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Garmin Software Version 0719.03 Cockpit Reference Guide

1. AEN 5649 2 olpny uqax svi syu unysu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy EM EE 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 MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation datab
2. ssssssseeennnnnn 3 Displaying Wind Data 3 Changing HSI Format nnns 4 ENGINE amp AIRFRAME SYSTEMS 5 Electrical System iiss eene eterne eti ttr tts 6 Fuel System tete tenere iste Mende nean 8 General mede oem een e etn RID n HORE RERO 0 NAV COM TRANSPONDER AUDIO PANEL 1 Enter or Change Flight ID sssseennnn 1 ADF Tuning 1 DME Tunihij e en t tme eem tta rem tht one be 1 Enter a Transponder Code seen 2 Selecting a COM Radio 2 Selecting a NAV Radio 2 NAV COM Tuning x rtr ree rt tene prit treno te t 2 lire 3 Passenger Address PA System 3 Clearance Recorder and Player 3 AUTOMATIC FLIGHT CONTROL 5 5 Flight Director Activation sssssssen nnne 5 Vertical Modes nnne 6 Lateral Modes asia dae iacta HU o LER ER RE 7 GPS NAVIGATION v a a a 9 Direct to Navigation sssssssseeee nnne 9 Activate a Stored Flight Plan 20 Activate a Flight Plan Leg 20 Stop Navigating a Flight 7755 21 Vertical
3. 4 AEN 540 nubi uoneiedo saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MED it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 7 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 30 1 2 3 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL K
4. XPDR2 SRVC XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL XPDRT is There is no communication with the 1 inoperative transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving 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 system 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 AHRS2 GPS AHRS2 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible The 2 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving any GPS information The 2 AHRS is not
5. 35 Activate A Missed Approach in the Active Flight Plan 36 HAZARD AVOIDANCE 37 Customizing the Hazard Displays on the Navigation 37 STORMSCOPE Optional XM Weather 7 Traffic Systeiis sisanne enni td teet tud Terrain And Obstacle Proximity Terrain SVS Terrain Awareness amp Warning System TAWS Display 45 Airborne Color Weather Radar 4 ADDITIONAL FEATURES ssssssss nn Synthetic Vision aoi ati em aimi atitem ra HIER HR TERR Terminal Procedure Charts XM Radio Entertainment Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Table of Contents ABNORMAL OPERATION Reversionary Mode sssssssssseeeenn entente Abnormal COM Operation sssssssssseennnennnnnn Hazard Displays with Loss of GPS Position Unusual Attitudes sseeennnnnnnnnnne Dead Reckonitig erem eerte er Rer er eerie ANNUNCIATIONS amp ALERTS CAS Messages sss Comparator Annunciations Reversionary Sensor Annunciations AFCS Alerts Terrain SVS Alerts Terrain SVS System Status An
6. Elevator Mistrim Up Pitch servo providing sustained force in the indicated direction Pitch Trim Failure or stuck MEPT Switch PTRM f AP engaged take control of the aircraft and disengage AP f AP disengaged move MEPT switches separately to check if a stuck switch is causing the annunciation Yaw Trim Failure or stuck MEYT Switch YTRM TAP engaged take control of the aircraft and disengage AP TAP disengaged move the MEYT switch to check if a stuck switch is causing the annunciation Yaw Damper Failure Y m YD control failure AP still operative Roll Failure ROLL Roll axis control failure AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure TELLE AFCS AP and MEPT are unavailable FD may still be available 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 65 Sonje2J eouepioAy s mp oold Buruue d AEN Sd5 yi oipny uddx sv3 Sjueumansu paezey nubi jeuonippy uoneiedo Jeuuouqy 55 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix end Annunciations amp Alerts A GARMIN Alert Condition Annunciation Description Preflight Test PFT Performing preflight system test aural alert sounds at complet
7. Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance 46 A GARMIN 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 Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS 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 Page is displayed select the INHIBIT Softkey 1 2 3 Or While the TAWS Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Hazard Avoidance AIRBORNE COLOR WEATHER RADAR WARNING Be
8. A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT GA Switch Go Around GA Go Around GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS NAV Key Navigation VOR Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT GPS Pitch Hold default PIT APR Key Approach VOR Glidepath GP LOC Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAVor APR Key press activates flight director The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director 190 007
9. METERS IN HPA A GARMIN 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 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Select to display the BARO setting as inches of mercury Select to display the BARO setting as hectopacals Sets altimeter setting to standard barometric pressure Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Appendix mumu mumu uu sjuauimasu yp XPDR1 XPDR2 STBY ON ALT GND VFR CODE IDENT BACK MSG Fu F3 5 09 9 n9 ru unun Select the BACK Softkey to return to the top level softkeys 5 3 LT TT T Ts L s L 5 L 7 ekse T back L veo A V3 F3 A 9n n o n EH Select the BACK Softkey to retur
10. Select the STD BARO or BACK Softkey to return to the top level softkeys oipny uddx U105 AeN TL 360 HSI ARC HSI F amp V3 77 7 7 onm j CL eres I C o F3 F3 Hu HU US ES nmn VS cm Torms 1 L 1L L L se L vse 1 EF V3 Hu 7 EE MH a meae OOOO p amp m nnxnnnnn PFD Configuration Softkeys 5 Displays second level softkeys for F additional PFD configurations SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features so1njeoJ jeuonippy PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan uoneiedo Jeuuouqy SYN TERR Enables synthetic terrain depiction HRZN HDG Displays compass heading along the Zero Pitch line Sue v unuuy APTSIGNS 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 gt 5 3 x x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix DFLTS VVIND DME BRGI HSI FRMT BRG2 ALT UNIT STD BARO 92 OPTN 1 OPTN 2 OPTN 3 OFF 360 HSI ARC HSI
11. The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX or NOTAM Softkey to access charts for departures arrivals approaches weather or NOTAMs 3 Select the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 3 sjuauimasu nubi s snp o4d Duruue d AEN Sd5 241V oipny uaddx 346 Tu102 AEN eou
12. x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Flight Instruments GARMIN El CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI Annun Abnormal Additional Hazard Flight Nav Com Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Appendix Index Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMI N Engine 8 Airframe Systems ENGINE amp AIRFRAME SYSTEMS CABIN PRESS ALT FT RATE FPM X1000 Vost 2 2 9300 B Sjueuinijsu sufi 0 0 DIFF PSI x wa og zs Bo 55 23 S24V L FUEL QTY R 122 usa 122 125 108 75 50 25 l 9 8 ELECTRICAL AMPS 33 VOLTS gi 276 STALL HEAT ON B 27 6 PROP DEICE ON PITOT HT ON L R IGNITION FUEL LOW L R ACN Sd5 Buiuue d G CABIN PRESS ALT FT 4408 DIFF PSI 2 7 SoJnpa20Jd 0077560700 GGG 2 G oo Qo saunjea4 leuonuppv uoneredo jeuuouqy EIS Display Normal Mode EIS Display Reversionary Mode Torque CAS Display 3 Fuel Flow lia Propeller Speed 5 Altitude and 14 Fuel Pressure gt Change Rate Generator Speed Differential Pressure 5 dn and Generator E Currents nterturbine Tempera
13. DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists Comments The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists PFD2 DB ERR PFD2 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a fail
14. Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Turn the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING 1 Press the ADF 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 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauimasu UATE 5 3 S24V oipny uddx JUI05 AEN SH lV uonesado so1njeoJ 2 Buruuejd AEN Sd junuuy paezey xipueddy x pul Flight Instruments Flight Planning Abnormal Additional Hazard Avoidance Annun Nav Com AFCS XPDR Audi 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 Press the XPDR1 or XPDR2 Softkey to select the active transponder Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering
