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Garmin Software Version 0829.00 Cockpit Reference Guide

1. 3 Turn the system ON A prompt is displayed 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card press any key to continue as instructed 7 Again press any key to continue as instructed on the display 8 Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting 9 Press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the small FMS Knob to select the System Status Page 12 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed alert will remain until the next power cycle 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This 109 S9JnjeaJ a UePIOAY SoJnpa20Jd Duiuue d AEN Sd5 j4V oipny uddx SV3 sjuauinajsu Jeuonippy puezey 114 wo gt AeNn HTTUTE uonej
2. sssssssseeeeennnnn 91 GMC 710 Message Advisories ssssseeennnn 92 GTS 820 Message Advisories sssssssseennnnn 92 Miscellaneous Message Advisories ssssssssseen 93 Flight Plan Import Export Messages 97 lidu4 99 PFD Softk y Map M TT 99 MED Softkey Map nennen 105 Loading Updated Databases 107 lp er Index 1 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 il TbleofCowens GARMIN Blank Page IV Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING m gt n Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE oipny uadx U0 AEN Press the BARO Knob CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS S 1V 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys buruue d AEN Sd5 1ubi 4 SoJnpo 20Jd SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS e2uepioAy
3. highlighted press the ENT Key Flight Planning 4 o S 7 o e a Hazard Avoidance LOAD AND OR ACTIVATE AN APPROACH PROCEDURE NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Additional Features Abnormal Operation 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT APPROACH 3 Press the ENT Key A list of available approaches for the destination airport is displayed 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed Annun Appendix Alerts Index 40 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN LLL Procedures 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Tu
4. GIA hardware one is SBAS capable mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced MANIFEST GIA2 software installed The G1000 system should be serviced mismatch communication halted settings are incorrect COM1 TEMP COM1 over temp The system has detected an over temperature Reducing transmitter power condition in COM1 and or COM2 The COM2 TEMP COM2 over temp transmitter is operating at reduced power If the Reducing transmitter power persists the G1000 system should be serviced COM1 SERVICE COM1 needs The system has detected a failure in COM1 service Return unit for repair and or COM2 COM and or COM2 may still be COM2 SERVICE COM2 needs usable The G1000 system should be serviced service Return unit for repair when possible COM1 PTT COMI push to talk The COM1 and or COM2 external push to talk key is stuck switch is stuck in the enable or pressed COM2 PTT COM2 push to talk Position Press the PTT switch again to cycle its key is stuck operation If the problem persists the G1000 system should be serviced 04 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADV
5. 6 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 oipny uadx SV3 Sjueuinajsu WO AeN SJdV SoJnpo 20Jd Duiuue d AEN Sd5 4f1 4 9 uepioAy puezey sue v uonejedo s9JnjeaJ unuuy Jeuuouqy jeuonippy xipueddy xepu 1ubi 4 Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A NEW FLIGHT PLAN 22 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight
6. Cabin pressure altitude 6 Warning 69 CDI 1 2 14 94 Cell 43 44 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Index Cell mode 44 Channel Presets 64 ChartView 60 61 Code selection softkeys 14 COM 14 65 D DB Mismatch 109 DCLTR Softkey 60 Dead Reckoning 66 Declutter 66 99 106 Designated altitudes 24 Differential cabin pressure 6 Warning 69 Direct to 21 DME 13 14 Door status 11 DR mode 66 67 68 E Edit a flight plan 36 Enable Terrain 52 Essential bus voltage 6 F Flap position 6 Asymmetrical deflection warning 69 Flight Director 17 Flight ID 13 Flight path marker 59 FliteCharts 60 61 Frequency Transfer 14 Fuel Alerts 69 70 Flow 6 Pressure 6 Quantity 6 Index 1 s9JnjeaJ a UePIOAY SoJnpa20Jd Duiuue d AEN Sd5 SD4V oipny uddx SV3 sjuauinajsu jeuonippy p1ezeH 14 U10 AEN i uonejedo Jeuuouqv sue v Junuuy Bud uid Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index G Gain 56 Generator Current 6 Speed 6 Ground mapping 56 H HF 14 Horizontal scan 55 Horizon heading 59 Inhibit 51 53 Inhibit TAWS 53 Inhibit Terrain 51 Inset Map 99 100 Interturbine Temperature ITT 6 Warning 69 IOI 73 75 76 J Jeppesen 61 L Lightning 43 44 M Map panning 45 Message advisories 78 83 85 89 9
7. Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description HRZN HDG Displays compass heading along the APTSIGNS DFLTS WIND OPIN I OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI BRG2 ALT UNIT METERS Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed Wind direction arrow with direction and speed Information not displayed Select to display the DME information window Cycles the Bearing 1 Information Window through NAVI or GPS waypoint identifier and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format 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 102 Garmin G1000 Cockpit Reference Guide for the Soca
8. I a gt o Tm j d gi z 05 N x lt U 2 gt x 3 2 m Z Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Levell Level2 Level3 Description 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 100 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN 4 Appendix Levell Level2 Level3 Description i AHRSI Selects the 1 AHRS g 2 AHRS2 Selects the 2 AHRS SV3 oipny uadx U0 AEN MSG nnnnnnnnmnunnYv pk or n SJV Select the BACK Softkey to return to the top level softkeys 1L 3 F amp V9 V3 V3 YF 28 1 C A S D 3 A S D A DS A V3 F3 nnnnxn n n n n E T PFD Configuration Softkeys EE Level 1 Level2 Level 3 Description xt PFD Displays second level softkeys for E additional PFD configurations gt SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan gt 5 D 5 x SYN TERR Enables synthetic terrain depiction xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 101 Additional Hazard Flight Nav Com Flight
9. SVS option is installed and the TAWS option has not been installed 75 degrees north or 60 degrees south Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Hazard Avoidance Display Terrain on the TERRAIN SVS Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude I I Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 51 AEN Sd5 S24
10. Sensor Window Text Both PFDs are displaying data from the number one Air Data Computer Both PFDs are displaying data from the number two Air Data Computer Both PFDs are displaying data from the number one Attitude amp Heading Reference System Both PFDs are displaying data from the number two Attitude amp Heading Reference System Both PFDs are displaying data from the number one GPS receiver Both PFDs are displaying data from the number two GPS receiver 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 90 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 11 soJnjeoJ 92uepioAy SsoJnpo20Jd Puruuejd AeN Sd5 4JV oipny uadx SV3 sjueuinajsu piezeH i W0 gt AeN i jeuonippv uoneJjedo jeuuouqv xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix LE Ammundatons amp Alets GARMIN Reversionary Sensor Window Text PFD1 is displaying data from the 2 AHRS USING GPS1 PFD2 is displaying data from the 1 GPS USING GPS2 PFD1 is displaying data from the 2 GPS AFCS ALERTS Alert Condition Annunciation Description Rudder Mistrim Right Yaw servo providing sustained force in the indicated dm direction Aircraft rudder retrim after
11. amp Notes GARMIN NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized
12. optional Displays NEXRAD weather and coverage information on Navigation Map optional Displays XM lightning information on Navigation Map optional Displays METAR flags on airport symbols shown on the Navigation Map optional Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Appendix LOADING UPDATED DATABASES In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected diaplays listed
13. 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 700 190 01247 00 Rev A GARMIN Flight Planning 6 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings 7 The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system 8 The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system 9 Theflashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page 10 The flashing cursor moves to the calibrated ai
14. unuuy Jeuuouqy jeuonippy xipueddy Xapu Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 6 7 8 9 A GARMIN The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select LAT LON latitude and longitude Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER 28 1 2 3 4 5 6 7 8 9 10 WAYPOINTS Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when
15. 5 nm and less than 1200 vertical separation S 1V AEN Sd5 Puruuejd oE SoJnpo 20Jd T og N ae Si EN ag D s n e j jeuonippy uoneJjedo Jeuuouqv sue v Junuuy Traffic Advisory Off Scale 2 Traffic Advisory TA arrow with ADS B directional information Points in the direction of the intruder aircraft track GTS 820 only 2 Proximity Advisory PA arrow with ADS B directional information Points in the direction of the aircraft track GTS 820 only Traffic Advisory TA closing rate distance and vertical separation meet TA criteria xipueddy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 4 Abnormal Additional Annun Flight Instruments Nav Com XPDR Audio Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Traffic Symbol Non threat traffic arrow with ADS B directional information Points in the direction of the intruder aircraft track GTS 820 only 48 PA or Non threat traffic arrow with ADS B directional information but positional accuracy is degraded Points in the direction of the aircraft track GTS 820 only Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Ser
16. 57 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Index Index 3 s9JnjeaJ a UePIOAY SoJnpa20Jd Duiuue d AEN Sd5 j4V oipny uddx SV3 sjuauinajsu Jeuonippy puezey 114 Wwo gt AeN 14 uonejedo Jeuuouqv sue v Junuuy GARMIN Index S uouunJjsu 1upi4 SV3 oipny dadx Wo gt AeN S21V AEN Sd5 Puruuejd IE Blank Page SoJnpo 0Jd 92UepIOAV puezey SoJnjeoJ jeuonippy uoneJoedo jeuuouqy Sue v unuuy Lb Eg 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Index 4 A GARMIN i c i io c RN T aso or ie gt i Y x d 11 Ak JI f aye 3 t a d ET _ 2 a B nis a S Pa D r La a i i p Garmin International Inc 00 East 151stStreet Olathe KS 66062 U S A Copse Road T en anes Park ithampton 5040 9RB U K Corporation No 68 apa 2nd oad Garmin 2010 Garmin Ltd or its subsidiaries 190 01247 00 Rev A
17. 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 jeuonippy paezey 1ubi 4 uonejedo jeuuouqv sue v junuuy xopu xipueddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix 1 GARMIN 8 9 10 11 12 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen Navigation Database as the Active Navigation Database 1 108 2 3 4 5 6 7 8 9 NOTE Loading the Jeppesen navigation database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display P
18. Ahead Pull Up Imminent Obstade PULL UP Obstacle Ahead Pull Up Impact Warning or 0 CAUTION TERRAIN or or Obstacle Obstacle Pull Up Pull Up Obstacle Ahead Pull Up Reduced Required Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead e Imminent Terrain TERRAIN AHEAD Terrain Ahead Terrain Ahead Impact Caution ITI or or CAUTION TERRAIN Caution Terrain Caution Terrain CAUTION OBSTACLE OBSTACLE AHEAD Terrain Clearance Caution RTC Reduced Required Caution Obstacle Caution Obstacle Clearance Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 75 SoJnjeoJ 92uepioAy SoJnpo 0Jd Puruuejd NEN Sd5 S 4JY oipny uddx SV3 SjueuinJjsu 1414 Wo gt AeN jeuonippv uonejedo jeunouqy Xapu 1ubi 4 puezey Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ Annunciations amp Alerts PFD MFD Alert Type TAWS B Page Annunciation MFD Pop Up Alert Imminent Obstacle Impact Caution IOI Premature Descent Alert Caution PDA Altitude Callout II 500 Excessive Descent Rate Caution EDR Negative Climb Rate Caution NCR TAWS System Status Annunciations A GARMIN Aural Messag
