Plan Catalog Page S Knob to activate the cursor 5 Select the DELETE Softkey A Delete flight plan amp 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 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 3 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 4 Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user way
118. ft registration number Press the ENT Key to complete the entry Turn the large FMS Knob to place the selection cursor over the Destination Airport field Enter the identifier of the destination airport used in the filed flight plan and press the ENT Key The Filed Departure Airport field is prefilled with the airport identifier corresponding to the current aircraft location If the flight plan was filed using a different airport identifier turn the large FMS Knob to place the selection cursor over the Filed Departure Airport field enter the departure airport and press the ENT Key Optional Turn the large FMS Knob to place the selection cursor over the Filed Departure Time field Optional Enter the departure time used in the filed flight plan and press the ENT Key Turn the large FMS Knob to place the selection cursor over SEND and press the ENT Key The Status immediately indicates Connecting After successful log on the Status indicates Waiting For CPDLC Once a CPDLC session is initiated by ATC the Status indicates Connected and the Current Facility field is populated with the name of the facility If a transfer to another facility is needed the Next Facility field is populated Pressing the LOGOFF Softkey terminates the log on process Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Nav Com XPDR Audio Panel Creating a Message Creating a message c
119. ght plan When available displays optional airport and terminal procedure charts When available displays optional checklists Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in maintenance being required to reboot the system 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 SYSTEM STATUS Page 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 145 s n e 4 e uepioAy 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuaumnasu jeuonippy paezey nubi Tuo2 NeN Yid uoneiedo Jeuuouqy Sue v unuuy 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 600071 GARMIN NOTE DO NOT use the database SD cards for any purpose other than database storage In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error me
120. gs level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle pon HDG Heading Select Captures and tracks Selected Heading Key HDG Navigation GPS GPS Arm Capture Track Navigation VOR Enroute Arm Captures and tracks selected navigation NAV VOR Capture Track source GPS VOR LOC Key Navigation LOC Arm Capture Track LOC No Glideslope Backcourse Arm Captures and tracks a localizer signal BC Ke BC Capture Track for backcourse approaches y Approach GPS GPS Arm Capture Track Approach VOR VAPP Arm Capture Track 1 Captures and tracks selected navigation APR Key Capture Track Glideslope Mode automatically armed Commands a constant preprogrammed Takeoff constant pitch attitude and wings level TO in preparation for takeoff GA Disengages autopilot and commands Switch Go Around a preprogrammed constant pitch GA j d annunciation 77 in the AFCS Status Box The low bank angle range is indicated in green along the Roll Sca 190 00708 05 Rev C of the Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 23 sv3 sjueunasu oipny uadx 0105 AEN ARN Sd5 S24V Sue v uoneiedo s m aoueplony saunpadold Duruue d Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul iui Wfil4 paezey GARMIN AFCS Ssjueuinijsu fila Sv3 U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4
121. gure DATABASE NAVIGATION WILL BE VERIFIED BEFORE USE DATABASE STANDBY NAU WILL BE VERIFIED BEFORE USE PRESS ANY KEY TO CONTINUE CONTINUING IN 6 SECONDS 7 Press any key to continue The display will now appear as shown in the following figure DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL OUERHRITE THE ACTIVE NAVIGATION DATABASE FROM TO REGION WORLDWIDE WORLDWIDE CYCLE 11 vay EFFECTIVE 26 806 2012 18 NOU 2812 EXPIRES 23 SEP 2812 15 DEL 2812 No WILL BE ASSUMED IN 8 SECONDS 8 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 9 Press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the small FMS Knob to select the System Status Page 150 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN 0000 Appendix 12 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 13 Turn system power OFF 14 Remove the SD card from the top card slot of the MFD 15 Turn system power ON 16 Press the ENT Key to acknowledge the startup screen 17
122. h LOAD highlighted 12 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 13 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 4 s tin sul sub 5 3 oipny uddx UI05JNeN 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 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 EAS Nav Com XPDR Audio TEMPERATURE COMPENSATED ALTITUDE AFCS When temperature compe
123. he AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 1 Sue v uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN Sd5 2 olpny uqax svi unuuy jeuuouqy jeuonippy paezey xipuaddy x pul wo gt AeN nu Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun Flight EAS Instruments AFCS Procedures GPS Nav Appendix Alerts Operation Features Index A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES 1 2 3 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the cyan tuning box over the NAV1 standby frequency in the upper left corner of the PFD Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the cyan tuning box over the NAV2 standby frequency Select the CDI Softkey a third time to return to GPS NOTE On some ILS approaches where the glideslope intercept point is at or in close proximity to the fix prior to the FAE it is possible to be above the glideslope when the navigation source automatically switches from GPS to LOC The probability of this occurring varies based on air temperature Review the Course Deviation Indicator CDI discussion in the
124. he CPDLC system After entering flight plan information in the required fields and successfully logging on to the system messages may be sent and received The following parameters are used to log on to the system Facility Flight ID e Destination Airport Filed Departure Airport File Departure Time Optional 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 15 Sjueunasu 5 3 52 oipny uadx U10 AEN Suelv uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 unuuy jeuuouqy jeuonippy 2 xipuaddy x pul Yid Wfi l4 Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audio EAS Procedures GPS Nav Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN Performing the system log on 1 2 3 4 5 6 1 8 9 10 11 12 13 14 From the MFD select the CPDLC Softkey Ensure Link Available is displayed in the Status Box Select the LOGON Softkey Turn the large FMS Knob to place the selection cursor over the Facility field Turn the small FMS Knob to select the desired ATC facility to which the CPDLC connection will be established Press the ENT Key to complete the entry Turn the large FMS Knob to place the selection cursor over the Flight ID field Turn the small FMS Knob to enter the Flight ID or aircra
125. he Socata TBM 850 900 190 00708 05 Rev C GARMIN avoidance Adjusting Gain WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated 5 3 oipny uddx UI0JNeN position 3 Press the FM S Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in t he GAIN field Ground Mapping 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 FM S Knob to activate the cursor 5 Turn the large 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 FM Sector Scan S Knob to remove the cursor 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 becom
