Home

Garmin Software Version 0321.23 Cockpit Reference Guide

Contents

1. Export a Hight Plan to an SD Card PROCEDURES LAL a cess tales R a aid 30 Load and Activate a Departure Procedure ls s sli 39 Activate A Departure Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure L 41 Activate An Approach in the Active Flight Plan 4 Activate a Vector to Final Approach Fix s s s s s 42 Activate A Missed Approach in the Active Flight 7 556 4 HAZARD AVOIDANCE cise R la 43 Customizing the Hazard Displays on the Navigation 43 STORMSCOPE Optional cccccccccsssssssscsssssssssssccsssssssssecesssssssssecesssssssssecesasssussnsess 43 XM WX Satellite Weather Optional 45 Worldwide Weather Optional 0 cccccccsssssssssssssssssssssssssssssscesssssssseesssssnseseessasn 48 Worldwide Weather Products Taffie Systems onneen nani Terrain And Obstacle Proximity s s s s s s s s s 63 Tertain SVS
2. 26 3 Displaying Wind Data 0 ccccccsusssssssssssssesssssssssssssssesssssnnsessssvsessssssnecssssvnessssnnessssnees 3 Changing HSI Format s s s s s s s s s ss s s ss s s ss s siss s sissess si 3 ENGINE INDICATION 5 9 5 DA40 Engine Display ccccccssusssssssessssssessssssessssssessssnsneessssvnessssnsnessssnsnesssssneesssnees 6 DA40F Engine Display v s s s s s s s ss s s ss s s ss s s ss s sisssss si 7 Engine Leaning R A A aden cde seed Ne 8 NAV COM TRANSPONDER AUDIO PAMEL 1 Enter or Change Flight 10 s s s s sss s sss s sss s 1 ADF Tuning 1 DME Tuning 1 Enter a Transponder Code cccsccccssssscssssscsssssscssssssscsssssssessssssessessscessnsscessnnseeeses 2 Selecting a COM Radio ccccccsusssssssscssssescsssssssscssssssessessseesssscessesscessesnssessnnnsseeses 2 Selecting a NAV Radio
3. paezey Level 1 Level 2 Level 3 Description PFD Displays second level softkeys for additional PFD configurations saunqee4 jeuonippy SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction uones do 1euuouqy su jy unuuy HRZN HDG Displays compass heading along the Zero Pitch line gt 5 APTSIGNS Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 121 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix Level 1 Level 2 Level 3 A GARMIN Description DFLTS WIND DME BRGI HSI FRMT BRG2 ALT UNIT STD BARO OPIN 1 OPTN 2 OPTN 3 OFF 360 HSI ARC HSI METERS IN HPA Resets PFD to default settings includ ing changing units to standard Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed
4. 2 NAV COM Tun ciconia 2 Digital Clearance Recorder and Player s s s si s sl n 3 Intercom System ICS Isolation l s 3 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM 5 Flight Director Activation s s s s s s s sss s sissss n 5 Vertical Modes snno naan nd Waal tae dad 6 7 9 Direct to Navigation 9 Activate a Stored Flight Plan 5 7 s s s s s s s s sin s s sssl 20 Activate a Flight Plan Leg s s s s s s 20 Stop Navigating a Flight Plan s s s s s s s sssss n 21 Vertical Navigation VNAV v s s s s s s ss s s s sis s s 21 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F Table of Contents GARMIN FLIGHT PLANNING a a aaa 25 Trip Planning Uca a ia itd adh ae Adana 25 Create a User Waypoint Defined by Latitude amp Longitude 27 Create a User W
5. Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver must have a valid VOR or LOC signal or active GPS course before NAVor APR Key press activates flight director 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 15 sia siu uin sul nubi olpny uqax uo2 AEN ARN 540 52 SH V uones do sainjea4 aoueplony s mp ooud buluueld Tunuuy qeuuouqy yeuonippy 2 n xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch Pitch Hold attitude may be used to climb default PIT descend to the Selected Altitude AFCS armed to capture the altitude 7702 displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds the current Altitude Key ALT Reference Maintains the current aircraft Vertical Speed vertical speed may be used to climb VS Key VS nnnn Fem descend to the Selected Altitude Maintains the current aircraft Flight Level Change airspeed in IAS while the aircraft is FLC Key FLC nner climbing descending to the Selected Altitude
6. 5 s s s s s s s ss s s ss s s ss s s l Hazard Displays with Loss of GPS Position Unusual Attitudes nerenin Dead Reckoning 3 5 03s se ic ANNUNCIATIONS amp ALERTS WARNING Annunciation CAUTION 6 Alert Message AFCS Alerts Terrain SVS Alerts Terrain SVS System Status Annunciations TAWS Alerts 25 5 N TAWS System Status Annunciations Voice Alerts enren MFD amp PFD Message Advisories Database Message Advisories GMA 1347 Message AdVISONIGS cccsssssssssssssssessssssseesssssseesssssseessssnatessssnseeen GIA 63 Message Advisories GIA 63 Message Advisories GEA 71 Message Advisories s s s s s s s s s s s s sss s sis 0 GTX 33 Message Advisories 1 GRS 77 Message Advisories 1 GSR 56 Message Advisories 12 GMU 44 Message Advisories s s s s s s s s s s sss s sis 2 GDC 74A Message 50115 2 GDL 69A Message Advisories 3 Miscellaneous Mess
7. Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old KJ Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Tur either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Tur the small FMS Knob to highlight Weather 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 43 s uawin jsu sub APN 549 S24Y olpnyyuqax uo2 AEN buluueld nubi aoueploay s mp oold paezey SH lV uones do sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 44 5 6 7 8 9 A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return t
8. Turn the large FMS Knob to highlight the desired flight plan d Press the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 35 olpny uaqax 59 syuawny su wio gt AeN 16114 52 2 4 ACN 540 nubi aoueplony paezey spay sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 4 5 A GARMIN With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key 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 desired flight plan Press the INVERT Softkey Invert and activate stored flight plan is displayed With OK highlighted press the ENT Key The selected flight plan is now inve
9. 2 Tum the small FMS Knob to select the AUX SYSTEM STATUS Note the System ID number in the AIRFRAME field 3 Turn the large FMS Knob to select the MAP Page group 4 Turn the small FMS Knob to select the MAP WEATHER DATA LINK Page 5 Press the MENU Key If necessary select Display GFDS Weather 6 Press ENT Key The GARMIN FLIGHT DATA SERVICE REGISTRATION Window is now displayed 7 Press the MENU Key The Page Menu window is now displayed 8 Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field 9 Press the ENT Key REGISTER will now be highlighted 10 Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field 48 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C Hazard Avoidance A GARMIN Accessing GFDS Worldwide Weather Products 1 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Use the MENU Key to select GFDS Weather if required When a weather product is selected for display on the GFDS Weather Data Link Page a box containing a symbol for the product and its age in minutes are shown in the upper right If weather data has not been requested N A is shown next to the product symbol instead of age The age of the weather product is based on the time difference between when the data was assembled on th
10. AMPS Vv l 88 VOLTS b 4 FUEL QTY GAL PRN 5 DA40 Engine Indication System A RPM 2330 FUEL FLOW GPH OIL Vv OIL PRES Vv Vv 6 80 FUEL QTY GAL 2 l DA40F Engine Instrument Display on the MFD Garmin G1000 Cockpit Reference Guide for the DA40 40F siu uinnsul 52 FO 524 sH ly uonesdo saunyea4 aoueplony saunpa20Jd Fuluueld ARN Sd5 2 euuouqy Jeuonippy paezey yunuuy xipuaddy x pul nb n Flight Instruments Nav Com XPDR Audio A Engine IndicationSysiem GARMIN DA40 ENGINE DISPLAY Pressing the ENGINE Softkey displays the EIS ENGINE Page Fuel used GALLONS USED endurance and range RANGE NM are all calculat ed based on the last manual adjustment of the fuel remaining GALLONS REMAIN Measured fuel quantity has no effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining The following softkeys allow for adjustment of the remaining fuel quantity Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index GALLONS USED 7 liz r 1 154 3 ENOURANCE x iH cae A F j RANGE NM culations so 2 7 Ta E TOTAL TIME IN SERVICE Aircraft L FLL zin b DEC FUEL Allows the pilot to decreas
11. VNAV Captures and tracks the VNAV flight GDU 1044 only path TUM VNAV Target Altitude 1 AFCS armed to capture the altitude Armed GDU 1044 displayed in the VNAV Target ss ALTV only Altitude window Glidepath SBAS only Cap ures and tracks the SBAS GP glidepath on approach APR Ke Captures and tracks the ILS y Glideslope i GS glideslope on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA i Switch and wings level in the air Autopilot engages and commands only by Level pitch angle necessary to establish zero LVL the ESP vertical fpm functi unction ALTS armed automatically when PIT VS FLC or GA active and under VPTH when Selected Altitude is to be captured instead of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll Roll Hold attitude or rolls the wings default ROL level depending on the commanded bank angle Captures and tracks the HDG PERANG RE Selected Heading Key Navigation GPS GPS Navigation VOR Enroute Captures and tracks the VOR Mode selected navigation source Navigation LOC Glideslope GPS VOR LOC NAV LO
12. Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Hazard avoidance GFDS Weather Data Requests The GFDS Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals if desired and the ability to send or cancel weather data requests The window also displays the status of the GFDS data request process Requesting GFDS Weather Data Manually 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With GFDS Weather Request highlighted press the ENT Key 4 Turn the large FMS Knob to highlight the desired coverage option s and press the ENT Key to check or uncheck one of more of the following coverage selections PRESENT POSITION Requests data based on current location DESTINATION Requests data based on active flight plan destination if the flight plan contains no destination dashes are displayed FPL Requests data based on active flight plan Turn the small FMS Knob to select the desired flight plan look ahead distance option or choose REMAINING FPL to request the remainder of the flight plan e WAYPOINT Requests data based on any valid waypoint 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field and turn the small
13. 2 select the PRECIP Softkey Radar data shown represents lowest level base reflectivity of radar returns The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the GFDS Weather Data Link Page For the Precipitation legend select the LEGEND Softkey when Precipitation is selected for display 56 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Hazard avoidance Precipitation Limitations Radar images may have certain limitations Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics wet hail vs rain For example it is not possible to distinguish between wet snow wet hail and rain e Radar base reflectivity is sampled at the minimum antenna elevation angle An individual radar site cannot depict high altitude storms at close ranges It has no information about storms directly over the site When zoomed in to a range of 30 nm each square block on the display represents an area of four square kilometers The following may cause abnormalities in displayed radar images Ground clutter Strobes and spurious radar data Sun strobes when the radar antenna points directly at the sun Interference from buildings or mountains which may cause shadows e Metallic dust from military aircraft which can cause alterations in radar scans Infrared
14. 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 highlighted 11 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F s tin su sub olpny 4uqax 93 Ju09 neN 52 APN 540 buluueld wold s mp old aoueplony paezey SH V uones do sainjea4 unuuy yeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio ee Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2
15. Wind direction arrow with direction and speed Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency 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 Win dow through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa 122 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN 0 Appendix optional umumummm rv uu 74 s tin sul sub TC ee Ee Tas Ev To ee 5 75 7 77 N NNN HANA 59 Press the BACK Softkey to return to the top level softkeys 444 Wi0 gt AeN oR ee ee NNN NNN mu uu Press the BACK Softkey to return to the previous level softkeys 52 Transponder Softkeys 2 Level 1 Level2 Level 3 Description XPDR Displays transponder mode selection softkeys 22 STBY Selects Standby Mode transponder does not reply to any interrogations 7 ON Selects Mode A tr
16. 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 31 olpny uqax s q s tin sui Vuo2 AEN 4613 52 2 4 540 nubi aoueplony paezey SH V uones do sainjea4 unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Ab