19. Alerts GARMIN DATABASE MESSAGE ADVISORIES CONT DB MISMATCH Navigation The PFDs and MFD have different navigation database type mismatch Xtalkis database types installed Americas European off etc Crossfill is off Install correct navigation database type in all displays DB MISMATCH Terrain database The PFDs and MFD have different terrain version mismatch database versions installed Install correct terrain database version in all displays EAS AFCS DB MISMATCH Terrain database The PFDs and MFD have different terrain type mismatch database types installed Install correct terrain database type in all displays GPS Nav DB MISMATCH Obstacle The PFDs and MFD have different obstacle database version mismatch database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain The PFDs and MFD have different airport terrrain database mismatch databases installed Install correct airport terrain database in all displays NAV DB UPDATED Active System has updated the active navigation navigation database updated database from the standby navigation database TERRAIN DSP PFD1 PFD2 or One of the terrain airport terrain or obstacle MFD1 Terrain awareness display databases required for TAWS in the specified PFD unavailable or MFD is missing or invalid Procedures Features GMA 1347D MESSAGE ADVISORIES GMAT FAIL GMAT is inop
20. Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level3 Description IDENT TMR REF NRST MSG 104 ALT GND VFR CODE 0 7 BKSP Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection softkeys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identitying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Message Window 190 01247 00 Rev A A GARMIN Appendix MFD SOFTKEY MAP optional optional SjueuinJdjsu 64 n CA FA FX SV3 DCLTR 1 DCLTR 2 DCLTR 3 Select the BACK Softkey on this level to return to the top softkey level oipny uadx Wo gt AeN optional optional optional optional optional Fr rv ry v rm sen ces we qm l ee ree eev esT MFD Softkeys in Level 1
21. 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 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 A GARMIN 190 01247 00 Rev A A GARMIN Engine amp Airframe Systems ENGINE amp AIRFRAME SYSTEMS S ueuunJjsu ubi 3 CABIN PRESS ALT FT RATE FPH oipny uadx UI0 AeEN 1866 E O H DIFF PSI BN E T S 4V L FUEL QTY R 71_ USG 71 125 188 AEN Sd5 i t 790 OIL PSI 115 Puruuejd 1u6i4 OIL PSI ELECTRICAL OIL C 75 AMPS oom 7 SoJnpa 20Jd CABIN PRESS ALT FT 1800 DIFF PSI B E 92UPpIOAV puezey FUEL QTY USG ob 2B soJnjeoJ Jeuonippy BATT 25 GEN 110 BATT 29 0 Ess 29 6 uoneJedo Jeuuouqy EIS Display Normal Mode EIS Display Reversionary Mode A J Models A B and C shown Models A B and C j Model N similar Model N similar g 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 D amp Engine amp Airframe Systems GARMIN 2 C1 Torque C Differential Pressure 2 Propeller Speed Fuel Quantity n G Generator Speed 11 Fuel Flow 4 Interturbine Temperature 12 Fuel Pressure 5 Oil Pressure 13 Battery and Generator Currents E E 6 Oil Temperature Battery and Essential Bus Voltages 7 CAS Display 15 Flevator Aileron and
22. Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT Key again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 22 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 Le
23. Level 2 Description E CAS 1 Scroll up Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling 92uepioAy puezey CAS 4 Scroll down Displayed only when a sufficient number of items are displayed in the Crew Alerting System Display to warrant scrolling SoJnjeoJ jeuonippy MAP Enables second level Navigation Map softkeys uonejedo Jeuuouqv TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map sue v unuuy TERRAIN Displays terrain information on Navigation Map gt ke o D 5 x Xapu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 105 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Description DCLTR 3 SHW CHRT CHKLIST 106 AIRWAYS STRMSCP NEXRAD XM LING METAR LEGEND BACK 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 Displays Stormscope weather and coverage information on Navigation Map
24. Radar Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Hazard Avoidance 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 the antenna If the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field W
25. Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 I SjueuinJjsu 1uDij3 SV3 oipny uadx Wo gt AeN AEN Sd5 S 1V SHa V uonejedo sainjea4 92uepioAy SoAnpo20Jd Puruuejd junuuy Jeuuouqy Jeuonippy paezey iui xipueddy xepu Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EAS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A AFS CT GARMIN VERTICAL MODES Holds the current aircraft pitch attitude Pitch Hold may be used to climb descend to the default PIT Selected Altitude AFCS armed to capture the altitude CC RING displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds the current Altitude Reference ALT Key Maintains the current aircraft vertical Vertical Speed speed may be used to climb descend VS Key nnnn FPM to the Selected Altitude Flight Level Change Maintains the current aircraft airspeed IAS Hold in KIAS or Mach Number while the Flight Level Change aircraft is climbing descending to the Mach Hold Selected Altitude VNAV a and tracks the VNAV flight VPTH VNAV Target AFCS armed to capture the altitude Altitude Armed displayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath on approach APR s Captures and tracks the ILS glideslope Glideslope on approach Commands a preprogrammed constant Takeoff pitch att
26. Rudder Trim s Cabin Pressure Altitude and Change d Ea Rate E ELECTRICAL SYSTEM s 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the ELEC Softkey to display the Electrical System Page O Qo o Abnormal Operation i81 BUS 2 E SS BUS BAT BUS Annun Alerts i J 760 27 6 Appendix QO Electrical Synoptics Page Index 6 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Engine amp Airframe Systems C1 Standby Generator C Essential Bus Main Generator Battery Bus Voltage G Ground Power Unit Door Essential Bus Voltage 4 Battery DC Buses Ithrough 4 5 Amperage 11 Main Bus 6 Battery bus Active generator currents are displayed below the generator icons A disconnected generator is indicated in gray the current is removed from the display and the switch symbol is closed sjueuinajsu 1uDiI4 EE oipny uadx U10 AeN S 1V Connected Disconnected Connected Disconnected AEN Sd5 ubi Puruuejd s np 201d Generator Status 92UepIOAY puezey GPU status information is removed from the electrical diagram when the GPU door is closed If the GPU door is open and selected the GPU status is shown in green when the door is open but not selected the status is shown in gray with the switch closed A CAS message GPU DOOR is generated if the GPU door is ope
27. 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 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 4 Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not d
28. 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 database error exists properly inserted Replace data card If problem PFD2 DB ERR PFD2 Safe Taxi persists The G1000 system should be serviced database error exists MFD1 DB ERR MFD1 Chartview The MFD detected a failure in the ChartView database error exists database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts The MFD detected a failure in the FliteCharts database error exists 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 Navigation The PFDs and MFD have different navigation database version mismatch Xtalk database versions installed Crosstill is off is off Install correct navigation database version in all displays 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 81 SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 4JV oipny uadx SV3 sjueuinajsu piezeH yi JU05 AEN i jeuonippv uoneJjedo Jeuuouqv Xapu Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Abnormal A Annunciations amp
29. e uepioAy puezey mul t fet e 1 n jeuonippv uonejedo Jeuuouqv Displaying Synthetic Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page xipueddy sue v unuuy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 59 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Abnormal Annun EAS AFCS GPS Nav Procedures T ua 5s 2 BB 2p m LL lt x Appendix Alerts Operation Index Additional Features A GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be nec
30. has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you December 2010 190 01247 00 Rev A Printed in the U S A A GARMIN Warnings Cautions amp Notes WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and coul
31. 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 gt ke D 5 x xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 99 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Levell Level2 Level 3 Description WX LGND Displays icon and age on the Inset Map for the selected weather products optional TRAFFIC Cycles through tratfic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Displays Stormscope weather and coverage information on the Inset Map optional NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional XM LING Displays XM lightning information on Inset Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optional p gt Q A e Q E g A m TI 3 o m gt iw ge 3 j GB U w 9 2 UJ is g
32. puezey 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in the SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF SoJnjeoJ Jeuonippy uonejedo Jeuuouqv SYNCHRONIZE CDI sue v unuuy 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF xipueddy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Flight Instruments GARMI N CHANGE NAVIGATION SOURCES 1 2 3 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency Select the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 2 3 Select the OBS Softkey to select OBS Mode Turn a CRS Knob to select the desired course to from the
33. s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT 13 The cursor is now displayed in the DIS distance field Enter the desired Key distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Tum the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint
34. select or deselect the intercom The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob switches between volume and squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciator is lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is 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 functi
35. sse 65 Hazard Displays with Loss of GPS Position 65 Unusual Attitudes sssssssseeeneenen nennen 66 Dead Reckoning 66 ANNUNCIATIONS amp ALERTS 69 CAS Messages 69 Comparator Annunciations sssssssssseeeeeeeenenens 11 Reversionary Sensor Annunciations sssssseeeeee 11 AFCS Alerts sisicata eesti esiasio 12 Terrain SVS Alerts gerne scp cce pct ton ccg uanceazencsescpcastenstecscanscasstesotansasaceantbeesieunssosuoteestconscen E Terrain SVS System Status Annunciations sse 74 TAWS AIGTIS oeste dp onU pU DG I emm NM UD IE 15 Voice Alerts cootra tubturtitesensitatustefenicutusm seitens fetus H MFD amp PFD Message Advisories sssssseeeee 78 Database Message Advisories cccccssssesssssessssesssesssssssesssesssessssssssssnsesssesssesseessees 19 GMA 1347D Message Advisories ssssssenennnn 82 GIA 63W Message Advisories ssssssssseeenennnn 83 GEA 71 Message Advisories ssssssssseeeeeeeennnnnn 86 GTX 33 33D Message Advisories 87 GRS 77 Message Advisories ssssssssseeenenen 87 GMU 44 Message Advisories ssssssssseeeennnn 89 GDL 69A Message Advisories ssssssssseeeeeeennn 90 GWX 68 Alert Messages 90 GDC 74B Message Advisories 91 GCU 475 Message Advisories
36. substantial pitch and neu na power changes required Aileron Mistrim Right Roll servo providing sustained force in the indicated Aileron Mistrim direction Left i Elevator Mistrim n D N Pitch servo providing sustained force in the indicated Elevator Misti direction May indicate a failure of the pitch trim servo or di Up on trim system Pitch Trim Failure If AP engaged take control of the aircraft and disengage AP Switch unstick Yaw Trim Failure If AP engaged take control of the aircraft and disengage AP or stuck MEYT If AP disengaged move the MEYT switch to check if a stuck Switch switch is causing the annunciation i pamper W YD control failure AP also inoperative Failure Roll Failure OL Roll axis control failure AP inoperative Pitch Failure a Pitch axis control failure AP inoperative System Failure AFCS AP and MEPT are unavailable FD may still be available Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A or stuck MEPT PT RM If AP disengaged move MEPT switches separately to A GARMIN ker Condition Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power up and preflight system tests as this may cause the preflight Preflight Test Annunciations amp Alerts 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
37. the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Flight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoi
38. waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at Arriving at waypoint xxxx where xxx is the waypoint Xxxx waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead Special use airspace is ahead of aircraft The less than 10 minutes aircratt will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and Special use airspace is near and ahead of the ahead aircraft position ARSPC NEAR Airspace near less Special use airspace is within 2 nm of the than 2 nm aircraft position APR INACTV Approach is not The system notifies the pilot that the loaded active approach is not active Activate approach when required SLCT FREQ Select appropriate The system notities the pilot to load the frequency for approach approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to approach 94 the correct NAV receiver Set the CDI to the correct NAV receiver Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT PTK FAIL Paral
39. yybi4 S4V SoJnpo 20Jd Duiuue d AEN Sd5 4f1 4 sue v uonejedo s9JnjeaJ 92uepioAy junuuy jewuouqy Jeuonippy puezey xipueddy Xapu Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Procedures Planning GPS Nav EAS AFCS Appendix Alerts Operation Features Index Flight Planning 26 4 A GARMIN For Direct to planning a Select the WPTS Softkey and verity that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present Position to display P POS c Press the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint c Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Select the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number c Turn the large FMS Knob to highlight the LEG field d Turn the small FMS Knob to select the desired leg of the flight plan or
40. 1 96 METAR 45 Minimums 77 MISCOMP 71 Mode S 104 Mode selection softkeys 14 Multi Function Display MFD Softkeys 105 Index 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 A GARMIN N NAV 14 NAV1 2 14 NAV2 2 14 Navigation database 23 24 NEXRAD 45 100 106 O OBS 2 Obstacles 82 84 Oil engine Alerts 69 Pressure 6 Temperature 6 Overspeed Protection 18 Oxygen Warning 69 P Pathways 59 60 PIT 71 Propeller speed 6 R Reversionary Mode EICAS 5 Reversionary mode 65 ROC 73 75 S SafeTaxi 60 SBAS 18 40 52 53 67 84 85 Sector scan 56 Sensor 71 STAB 57 Standby 54 Standby Navigation Database 109 Store Flight Plan 35 190 01247 00 Rev A A GARMIN Stormscope lightning data 43 44 Weather data link page 45 Strike 43 Weather radar 54 Strike mode 44 Wind data 102 SVS 59 96 Synchronization 107 X SYNC Status 109 XM lightning 100 106 Synthetic Vision System 59 XM weather 45 T TA 77 TAF 45 TAS 49 77 87 TAWS 52 53 54 75 TAWS B 52 Terrain 50 52 82 100 105 Terrain SVS 50 51 52 Tilt line 55 Timer 2 93 Topographical data 100 105 Torque 6 Warning 69 Traffic 43 48 105 Traffic advisory 48 Traffic Advisory 77 Traffic map page 48 49 50 Transponder 13 14 103 104 Trim 6 V Vertical speed guidance 24 Vertical track 77 VNV 21 66 95 Vspeed 2 W WATCH 57 Waypoint Selection Submenu 32 Weather Attenuated Color Highlight
41. 1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage Comments The PFD and or MFD is overheating and is reducing power consumption by dimming the display It problem persists the G1000 system MFD1 COOLING MFD1 has poor Should be serviced cooling Reducing power usage PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck CNFG MODULE PFD1 configuration module is inoperative PFD1 VOLTAGE PFD1 has low voltage Reducing power usage PFD2 VOLTAGE PFD2 has low voltage Reducing power usage MFD1 VOLTAGE MFD1 has low voltage Reducing power usage A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists The PFD1 configuration module backup memory has failed The G1000 system should be serviced The PFD1 voltage is low The G1000 system should be serviced The PFD2 voltage is low The G1000 system should be serviced The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sju
42. 1V oipny dadx SV4 sjueuingjsu Wi0 AeN yybi4 Puruuejd oE e2uepioAy SoJnpa20Jd puezey sue v uoneJjedo sainjee4 unuuy jeuuouqy jeuonippy xipueddy xepu Abnormal Additional Annun Flight Instruments Nav Com XPDR Audio Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N Enable Terrain While the Terrain SVS Page is displayed select 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 A NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY eee 52 WARNING The TAWS display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south eo NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS
43. 1ubi 4 wio gt AeN A Engine amp Airframe Systems GARMIN Flight Instruments z Es oc Se 88 x lt FO Flight Planning Procedures Rear Cargo Door Open 5 Pitot Probe 2 2 Cabin Door Open 6 Forward Cargo Door Open 3 Pilot Door Open 7 Propeller Heaters 4 Pitot Probe 1 Stall Warning Sensor General Synoptics Page Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Appendix Index 12 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN NAV COM TRANSPONDER AUDIO PANEL ENTER OR CHANGE FLIGHT ID Nav Com XPDR Audio Panel 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 Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accep
44. 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Hazard Avoidance 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Terrain Obstacle above or within 100 below current aircraft altitude Black Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final A
45. 475 The GCU 475 is unavailable MANIFEST GCU software The GCU 475 has incorrect software installed mismatch communication halted The G1000 system should be serviced GCU KEYSTK GCU key name A key is stuck on the GCU 475 bezel Attempt Key is stuck to tree the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 91 SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi WO gt AeN i jeuonippv uoneJjedo jeunouqy bid OAM xepu Ammundatons amp Alets GARMIN GMC 710 MESSAGE ADVISORIES ame Ne J oi SO Error in the configuration of the GMC 710 Config service req d GMC FAIL GMC is inoperative A failure has been detected in the GMC 710 The GMC 710 is unavailable Flight Instruments EAS Nav Com XPDR Audio MANIFEST GMC software The GMC 710 has incorrect software installed mismatch Communication halted The G1000 system should be serviced GMC KEYSTK GMC key name A key is stuck on the GMC 710 bezel Attempt Key is stuck to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists AFCS GPS Nav GTS 820 MESSAGE ADVISORIES GTS CONFIG GTS config error The GTS and GDU have incompatible Config service req d configurations This alert is also
46. A1 audio contig error Config service req d The GIA1 and or GIA2 have an error in the audio figuration The G1000 system should b GIA2 CONFIG GIA2 audio config Samon e Ss system shoud oe serviced error Contig service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 COOLING GIA1 The GIA1 and or GIA2 temperature is too low GIA COOLING GIA to operate correctly Allow units to warm up to temperature too low GIA1 COOLING GIAT over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 03 SoJnjeoJ 92uepioAy soJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH i WO gt AeN i jeuonippv uonejedo jeuuouqv bid E Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN GIA 63W MESSAGE ADVISORIES CONT GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted A GIA mismatch has been detected where only HW MISMATCH
47. AY puezey s n e 4 Jeuohippy uolje1ado Jeuuouqy Sue v unuuy xipueddy xopu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 58 GARMIN Ad itional Features ADDITIONAL FEATURES Sjueuinjijsu 64 SYNTHETIC VISION SV3 WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic oipny dadx Wo gt AeN SJdV Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD SVS offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting e Three dimensional Traffic e Airport Signs e Runway Display buruue d AEN Sd5 ui SoJnpo 20Jd
48. Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes Terrain Proximity TERRAIN SVS and TAWS are also disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy Flight Procedures Planning GPS Nav Hazard Avoidance Additional Features Annun Appendix Alerts Index 68 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS CAS MESSAGES Warning Messages Messages Comments Battery temperature over 0 C EDAM Bleed temperature high CABIN ALTITUDE Cabin altitude over 10 000 ft Cabin pressure differential over 6 2 psi TE Pilot or cabin door open OO ARE Engine compartment fire temperature over 200 C if installed SE Dissymmetry between left and right hand flaps FUELOFF Fuel tank selectors set to Off DESEE fuel pressure below 10 psi Engine start models A B amp C ITT over 1000 C 870 C 5 seconds or 800 C 20 seconds Engine start model N only ITT over 1000 C 870 C 5 seconds or 840 C 20 seconds Engine running ITT over 840 C OILPRESS Oil pressure below 60 psi OGN Oxygen cylinder closed gaseous oxygen systems Oxygen system has been activated chemical oxygen systems eae Parking brake applied ENT
49. Configure Vspeed Bugs nnne 2 Set Barometric Radar Altimeter Minimum Descent Altitude 3 Manually Testing the Radar Altimeter KRA 405B only S Displaying Wind Data ssssssssseseeeeeen tenen 3 Changing HSI Format 4 ENGINE amp AIRFRAME SYSTEMS 5 Electrical System 6 RU CI RR Tm 10 General Systems erret tenentes 11 NAV COM TRANSPONDER AUDIO PANEL 13 Enter or Change Flight ID aoeecunaetop qu e UDTERPR A TUDIN NOANTONUDAUEUIAQURI 13 ADF Tuning Optional sssssssseeeeeeteenenenes 13 DME TUNNO uroer en a EAE AAE AEA AA 13 Enter a Transponder Code sss 14 Selecting a COM Radio css cerca ar EPOD quU PUEDE UP EODD NOTE 14 Selecting a NAV Radio 14 NAV COM Tuning csc serearts stones soncnosetaransvetononveearonsesoroncsecetonseeton ctv abnanais CALI REVENU TUNE 14 luin nce Reena ere ere ee tet ete ec eee er re ee 15 Passenger Address PA System 15 Clearance Recorder and Player sssssssee 15 AUTOMATIC FLIGHT CONTROL SYSTEM 17 Flight Director Activation sssssseeeeeeeenn 17 Vertical Modes ette odi pedem deidin m dU Hen dU 18 Lateral MOSS coeno etri EM MUCIUS 19 GPS NAVIGATION nois ices REDUCE EU DM MU DUM ME 21 Direct to Navigation 21 Activate a Stored Flight Plan 22 Activate a Flight Plan Leg sss 22 Stop Navigating a Flight
50. D Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD DIS radial distance Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft
51. FD1 PFD2 or MFD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database After the update completes the display starts in normal mode Turn the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD Apply power to the system and press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Appendix 11 Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database cycle information is shown for each display Loading the Jeppesen Navigation Database as the Standby Navigation Database NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of each PFD and the MFD
52. Flight Planning Hazard Additional Annun EAS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index amp Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes e Traffic Annunciations System Time e Glideslope Glidepath e AFCS Annunciations PFD Setup Menu and Vertical Deviation Flight Director Windows displayed in Indicators Command Bars the lower right corner Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References e Radar Altimeter e DME Information Nearest Airports Selected Altitude Window Flight Plan e VNV Target Altitude Wind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status e Barometric Minimum Box Descent Altitude Box Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and disp
53. G1000 Integrated Flight Deck Cockpit Reference Guide TBM700 by DAHER SOCATA A GARMIN Copyright O 2010 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0829 00 or later for the Socata TBM 700 A B C and N Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton S040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 For after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a har
54. GEA1 contig error The GEA1 configuration settings do not match Contig service req d those of backup configuration memory The G1000 system should be serviced GEA2 CONFIG GEA2 config error The GEA2 configuration settings do not match Contig service req d those of backup configuration memory The G1000 system should be serviced MANIFEST GEAT software The 1 GEA 71 has incorrect software installed mismatch communication halted The G1000 system should be serviced MANIFEST GEA2 software The 42 GEA 71 has incorrect software installed mismatch communication halted The G1000 system should be serviced 86 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts GTX 33 33D MESSAGE ADVISORIES XPDR1 CONFIG XPDR1 config The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced XPDR2 CONFIG XPDR2 config The transponder configuration settings do not error Contig service req d error Contig service req d MANIFEST GTX1 software match those of backup configuration memory The G1000 system should be serviced mismatch communication halted The G1000 system should be serviced The transponder has incorrect software installed MANIFEST GTX2 software mismatch communication halted The G1000 system should be serviced GTX 33 33D MESSAGE ADVI