126. how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey Nav Com XPDR Audio 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 Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS Index 4 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Engine amp Airframe Systems ENGINE amp AIRFRAME SYSTEMS CABIN PRESS ALT FT RATE FPM X1000 1800 0 0 DIFF PSI OIL PSI ELECTRICAL AMPS E 25 L 118 VOLTS EIS Display Normal Mode TBM 850 shown TBM 850 shown O Torque CAS Display 13 Fuel Fuel Flow Propeller Speed Cabin Pressure Altitude and 13 Fuel Fuel Pressure N installed Change Rate TBM 850 only Q Generator Speed Differential Pressure Baen and Generator urrents Interturbine Temperature elected 7 Altitude Battery and Essential Bus Volta G Oil Pressure LFE TBM 900 Ee Aileron and Oil Temperature Rudder Trim and Flap 2 Fuel Quantity 190 00708 05 Rev C G G G Ge CO 2 PROP RPM 1800 OIL PSI ae OIL C 75 SEE CABIN PRESS ALT FT 1800 DIFF PSI 8 8 FUEL QTY USG 51 48 GPH 24 25 GEN 110 BATT 29 0 VOLTS Ess 29 0 EIS
127. ht plan 41 Enable Terrain 66 67 Engine display 5 Essential bus voltage 5 F Flap position 5 Asymmetrical deflection warning 105 Flight Director 21 Flight ID 13 Flight path marker 73 FliteCharts 74 75 Frequency Transfer 14 Index 1 uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax sv sjuaumasu jeuonippy u105 AEN jeuuouqy Sue v unuuy iui n paezey m Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Appendix Index Fuel Alerts 105 106 Flow 5 Pressure 5 Quantity 5 G Gain 71 Generator Current 5 Speed 5 Ground mapping 71 H Horizontal scan 70 Horizon heading 73 Inhibit 66 68 Inhibit TAWS 68 Inhibit Terrain 66 Inset Map 137 138 144 145 Interturbine Temperature ITT 5 Warning 105 IOI 109 111 Iridium 79 82 Iridium satellite network 79 J Jeppesen 75 L Landing Field Elevation 11 LFE 11 12 Lightning 51 52 Index 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A GARMIN M Map panning 53 Message advisories 113 119 122 126 129 134 Message dialogs 18 Messages window 93 METAR 53 Minimums 113 MISCOMP 107 Mode S 142 Mode selection softkeys 14 Multi Function Display MFD Softkeys 143 N NAV 14 NAV1 2 14 NAV2 2 14 Navigation database 27 28 NEXRAD 53 138 144 0 OBS 2 O
128. iew 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 74 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C 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 airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day
129. ilure for specified tank LOWVOLTAGE Battery voltage below 26 V Starter generator unconnected MAX DIFF PRESS MODE activated NGH e Generator speed is more than 103 ENT Oil pressure is in the caution zone OILTEMP Oil temperature below 0 C or above 104 C Specified pitot heat left or right on while engine off Specified pitot heat left or right off PROP DEICE FAIL Prop deice selected and not on BUL Pop deice on while engine off EZ Rear cargo door open EEO Stall warning heat on while engine off BE TET M Stall warning heat off sw Starter generator running VACUUMLOW Vacuum pressure in the circuit is low Only affected side L R or L R displayed in CAS message applicable messages listed here display L R for example t TBM 900 only 106 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Annuneiations amp Alerts COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is gt 200 ft f both airspeed sensors detect 35 knots this is inhibited ts f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 ts Difference in heading sensors is gt 6 degrees
130. ing 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 list of the available flight plans on the SD card If overwriting the existing flight plan is not SjueuinJjsu iui oipny uddx UI05JNeN 52 desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoin 4 Turn the small FMS Knob The Waypoint Information Window is now displayed tis inserted before the highlighted waypoint 5 Enter the new flight plan waypoint by one of the following a Enter the b Press the Or 190 00708 05 Rev C user waypoint identifier facility or city ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 37 SoJnpa20Jd 4 AEN 540 nubi aoueplony paezey Sue v
131. inhibit the alert on the PFD Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVT 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 Synthetic Vision Technology SVT functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVT 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 SVT information is shown on the primary flight display PFD SVT offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVT enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displayi
132. ion 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 131 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax sv Sjueumasu puezey 346 wio gt AeN ubi jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message ARSPC NEAR Airspace near less than 2 nm Comments Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active SLCT FREQ Select appropriate frequency for approach The system notifies the pilot that the loaded approach is not active Activate approach when required The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offse
133. ion Index Appendix n Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message MANIFEST GRS1 software mismatch communication halted Comments The 1 AHRS has incorrect software installed The G1000 system should be serviced MANIFEST GRS2 software mismatch communication halted The 42 AHRS has incorrect software installed The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted GSR 56 MESSAGE ADVISORIES Message The GMU 44 has incorrect software installed The G1000 system should be serviced Comments GSR1 FAIL GSR1 has failed A fault has been detected in the 1 GSR 56 The system should be serviced Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts GDR 66 VHF DATA LINK TRANS
134. k 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 mismatch The PFDs and MFD have different terrain 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 database mismatch The PFDs and MFD have different obstacle 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 118 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Airport Terrain database mismatch Comments The PFDs and MFD have different airport terrain 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
135. lace 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 850 900 190 00708 05 Rev C 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 2 Turn either FMS Knob to select the desired message 3 Press the MR Or a Press the K READ Softkey MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Mark Selected Message As Read Press the The message ENT Key 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
136. layed for reference only An arrival waypoint altitude may be used 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 FAF The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this GPS Navigation case the FAF altitude can be designated the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance entered by the pilot Altitude is designated for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no published altitude exists White Text Cyan Text Cyan Subdued Text Large Text Altitude calculated by 1 Altitude