15. information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Socata TBM 850 Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Warnings Cautions amp Notes GARMIN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable
16. the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC or COM2 MIC on the audio panel Receive Only Press the COM1 or COM2 on the audio panel SELECTING A NAV RADIO 1 Press the CDI Softkey to select NAV1 VOR1 LOC1 or NAV2 VOR2 LOC2 2 Pressing the NAV1 NAV2 DME or ADF Key on the audio panel selects and deselects the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Pav Com XPDR Audio Panel INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom
17. to indicate when play is in progress The PLAY annunciator turns off after playback is finished 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjueumasu SV3 S24V oipny uddx JUI05 AEN Suelv uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN SdD unuuy jeuuouqy jeuonippy 2 xipuaddy x pul iui nu Flight Instruments Nav Com AFCS XPDR Audi EAS Flight Planning Abnormal Additional Hazard Avoidance Annun Procedures GPS Nav Appendix Alerts Operation Features 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 If a 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 recorded block Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis AFCS
18. 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy mun 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index 4 A GARMIN Garmin International Inc 1200 East 1 51 st Street Le 66062 U A ud AU a 5040 9RB n No 68 Jangshu 2nd Shiir Taipei County 2007 2008 Garmin Ltd or its subsidiaries 190 00708 01 Rev B
19. 540 buluueld nf s mp old uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 36 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the go around button Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B 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 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
20. Altitude ALTV window Glidepath Cap ures and tracks the WAAS GP glidepath on approach APR Key Glideslope Captures 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 Switch Go Around commands a constant preprogrammed GA pitch attitude and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured inste ad of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 16 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN attitude and wings level AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Low Bank Limits maximum commanded roll angle 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 Tra
21. Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 SjueuinJjsu iui oipny uadx 0105 AEN 52 eouepioAy 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 5 6 A GARMIN Select the DELETE Softkey A Delete flight plan 22 confirmation window is displayed With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 32 1 2 3 4 5 Press the FPL Key to display the Active Flight Plan Page on the MFD Press the Joystick to a
22. Parallel track unavailable Comments Bad parallel track geometry invalid leg type PTK FAIL Parallel track unavailable Invalid leg type for parallel offset past IAF PTK FAIL Parallel track unavailable IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation Doox The selected waypoint box does not use the WGS 84 datum Cross check position with alternate navigation sources TRAFFIC FAIL Traffic device has failed The G1000 is
23. 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 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Terrain and s mp oo4d Buruuejd AeN Sd5 S24V oipny uadx sva siu u nnsul D E Tu102 AEN 346 eouepioAy paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on
24. 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 annunciatoris lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is extinguished the ICS Knob controls only volume PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the INTR COM Key is enabled PA messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator flashes
25. again to cyde its operation If the problem persists the G1000 system should be serviced 6 51 FAIL 6 51 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 190 00708 01 Rev B 7 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauimasu sub SoJnjeaJ aoueplony Fuluueld AEN Sd5 2 oipny uadx paezey 346 u102 AEN jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix eu Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings d
26. all altitude airways and then high altitude airways 6 Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted 7 Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 29 sjuauimasu nubi olpny uqax 0105 AEN 52 2
27. attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference
28. 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 75 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 saunyea4 AEN 540 2 oipny uadx paezey 346 u102 AEN jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted Comments A GIA mismatch has been detected where only one is WAAS capable MANIFEST G A1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power The system has detected a
29. press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional System Self Test 1 Setthe range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert TAS System Test Fail is heard 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuaumnasu sub AEN Sd5 52 oipny uadx 0105 AEN Duruue d ni aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOV
30. that may cause undesired operation Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B da GARMIN Serin Cautions amp Notes NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the complete system are found in the G1000 Pilot s
31. the CHNL Softkey 2 Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Select the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 55 sjuauimasu nubi xipueddy suelv uoneiedo sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 52 olpny uqax unuuy Jeuuouqy jeuonippy paezey U10 AEN x pul Nav Com XPDR Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 56 3 Select any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Select the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 With the XM Radio Page display
32. the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying 32 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Additional Redhires the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle ChartView ChartView resembles the paper version of Jeppesen 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
33. 0 ft Cabin pressure differential over 6 2 psi X Pilot or cabin door open Engine compartment fire temperature over 200 C if installed Dissymmetry between left and right hand flaps uel tank selectors set to Off uel pressure below 10 psi Engine start ITT over 1000 C 870 C 5 s or 840 C 20 s Engine running ITT over 840 C Oil pressure below 60 psi Oxygen cylinder closed Parking brake applied Torque greater than or equal to 124 5 maximum torque gt lt 1 TE EE 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 SoJnjeaJ e2ueproAy SaJnpa20Jd Duruue d AEN Sd5 241V oipny uddx Sv3 Sjueuingjsu puezey ubi uH02 AEN ubiu jeuonippy uoneiedo jJeuuouqv x pul Annunciations amp Alerts Caution Messages Flight Instruments A GARMIN Inhibits EAS Messages Comments ENGINE OFF ENGINE ON GROUND LOPI Nav Com Fuel timer off or out of service gt lt TOPI AIR XPDR Audio Electric fuel pump running manual or automatic mode AFCS Battery current over 50 A while on ground Battery off Flow control and shut off valve shut off valve dosed GPS Nav Oil chip detector on if installed Forward baggage door open gt lt gt lt lt gt lt Flight Planning Fuel tanks imbalanced b