55. GPS AHRS1 using backup The 1 AHRS is using the backup GPS path GPS source Primary GPS path has failed The G1000 system should be serviced when possible AHRS2 GPS AHRS2 using backup The 2 AHRS is using the backup GPS path GPS source Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving any or any useful any GPS information GPS information Check AFMS limitations The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving The 2 AHRS is not receiving any or any useful any GPS information GPS information Check AFMS limitations The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving backup GPS backup GPS information information The G1000 system should be serviced AHRS2 GPS AHRS2 not receiving The 2 AHRS is not receiving backup GPS backup GPS information information The G1000 system should be serviced AHRS1 GPS AHRS1 operating The 1 AHRS is operating exclusively in no GPS exclusively in no GPS mode mode The G1000 system should be serviced AHRS2 GPS AHRS2 operating The 2 AHRS is operating exclusively in no GPS exclusively in no GPS mode mode The G1000 system should be serviced AHRS MAG DB AHRS magnetic The 1 AHRS and 2 AHRS magnetic model model database version mismatch database versions do not match AHRS1 SRVC AHRS1
56. ISORIES CONT COM1 RMT XFR COM1 remote The COM1 and or COM2 transfer switch is stuck transter key is stuck in the enabled or pressed position Press the COM2 RMT XFR COM2 remote transfer switch again to cycle its operation If transfer key is stuck the problem persists the G1000 system should be serviced LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase with other NAVS of flight GPS NAV LOST Loss of GPS Loss of GPS navigation due to insufficient navigation Insufficient satellites satellites ae iut 2d B A Loss of GPS navigation due to position error navigation Position error E E US Loss of GPS navigation due to GPS failure navigation GPS fail ABORI AEN SUE Abort approach due to loss of GPS navigation navigation Abort approach APR DWNGRADE Approach Vertical guidance generated by SBAS is downgraded unavailable use LNAV only minimums TRUE APR True north approach Displayed after passing the first waypoint of a Change HDG reference to TRUE true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be GPS2 SERVICE GPS2 needs available The G1000 system should be serviced service Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return uni
57. Magnetic The 1 AHRS earth magnetic field model is out field model needs update of date Update magnetic field model when practical AHRS2 SRVC AHRS2 Magnetic The 2 AHRS earth magnetic field model is out field model needs update of date Update magnetic field model when practical 88 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Annunciations amp Alerts GRS 77 MESSAGE ADVISORIES CONT GEO LIMITS AHRS1 too far Te North South no magnetic compass The aircraft is outside geographica limits for approved AHRS operation Heading is flagged GEO LIMITS AHRS2 too far seme North South no magnetic compass MANIFEST GRS1 software The 1 AHRS has incorrect software installed mismatch communication halted The G1000 system should be serviced MANIFEST GRS2 software The 42 AHRS has incorrect software installed mismatch communication halted The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES HDG FAULT AHRS1 A fault has occurred in the 1 GMU 44 magnetometer fault has occurred Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced HDG FAULT AHRS2 A fault has occurred in the 2 GMU 44 magnetometer fault has occurred Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced mismatch communication h
58. NCEL and press the ENT Key SoJnjeoJ a UEPIOAY SoJnpa20Jd Jeuonippy puezey uonejedo Jeuuouqv sue v unuuy GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan xipueddy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 3 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 3 4 5 A GARMIN The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USROO0 USROO1 USROO2 and so On To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 38 1 2 3 4 5 6 7 Insert the SD card into the top card slot on the MFD Press the FPL Key on the MFD Contol Unit to display t
59. NT Key Or Press the go around button Nav Com GPS Nav AFCS XPDR Audio EAS Flight Planning 4 o S 7 o e a Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Appendix Index 42 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Hazard Avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Strike is between 1 and 2 min
60. Plan 23 Vertical Navigation VNAV ssssssseeeeeeen eene 23 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Table of Contents GARMIN FLIGHT PLANNING sss 25 Weight Planning 25 a eterne 25 Create a New User Waypoint Defined by Latitude amp Longitude 2 Create a New User Waypoint Defined by Radials from Other Waypoints 28 Create a New User Waypoint Defined by a Radial amp Distance from Another Waypoint sssseeeeneten eterne tete 30 Delete a User Waypoint sssssssssseeenenenn 21 Create a New Flight Plan 5 sssssseeeeenenns 22 Import a Flight Plan from an SD Card 33 Insert a Waypoint in the Active Flight Plan 33 Enter an Airway in a Flight Plan 34 Invert An Active Flight Plan 29 Remove a Departure Arrival Approach or Airway from a Flight Plan 35 Store a Flight Plan 35 Edit a Stored Flight Plan sss 36 Delete a Waypoint from the Flight Plan 36 Invert and Activate a Stored Flight Plan 36 Copy a Flight Plan eene 37 Delete a Flight PLM ss ccccscnscidcstesctexesacosasteconenssnecscrossostevoreqsseustinedeuseascsacchesdiauneancsassteeniamenidien 37 Graphical Flight Plan Creation ssssssseeen 37 Export a Flight Plan to an SD Card sss 38 PROCEDURES eurei i a
61. R REN ELE 39 Load and Activate a Departure Procedure sse 39 Activate A Departure Leg 39 Load An Arrival Procedure 39 Activate An Arrival Leg ssssssssssseeeeee eene 40 Load and or Activate an Approach Procedure ssssss 40 Activate An Approach in the Active Flight Plan 41 Activate a Vector to Final Approach Fix 41 Activate A Missed Approach in the Active Flight Plan 42 HAZARD AVOIDANCE sssssssennnn 43 Customizing the Hazard Displays on the Navigation Map 43 STORMSCOPEG Optional 43 XM Weather Optional 45 Traffic Systems sssssssssseeeeeettettettete tnter tentent 4 Terrain And Obstacle Proximity ssssssssseeeee 50 TEE ANIM SVS RR TE s 50 Terrain Awareness amp Warning System TAWS Display 52 Airborne Color Weather Radar 54 I Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Table of Contents ADDITIONAL FEATURES sssssnnnnnnnnne 59 Synthetic Vision 59 Terminal Procedure Charts sssssssseeeenn 60 AOPA Airport Directory ssssseseeeeeeeten nennen 62 XM Radio Entertainment 63 ABNORMAL OPERATION 65 Reversionary Mode sss 65 Abnormal COM Operation
62. Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key SoJnpo 20Jd e uepioAy puezey mul t fet e 1 n jeuonippv Select an Available Channel within the Selected Category uonejedo Jeuuouqv 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go down through the list in the Channel Box or move up the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key xipueddy sue v unuuy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 63 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Abnormal Annun EAS AFCS GPS Nav Procedures Avoidance S ua e BB e Be e LL lt x Appendix Alerts Operation Index A Additional Features CG ARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys lo
63. SORIES CONT XPDR1 SRVC XPDR1 needs The 1 transponder should be serviced when service Return unit for repair possible XPDR2 SRVC XPDR2 needs The 2 transponder should be serviced when service Return unit for repair possible XPDR1 FAIL XPDR 1 is inoperative The transponder has incorrect software installed There is no communication with the 1 transponder XPDR2 FAIL XPDR2 is There is no communication with the 2 inoperative transponder GRS 77 MESSAGE ADVISORIES AHRS1 TAS AHRS1 not receiving The 1 AHRS is not receiving true airspeed from valid airspeed valid airspeed 190 01247 00 Rev A the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS2 TAS AHRS2 not receiving The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 sainjea4 92uepioAy soJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH i U0 AEN i jeuonippv uonejedo jeunouqy xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ Ammundatons amp Alets GARMIN GRS 77 MESSAGE ADVISORIES CONT AHRS1
64. TAN Torque greater than or equal to 121 496 maximum torque N only 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 69 s n e j 92UueploAy SoJnpo20Jd Puruuejd AeN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi JU0 AEN i jeuonippv uoneJjedo jeunouqy bid E xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ Ammundatons amp Alets GARMIN Caution Messages Fuel timer off or out of service ESSE Electric fuel pump running manual or automatic mode BATAMP Battery current over 50 A while on ground RN Battery of DEBES flow control and shut off valve shut off valve closed CHP Oil chip detector on if installed FRONT CARGO DOOR Forward baggage door open FUELIMBALANCE Fuel tanks imbalanced by more than 25 USGAL A B and C or 15 USGAL N for gt 30 seconds Fuel quantity less than or equal to 9 1 USGAL in specified tank a ae GPU receptacle door not closed IGNITION Ignition exciter running PSs ae eee Inertial separator failure BEMITSESBE Inertial separator extended Low fuel level sensor failure for specified tank LOWVOLTAGE Battery voltage below 26 V DEAS TEES Starter generator unconnected NGHE Generator speed is more than 103 OILPRESS Oil pressure between 60 and 100 psi i Oil temperature below 0 C or above 104 C Specifie
65. TAWS Not Available Traffic Played when a Traffic Advisory TA is issued with the TIS system Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued with a TAS system TAS System Test OK Played when the TAS system passes a pilot initiated self test TAS System Test Failed Played when the TAS system fails a pilot initiated self test One o clock through Played to indicate bearing of traffic from own aircraft GTS 820 only Twelve o clock or No Bearing High Low Same Played to indicate altitude of traffic relative to own aircraft GTS 820 only Altitude if within 200 feet of own altitude or Altitude not available Less than one mile Played to indicate distance of traffic from own aircraft GTS 820 only One Mile through Ten Miles or More than ten miles 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 11 SoJnjeoJ 92uepioAy SoAnpo20Jd Puruuejd AeN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi JU05 AEN i jeuonippv uoneJjedo Jeuuouqv xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN MFD amp PFD MESSAGE ADVISORIES DATA LOST Pilot stored data was The pilot profile da
66. affic device has The G1000 is no longer receiving data from failed the traffic system The traffic device should be serviced FAILED PATH A data path has A data path connected to the GDU or the GIA failed 63 W has failed 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 95 sainjea4 92uepioAy SoAnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi WO gt AeN i jeuonippv uoneJjedo Jeuuouqv Xapu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT MAG VAR WARN Large magnetic The GDU s internal model cannot determine variance Verify all course angles the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of Synthetic Vision is disabled because the aircraft available terrain region is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB Synthetic Vision is disabled because a terrain resolution too low 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 e
67. after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or SjueuinJjsu 1ubi 4 oipny uadx SV3 Wi0 gt AeN S4V Err is shown Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted System timed out prior to the database transfer completing Loading Garmin Database Updates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the small FMS Knob to select the System Status Page 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 107 sainjea4
68. alted The GMU 44 has incorrect software installed MANIFEST GMU software The G1000 system should be serviced 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 89 sainjea4 92uepioAy soJnpo20Jd Puruuejd AeN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH i JU05 AEN i jeuonippv uonejedo jeunouqy xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ Annunciations amp Alerts GDL 69A MESSAGE ADVISORIES GDL69 CONFIG GDL 69 config error Config service req d GDL69 FAIL GDL 69 has failed MANIFEST GDL software mismatch communication halted GWX 68 ALERT MESSAGES A GARMIN GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced 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 GWX CONFIG GWX config error Config service req d GWX FAIL GWX is inoperative GWX 68 configuration settings do not match those of the GDU configuration The G1000 system should be serviced The GDU is not recieving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar system should be serviced GWX SERVICE GWX needs A fai
69. ancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key HF if installed on the audio panel Receive Only Press the COM1 COM2 or COMB Key HF if installed on the audio panel SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV 2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio trequency 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 700 190 01247 00 Rev A A GARMIN Nav Com XPDR Audio Panel INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may
70. ase the FAF altitude can be designated White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot the system estimating entered by the pilot use this altitude the altitude of the Altitude is designated in determining aircraft as it passes over for use in giving vertical vertical flight path the navigation point flight path guidance guidance This altitude is provided Altitude does not match as a reference and is the published altitude not designated to be in navigation database used in determining or no published altitude vertical flight path exists 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 path guidance Altitude determining vertical flight path guidance has been retrieved from flight path guidance Altitude has been the navigation database retrieved from the or has been entered by navigation database the pilot and matches a and is provided as a published altitude in the reference navigation database 24 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN WEIGHT PLANNING Flight Planning FLIGHT PLANNING All procedures apply to the MFD unless otherwise stated Entering Weight Parameters The Weight Planning Page is displayed after system power up If it i
71. ather 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 700 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce t
72. ation on the remaining display SV3 SjueuinJjsu 64 olpny YddX Wo gt AeN Activation of reversionary display mode is accomplished by pressing the DISPLAY BACKUP Button on the appropriate audio panel PFDI By pressing the DISPLAY BACKUP Button on the left audio panel e MFD By pressing the DISPLAY BACKUP Button on the left or the right audio panel PFD2 By pressing the DISPLAY BACKUP Button on the right audio panel AEN Sd5 S 1V Puruuejd 1461 4 NOTE The Socata TBM 700 Airplane Flight Manual AFM always takes precedence over the information found in this section SoJnpo 20Jd ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios e2uepioAy puezey SoJnjeoJ jeuonippy HAZARD DISPLAYS WITH LOSS OF GPS POSITION i If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established sue v unuuy xipueddy Loss of Hazard Functions with Loss of GPS Position xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 65 Flight Instruments Nav Com XPDR Audio
73. cated on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select the SET Softkey 4 Select any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 With the XM Radio Page displayed select the VOL Softkey 2 Select the VOL Softkey to reduce volume or select the VOL Softkey to increase volume Once the VOL Softkey is selected the volume can also be adjusted using the small FMS Knob 3 Select the MUTE Softkey to mute the audio Select the MUTE Softkey again to unmute the audio XM Radio volume may also be adjusted on each passenger headset 64 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Reversionary mode must be entered manually in the case of PFD1 PFD2 or MFD failure In reversionary mode critical flight instrumentation is combined with engine instrument
74. ce Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Flight Planning 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location SV3 SjueuinJjsu 64 oipny uadx Wo gt AeN COPY A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 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 S 1V AEN Sd5 ag D 5 Cs DELETE A FLIGHT PLAN 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CA
75. d drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries WATCHS FliteCharts and SateTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fitness for a particular purpose The information is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances including negligence shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative
76. d pitot heat 1 or 2 on while engine off Specified pitot heat 1 or 2 off A Prop deice selected and not on BEZSPES Prop deice on while engine off EZ Rear cargo door open STALLHEATON Stall warning heat on while engine off STALLNOHEAT Stall warning heat off STARTER Starter generator running VACUUM LOW Vacuum pressure less than 3 75 in Hg Only affected side L R L R or 1 2 1 2 displayed in CAS message applicable messages listed here display L R or 1 2 for example 70 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Annunciations amp Alerts COMPARATOR ANNUNCIATIONS Comparator Condition Window Text Difference in altitude sensors is gt 200 ft If both airspeed sensors detect 35 knots this is inhibited If either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts If either airspeed sensor detects gt 80 knots and the difference in sensors is gt 7 kts Difference in heading sensors is gt 6 degrees Difference in pitch sensors is gt 5 degrees Difference in roll sensors is gt 6 degrees AVG eR ee No data from one or both altitude sensors PENH NUM No data from one or both airspeed sensors Lem eRe 0 Iam No data from one or both heading sensors ul NM No data from one or both pitch sensors SUM Eee No data from one or both roll sensors REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Condition
77. d vary significantly from the altitude displayed by pressure altimeters such as the GDC 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 A Warnings Cautions amp Notes GARMIN AN WARNING XM Weather should not be used for hazardous weather penetration We
78. dio Flight Planning AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired select the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude I I Terrain Obstacle between 100 and 1000 below current aircraft altitude Black Terrain Obstacle is more than 1000 below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map TERRAIN SVS A NOTE Terrain data is not displayed when the aircraft latitude is greater than 50 NOTE Terrain SVS is only available when the Synthetic Vision System
79. e Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Too Low Terrain Five Hundred Sink Rate Don t Sink or Too Low Terrain Alert Type AAA TAWS B Page Annunciation aula PETENS Message System Test in Progress TANS TEST TEST TAWS System TAWS Alerting is disabled TAWS INH None MED Terrain or Obstacle database unavailable or invalid TAWS operating with PFD Terrain or Obstacle databases TAWS B System Test Fail Terrain or Obstacle database unavailable or invalid invalid software configuration system audio fault 76 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 None TAWS System Failure TAWS System Failure 190 01247 00 Rev A GARMIN Annunciations amp Alerts Alert Type TUUM AEN TAWS B Page Annunciation Aura Annunciation Message TAWS Not Excessively degraded GPS signal Out of database coverage area Sufficient GPS signal Sane T TAWS received after loss Available VOICE ALERTS Voice Alert Minimums minimums The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Airspeed Airspeed Played when the indicated airspeed is below a given threshold for a given aircraft configuration Note this alert may be heard under normal conditions during the landing flare
80. e small FMS Knob The Waypoint Information Window is now displayed xipueddy 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 33 Additional Hazard Avoidance Abnormal Annun Flight Instruments Nav Com XPDR Audio EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airport waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 34 1 2 3 4 5 6 7 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint field after the desired airway entry point If this previous waypoint is not a valid air
81. ed readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Hazard Avoidance Antenna Stabilization 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert select the WX ALRT 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 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 5 AEN Sd5 S241V oipny dadx SV4 sjueuingjsu Wi0 AeN yybi4 Puruuejd oE e2uepioAy SoJnpa20Jd puezey sue v uone1edo sainjee4 unuuy jeuuouqy jeuonippy xipueddy xepu GARMIN Hazard Avoidance SjuouunJjsu 1ubi4 SV3 oipny qadx Wo gt AeN S21V AEN Sd5 Puruuejd IE Blank Page soinpsd0ld a UepIO
82. edo unuuy Jeuuouqv xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 61 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Abnormal Annun EAS AFCS GPS Nav Procedures Avoidance S ua 5s 2 BB e Be e LL lt x Appendix Alerts Operation Index A Additional Features CG ARMIN View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to 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 crossov
83. edo jeuuouqv sue v junuuy xopu xipueddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN 110 13 Turn system power OFF 14 Remove the SD card from the top card slot of the MFD 15 Turn system power ON 16 Press the ENT Key to acknowledge the startup screen 17 Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the System Status Page 19 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN A Activate a flight plan 22 Active Channel 63 Active database 108 Active Navigation Database 108 ADF 13 14 66 AHRS 87 88 89 91 92 Airport Signs 59 60 Airways 106 Air Data Computer 71 Alert messages 90 ALT 49 Altimeter setting 1 66 Altitude mode 49 Altitude volume 49 Antenna stabilization 57 Antenna tilt 55 AOPA s Airport Directory 62 Attitude amp Heading Reference System 71 Audio panel controls NAV1 NAV2 14 Barometric Altitude Minimums 3 Battery Alerts 70 Current 6 Overheat warning 69 Voltage 6 Bearing line 55 56 C
84. eg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 sue v uoneJjedo SoJnjeaJ o2uepioAy seJnpo2o0Jd Duiuue d ACN Sd5 j4V oipny uddx SV3 sjuauinajsu unuuy Jeuuouqy jeuonippy U10 AEN xipueddy xepu 1ubi 4 1ubi 4 puezey Procedures GARMIN 4 Turn the large FMS Knob to highlight the desired arrival 5 Press the ENT Key A list of transitions is displayed for the selected arrival 6 Turn either FMS Knob to select the desired transition 7 Press the ENT Key A list of runways may be displayed for the selected arrival 8 Turn the large FMS Knob to highlight the desired runway 9 Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan Nav Com Flight XPDR Audio EAS Instruments AFCS ACTIVATE AN ARRIVAL LEG GPS Nav 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE
85. er point based on backlighting intensity Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check fly garmin com for the current database View Airport Directory Information 62 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport intormation is displayed on the right half of the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Additional Features XM RADIO ENTERTAINMENT Sjueuinjijsu 1uDij3 The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page SV3 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select XM Radio 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled oipny uddx JUI0 AEN S 1V Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category AEN Sd5 Puruuejd 1461 4 Selecting a Category The Category Box of the XM
86. erative The audio panel self test has detected a failure GMA2 FAIL GMA2 is inoperative The audio panel is unavailable The G1000 system should be serviced Operation GMA XTALK GMA crosstalk error An error has occurred in transferring data has occurred between the two GMAs The G1000 system should be serviced Index Appendix LE 82 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES CONT GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Contig service req d MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The MANIFEST GMA software G1000 system should be serviced mismatch communication halted GMA1 SERVICE GMAT needs The audio panel self test has detected a problem in service Return unit for repair the unit Certain audio functions may still be avail GMA2 SERVICE GMA2 needs able and the audio panel may still be usable The service Return unit for repair G1000 system should be serviced when possible The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced GIA 63W MESSAGE ADVISORIES GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Contig service req d GIA1 CONFIG GI