137. le copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use prov revision hereto is strictly prohibited Garmin and G10009 WATCHS FliteCharts and SafeTaxi are r ided 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 distribut ion of this manual or any egistered trademarks of Garmin Ltd or its subsidiaries Connext is a trademark of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of NavData is a registered trademark of Jeppesen Inc Stormscope is of L 3 Communications Garmin a registered trademark SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AC U KWIK is a registered trademark of Penton Business Media Inc AOPA Membership Publications Inc and it sdaim all warranties with ied including but not lim The infor AOPA expressly di data express or imp and fitness for a pa warrant or make an no circumstances including n consequential damages that documentation even if AOPA possibility of such damages U by law to release and ho ticular pu to any actual or alleged inaccuracies in the in itation or exclusion of implie exclusion lim 50 the abov
138. ll 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 67 AEN Sd5 S24V olpny uqax sv4 Sjuouinsu u102 AEN T Duruue d Wil aoueploay s mp oold paezey Sue v uoneiedo s n e 4 Tunuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may ap
139. lls Change the Viewing Mode Between 360 and 120 1 2 Select the Stormscope Page Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Ves niAvdidanca SIRIUSXM WEATHER OPTIONAL WARNING Use of SiriusXM Weather for hazardous weather penetration is not recommended Weather information provided by SiriusXM is approved only for weather avoidance not penetration Displaying SiriusXM 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 select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkey
140. losed Battery overheating is indicated in red with a BAT OVHT annunciation a CAS message is also generated Switch Open Switch Closed Standby Generator Switch Status BAT Battery Overheat Indication 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 7 sjueumasu 3g BO 54 sH ly uoneiado saunyea4 eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui nu A EnpnesARamessems 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 TRK Nav Com XPDR Audio 0 0 DIFF PSI L a ALT StL FT S800 OOO 90000 Procedures Hazard Avoidance SYSTEH Left Fuel Tank O Auxiliary Boost Pump 0 Right Fuel Line Left Fuel Line G Fuel Selector Fuel Flow Data Fuel Pressure TBM Right Fuel Tank 850 only Additional Features Abnormal Operation Fuel Synoptics Page Annun Alerts Appendix Index 8 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C amp GARMIN Engine S AIHTdme 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 sel
141. ly to activate the flashing cursor Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box Turn the small FMS Knob to display the pilot profile list and highlight the desired profile Press the ENT Key The system loads and displays the system settings for the selected profile Press the FMS Knob to deactivate the cursor Renaming a Profile 1 2 3 4 5 6 Use the FMS Knob to select the AUX System Setup Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight RENAME in the Pilot Profile Box Press the ENT Key In the Rename Profile window turn the FMS Knob to select the profile to rename Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN 7 Use the FMS Knob to enter a new profile name up to 16 characters long and press the Additional Features ENT Key 8 With RENAME highlighted press the ENT Key 9 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key 10 Press the FMS Knob to deactivate the cursor Deleting a Profil e NOTE The profile that is currently active cannot be deleted If this is the desired profile to delete select another profile then delete the desired profile 1 Use the FMS 2 Press the FM 3 Turn the large FMS Knob to highlight DELETE in the Pilot Pro
142. mation Weather Products and Symbols Wx Product Status Icons Description US 3m CN Bm NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right 5m 12m ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed QJ m XM LIGHTNING The age of the displayed data is shown at the right CELL MOVEMENT The age of the displayed data is shown at the right SIGMET 2m AIRMET 5m SIGMET amp AIRMET The age of the displayed data for each is shown at the right F us 8m CN 8m METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right 54 Garmin G1000 Cockpit Reference Guide for the Socata TBM
143. mer countdown is resumed Entering a Scheduler Message 1 Select the AUX Utility Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight the first empty scheduler message naming field 4 Usethe FMS Knob to enter the message text to be displayed in the Messages Window and press the ENT Key 5 Press the ENT Key again or use the large FMS Knob to move the cursor to the field next to Type 6 Turn the small FMS Knob to select the message type Event Message issued at the specified date time One time Message issued when the message timer reaches zero default setting e Periodic Message issued each time the message timer reaches zero 7 Press the ENT Key again or use the large FMS Knob to move the cursor to the next field 8 For periodic and one time message use the FMS Knob to enter the timer value HH MM SS from which to countdown and press the ENT Key 9 For event based messages a Use the FMS Knob to enter the desired date DD MM YY and press the ENT Key b Press the ENT Key again or use the large FMS Knob to move the cursor to the next field c Use the FMS Knob to enter the desired time HH MM and press the ENT Key 92 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Additional Features 10 Press the ENT Key again or use the large FMS Knob to move the cursor to enter the next message
144. n 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 850 900 190 00708 05 Rev C 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 Predefined Text Messages Time and effort can be saved in typing text messages that are used repeatedly by saving these messages asa predefined message 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 the NEW Softkey Or a Press the b Turn either FMS Knob to place the cursor on Draft New Predefined Message c Press the ENT Key The PREDEFINED SMS T
145. n yellow NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or MFD to be updated label of SD card facing left 2 Turn the system ON A prompt is displayed in the upper left corner of the display DO YOU WANT TO UPDATE THE STANDBY NAVIGATION DATABASE ON THE BOTTOM CARD THE STANDBY DATABASE WILL BE ACTIVATED UPON THE FIRST ON GROUND POWER CYCLE ON OR AFTER 00 00 SYSTEM TIME ON THE EFFECTIVE DATE FROM TO WORLDWIDE WORLDWIDE 1211 1212 26 AUL 2812 18 NOU 2012 23 SEP 2812 15 DEL 2812 NO WILL BE ASSUMED IN 21 SECONDS 3 Press the NO Softkey to proceed to loading the active database 4 A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL QUERWRITE THE ACTIVE NAVIGATION DATABASE FROM TO REGION WORLDWIDE WORLDWIDE CYCLE 1211 1212 EFFECTIVE 26 806 2012 18 NOU 2012 EXPIRES 23 SEP 2012 15 DEC 2012 NO WILL BE ASSUMED IN 8 SECONDS UPDATING THE ACTIVE NAVIGATION DATABASE PLEASE WAIT UPDATED 1 FILES SUCCESSFULLY PRESS ANY KEY TO CONTINUE CONTINUING IN 8 SECONDS 148 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Appendix 5 After the updat