34. 08 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 15 sjuauimasu sub SV3 oipny uadx wio gt AeN ARN Sd5 52 suey uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy 2 xipueddy 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 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 2 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 Altitude Flight Level Change Maintains the current aircraft airspeed HC mna IAS Hold in KIAS or Mach Number while the 207 FLC Key Flight Level Change aircraft is climbing descending to the Mach Hold elected Altitude VNAV Captures and tracks the VNAV flight VNV VPTH path Key AFCS armed to capture the altitude VNAV Target i Altitude Amed disp ayed in the VNAV Target
35. 1000 system should be serviced G mismatch communication halted GMA1 SERVICE GMAT needs f sjuaumnasu sub SV3 The audio panel self test has detected a problem in the unit Certain audio functions may still be avail able and the audio panel may still be usable The G1000 system should be serviced when possible Service Return unit for repair u GMA2 SERVICE GMA2 needs Service Return unit for repair GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIAT over The GIA1 and or GIA2 temperature is too high 57 If problem persists the 61000 system should be j GIA2 COOLING GIA2 over pri p serviced temperature PE GIA1 SERVICE G A1
36. ARMI N 44 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN Hazara avoidance A NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAW
37. Alerting is disabled No GPS position or excessively degraded GPS signal Annunciations amp Alerts PFD MFD TERRAIN SVS Page Annunciation TER FAIL TER N A System Test in progress TER TEST System Test pass Terrain System Test OK Aural Message Terrain System Failure one Terrain System Not Available Terrain System Available will be heard when sufficient GPS signal is re established one TAWS ALERTS PFD MFD MFD Alert Type TAWS Page Aural Message nr Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance or Pull Up Waring RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up m Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstade Obstacle Pull Obstade Clearance or Up Pull Up Waning ROC Obstacle Ahead Pull Up Obstacle Ahead Pull Up 190 00708 01 Rev B 67 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Sonje2J eouepioAy s mp oold Buruue d AEN Sd5 2 olpny uqax svi sjueumasu paezey u102 AEN nubi jeuonippy uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Oper
38. E or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AND OBSTACLE PROXIMITY 42 NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the last rectangular page icon If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN avoidance Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 a
39. G 1000 ntegrated Flight Deck Cockpit Reference Guide System Software 0719 03 or later TBM 850 SOCATA A GARMIN Copyri This m 850 ght 2007 2008 Garmin Ltd or its subsidiaries All rights reserved anual reflects the operation of System Software version 0719 03 or later for the Socata TBM Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin 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 be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express W not be itten permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided tha
40. GARMIN Hazard Avoidance Sjueuinijsu fila 593 oipny uadx U105 AEN s24v AeN Sd5 Duruue d Blank Page 6 2 4 eouepioAy paezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 50 A GARMIN SYNTHETIC VISION Additional Features ADDITIONAL FEATURES Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements have been added to the e Pathways PFD e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Traffic Airport Signs e Runway Display Displaying Synthetic Terrain 1 Press the PFD 2 Press the SYN 3 Press the SYN Softkey VIS Softkey TERR Softkey 4 Press the BACK Softkey to return to the previous page Displaying Pathways 1 Press the PFD 2 Press the SYN Softkey VIS
41. GWX is inoperative The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 The GWX 68 may still be usable MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The G1000 system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm GDC 74B MESSAGE ADVISORIES Message Comments ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable ADC2 AS EC ADC2 airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed error correction is unavailable MANIFEST GDC1 software mismatch communication halted MANIFEST GDC2 software mismatch communication halted The GDC 74B has incorrect software installed The G1000 system should be serviced 82 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN GCU 475 MESSAGE ADVISORIES Annuncia
42. Guide for this aircraft 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Warnings Cautions amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Revisions Part Number Change Summary 190 00708 00 nitial Release 190 00708 01 Added SVS and other GDU 9 02 parameters RevA Revision Date of Revision Affected Pages July 2008 Clerical changes 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Record of Revisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Tibleof Contents FLIGHT INSTRUMENTS atrii tti teat tn 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure sssssssse 1 Change Altimeter Barometric Pressure Setting Units 1 Synchronizing the Altimeter Barometric Pressure Settings 5 1 Synchronize CD isis sich ue eee s n d d aon e HR Change Navigation Sources Enable Disable OBS Mode While Navigating with 6 5 5 2 Generic TMG sii on eoo E I ad ded in edid Configure Vspeed Bugs Set Barometric Radar Altimeter Minimum Descent Altitude 3 Testing the Radar Altimeter
43. HE unuuy gt 5 3 m x x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 89 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio FAS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix 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 coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature INSET SENSOR rro o8s DI ADF DME XPDR IDENT TMRREF NRST MSG LA S D S HO DAD D E L IL IL 1 LA EY F3 V3 V3 V3 P3 73 Select the BACK Softkey to return to the top level softkeys Sensor Softkeys SENSOR Displays softkeys for selecting the 1 and 2 AHRS and Air Data Computers ADCI Selects the 41 Air Data Computer ADC2 Selects the 42 Air Data Computer AHRSI Selects the 1 AHRS AHRS2 Selects the 22 AHRS 90 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Appendix per E223 zi nnnnnnnnnsnmntou o gt s n r m r SV3
44. IONARY SENSOR ANNUNCIATIONS Reversionary Condition Sensor Window Text Both PFDs are displaying data from the n mber one Air Data Computer Both PFDs are displaying data from the n mber two Air Data Computer Both PFDs are displaying data from the n System mber one Attitude amp Heading Reference fi Both PFDs are displaying data from the n System mber two Attitude amp Heading Reference mber one GPS receiver e Both PFDs are displaying data from the n Both PFDs are displaying data from the number two 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 RP Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts Reversionary Condition Sensor Window Text PFD1 is displaying data from the 2 AHRS PFD2 is displaying data from the 1 GPS PFD1 is displaying data from the 2 GPS AFCS ALERTS Alert Condition Annunciation Description Rudder Mistrim Right Rudder Mistrim Left Yaw servo providing sustained force in the indicated direction Aileron Mistrim Right Aileron Mistrim Left Roll servo providing sustained force in the indicated direction Elevator Mistrim Down
45. MIN Airframe Systems Status of the fuel selector is indicated between the fuel tank symbols The mode automatic AUTO manual MAN or off no indication CAS message FUEL OFF generated is shown beneath the fuel selector symbol Left Fuel Switching Right 1 Unknown Tank Fuel Tank Fuel Tank Fuel Tank Selected Selection Selected Selection 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 light blue automatic mode or red manual mode GENERAL SYSTEMS 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the GEN Softkey to display the Fuel System Page The General Synoptics Page aircraft diagram displays open doors in red CAS messages also generated Statuses of propeller stall sensor heater pitot probe and windshield heat are also indicated on the diagram White indicates that heat is off propeller and windshield Light blue indicates heat has been selected windshield Green indicates heat is on Yellow indicates heat has failed propeller pitot tube and stall sensor 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauimnasu nubi E SH lV uonesado soJnjeoJ s np 01d Buruuejg AEN 5640 S24V oipny uad