87. ess the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey AEN Sd5 S dV Puruuejd oE MANUALLY TESTING THE RADAR ALTIMETER KRA 405B ONLY SoJnpo 20Jd 1 Select the AUX SYSTEM STATUS Page on the MFD 2 Select the RA TEST Softkey The Radar Altitude window displays 50 feet and RA TEST is displayed to the left of the Radar Altitude window indicating a properly functioning system e2uepioAy puezey 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test SoJnjeoJ Jeuonippy DISPLAYING WIND DATA uonejedo Jeuuouqv 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data below the Selected Heading 3 Select one of the OPTN softkeys to change how wind data is displayed 4 Toremove the Wind Data Window select the OFF Softkey xipueddy sue v unuuy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 3 m E ns Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun Instruments EAS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments
88. essary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station 60 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Additional Features ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView ChartView resembles
89. euinajsu piezeH yi U0 AEN i jeuonippv uoneJjedo jeunouqy MFD1 DB ERR MFD1 navigation database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 navigation navigation database Attempt to reload the database error exists navigation database If problem persists the PFD2 DB ERR PFD2 navigation 61000 system should be serviced database error exists 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 19 xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN DATABASE MESSAGE ADVISORIES CONT MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1basemap The MFD and or PFD detected a failure in the database error exists basemap database PFD2 DB ERR PFD2 basemap database error exists MFD1 DB ERR MFD1 terrain M database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 terrain terrain database Ensure that the terrain card is M properly inserted in display Replace terrain card If problem persists The G1000 system should be PFD2 DB ERR PFD terrain serviced database error exists MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain The terrain database is present on another LRU database missing bu
90. eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Record of Revisions Part Number Change Summary 190 01247 00 Initial Release buts Date of Revision Affected Pages December 2010 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 RR 1 Record of Revisions GARMI N Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Table of Contents FLIGHT INSTRUMENTS ssssssssnnnnnnnnnn Selecting the Altimeter Barometric Pressure Setting Selecting Standard Barometric Pressure Change Altimeter Barometric Pressure Setting Units Synchronizing the Altimeter Barometric Pressure Settings Synchronize CDI sssssssssseeeeeetetnetetent rentrer Change Navigation Sources ssssssseeeeeeenennenennnnn 2 Enable Disable OBS Mode While Navigating with GPS 2 Generi UTM eona EAE E EE A EE 2
91. f the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGL 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 ffl on the PFD or controller 2 Turn 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 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 SV3 SjueuinJjsu 4614 oipny uadx U0 AEN AEN Sd5 S 1V Sov uoneJjedo SoJnjeoJ 92uepioAy soJnpo20Jd Duiuue d junuuy Jeuuouqy Jeuonippy paezey LTE xipueddy xepu Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EAS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS
92. ference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Engine amp Airframe Systems Left Fuel Switching Right Unknown Fuel Tank Fuel Tank Fuel Tank Fuel Tank Selector Selected Selection Selected Selection Off D QO Fuel Selector Status If the auxiliary fuel boost pump is on the symbol is displayed in green The mode automatic AUTO or manual MAN is displayed next to the pump symbol If the boost pump is off the symbol is shown in light blue automatic mode or red manual mode Fuel Boost Pump Fuel Boost Pump Fuel Boost Pump On Off Auto Off Manual Auxiliary Boost Pump Status 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 mes sages also generated Statuses of stall sensor propeller and pitot probes heat are also indicated on the diagram White indicates that heat is off propeller Green indicates heat is on Yellow indicates heat has failed stall sensor propeller and pitot tube Invalid sensor information is indicated with a red X 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 11 Sov uonejedo SoJnjeoJ 92uepioAy SoAnpo20Jd Puruuejd AeN Sd5 S j4JV oipny 4adx SV3 sjueuinajsu junuuy Jeuuouqy Jeuonippy puezey LTE xipueddy xepu
93. fi xipueddy iin Cross AT or BELOW 3 000 fi xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 23 1ubi 4 ouem i puezey jeuonippv Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EAS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index GPS Navigation GARMI N Since altitudes loaded with an arrival procedure are published only for turbojet aircraft the altitudes are displayed as white text indicating that the altitudes are displayed for reference only An arrival waypoint altitude may be used or designated as is or changed to a different altitude An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or entering a different value and pressing the ENT Key The altitude is now displayed as blue text indicating that the altitude is now designated to give vertical speed and deviation guidance Approach waypoint altitude constraints are designated in the same way as previously described for arrivals These altitudes are also displayed as blue text after being designated for use Waypoint altitude constraints may be designated up to but not including the FAE The FAF is always a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this c
94. g option trom the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN GPS Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan SV3 sjuauinajsu oipny uadx U0 AEN VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN KIXD KDFW Puruuejd oE KARLA Am a Large White COVIE 221 9 NM 12400FT inn LEMYN 220 8 0NN F Large Light 4 B E f Blue Text g Approach KDFW RNAV 17LGPs LPY RIVET iaf 259 18 8NH gee Small Light z DRAAK 176 3 3MM Blue Text 3 INWOD 176 3 2NM Small Light MENOL faf 176 39NW A 7 RW17L map 176 5 3NM 3 d ds e Small White Text POLKE Restriction Bar uoneJjedo Jeuuouqv sue v junuuy SIS Cross AT or ABOVE 5000 ft FAS Cross AT 2 300
95. he Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Turn the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key for the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected l
96. he FPL Key to display the active flight plan Press the FMS Knob to activate the cursor AEN Sd5 Or for a stored flight plan a Press the MFD FPL Key and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor c Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints ag D 5 ts e uepioAy SoJnpa20Jd puezey SoJnjeoJ Jeuonippy 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 uoneJjedo Jeuuouqv STORE A FLIGHT PLAN sue v unuuy 1 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan xipueddy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 35 Flight Planning GARMI N EDIT A STORED FLIGHT PLAN 1 Press the FPL Key for the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight pla
97. he SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 97 sainjea4 92uepioAy soJnpo20Jd Puruuejd AeN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi U0 AEN i jeuonippv uonejedo Jeuuouqv bid E xepu GARMIN Annunciations amp Alerts SjuouunJjsu 1ubi4 SV3 oipny dadx Wo gt AeN S21V AEN Sd5 Puruuejd IE Blank Page SoJnpo oJd 92UepIOAV puezey s n e 4 jeuonippy uoneledo Jeuuouqy OA xipueddy xopu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 98 GARMI N LLL Appendix APPENDIX SjueuinJjsu 64 PFD SOFTKEY MAP SV3 inset Sensor ero oss cov apeowe xeon oent reer nest mse nnn D S O FA v3 v3 D CDI NAV1 CDI NAV2 oipny uadx Wo gt AeN gt A CDI GPS i Top Level PFD Softkeys a Nn g S O n F3 V3 P3 DNAD D OD 38 ae optional optional optional optional optional ry a mon n SoJnpo 20Jd Select the BACK Softkey to return to the top level softkeys 92uepioAy puezey Inset Map Softkeys sainjea4 jeuonippy Levell Level2 Level 3 Description uoneJjedo Jeuuouqv INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map sue v junuuy DCLTR 3 Selects desired amount of
98. he risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Socata TBM 700 Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Warnings Cautions amp Notes WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at al
99. hen scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 22 AEN Sd5 S241V oipny dadx SV4 sjueuinajsu Wi0 AeN yybi4 Puruuejd oE e2uepioAy SoJnpa20Jd puezey sue v uoneJjedo s9JnjeaJ unuuy jeuuouqy jeuonippy xipueddy Xapu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 56 A GARMIN Adjusting Gain WARNING Changing the gain in Weather Mode will cause precipitation intensity to be d
100. ilot and commands Switch Go Around a preprogrammed constant pitch attitude and wings level i d mo in the AFCS Status Box The low bank angle range is indicated in green along the Roll Scale of the Attitude Indicator 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 19 SjueuunJdjsu HJ SV3 oipny uadx U105 AeN AEN Sd5 S 1V Sov uonejedo sainjea4 92uepioAy SoAnpo20Jd Duiuue d junuuy Jeuuouqy Jeuonippy pieze iui xipueddy xepu GARMIN AFCS SjuouunJjsu 4614 SV3 oipny dadx Wo gt AeN AEN Sd5 Puruuejd IE Blank Page SoJnpo 0Jd 92UepIOAV puezey SoJnjeoJ jeuonippy uoneJoedo jeuuouqy Sue v unuuy xipueddy xopu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 20 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation using the MFD 1 Press the Direct to fJ Key on the MFD Control Unit 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter 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 I
101. isplay more 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 45 AEN Sd5 S241V oipny dadx SV4 sjueuingjsu Wi0 AeN yybi4 Puruuejd oE e2uepioAy SoJnpa20Jd puezey sue v uone1edo s9JnjeaJ unuuy jeuuouqy jeuonippy xipueddy xepu Nav Com Flight GPS Nav AFCS XPDR Audio EAS Instruments Flight Planning Hazard Avoidance Procedures Annun Abnormal Additional Alerts Operation Features Appendix Index Hazard Avoidance GARMI N 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 CHE Description Status Icons P Ug C1 NEXRAD Available for the US and Canada The age of the displayed data CN Inf for each is shown at the right 5 ECHO TOP The age of the displayed data is shown at the right Not i displayed when CLOUD TOP is displayed 12 CLOUD TOP The age of the displayed data is shown at the right Not n displayed when ECHO TOP is displayed 1 XM LIGHTNING The age of the displayed data is shown at the right 4 3 CELL MOVEMENT The age of the displayed data is shown at the right zT Eu 1 SIGMET amp AIRMET The age of the displayed data for each is shown at the AIRMET 5m lliyi SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lowe
102. isplayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field Ground Mapping 1 Press the MODE Softkey 2 Press the GROUND Softkey to place the radar in Ground Map Mode 3 Press the BACK Softkey 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to place the cursor in the TILT field 6 Adjust the antenna tilt angle by turning the small FMS Knob to position the ground returns as desired 7 Press the FMS Knob to remove the cursor Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select FULL 60 40 or 20 scan 5 If desir
103. itude and wings level in preparation for takeoff Disengages the autopilot and a Go Around commands a constant preprogrammed pitch attitude and wings level ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 18 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN AM MAK LATERAL MODES Lateral Mode Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Limits maximum commanded roll angle p co Heading Select Captures and tracks Selected Heading Navigation GPS Arm Capture Track Navigation VOR Enroute Arm Captures and tracks selected navigation Capture Track source GPS VOR LOC Navigation LOC Arm Capture Track No Glideslope Backcourse Arm Captures and tracks a localizer signal BC Ke Capture Track for backcourse approaches Approach GPS Arm Capture Track Approach VOR Arm Capture Track Captures and tracks selected navigation APR Ke Approach ILS Arm Source GPS VOR LOC y Capture Track Glideslope Mode LOC automatically armed Commands a constant preprogrammed Takeoff constant pitch attitude and wings level in preparation for takeoff Disengages autop
104. l longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 A Warnings Cautions