146. nce Connext Server Temporarily Inop The Connext weather data server is temporarily out of service but is expected to return to service in less than 30 minutes Connext Server Inop The Connext weather data server will be out of service for at least 30 minutes Invalid Coverage Area The weather data request coverage area does not contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled checked and contains required criteria then re send the data request NO Connext Subscription The system is not be currently subscribed to Connext or the access code is incorrect Verify the access code Contact Garmin at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance Reduce Request Area The Connext weather data request area exceeds size limits Reduce weather coverage area and re send data request Request Cancelled The user has cancelled a Connext weather data request Requested area too large Reduce coverage area The size of the Connext weather data request has exceeded limits Reduce the size of the coverage area and try the weather data request again Request Failed Try Again The weather data request timed out Re send data request Transfer Preempted The GDL 59 is busy Retry request later 190 00708 05 Rev C Garmin G1000 Cockpit Reference
147. nce Guide for the Socata TBM 850 900 103 AEN 540 S24V oipny uadx sva sjueumajsul eouepioAy paezey s E 2 E 5 2 Sue v unuuy xipueddy x pul iui UI0JNeN nu jeuonippy Annun Additional Hazard Flight Nav Com Flight Appendix Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Index Abnormal Operation 104 Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A GARMIN 190 00708 05 Rev C GARMIN Amunciations amp Alerts ANNUNCIATIONS amp ALERTS CAS MESSAGES Warning Messages Messages Comments Battery temperature over 70 C Cabin altitude over 10 000 ft BLEEDTEMP Bleed temperature high EXPE Cabin pressure differential over 6 2 psi Pilot or cabin door open BEES feathering system failure Engine compartment fire temperature over 200 C if installed 2121011 Dissymmetry between left and right hand flaps MEH coe tank selectors set to Off FUEL PRESS Fuel pressure below 10 psi Gears are in an unsafe configuration Engine start ITT over 1000 C 870 C 5 s or 840 C 20 s Engine running ITT over 840 C EU SM Oil pressure below 60 psi OXYGEN O Oxygen cylinder closed Parking brake applied Torque greater than or equal to 121 4 m
148. ndow select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Hazard avoidance Setting Up and Customizing Weather Data for the Navigation Map Page 1 2 3 4 5 6 7 8 Select the Navigation Map Page Press the MENU Key With Map Setup highlighted press the ENT Key Turn the small FMS Knob to select the Weather Group and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to scroll through options for each product ON OFF range settings Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings Connext Weather Data Requests The Connext Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals if desired and the ability to send or cancel weather data requests The window also displays the status of the Connext data request process Requesting Connext Weather Data Manually 1 2 3 4 Select the Connext Weather Data Link Page Press the MENU Key With Connext Weather Request highlighted press the ENT Key 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
149. ndshield Cyan indicates heat has been selected windshield Green indicates heat is on Yellow indicates heat has failed propeller pitot tube and stall sensor CABIN PRESS ETE SYSTEM GENERAL ALT FT RATE FPM 1000 muc NORTH UP EL TFR pno DATA y SE vTaz zar muc bai q ELEC FUEL General Synoptics Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C amp GARMIN Ay rma Systems CABIN PRESSURIZATION Cabin pressurization information cabin altitude rate of change and differential cabin pressure is shown at the top of the right EIS column Only readouts for cabin altitude and pressure differential are displayed in Reversionary Mode Cabin altitude ALT FT is shown on a color coded scale labeled in 5 000 ft increments with a readout in feet below Cabin altitude change rate RATE FPM is displayed on a scale in terms of 2 000 fpm increments with a readout in fpm below Cabin pressure differential DIFF PSI in pounds per square inch psi is indicated on a color coded scale with a readout Selected Cabin Altitude is displayed as a digital readout in 100 ft increments with a range from 1 000 to 11 000 feet CABIN PRESS ALT FT RATE FPM 1000 15 2 7 Change Pressure 16 Rate Altitude Landing Field Elevation Entered Manually Pressure DIFF S Differential R Altitude LFE FT 1858 7 rs i es ot FT LFE 5187
150. nformation related to the use of databases in the National Airspace System e Garmin equipment will only recognize and use databases that are obtained from Garmin or Jeppesen Databases obtained from Garmin or Jeppesen are assured compliance with all data quality requirements DQRs by virtue of a Type 2 Letter of Authorization LOA from the FAA A copy of the Type 2 LOA is available for each database and can be viewed at http fly garmin com by selecting Type 2 LOA Status Use of a current Garmin or Jeppesen database in your Garmin equipment is required for compliance with established FAA regulatory guidance but does not constitute authorization to fly any and all terminal procedures that may be presented by the system It is the pilot s responsibility to operate in accordance with established AFM S and regulatory guidance or limitations as applicable to the pilot the aircraft and installed equipment NOTE The pilot operator must review and be familiar with Garmin s database exclusion list as discussed in SAIB CE 14 04 to determine what data may be incomplete The database exclusion list can be viewed at www flygarmin com by selecting Database Exclusions List NOTE The pilot operator must have access to Garmin and Jeppesen data base alerts and consider their impact on the intended aircraft operation The database alerts can be viewed at www flygarmin com by selecting Aviation Database Alerts 190 00708 05 Rev
151. ng 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 13 sjuauimasu Yid SoJnpa20Jd Duruue d AEN Sd5 241V oipny uadx 3461 WO gt AeN eouepioAy paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 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 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartV
152. ning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the system utilize GPS as a precision elec tronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the system can be misused or misinterpreted and therefore become unsafe 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 environ ment disposal jsp Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C amp GARMIN ningscautons amp Notes WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the Pilot s Guide documentation and the TBM 850 900 Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the system to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING The illustrations in this guide are only examples Never use the system to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thun
153. nsated altitude is enabled for the loaded approach the altitudes associated with the approach waypoints are displayed in slanted text GPS Nav z 8 HABUK iaf 021 5 7NM_ g n rr HABUK iaf 021 5 7NM 8 FALUR 261 4 7NM 860GFT FALUR iL 4 7NM CEGIX faf 35T 5 9NM 7800 CEGIX faf g r 5 9NH RW35R map 351 5 1NM RW35R map 351 5 1NM 6368FT 348 5NM B3BBFT 6368FT 348 5NM E MOGAL 10000F1 MOGAL mahp HOLD 168 211 HOLD 68 6 0NH 25 85 Altitudes Displayed Without Altitudes Displayed With 5 Temperature Compensation Temperature Compensation Bu 52 9 2 lt Enabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed Abnormal Operation 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Annun Alerts 4 Use the small FMS Knob to select the temperature at the airport The compensated altitude is computed as the temperature is selected 5 Press the ENT Key ACTIVATE COMPENSATION is highlighted 6 Press the ENT Key The compensated altitudes for the approach are shown in the flight plan Appendix Index 48 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Disabling temp 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed Procedures