46. Navigation VNAV V l l s s s s nnne 21 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Table of Contents GARMIN FLIGHT PLANNING 1 ertt batte Weight Planning ssssesseeennnnennennnnnnnnnnnnnnn Trip Planriirig 55 reote reos reete uu ds Create a New User Waypoint Delete a User Waypoint sssssseee nnne Create a New Flight Plan ssssennnnnn Insert a Waypoint in the Active Flight Plan 28 Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 29 Store a Flight Plan Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan ss 30 Invert and Activate a Stored Flight Plan 31 Copy a Flight Plan mite me e teens 31 Delete a Flight Plan ee etr ert ts 31 Graphical Flight Plan Creation 32 PROCEDURES A 33 Load and Activate a Departure Procedure sss 33 Activate A Departure Leg sssssssseeeenennennnnnn Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure L L s si s s 34 Activate An Approach in the Active Flight Plan 35 Activate a Vector to Final Approach
47. PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists PFD2 DB ERR PFD2 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 soJnjeoJ 2 AEN Sd 2 oipny uadx svi sjuawinasu paezey nubi jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio FAS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap databa
48. S DISPLAY WARNING The TAWS display shows supplemental information only It should not be used for navigation A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS 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 Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS 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 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 4 AEN 640 S24V oipny uddx sv3 Tuo2 AEN iui Duruue d Wil s mp oold paezey suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun
49. activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN STOP NAVIGATING A FLIGHT PLAN GPS Navigation 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually 221 221 220 Appronch KDFH RNAV 17LePs LPY MENOL faf RW17L map 930FT POLKE Ul Ww e Large Whi Te
50. ainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 1 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or tum the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to
51. ase update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 84 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahea
52. ata TBM 850 190 00708 01 Rev B GARMIN Hlghtinstruments 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF Softkey ze zi a g 2 o a sv4 SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 Toremove the window press the CLR Key or the TMR REF Softkey oipny uadx 0105 AEN 52 AEN 540 Duruue d Juil TESTING THE RADAR ALTIMETER SeJnpa20Jd 1 Select the SYSTEM Softkey on the MFD 2 Select the RA TEST Softkey The Radar Altitude window displays 50 feet indicating a properly functioning system aoueplony paezey 3 Selecting the RA TEST Softkey again or exiting the System Page cancels the test saunqea4 jeuonippy DISPLAYING WIND DATA uoneiedo Jeuuouqy 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey xipueddy suelv unuuy
53. ation Index Appendix od Annunciations amp Alerts A GARMIN PFD MFD MFD Alert Type TAWS Page Aural Message e Pop Up Alert Annunciation Imminent Obstade Obstacle Ahead Pull Up Impact Waming or Obstacle Ahead Pull Up 0 or Obstacle Obstacle Pull Up Pull Up Reduced Required CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain Caution RTC TERRAIN AHEAD or Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN AHEAD 01 Terrain Ahead Terrain Impact Caution ITI or Ahead CATION TERRAIN 9 Caution Terrain Caution Terrain Reduced Required CAUTION OBSTACLE Caution Obstacle Cau Obstade Clearance or tion Obstade Caution ROC HB o Obstacle Ahead Obstacle Ahead Imminent Obstacle OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead CATION OBSTACLE Caution Obstacle Cau tion Obstacle Premature Descent T LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN m Don t sink Rate Caution NCR or or DTO Low Terain Default configuration 68 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations 8 Alerts TAWS System Status Annunciation
54. ck 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 No annunciation 7 in the AFCS Status Box The acceptable bank angle range is indicated in green along the Ro 190 00708 01 Rev B Sca le of the Attitude Indicator Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sv3 sjueuinasu oipny uadx 0105 AEN ARN Sd5 52 Suelv uoneiedo sainjea4 aoueplony SoJnpa204d buluueld Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul iui nu paezey GARMIN AFCS Sjueuinijsu fila 593 Tu102 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 18 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 fiel
55. ctivate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on To change the user waypoint name follow the procedure for modifying a user waypoint Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 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 high
56. d 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 position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CD for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 190 00708 01 Rev B 85 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuaumnasu sub So1nje2J s mp oold Buruue d AEN Sd5 2 oipny uddx paezey 346 u102 AEN jeuonippy uoneiedo Jeuuouqy EE 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 MISCELLANEOUS MESSAGE ADVISORIES CONT Message bad geometry PTK FAIL
57. d is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation using the PFD 1 Press the Direct to Key Z on the PFD or controller 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauimasu nubi oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo s
58. 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 VVhen available displays optional airport and terminal procedure charts VVhen available displays optional checklists Garmin 61000 Cockpit Reference Guide for the Socata TBM 850 95 sjuaumasu nubi soJnjeoJ exuepiony seinpe2oJd Buruuejd AEN Sd S24V oipny uadx Jeuonippy paezey M fid uo2 AEN uoneiedo Jeuuouqy Sue v unuuy ka GARMIN Appendix Sjueuinijsu fila Sv3 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page SoJnpe oJd aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 96 A GARMIN A Activate a flight plan 20 Active Channel 54 ADF 11 12 58 AHRS 79 80 81 83 Airport Signs 51 52 Airways 95 Air Data Computer 64 Alert messages 82 ALT 42 Altimeter setting 1 58 Altitude mode 42 Altitude volume 42 Attitude amp Heading Reference System 64 Audio panel controls NAV1 NAV2 12 Barometric Altitude Minimums 3 Battery Alerts 62 Current 5 Overheat warning 61 Voltage 5 C Cabin pressure altitude 5 Warning 61 CDI 1 2 12 Cell 37 38 Cell mode 38 Channel Presets 55 ChartView 52 53 Code selection softk
59. e for the Socata TBM 850 190 00708 01 Rev B A GARMIN MazaniAvaldante XM WEATHER OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Turn 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 softkeys to select the desired XM weather product 4 Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arr
60. e the Joystick right or left to move the scanned slice a few degrees right or left Turn the Joystick to adjust the range To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain 1 2 3 4 48 WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation Select the GAIN Softkey to activate the cursor in the GAIN field Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position Press the FMS Knob to remove the cursor Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Ground Mapping Hazard Avoidance 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will becom
61. e the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Tum the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or inhibit the alert on the PFD Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 49 sjuaumasu UATE AEN Sd5 52 oipny uadx 010 AEN buluueld nf aoueploay s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipueddy x pul