105. lay the aircrafts current estimated position 66 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Abnormal operation NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position i
106. lel track unavailable Bad parallel track geometry bad geometry PTK FAIL Parallel track unavailable os Invalid leg type for parallel offset invalid leg type PTK FAIL Parallel track unavailable IAF waypoint for parallel offset has been past IAF passed UNABLE V WPT Can t reach The current vertical waypoint can not be current vertical waypoint reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported The lateral flight plan contains a procedure leg type in flight plan turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track The current track angle error exceeds the limit angle error causing the vertical deviation to go invalid VNV Unavailable Excessive The current crosstrack exceeds the limit crosstrack error causing vertical deviation to go invalid VNV Unavailable Parallel course A parallel course has been selected causing selected the vertical deviation to go invalid NON WGS84 WPT Do not use GPS The position of the selected waypoint xxxx navigation to boox is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint TRAFFIC FAIL Tr
107. lure has been detected in the GWX 68 The service Return unit for repair GWX 68 may still be usable MANIFEST GWX software The GWX 68 has incorrect software installed mismatch communication halted The G1000 system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 90 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts GDC 74B MESSAGE ADVISORIES ADC1 ALT EC ADC1 altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude ADC2 ALT EC ADC2 altitude error error correction is unavailable correction is unavailable ADC1 AS EC ADCT airspeed error correction is unavailable GDC1 or GDC2 is reporting that the airspeed ADC2 AS EC ADC2 airspeed error error correction is unavailable correction is unavailable MANIFEST GDC1 software mismatch communication halted The GDC 74B has incorrect software installed MANIFEST GDC2 software The G1000 system should be serviced mismatch communication halted GCU 475 MESSAGE ADVISORIES GCU CNFG GCU Config error GCU 475 configuration settings do not match Config service req d those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative A failure has been detected in the GCU
108. n GPU Door Open Selected Not Selected soJnjeaJ jeuonippy uonejedo Jeuuouqv GPU Door Closed sue v unuuy xipueddy Xapu GPU Door Status 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 l A Engine amp Airframe Systems GARMIN Battery connection status to the main bus is indicated in green direction of current flow is indicated with an arrow next to the current readout If the battery is disconnected from the main bus the switch is closed Battery overheating is indicated in red with a BAT OVHT annunciation a CAS message is also generated Flight Instruments Connected Disconnected Battery Overheat T z ES oc Se 88 x AFCS Battery Status FE Battery and essential bus voltages are displayed using gauges DC buses are shown in green when energized When not energized the connection line to the main bus is removed and the bus label is displayed in red E BAI BUS ESS BUS 2 Battery and Essential Bus Low Voltage Abnormal Operation Annun Alerts Appendix BUS 1 BUS 2 Bus Not Energized Index DC Bus Status 8 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Engine amp Airframe Systems The Emergency Buses switch has two positions UP open and DN ground If the switch is in the UP position the essential bus is connected to the battery bus If the switch is in
109. n 4 Select the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location Flight Instruments EAS Nav Com XPDR Audio 6 Enter the changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page AFCS DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor GPS Nav c XS a Or for a stored flight plan a Press the FPL Key of the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor c Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Turn the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window Hazard Avoidance Procedures Additional Features 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key 5 Once all changes have been made press the FMS Knob to remove the CUISOF Abnormal Operation Annun Alerts INVERT AND ACTIVATE A STORED FLIGHT PLAN Appendix 1 Press the FPL Key for the MFD 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor Index 36 Garmin G1000 Cockpit Referen
110. n the top card slot on the MFD 2 Press the FPL Key on the MFD Control Unit to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Select the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key S23V oipny dadx SV3 U10 AEN AEN Sd5 vu o e D e z D Nn 92uepioAy puezey SoJnjeoJ Jeuonippy INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan uonejedo Jeuuouqv 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint sue v junuuy 4 Turn th
111. nformation displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 67 e2uepioAy SoJnpo20Jd Puruuejd AeN Sd5 S JY oipny YddX SV3 sjueuinajsu ubi U0 AEN puezey soJnjeaJ Jeuonippy sue v unuuy xipueddy xopu 1ubi 4 Abnormal Operation GARMIN As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator e All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Nav Com Flight XPDR Audio EAS Instruments AFCS
112. nts c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial trom the reference waypoint 12 Press the ENT Key 13 Repeat step 10 to enter the next waypoint name 14 Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 29 oipny uadx SV3 Sjueuindjsu U10 AEN yybi4 S4V soinpsd01d Duiuue d AEN Sd5 614 sue v uoneJjedo S9JnjeaJ e2uepioAy junuuy jewuouqy Jeuonippy puezey xipueddy xepu Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EAS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 30 1 2 3 4 5 6 7 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MF
113. nvironmental control system has failed CRUISE Cruise conditions met Cruise engine trend data log has been captured CRUISE II Cruise Il conditions met Cruise Il engine trend data log has been captured PAEDR E E CEAR An engine exceedance log has been captured data is being logged 96 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Description Results Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only The file stored on the SD card did not contain a flight plan User waypoints imported success only user waypoints These waypoints have been saved to the fully No stored flight plan data was system user waypoints No flight plans stored in the system modified have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the s
114. on The PLAY annunciator flashes to indicate when play is in progress The PLAY annunciator turns off after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play If a COM input signal is detected during play of a recorded memory block play is halted 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 15 sjuauinajsu S24V oipny uadx Sv3 WOD AEN SHa V uonejedo SoJnjeoJ 92uepioAy SoJnpo20Jd Puruuejd AeN Sd5 junuuy Jeuuouqy Jeuonippy ubi xipueddy Xapu 1ubi 4 puezey A Nav Com XPDR Audio Panel GARMIN Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block Flight EAS Instruments Nav Com I 5 gt ce e a x Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS Appendix Index 16 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN AG 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 reve
115. plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the Cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identitier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN FightPlanning IMPORT A FLIGHT PLAN FROM AN SD CARD SjueuinJjsu 1uDij3 1 Insert the SD card containing the flight plan i
116. pproach Fix Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT Key 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 53 AEN Sd5 S241V oipny dadx SV4 sjueuingjsu Wi0 AeN yybi4 Puruuejd oE 92UuepioAy SoJnpa20Jd puezey sue v uone1edo S9JnjeaJ unuuy jeuuouqy jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS 2 o z ue A o Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Enable TAWS 1 2 3 While the TAWS B Page is displayed select the INHIBIT Softkey Or While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key AIRBORNE COLOR WEATHER RADAR 94 WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather
117. r symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom T us Tm METAR Available for the US and Canada The age of the displayed data for CN Em Jml COUNTY WARNING The age of the displayed data is shown at the right 46 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMI N LLL LL Hazard Avoidance YO rorun Description Status Icons P e a CYCLONE WARNING The age of the displayed data is shown at the right AIREP The age of the displayed data is shown at the right SV3 SjueuinJjsu 1uDij3 oipny uadx U105 AeN PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow zi TURBULENCE The age of the displayed data is shown at the right The e1 soon altitude selection is shown at the bottom aiil ICING POTENTIAL The age of the displayed data is shown at the right BOOO0FT The altitude selection is shown at the bottom TRAFFIC SYSTEMS e If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed e Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed Traffic Symbol Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within
118. rain System zt oma MFD Terrain or unavailable or Terrain System Fail database unav or invalid invalid softwar audio fault Terrain or Obstacle ailable TER FAIL configuration system Obstacle database invalid T Terrain SVS operating with PFD Terrain or Obstacle databases Test No GPS position Excessively degraded GPS signal Ou database coverage area A GARMIN None None Terrain System Failure Terrain System Failure Terrain System Not Available t of TER WA None Terrain System Not Available Sufficient GPS signal Terrain System l None None i i received after loss Available 14 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Annunciations amp Alerts TAWS ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message LN Pop Up Alert Annunciation Excessive Descent PULL UP UP PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Pull Up Terrain Clearance Warning RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Terrain or Ahead Pull Up Impact Warning ITI TERRAIN PULL UP 8 7 i Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Up Obstacle Clearance or Pull Up Waming ROC I Obstacle Ahead Pull Up Obstacle
119. rn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to 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 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 41 AEN Sd5 S241V oipny dadx SV4 sjueuingjsu Wi0 AeN HL Puruuejd 1461 4 sue v uone1ado SoJnjeoJ o2uepioAy SoJnpa20Jd Junuuy Jeuuouqy Jeuonippy puezey xipueddy xepu A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN Flight Instruments 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the E
120. rspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system 11 The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system 12 w The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature 13 w CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tur the large FMS Knob on the MFD Control Unit to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 27 oipny 4ddX sV3 sjueuingsu 1uDiI4 UI05 AeN S 1V SoJnpo 20Jd Duiuue d AEN Sd5 614 e2uepioAy puezey sue v uoneJjedo S9JnjeaJ
121. rts to the default mode for that axis A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed r 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 Takeoff on ground TO Takeoff on ground TO Go Around in air GA Go Around in air GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS Navigation VOR Pitch Hold default PIT LOC BC Key Backcourse BC Pitch Hold default PIT Pitch Hold default PIT Approach Glidepath GP Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director P i selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector 190 01247 00
122. s necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the first rectangular page icon 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enter the desired weight of Pilot amp Stores 5 Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered Entering Fuel Parameters 1 If necessary press the FMS Knob to activate the cursor 2 Turn the large 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 Knob to select the second rectangular page icon 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode select the AUTO or MANUAL Softkey 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 25 oipny uadx SV3 Sjueuindjsu U10 AEN