154. ob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN Ps Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key
155. oint 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 Turn the d Press the arge FMS Knob to select the desired waypoint ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FM S Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FM S Knob to activate the cursor 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 35 sjuauimasu Yid oipny udd
156. onnext prior to registration 3 If the system displays the Garmin Flight Data Service Registration window proceed to step 7 Otherwise press the MENU Key The Page Menu window is now displayed 4 Turn the large FMS Knob to select Register With Connext in the menu list 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 55 suelv uoneiedo s m p q SoJnpa204d Duruue d AEN Sd5 S24V oipny uadx Sv3 Sjueumasu junuuy Jeuuouqy Jeuonippy puezey Wo gt AeN xipuaddy x pul iui Wfi l4 Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 5 Press the ENT Key The Garmin Flight Data Service Registration window is now displayed 6 Enter the access code provided by Garmin Connext in the ACCESS CODE field 7 Press the ENT Key REGISTER will now be highlighted 8 Press the ENT Key The system will contact Garmin Connext System registration is complete when REGISTERED is displayed in the STATUS field Accessing Connext Weather Products Weather data is provided when the pilot initiates either a manual or automatic Connext data request on the Connext Weather Data Link Page on the MFD No weather data is displayed until the first Connext Weather Data Request is made 1 Turn the
157. onsists of choosing from a pre determined list of requests entering the required information and sending the request To create messages 1 From the MFD select the CPDLC Softkey 2 Select the NEW Softkey The CPDLC Thread Window appears 3 With the Response Request field highlighted turn the small FMS Knob to select the desired request from the list and press the ENT Key For discussion purposes Request level is selected 4 Highlight the Level field and enter the desired altitude To toggle between multiple units of measure FT or FL highlight the first numeric position and turn the small FMS Knob counterclockwise 5 Press the ENT Key to complete the entry 6 Highlight the Reason field and enter the desired reason from the list 7 Press the ENT Key to complete the entry 8 Highlight the SEND Button and press the ENT Key Responding to an ATC Message Responding to an ATC message consists of choosing from a pre determined list of responses or acknowledgements then sending the response or acknowledgement To respond to a message 1 From the MFD select the CPDLC Softkey 2 Turn the large FMS Knob to place the selection cursor over the desired message and press the ENT Key 3 Turn the small FMS Knob to select the desired Response Request from the list and press the ENT Key 4 Highlight the SEND Button and press the ENT Key 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 9
158. p Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments The MFD and or PFD detected a fault in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a fault in the Safe Taxi database Ensure the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a fault in the ChartView 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 database error exists The MFD detected a fault in the FliteCharts database op
159. passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A fault has been detected in the GPS1 and or GPS 2 receiver The receiver may still be available If the message persists through a normal power cycle the system should be serviced when practical NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A fault has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced 122 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck Comments The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A fault has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G S1 needs service Return
160. pear 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 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C 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 Ay CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Navigation Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the smal FMS Knob to select the Navigation Map Page 3 Select the MAP Softkey 4 Select the WX RADAR Softkey Displaying Weather on the Weather Radar Page 1
161. point naming is USR000 USR001 USR002 and so On 5 change the user waypoint name follow the procedure for modifying a user waypoint 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 43 sjuauimasu UATE oipny uddx UI0JNeN 52 2 4 AEN 540 nubi eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Flight Procedures Planning GPS Nav Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Appendix Alerts Operation Features Index Flight Planning A GARMIN EXPORT A FLIGHT PLAN TO AN SD CARD 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 Control 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 850 900 190 00708 05 Rev C GARMIN _ PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPART
162. r inability to use the software or re or an AOPA authorized representative has been sue AOPA and to the maximum ovided as is g its accuracy nd to the m zations from a uracies in the information arising isdictions do not allow the or consequential damages dental special or ated advised of the extent allowed ated s or losses re ation Some jurisdictions do not allow the lity for incidental or conseque ntial damages ganizations cluded in this of merchantability and AC U KWIK eliability or axlmum extent ny cause of n inted in the U S A amp GARMIN __ Warnings Cautions 5 Notes e e e 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
163. ress 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 OPTI 1 Press the AD ONAL F DME or DME Softkey 2 Tum 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 13 sjuauimasu UATE S24V sva JUI05 AEN sualy uonesado saunqea4 2 4 AEN Sd junuuy jeuuouqy paezey Wfila x pu ddy x pul Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audio EAS GPS Nav Procedures Appendix Alerts Operation Features Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder mode selection softkeys If two transponders are available press XPDR1 or XPDR2 to set the active transponder Otherwise proceed to step 3 Press the CODE Softkey to display the transponder code selection softkeys for digit entry Use the digit keys to enter the code in the code field When entering the code the next key in sequence must be presse
164. rn the large FMS Knob to highlight the ON OFF a field 52 5 the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey AEN Sd5 SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO TEMP COMP 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 aoueplony SoJnpa204d Duruue d Wil paezey saunqea4 jeuonippy MANUALLY TESTING THE RADAR ALTIMETER KRA 405B ONLY 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 uoneiedo Jeuuouqy Sue v unuuy 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test xipuaddy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 3 A Flight Instruments GARMIN El DISPLAYING WIND DATA 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change