62. ed 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 XM Radio volume may also be adjusted on each passenger headset Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN Abnormal operation ABNORMAL OPERATION REVERSIONARY MODE Reversionary mode must be entered manually in the case of PFDI PFD2 or MFD failure In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display sjuauimasu sub SV3 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 oipny uddx UI0JNeN 52 AEN 540 Duruue d 1ubil NOTE The Socata TBM 850 Airplane Flight Manual AFM always takes precedence over the information found in this section SeJnpa20Jd ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically l
63. ed by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B amp GARMIN ___ _ Warnings Cautio
64. epioAy paezey s n ze 4 xipueddy 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 3 4 Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu XM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Pa
65. ess the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active 27 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjueuimasu UATE olpny uqax 0105 AEN 52 2 4 AEN 540 nubi sual uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com Fight EAS Instruments XPDR Audio AFCS Flight Procedures Planning GPS Nav Hazard Features Avoidance Additional Abnormal Operation Appendix Index Flight Planning A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b o d a b o d e Enter the user vvaypoint identifier facility or city Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoin
66. ey of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN ligt Planning 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key 5 Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location 2 AEN 540 nubi COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS
67. ey when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed field Enter a calibrated airspeed Press the ENT Key when finished CREATE A NEW USER WAYPOINT 1 2 3 4 5 6 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Use one of the following methods to enter the reference waypoint a Turn the small FMS Knob to the left to display a list of flight plan waypoints This list is populated only when there is an active flight plan b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or 25 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 sjuauimasu nubi oipny uadx 0105 AEN 52 SoJnpa204d 4 AEN 540 nubi s
68. eys 12 COM 12 57 190 00708 01 Rev B Index D DCLTR Softkey 52 Dead Reckoning 59 Declutter 58 89 95 Designated altitudes 22 Differential cabin pressure 5 Warning 61 Direct to 19 DME 11 12 DR mode 59 60 E Edit a flight plan 30 Enable Terrain 44 Engine display 5 Essential bus voltage 5 F Flap position 5 Asymmetrical deflection warning 61 Flight Director 15 Flight ID 11 Flight path marker 51 FliteCharts 52 53 Frequency Transfer 12 Fuel Alerts 61 62 Flow 5 Pressure 5 Quantity 5 G Generator Current 5 Speed 5 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index 1 sjuauimasu sub saunqea4 2 AEN Sd 24V oipny uadx Jeuonippy paezey L L ulo2 AEN uoneiedo Jeuuouqy sue v unuuy d Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio FAS Instruments Abnormal Operation Annun Alerts ES Appendix Index H Horizon heading 51 Inhibit 44 46 Inhibit TAVVS 46 Inhibit Terrain 44 Inset Map 89 90 Interturbine Temperature ITT 5 Warning 61 IOI 66 68 J Jeppesen 53 L Lightning 37 38 M Map panning 39 Message advisories 70 75 77 81 83 84 METAR 39 Minimums 69 MISCOMP 64 Mode 93 Mode selection softkeys 12 Multi Function Display MFD Softkeys 94 N NACO 53 NAV 12 NAV1 2 12 NAV2 2 12 Naviga
69. fic Symbol Description Non Threat Tratfic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale 40 Traffic Symbol Description Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Hazard Avoidance 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 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 EnsureTIS is operating With the Navigation Map displayed
70. ftware mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed MANIFEST GDL software mismatch communication halted A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced The GDL 69 has incorrect software installed The G1000 system should be serviced 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 so1njeoJ 2 AEN 5640 2 oipny uadx sv3 syu unysu paezey nubi u102 NEN nubi jeuonippy uoneiedo Jeuuouqy Ins E x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix Med Annunciations amp Alerts GWX 68 ALERT MESSAGES A GARMIN Message GWX CONFIG GWX config error Config service req d Comments GWX 68 configuration settings do not match those of the GDU configuration The G1000 system should be serviced GWX FAIL
71. ge 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled 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 54 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page select
72. gin 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 Weather Radar Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Radar Page 3 Select the MODE Softkey 4 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 select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Monitor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of t
73. h backup configuration memory The G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The G1000 system should be serviced 70 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations 8 Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the 61000 system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE
74. he 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 the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Sue v uoneiado SoJnjeaJ aoueplony 2 Fuluueld AEN SdD 2 oipny uadx svi yunuuy jeuuouqy jeuonippy paezey xipuaddy x pul uo2 AEN TL A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES iz T Instruments 1 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box o
75. he antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Tum the large FMS Knob to select Show Tilt Line 3 Press the ENT Key 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 4 sjuauimasu nubi AEN 540 52 444 010 AEN Duruue d nf s mp oold paezey suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipueddy 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 GARMI N Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 2 3 Press the MENU Key Turn the large FMS Knob to select Show Bearing Line Press the ENT Key Vertically Scan a Storm Cell 1 2 3 4 5 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 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed Mov
76. he lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures ADF DME Tuning Barometric Minimum Descent Altitude Box Glideslope Glidepath and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Extreme Pitch Indication 190 00708 01 Rev B GARMIN Abnormal operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is remo
77. icient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach APR DWNGRADE Approach downgraded Abort approach due to loss of GPS navigation Vertical guidance generated by WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch
78. igation database 22 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN WEIGHT PLANNING Flight Planning FLIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the first rectangular page icon 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enter the desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Select the FOB SYNC Softkey to enter the fuel on board quantity as read from the aircraft fuel quantity sensors Or Manually enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS K
79. in air AIR Engine on Landing Operation Phase Inhibit Aircraft on ground Ground LOPI Takeoff Operation Phase Inhibit TOPI 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 63 s n e 4 2 Duruue d AEN Sd5 S24JV olpny uqax sv sjuaumasu 2 nf uone Yid jeuonippy uoneiedo Jeuuouqy 5 ca x pul Flight EAS Instruments Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Additional Abnormal Operation Index Appendix m A Annunciations amp Alerts GARMIN COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is 5 200 ft f both airspeed sensors detect 35 knots this is inhibited f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 ts f either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 ts Difference in heading sensors is 6 degrees Difference in pitch sensors is 5 degrees Difference in roll sensors is 6 degrees PY eee No data from one or both altitude sensors IAS NO COMP HDG NO COMP o data from one or both airspeed sensors o data from one or both heading sensors di OE ME No data from one or both pitch sensors TM LORS No data from one or both roll sensors REVERS