123. set when the GTS has an invalid mode S address configured or Flight Planning Procedures the mode S address does not match both XPDR mode S addresses MANIFEST GTS software The GTS has incorrect software installed The mismatch communication halted G1000 system should be serviced Hazard Avoidance Additional Features Abnormal Operation Index Appendix EJ 92 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES FPL WPT LOCK Flight plan Upon power up the G1000 system detects that waypoint is locked a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identitier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint waypoint moved coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notities the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan con
124. situation Preflight system test failed aural alert sounds at failure TERRAIN SVS ALERTS PFD MFD TERRAIN SVS Page Annunciation Alert Type Reduced Required Terrain Clearance Warning RTC Imminent Terrain Impact Warning ITI Reduced Required Obstacle Clearance Warning ROC Imminent Obstacle Impact Warning lOl Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Reduced Required Obstacle Clearance Caution ROC Imminent Obstacle Impact Caution IOl TERRAIN 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 Aural Message MFD Pop Up Alert WARNING TERRAIN WARNING TERRAIN Warning Terrain Terrain Warning Terrain Terrain WARNING OBSTACLE Warning Obstade Obstacle Warning Obstacle Obstacle Caution Terrain Terrain WARNING OBSTACLE Caution Terrain Terrain Caution Obstade Obstade Caution Obstade Obstade Sm sainjea4 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 4JV oipny uadx SV3 sjueuinajsu piezeH yi U0 AEN i jeuonippv uoneJjedo Jeuuouqv xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ Annunciations amp Alerts TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS PFD MFD Alert TERRAIN SVS Page System Test in Ter
125. t Fail is heard Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 7 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Select the FLT ID Softkey GTS 820 only to enable or disable Flight ID displayed with the intruder information Displaying Traffic on the Navigation Map 1 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 S21V oipny uddx sv3 s u wuna su UI05 AeN AEN Sd5 Puruuejd e2uepioAy SoJnpa20Jd puezey saunyeaj Jeuonippy sue v uoneJjedo junuuy Jeuuouqy xipueddy xepu 1ubi 4 1ubi 4 Abnormal Additional Annun Flight Instruments Nav Com XPDR Au
126. t 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 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 85 sainjea4 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi U0 AEN i jeuonippv uonejedo Jeuuouqv xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN GIA 63W MESSAGE ADVISORIES CONT NAV1 RMT XFR NAV1 remote The remote NAV1 and or NAV2 transfer switch transfer key is stuck is stuck in the enabled or pressed state NAV2 RMT XFR NAV2 remote Press the transfer switch again to cycle its transfer key is stuck operation If the problem persists the G1000 system should be serviced G S1 FAIL G 5T is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G 51 needs A failure has been detected in glideslope service Return unit for repair receiver 1 and or receiver 2 The receiver may G S2 SERVICE G S2 needs still be available The G1000 system should be service Return unit for repair serviced when possible G S2 FAIL G 52 is inoperative GEA 71 MESSAGE ADVISORIES GEA1 CONFIG
127. t is missing on the specified LRU PFD2 DB ERR PFD2 terrain database missing MFD1 DB ERR MFD1 obstacle database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 obstacle obstacle database Ensure that the data card is database error exists properly inserted Replace data card If problem PFD2 DB ERR PFD2 obstacle persists The G1000 system should be serviced database error exists MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle The obstacle database is present on another LRU database missing but is missing on the specified LRU PFD2 DB ERR PFD2 obstacle database missing 80 Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT 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 MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport The airport terrain database is present on terrain database missing another LRU but is missing on the specified LRU PFD2 DB ERR PFD2 airport terrain database missing MFD1 DB ERR MFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the PFD1 DB ERR PFD1 Safe Taxi Safe Taxi database Ensure that the data card is The MFD and or PFD
128. t 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 Turn the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 sjuauinajsu SV3 S24V oipny uadx UI0 AEN sue v uonejedo s9JnjeaJ e uepioAy SoJnpa20Jd Duiuue d ACN Sd5 junuuy jewuouqy Jeuonippy puezey xipueddy xepu 1ubi 4 1ubi 4 Flight Instruments Abnormal Additional Hazard Flight Planning Annun EAS Nav Com AFCS XPDR Audio GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 If two transponders are available press XPDR1 or XPDR2 to set the active transponder Otherwise proceed to step 3 3 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 4 Use the digit keys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is c
129. ta TBM 700 190 01247 00 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description IN HPA STD BARO ON nnn VF V V 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 pmmm n ETENE srev ow A7 awe ve amp cook oes ALT VFR FX V V3 V9 V3 V3 V3 YF to the top level softkeys Select the BACK Softkey to return Lo Woe ps ps Ws p e Il Jes j ekse guck vs Fy V V3 V9 V3 V3 V3 V3 V3 V3 V3 YF Select the BACK Softkey to return to the top level softkeys Transponder Softkeys Level 1 Level 2 Level3 ADF DME XPDR XPDRI XPDR2 STBY ON Description Displays the ADF DME Tuning Window Displays transponder mode selection softkeys Selects the 1 transponder as active Selects the 2 transponder as active Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 103 uonejedo sainjea4 aueploAy SoJnpa20Jd Puruuejd NEN Sd5 S 4Y oipny uadx SV3 sjuauingjsu Jeuonippy Wio gt AeN jewuouqy sue v unuuy gt gt D 5 e E xepu 1ubi 4 1ubi 4 puezey Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR
130. ta was lost System reverts lost Recheck settings to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings it desired XTALK ERROR A flight display The MFD and PFDs are not communicating crosstalk error has occurred with each other The G1000 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs The PFD and or MFD self test has detected a service Return unit for repair problem The G1000 system should be serviced MFD1 SERVICE MFD1 needs service Return unit for repair MANIFEST PFD1 software mismatch communication halted MANIFEST PFD2 software The PFD and or MFD has incorrect software mismatch communication halted installed The G1000 system should be serviced MANIFEST MFD1 software mismatch communication halted PFD1 CONFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Contig service req d MFD1 CONFIG MFD1 config The MFD configuration settings do not match error Contig service req d backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software The MFD and PFDs have different software version mismatch Xtalk is off versions installed The G1000 system should be serviced The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced 18 Garmin G
131. tains Verity user modified procedures procedures that have been manually edited This alert is issued only after an navigation database update Verity that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed This occurs when a stored flight plan contains Verify stored airways an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verity use of airways in stored flight plans and reload airways as needed 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 93 sainjea4 92uepioAy SoJnpo20Jd Puruuejd NEN Sd5 S JY oipny YddX SV3 sjueuinajsu piezeH yi U0 AEN i jeuonippv uoneJjedo Jeuuouqv xepu Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EAS Instruments Additional Abnormal Operation Index Appendix EJ A Annunciations amp Alerts GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT FPLTRUNC Flight plan has been This occurs when a newly installed navigation truncated 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 This occurs when the pilot attempts to activate locked flight plan a stored flight plan that contains locked
132. the DN position the essential bus is connected to the main bus SjueuinJjsu 1uDi 3 Essential Bus Connected to Essential Bus Connected to the Battery Bus the Main Bus oipny uddx JUI0 AEN SJV E55 BUS BAT BUS ESS BUS BAT BUS AEN Sd5 Essential Bus Connections Puruuejd oE A red X over a component indicates invalid data or a failed unit sue v uoneJjedo soJnjeaJ 92UepIOAY SoJnpa20Jd unuuy jewuouqy jeuonippy puezey xipueddy xepu 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 9 Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index A Engine amp Airframe Systems GARMIN FUEL SYSTEM 1 Select the SYSTEM Softkey to display the softkeys for the synoptics system 2 Select the FUEL Softkey to display the Fuel System Page 34 8 PSI aT AUTO A MAN FUEL FLOW 114 USG h FUEL USED 11 USG GH 6493 LBS FUEL REH 263 USG C1 Left Fuel Tank 6 Fuel Selector Left Fuel Line 7 Right Fuel Tank 3 Fuel Pressure Right Fuel Line 4 Engine Driven Boost Pump C Fuel Flow Data 5 Auxiliary Boost Pump e m D wi M Fuel Synoptics Page Status of the fuel selector is indicated between the fuel tank symbols The mode automatic AUTO or manual MAN is shown beneath the fuel selector symbol Garmin G1000 Cockpit Re
133. the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts Ihe FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function buiuue d AEN Sd5 S24V oipn uadx svi s u wn zsu yi JW0 AEN ui SoJnpo 20Jd aUEPIOAY puezey gt e Q zi E D View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page xipueddy sue v uonej
134. urn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of 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 Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Hazard Avoidance 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
135. utes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 01247 00 Rev A Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 43 AEN Sd5 S241V oipny dadx SV4 sjueuingjsu Wi0 AeN yybi4 Puruuejd 1461 4 a UePIOAY SoJnpa20Jd puezey sue v uonejedo S9JnjeaJ unuuy jeuuouqy Jeuonippy xipueddy xepu Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EAS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance GARMI N 44 5 Press the ENT Key 6 Turn the large FMS Knob to place the cursor in the STRMSCP MODE field 7 Turn the small FMS Knob to display the Cell Strike window 8 Turn either FMS Knob to select Cell or Strike Press the ENT Key 9 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each t
136. vice 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 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Select the TNA MUTE Softkey to mute the TIS Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN Traffic Advisory System TAS Optional System Self Test 1 2 3 4 Set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey Self test takes approximately eight seconds to complete When completed Hazard Avoidance 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 Tes
137. way entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A A GARMIN SSS fight Planning INVERT AN ACTIVE FLIGHT PLAN Sjueuinjijsu 64 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN oipny uadx Sv3 JUI0 AEN S 1V 1 Press t
138. waypoint Press the CRS Knob to synchronize the Selected Course with the bearing to the next waypoint Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 2 3 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS 1 2 3 Select the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin G1000 Cockpit Reference Guide for the Socata TBM 700 190 01247 00 Rev A GARMIN Flight Instruments 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 Toremove the window press the CLR Key or the TMR REF Softkey m gt n SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE oipny uadx U0 AEN 1 Pr
139. ystem File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan trun The flight plan on the SD card contains more waypoints than cated the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Way The flight plan on the SD card contains one or more waypoints points locked that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all The flight plan file on the SD card contains user waypoints loaded The quantity of stored user waypoints has exceeded system Capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successtully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to t

Garmin Software Version 0829.00 Cockpit Reference Guide

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