165. rrection is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable correction is unavailable ADC2 AS EC ADC2 airspeed error GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN GCU 475 MESSAGE ADVISORIES Annunciations amp Alerts Message GCU CNFG GCU Config error Config service req d Comments GCU 475 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative MANIFEST GCU software mismatch communication halted A fault has been detected in the GCU 475 The GCU 475 is unavailable The GCU 475 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORI
166. rrors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun cated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way points locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was
167. rts Operation Features Avoidance Index 4 5 6 7 Flight Planning GARMI N Use the FMS Knobs to edit the length and press the ENT Key Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while ACTIVATE is highlighted to immediately activate the hold REMOVING A USER DEFINED HOLD CREATED AT THE AIRCRAFT P POS 1 2 3 4 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the PPOS H waypoint Press the CLR Key A Remove Holding Pattern confirmation window is displayed Select OK and press the ENT Key The holding pattern is removed from the active flight plan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern REMOVING A USER DEFINED HOLD CREATED AT AN ACTIVE WAYPOINT 1 2 3 4 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the HOLD waypoint Press the CLR Key A Remove Holding Pattern confirmation window is displayed Select OK and press the ENT K
168. s The GTS has incorrect software installed The G1000 system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments 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 find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Verify user modified procedures DB CHANGE Database changed Comments This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified proc
169. s different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced 114 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message Comments 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 A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low
170. s to select the desired SiriusXM 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 Panning over an airport with METAR information does not display more 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 53 AEN Sd5 S24V oipny uadx Sv3 s u umn sul u102 AEN nubi buluueld nf aoueploay s mp oold paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav p Hazard Avoidance Procedures JL Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific infor
171. semap database error exists Comments The MFD and or PFD detected a fault in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists The MFD and or PFD detected a fault in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a fault in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU 116 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations am
172. sired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint pr 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00708 05 Rev C oceed to step 6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 25 sjueuimnasu Yid oipny uddx JUI0JNeN ACN 540 52 Suelv uoneiedo sainjea4 aoueplony sainpadold Duruue d unuuy Jeuuouqy Jeuonippy 2 Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Kn
173. ssage will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Updating Basemap SafeTaxi Airport Terrain Obstacle and Airport Directory Databases These databases may be copied to one Supplemental Data Card then automatically synchronized to other card in the system 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the basemap SafeTaxi airport terrain obstacle and or airport directory databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen If a Verifying message is
174. stem check that the databases are initialized and displayed on the power up screen A Verifying message may be seen If this message is present wait for the system to finish loading before database is inserted in the MFD proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right mos 6 Turn the large FMS Knob to select the AUX Page group on the MFD t softkey 7 Turn the small FMS Knob to select the System Status Page 8 Press the Display Database Selection Softkey to show database information for each display MFD1 DB or PFD1 DB Verify the correct database cycle information is shown for each database for each display 190 00708 05 Remove power from the system Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 147 sjuauimasu Yid soJnjeaJ 2 AEN Sd 24V oipny uadx Jeuonippy paezey nubi uo2 AEN uoneiedo Jeuuouqy sue v unuuy GARMIN Loading the Jeppesen Navigation Database as the Active Navigation Database The Jeppesen Navigation Database that is loaded to internal memory as the active database will be used by the system NOTE Loading the Jeppesen Navigation Database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed i
175. su fila Sv3 oipny uadx U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s l Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 98 GARMIN 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 Activation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel e PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MED By pressing the DISPLAY BACKUP Button on the left or the right audio panel PFD2 By pressing the DISPLAY BACKUP Button on the right audio panel NOTE The Socata TBM 850 900 Airplane Flight Manual AFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios HAZAR
176. 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 135 sjuaumasu yp s n 2 4 Buruue d AEN Sd5 2 444 paezey 346 UI05 AeN jeuonippy uoneiedo Jeuuouqy iic Eu x pul Flight Instruments Nav Com XPDR Audio Additional Hazard Flight Planning Abnormal EAS AFCS GPS Nav Features Avoidance Procedures Operation Appendix Index Annunciations amp Alerts 136 Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 A GARMIN 190 00708 05 Rev C amp GARMIN o Appendix APPENDIX sjueuimasu UATE PFD SOFTKEY MAP m rs pmpnnunnn 5 3 CDI NAV1 olpny uqax uo2 AEN CD NAV2 CDI GPS 52 Top Level PFD Softkeys AEN Sd5 uNummummumm 9n wn optional optional optional Duruue d nubi s snp oold Select the BACK Softkey to return to the top level softkeys Ec Inset Map Softkeys as Level 1 Level2 Level 3 Description INSET Displays Inset Map in PFD lower left corner HE HE OFF Removes Inset Map DCLTR
177. synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable System has updated the active navigation database from the standby navigation database One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid GMA 1347D MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA2 FAIL GMA2 is inoperative The audio panel self test has detected a fault The audio panel is unavailable The G1000 system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d error Config service req d GMA2 CONFIG GMA2 config The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The MANIFEST 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
178. t 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 Fus selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 21 svi Sjueumasu oipny uadx 0105 AEN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony 2 Duruue d Junuuy jeuuouqy jeuonippy xipuaddy x pul ii nu paezey Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude AFCS armed to capture the altitude displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key ALT nnnnn rr Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key VS nnnn Fem to the Selected