80. ing logged An engine exceedance log has been captured 190 00708 01 Rev B 87 Garmin 61000 Cockpit Reference Guide for the Socata TBM 850 sjuaumasu sub So1nje2J aoueplony s mp oold Buruue d AEN Sd5 2 oipny uddx paezey 346 u102 AEN jeuonippy uoneiedo Jeuuouqy 5 Ea x pul GARMIN Annunciations 8 Alerts Ssjueuinijsu Bi 573 U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy P xipuaddy 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 88 A GARMIN o Appendix APPENDIX sjueuimasu sub PFD SOFTKEY MAP 5 3 r mu m r r mu 75 75 s r CDI NAV1 olpny uqax uo2 AEN CDI GPS Top Level PFD Softkeys E SENSOR PFD OBS ADF DME ITMR REF NS v vi 9 n Duruue d Wil optional optional n rs FE vv m na Select the BACK or OFF Softkey to return to the top level softkeys gt ES a m TE Inset Map Softkeys ae 52 os dai INSET Displays Inset Map in PFD lower left corner 2 2 OFF Removes Inset Map EH DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan S
81. ion Do not press the AP DISC Switch during servo power up and preflight system tests as this may cause the preflight system test to fail or never to start if servos fail their power up tests Power must be cycled to the servos to remedy the situation PFT Preflight system test failed aural alert sounds at failure TERRAIN SVS ALERTS PFD MFD Alert Type TERRAIN SVS 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 1 CAUTION TERRAIN Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN 1 CAUTION TERRAIN Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRATN cautton OBSTACLE Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRAIN cautton OBSTACLE Caution Obstacle Caution 101 Obstacle 66 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS Alert Type System Test fail Terrain
82. itch is closed 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 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Sjueumasu 3f BES BO a3 o sH ly uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui TL A Engine amp Airframe Systems GARMIN FUEL SYSTEM 2 x SE 25 iz 2 2 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 select the FUEL Softkey to display the Fuel System Page 23 Es ox mx x 0 aA 41 7 Pal 2 oxy rst E L FUEL QTY R 1 m a 125 4 4 AUTE s 2 so 2 5 vr d 25 s AI amp ir IY BTA OIL PSI ory PSI 00 P Ium OIL 0 FUEL FLOM 110 USGA FUEL USED ar FUEL REM y usu Flight Planning STALL HEAT ON PROP DEICE ON PITOT HT ON L R IGNITION FUEL LOW L R Procedures Hazard Avoidance y Left Fuel Tank Auxiliary Boost Pump 0 Right Fuel Line 55 Left Fuel Line G Fuel Selector Fuel Flow Data 0 Fuel Pressure 5 Right Fuel Tank Fuel Synoptics Page Annun Abnormal Appendix Alerts Operation Index Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GAR
83. l provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key 10 APPROACH IN THE ACTIVE PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 35 sjuauimasu nubi SV3 olpny uqax 0105 AEN 52 AEN
84. lighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 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 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 33 sjuauimasu nubi olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMI N 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
85. like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN 26 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN ligt Planning Using the MFD 1 Press the FPL Key 2 Tum the small FMS Knob to display the Flight Plan Catalog Page 3 Select the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Using the PFD 1 2 3 4 5 6 7 8 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Pr
86. n to the top level softkeys oipny uadx 0105 AEN 52 Transponder Softkeys AEN Sd5 ADF DME Displays the ADF DME Tuning Window XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations Duruue d nubi s snp old ON Selects Mode A transponder replies to interrogations ALT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations GND 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 aoueplony paezey saunyea4 jeuonippy uoneiedo Jeuuouqy VFR Automatically enters the VFR code 1200in 3 the U S A only iis CODE Displays transponder code selection softkeys 0 7 0 7 Use numbers to enter code gt 5 3 m x BKSP Removes numbers entered one at a time x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 33 Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Index A Appendix GARMIN IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen TMR REF Displays Timer References Wind
87. n over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 1 and or COM2 may still be usable The G1000 system should be serviced when possible COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR 2 remote transfer key is stuck The COM1 and or COM2 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 76 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message with other NAVS LOI GPS integrity lost Crosscheck Comments GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insuff
88. nd 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 press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map TERRAIN SVS NOTE Terrain SVS is only available when the Synthetic Vision System SVS 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 Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 43 sual uonesado s n e 4 e uepioAy s mp oold Buruue d AEN Sd5 2 oipny uddx sv3 Sjueumansu unuuy jeuuouqy jeuonippy paezey 0105 AEN xipueddy x pul nubi TL 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 G
89. needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced MANIFEST GR32 software mismatch communication halted The 2 AHRS has incorrect software installed The G1000 system should be serviced 80 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations 8 Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 12 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 so
90. 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 86 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message MAG VAR WARN Large magnetic variance Verify all course angles Comments 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 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user ECS Service required The environmental control system has failed CRUISE 1 Cruise conditions met Cruise engine trend data log has been captured CRUISE l Cruise l conditions met Cruise l engine trend data log has been captured EXCEEDANCE Engine exceedance data is be
91. nob 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 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 23 sjuauimnasu UATE olpny uqax 0105 AEN 52 SoJnpa204d AEN 540 nubi uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey 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 24 4 For a b o d Or Fo a b d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending wayp
92. ns amp Notes O WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING The Garmin G1000 as installed in the Socata TBM 850 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 t is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs
93. nstalled Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays GMA 1347D MESSAGE ADVISORIES Message Comments GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The G1000 system should be serviced GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced 74 Garmin 61000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES CONT Message MANIFEST GMAT software mismatch communication halted e MANIFEST GMA2 software Comments The audio panel has incorrect software installed The G