179. t has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid 132 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message VNV Unavailable Parallel course selected Comments A parallel course has been selected causing the vertical deviation to go invalid NON WGS84 WPT Do not use GPS for navigation to xxx STRMSCP FAIL Stormscope has failed The position of the selected waypoint xxxx 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
180. t 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C GARMIN ight Planning 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted CREATING A USER DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the waypoint for the hold 3 Press the MENU Key highlight Hold At Wpt and press the ENT Key The HOLD AT window appears with the course field highlighted 4 Usethe FMS Knobs to edit the entry co
181. t 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 AIRPORT DIRECTORY The AOPA or AC U KWIK 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 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A SIRIUSXM SATELLITE RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Tum 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 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
182. tem should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when practical Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES CONT Message AHRS2 GPS AHRS2 using backup GPS source Comments The 2 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when practical AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The G1
183. teness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C amp GARMIN Cautions E Notes NOTE Operating the system in the vicinity of metal buildings metal structures or electromagnetic fields can cause sensor differences that may result in nuisance miscompare annunciations during start up shut down or while taxiing If one or both of the sensed values are unavailable it will be annunciated as a NO COMP no compare NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The FAA has asked Garmin to remind pilots who fly with Garmin database dependent avionics of the following t is the pilot s responsibility to remain familiar with all FAA regulatory and advisory guidance and i
184. th the navigation database At startup the system compares this version of the MV DB with that presently being used by each AHRS GRS1 and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure GRS1 MV DB Update Available Update from 2005 to 2010 GRS1 Magnetic Field Variation Database Update Prompt 1 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed Uploading GRS1 Mag Var Database STARTING UPLOAD Uploading Database to GRS1 2 When the upload is complete the prompt for the next GRS upload is displayed GRS2 MV DB Update Available Update from 2005 to 2010 OK GRS2 Magnetic Field Variation Database Update Prompt 152 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN Appendix 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed When the upload is complete the system is ready for use sjueuinasu BUT 593 Uploading 5852 Mag Var Database STARTING UPLOAD oipny uddx JUI0JNeN 52 Uploading Database to GRS2 uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 jeuuouqy jeuonippy paezey wd Sue v yunuuy gt 5 4 x 3 x x pul 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 153 GARMIN Appendix Sjueuinijsu fila
185. 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 h now indicate ighlighting YES press the ENT Key The message symbols all the message have been opened Delete a Message 1 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor 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 Press the 190 00708 05 Rev C ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 89 xipuaddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S241V olpny uqax sv sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u05 AeN 3461 x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 8 11 GARMIN MAINTENANCE LOGS The system provides recording of CAS CMC exceedances and other critical aircraft data that occur while the aircraft is on the ground or in flight The Maintenance Logs feature is accessible by entering a password No pilot action is required
186. 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 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 19 sjueuimasu nubi 5 3 S24V oipny uddx JUI05 AEN sualy uonesado saunqea4 2 Buruuejd AEN 5649 junuuy jeuuouqy jeuonippy paezey Wfila x pu ddy x pul Flight Instruments Nav Com AFCS XPDR Audio EAS Abnormal Additional Hazard Flight Planning Annun GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN 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 Ifa COM input signal is detected during play of a recorded memory block play is halted 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 r
187. the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a 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 CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 101 aoueplony Buruuejd AEN 540 S24V oipny uadx sv3 Sjueumajsul piezeg wio gt AeN sub saunyea4 jeuonippy xipuaddy suelv unuuy x pul Flight Ins
188. 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 2 3 4 5 6 1 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 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 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C 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 d
189. the starting vvaypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending vvaypoint field Enter the identifier of the ending vvaypoint and press the ENT Key to accept the vvaypoint Or Fo a b d Or For a b o d point to point planning Enter the identifier of the starting vvaypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint Press the ENT Key to accept the waypoint flight plan leg planning Select the FPL Softkey at the bottom of the display Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps 5 Turn the large FMS Knob to highlight the departure time DEP TIME field
190. then turn the small FMS Knob to highlight a profile from the list and press the ENT Key If desired the profile name to be used after profile has been imported can be changed by turning the FMS Knob to highlight the PROFILE NAME field then use the large and small FMS Knobs to enter the name and press the ENT Key Imported profile names cannot begin with a blank space or be named DEFAULT GARMIN DEFAULTS or DEFAULT SETTINGS With IMPORT highlighted press the ENT Key If the imported profile name is the same as an existing profile on the system the system displays an Overwrite existing file OK or CANCEL prompt Press the ENT Key to replace profile on the system with the profile imported from the SD card or turn the FMS Knob to highlight CANCEL and press the ENT Key to return to the Pilot Profile Importing Window If successful the system displays Pilot profile import succeeded in the IMPORT RESULTS window below With OK highlighted press the ENT or CLR Keys or press the FMS Knob to return to the AUX System Setup Page The imported profile becomes the active profile Exporting a Profile to an SD Card 1 2 3 4 5 Insert the SD card for storing the Pilot Profile into the top card slot on the MFD Turn the FMS Knob to select the AUX System Setup Page If necessary activate the desired pilot profile to export Only the currently active Pilot Profile can be exported