94. nunciations TAWS Alerts ere resus E du der de dau iau a Voice Alerts MFD amp PFD Message Advisories ssssssssene Database Message Advisories GMA 1347D Message Advisories GIA 63W Message Advisories GEA 71 Message Advisories ssssssseeee enne GTX 33 33D Message Advisories GTX 33 33D Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GWX 68 Alert 55 65 GDC 74B Message Advisories GCU 475 Message Advisories GMC 710 Message Advisories Miscellaneous Message Advisories sssssss APPENDIX dead too abt dba du tip epica PFD Softkey Map MED Softkey Map nennen 94 INDEX P Index 1 ii 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Table of Contents GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B 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 t
95. o not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The G1000 system should be serviced GTX 33 33D MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config error Config service req d 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 78 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations 8 Alerts GTX 33 33D MESSAGE ADVISORIES Message XPDR1 SRVC XPDR1 needs service Retum unit for repair Comments The 1 transponder should be serviced when possible
96. oaded 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 eouepioAy paezey saunqee4 Jeuonippy HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established sue v unuuy BOOO0d xipuaddy Loss of Hazard Functions with Loss of GPS Position x pul 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 37 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES A GARMIN 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 58 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Status Box System Time PFD Setup Menu Windows displayed in t
97. oint Press the ENT Key to accept the waypoint For flight plan leg planning a b o d 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 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 850 190 00708 01 Rev B GARMIN ligt Planning 6 7 8 9 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT K
98. om the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guid
99. ow NRST Displays Nearest Airports Window MSG Displays Message Window MFD SOFTKEY MAP V3 T a ES Select the BACK Softkey on this level to return to the top softkey level optional optional nen A MFD Softkeys CAS T Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling CAS Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alert ing System Display to warrant scrolling MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map 94 Garmin 61000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Appendix DCLTR 3 SHW CHRT CHKLIST 190 00708 01 Rev B TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON AIl airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed NEXRAD Displays NEXRAD weather and coverage information on Navigation Map optional feature XM LING Displays XM lightning information on Navigation Map optional feature BACK Returns to top level softkeys Selects desired amount of map detail cycles through
100. ow on AIRMETs TFRs METARS or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 39 AEN Sd5 52 olpny qqax 0105 AEN buluueld ni aoueploay s mp oold paezey Suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Alerts Operation Features Avoidance Procedures Appendix Index Hazard Avoidance GARMI N information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Echo Top Cloud Top and Echo Top Mutually Exclusive Cloud Top Cell Movement City Forecast Freezing Levels Cyclone Warnings SIGMETs AIRMETs Winds Aloft TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE soltkeys are displayed e Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed Traf
101. ppy uoneiedo Jeuuouqy E 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 A GARMIN MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The MFD and PFDs are not communicating with each other The G1000 system should be serviced 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 matc
102. receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced 190 00708 01 Rev B 19 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 soJnjeoJ 2 AEN Sd 24V oipny uadx svi sjuawinasu paezey nubi nubi jeuonippy uoneiedo Jeuuouqy ud 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 A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 GPS AHRST not receiving backup GPS information Comments The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match AHRS1 SRVC AHRS1 Magnetic field model
103. s PFD MFD MFD Alert Type TAWS Page Aural Message Pop Up Alert Annunciation TAWS System Test Fail TAWS FALL None TAWS System Failure TAWS Alerting is disabled TAWS INHB None None No GPS position or TAWS N A None TAWS Not Available excessively degraded GPS TAWS Available will be signal heard when sufficient GPS Signal is re established System Test in progress TAWS TEST None None System Test pass None None TAWS System Test OK VOICE ALERTS Voice Alert Description Minimums minimums he aircraft has descended below the preset barometric minimum tude Vertical track 1 descent alt 1 V he aircraft is o ertical navigat ion is enabled ne minute from Top of Descent Issued only when Traffic Played when a Traffic Advisory TA is issued with the TIS system Traffic Not Available The aircraft is o utside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued with a TAS system TAS System Test OK Played when the TAS system passes a pilot initiated self test TAS System Test Played when the TAS system fails a pilot initiated self test Failed 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 69 So1nje24 e uepioAy s mp oold Buruue d AEN Sd5 2 oipny uddx sv3 Sjueumasu paezey nubi Wil jeuoni
104. se error exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU n Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Annunciations amp Alerts
105. selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 34 1 2 3 4 5 6 NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMIN 17719 Procedures the approach and wil
106. t list is displayed Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 28 1 2 3 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint field after the desired airway entry point If this previous waypoint is not a valid airway entry point a valid entry point should be entered at this time Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN 4 Tum the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway Flight Planning menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by
107. t such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision heret is strictly prohibited Garmin and G10009 are registered trademarks of Garmin Ltd or its subsidiaries WATCHS FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope and SkyWatch are registered trademarks of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc July 2008 190 00708 01 Rev B Printed in the U S A A Warnings Cautions amp Notes GARMIN e o 6 WARNING The G1000 TAWS feature does not relieve the pilot from the responsibility of being aware of surroundings during flight The TAWS feature isonly to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculat
108. tion database 21 22 NEXRAD 39 40 90 95 ndex 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A GARMIN 0 OBS 2 Obstacles 74 76 Oil engine Alerts 61 Pressure 5 Temperature 5 Overspeed Protection 16 Oxygen Pressure 5 Warning 61 P Pathways 51 PIT 64 Propeller speed 5 R Reversionary Mode EICAS 5 Reversionary mode 57 ROC 66 67 68 S SafeTaxi 6 52 Sensor 64 Store Flight Plan 30 Stormscope lightning data 37 38 Strike 37 Strike mode 38 SVS 51 Synthetic Vision System 51 T TA 69 TAF 39 TAS 41 42 69 79 190 00708 01 Rev B A GARMIN TAWS 45 46 67 69 TAVVS B 45 Terrain 42 43 45 74 90 95 Terrain SVS 43 44 Timer 2 84 Topographical data 90 95 Torque 5 Warning 61 Traffic 37 41 94 Traffic advisory 41 Traffic Advisory 69 Traffic map page 41 42 43 Transponder 11 12 93 94 Trim 5 V Vertical speed guidance 22 Vertical track 69 VNV 19 58 Vspeed 2 W WAAS 76 Weather data link page 39 Wind data 92 X XM lightning 90 95 XM weather 39 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 Index Index 3 sjuauimasu sub saunqea4 uepjoay sanpa20Jq Buruuejg AEN Sd 24V oipny uadx Jeuonippy paezey L L U105JNeN uoneiedo Jeuuouqy SHE unuuy ES d GARMIN index Sjueuinijsu sub Sv3 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6