191. tional feature Ensure the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a fault in the Airport Directory database Ensure the data card is properly inserted Replace data card If problem persists the system should be serviced 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 117 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax Sv3 sjueumasu puezey ubi UI05 AeN ubi jeuonippy uoneiedo Jeuuouqy a x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments The PFDs and MFD have different navigation 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 Navigation database mismatch The PFDs and MFD have different standby navigation database versions or regions installed Chec
192. to deactivate the flight plan This will not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN zu aa ri MK EI arce White 22177 90M 12400FT T 220 MSS nnam a Large Cyan sin KDFW RNAV 17LsPs LPV RIVET iaf MEI ME SES Small Cyan 3 3NM 2000FT Text INWOD 76 Small Cyan MENOL fuf 176 3 9MM Subdued Text RW17L map b 3NH 3 Small White Text 990FT 2 8 with Altitude POLKE Restriction Bar SUS Cross AT or ABOVE 5 000 fi Fac Cross AT 2 300 ft Cinn ia Cross AT or BELOW 3 000 ft 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 2 sv sjuauimasu Yid olpny uqax uo2 AEN Suelv uoneiedo sainjea4 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EAS Appendix Alerts Operation Features Avoidance Procedures Index A GARMIN 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 disp
193. truments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation A GARMIN As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes Terrain Proximity TERRAIN SVT 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 SUSPECTED AUTOPILOT MALFUNCTION NOTE Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure If an autopilot failure or trim failure is suspected to have occurred perform the following steps 1 Firmly grasp the control wheel 2 Press and hold the AP DISC Switch The autopilot will disconnect and power is removed from the trim motor Pow
194. ts 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 identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Message Window Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C A GARMIN 7 X MAppendix MFD SOFTKEY MAP sjueuimasu Yid CAS or optional optional Boum SHORT s gt Es Es 7 A Se on Rs ES miz s Select the BACK Softkey on this level optional optional to return to the top softkey level PRECIP DL LTNG optional optional optional optional TERRAIN NEXRAD XM LTNG WX RADAR e a t lt AIRWAY HI Duruue d ni F3 F3 V3 V3 V3 V3 HS V3 VS 7 7 7 svsrew cas J we I ee et een Test F3 ES V3 V3 V3 EN V3 V3 IN 3 3
195. umasu puezey ubiu wio gt AeN ubi jeuonippy uoneiedo Jeuuouqy iic EA x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Ed Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message transfer key is stuck COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote Comments The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced with other NAVS GPS NAV LOST Loss of GPS navigation Insufficient satellites LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase of flight Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after
196. unication halted MANIFEST COM2 software mismatch communication halted The COM1 and or COM2 has incorrect software installed The system should be serviced MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted The NAV1 and or NAV2 has incorrect software installed The system should be serviced COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a fault in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when practical COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck 190 00708 05 Rev C 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 121 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax sv sjue
197. urse and press the ENT Key 5 Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key 6 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 7 Use the FMS Knobs to edit the length and press the ENT Key 8 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 9 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key 10 Press the ENT Key while LOAD is highlighted to add the hold into the flight plan CREATING A USER DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the MENU Key highlight Hold At Present Position and press the ENT Key The HOLD AT window appears with the Length mode highlighted 3 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key SoJnpa20Jd AEN 540 nubi 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 39 SjueuinJjsu iui oipny uddx UI0JNeN 52 2 Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Ale
198. ve 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 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 190 00708 05 Rev C E GARMIN Additional Features SATELLITE TELEPHONE amp SMS MESSAGING SERVICE Operation of these features in the cockpit is accomplished through the AUX TELEPHONE AUX
199. ve been entered Entering Fuel Pa rameters 1 If necessary press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the des 6 Press the FM TRIP PLANNING ired reserve fuel quantity S Knob to remove the cursor 1 Tum 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 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 29 sjuauimasu UATE oipny uddx UI0JNeN 52 2 4 AEN 540 Juil eouepioAy 2 suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 For a b o d A GARMIN Direct to planning Select the VVPTS Softkey and verify that
200. was removed from the top card slot of the PFD or MFD The SD card needs to be reinserted 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 133 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax sv sjueumasu puezey BITTE UI05 AeN ubi jeuonippy uoneiedo Jeuuouqy nies Eu x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix n Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card Comments The SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data The SD card in the bottom card slot of the PFD or MFD contains invalid data ECS Service required The Environmental Control System has failed EPS Service required Electrical Power System needs servicing EPS S G speed sensor failed Starter Generator speed sensor has failed CRUISE 1 Cruise conditions met Cruise engine trend data log has been captured CRUISE l Cruise l conditions met
201. x UI0JNeN 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 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 modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the Cursor Creating a stored flight plan 1 2 3 4 5 6 7
202. y Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor 11 12 13 14 190 00708 05 Rev C Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 900 33 s tin sul sub oipny uddx UI0JNeN 52 2 4 AEN 540 nubi aoueplony paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 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
203. yuqax 573 siu u nnsul Tu102 AEN 346 aoueplony paezey s m e q jeuonippy xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN Enable Disable Incoming Text Message Pop Up Alerts 1 2 3 With the AUX TEXT MESSAGING Page displayed press the MENU Key on the MFD to display the Page Menu Turn either FMS Knob to place the cursor on Disable New Message Popups or Enable New Message Popups 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 Press the ENT Key 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 o

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