109. tions 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 failure has been detected in the GCU 475 The GCU 475 is unavailable The GCU 475 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 475 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists GMC 710 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The G1000 system should be serviced GMC KEYSTK GMC key name Key is stuck 190 00708 01 Rev B 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 83 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 soJnjeoJ 2
110. ture 0 sel Selected Cabin Altitude 16 17 and Essential Bus Voltages 2 G oil Oil Pressure 19 Oxygen Pressure 2 Elevator Aileron and Rudder Trim and Oil Temperature 2 Fuel Quantity Poli 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 A Engine amp Airframe Systems GARMIN ELECTRICAL SYSTEM 2 x SE 2s iz 2 2 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 select the ELEC Softkey to display the Electrical System Page Nav Com XPDR Audio AFCS L FUEL OTY R uso Fr 125 7 A RN 100 f bl J se 25 ha GPS Nav 2 GPH ma 00 ELECTRICAL D OIL PSI H S BUS BAT BUS Flight Planning zrtev STALL HEAT ON PROP DEICE ON 1 PITOT HT ON L R Procedures Hazard Avoidance EX FUEL GEN E O Standby Generator Battery Battery Bus 8 Q Main Generator G Main Bus Essential Bus Ps 0 Ground Power 5 Emergency Switch Power Buses Unit Door Electrical Synoptics Page Annun Abnormal Appendix Alerts Operation Index Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Engine amp Airframe Systems Battery connection status to the main bus is indicated in green direction of current flow is indicated with an arrow next to the current readout If the battery is disconnected from the main bus the sw
111. ual uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey 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 7 8 9 10 A GARMIN a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key After pressing the ENT Key the cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Press the ENT Key The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 2 3 4 5 6 7 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Select the DELETE Softkey The message Would you
112. ure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays 190 00708 01 Rev B 73 Garmin 61000 Cockpit Reference Guide for the Socata TBM 850 sjuaumnasu sub s m s mp oold Buruue d AEN Sd5 yi oipny uddx paezey 3461 u102 AEN jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio FAS Instruments Additional Abnormal Operation Index Appendix ee Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Aviation database type mismatch Xtalk is off Comments The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays The PFDs and MFD have different terrain database types i
113. ved from the display Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function is not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 9 eouepioAy s np odd Fuluueld AEN Sd5 2 olpnyyuqax Sjueunasu wio gt AeN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul 3 Nav Com XPDR Audio Ha
114. ver the NAV2 standby frequency 3 Select the CDI Softkey a third time to return to GPS Nav Com XPDR Audio AFCS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Select the OBS Softkey to select OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GPS Nav Flight Planning GENERIC TIMER Procedures 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOVVN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window Hazard Features Avoidance Additional Abnormal Operation HE CONFIGURE VSPEED BUGS 1 Select the TMR REF Softkey B 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 5 speed has been changed from a default value an asterisk appears next to the speed 2 Garmin 61000 Cockpit Reference Guide for the Soc
115. weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old m Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LING 2 Tum the large FMS Knob to select STRMSCP MODE 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 37 AEN Sd5 S24V oipny duadx sv4 s u umnnsul u102 AEN T R Duruue d nf aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy 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 GARMI N 38 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data fr
116. x junuuy jeuuouqy feuonippv paezey ETSI xipuaddy x pul A Engine amp Airframe Systems GARMIN ER 213 SYSTEM ENERAL x1000 4 15 7 2 16 om Flight Instruments 2 PROP 0 0 DIFF PSI P 1800 L FUEL QTY R 122 usa 122 125 ze ES ys ce so za gt x lt OIL PSI o 5 5 22 z vasa E ir Ir RA es 73 o EX General Synoptics Page Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Appendix Index Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ENTER OR CHANGE FLIGHT ID 1 Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Turn the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Turn the small FMS Knob to enter the next desired character 5 Repeat steps 3 and 4 until the desired Flight ID is entered 6 Press the ENT Key to update the Flight ID Do not perform any other G1000 functions until updating is no longer displayed ADF TUNING OPTIONAL 1 Press the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large FMS Knob to select the next desired field 4 Turn the small FMS Knob to enter the desired number 5
117. xt Large Light Blue Text small Light Blue Tex Small White Text with Altitude Restriction Bar SIUE Cross AT or ABOVE 5 000 fi Facing Cross AT 2 300 fi Cinn Cross AT or BELOW 3 000 ft 190 00708 01 Rev B Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 siu uinnsu nubi 5 3 oipny uadx 010 AEN suelv uoneiedo sainjea4 2 Duruue d Tunuuy Jeuuouqy Jeuonippy p EZEH 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 displayed 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 displa
118. y more than 15 USGAL for gt 30 seconds Procedures Fuel quantity less than or equal to 9 1 USGAL in specified tank GPU receptacle door not closed Hazard Avoidance Ignition exciter running Inertial separator failure Inertial separator extended Additional Features Low fuel level sensor failure for specified tank Abnormal Operation Battery voltage below 26 V a c Starter generator unconnected gt lt Oil pressure between 60 and 100 psi gt lt 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 gt lt Index Appendix Prop deice selected and not on Prop deice on while engine off 62 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 90 00708 01 Rev B A GARMIN Inhibits uz ee Messages Comments og la 2 amp msogag Rear cargo door open X Stall warning heat on while engine off X Stall warning heat off X Starter generator running Vacuum pressure less than 3 75 in Hg X X Only affected side L R or L R displayed in CAS message applicable messages listed here display L R for example Inhibits prevent certain CAS messages from being displayed during the following conditions Engine off Aircraft
119. yed 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 White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated Altitude has been The system cannot the system estimating entered by the pilot use this altitude the altitude of the Altitude is designated in determining aircraft as it passes over for use in giving vertical vertical flight path the navigation point flight path guidance guidance This altitude is provided 1 Altitude does not match as a reference and is the published altitude not designated to be in navigation database used in determining or no published altitude vertical flight path exists 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 nav
120. zard Avoidance Additional Flight Instruments Flight Planning EAS AFCS Procedures GPS Nav Features Annun Appendix Alerts Index A Abnormal Operation GARMIN TEESDALESEYSE CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Track Bug All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and Terrain Proximity TERRAIN SVS and TAWS are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 60 Garmin G1000 Cockpit Reference Guide for the Socata TBM 850 190 00708 01 Rev B GARMI N ANNUNCIATIONS amp ALERTS CAS MESSAGES Warning Messages Inhibits Comments Messages ENGINE OFF ENGINE ON GROUND TOPI AIR LOPI Battery temperature over 70 C Bleed temperature high X Cabin altitude over 10 00

Garmin Software Version 0719.03 Cockpit Reference Guide

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