17. 2 HM 12 ede Indicates File 2 Difference qz inl r 410 410 Between Present 494 75 0 356 382 and Peak FUEL CALCULATOR Temperature of GALLONS REMAIN 40 6 the First Peaked GALLONS USED 34 2 7 5 4 ENDURANCE z l Cylinder g A 2 A RANGE NM 227 Wir o b TOTAL TIHE IN SERVICE L FUEL GAL mr SE 0 0 HRS Procedures Hazard Avoidance DEC FUEL INC FUEL RST FUEL Leaning to First Peak DA40 shown Annun Abnormal Additional Alerts Operation Features Appendix Index 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN ___Engine indication system Continuing to lean the mixture will cause each cylinder to peak until the last of the cylinders peaks This is indicated by Last being displayed below the last peaking cylinder as shown in the second figure z 5 s 123 808 Cylinder Peak ELECTRICAL lemperature 52 HAN IN HG 5 82 24 3 Bi Last Cylinder 1 to Peak y OIL Az a M toe 3 Indicates a Difference 1 b ms Between Present 3 194 75 0 16 8 25 04 and Peak 8 s FUEL CALCULATOR Tem erature of REMAIN 402 he Last Peaked j ENDURANCE 2 23 Cylinder m RANGE NM 239 K w 1 buluueld nubi ERVICE 40 L FUEL R FUEL TY GAL GAL DEC FUEL INC FUEL RST FUEL s snp old Leaning to Last Peak DA40
18. Reducing power usage PFD1 has poo MFD1 has poor cooling Reducing power usage The cooling fan for the PFD is inoperative The cooling fan for the MFD is inoperative Single Aural Tone 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 93 s n e 4 2 buluueld ACN 540 52 olrpny uqax 593 siu umnnsul 2 Wil uio AeN qb euonippv uoned do euuouqy 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix n Annunciations amp Alerts A GARMIN ALERT MESSAGE Alerts Window Message Audio Alert ESP DEGRADE ESP IAS mode is inoperative ESP FAIL ESP is inoperative None ESP OFF ESP selected off ESP CONFIG ESP config error Config service req d GFC 700 equipped aircraft with ESP 94 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN AFCS ALERTS Pitch Failure Roll Failure MET Switch Stuck or Pitch Trim Axis Control Failure Elevator Mistrim Up System Failure AFCS AP ite MET are unavailable FD may still be available Elevator Mistrim Down Aileron Mistrim Left Annunciations amp Alerts Description PTCH PTRM Pitch axis control failure AP is ino
19. transfer switch is stuck in the enabled or pressed position Press the trans fer switch again to cycle its operation If the problem persists the G1000 system should be serviced RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM from the FAF to the MAP waypoints 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 105 saunqea4 sanpa20Jg Bujuuejd ACN SdD 2 olpny uqax sia s u un su paezey nubi wi0 gt AeN Wil leuonippv uones do 1euuouqy 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ea Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments LOI GPS integrity lost Crosscheck with other NAVS GPS NAV LOST Loss of GPS naviga tion Insufficient satellites Loss of GPS integrity monitoring f Loss of GPS navigation due to insufficient satel lites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach
20. uones do pulouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 14 A GARMIN 0000080 A AFcs GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Switch Roll Hold default ROL Pitch Hold default PIT GA Switch Go Around GA Go Around GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS a VOR NAV Key Navigation LOC Pitch Hold default PIT BC GPS Pitch Hold default PIT APR Key Approadh VAPP Glidepath GP LOC Glideslope GS HDG Key Heading Select HDG 1 Pitch Hold default PIT
21. 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 87 s mp o4d Puluueld AeN Sd 52 olpny uqax sia s u u nnsul Wfl Tu102 AEN sub aoueplony paezey xipuaddy SH V uones do sainjea4 unuuy jeunouqy Jeuonippy x pul Nav Com XPDR Audio Hazard Additional Features Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Procedures Avoidance Appendix Alerts Operation Index A Additional Features GARMIN Display Selection Pressing the HIDE MAP Softkey removes the map and displays video on the full screen The softkey label changes to grey with black characters Pressing the HIDE MAP Softkey again restores the map view and the small video image The softkey label returns to white characters on a black background Zoom Range Pressing the VID ZM or VID ZM Softkeys increases or decreases video display magnification between 1x and 10x The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and out on the video display While in the Split Screen mode pressing the MAP ACTV or VID ACTV Softkey determines which display the RANGE Knob adjusts Pressing the softkey to display MAP ACTV allows the RANGE Knob to control the range setting of the map display Pressing the softkey to display VID ACTV allows the RANGE Knob to control the zoom setting of the video display NOTE Images provi
22. 2 AOPA airport information is displayed on the right half of the display 70 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Md itimal Features SIRIUSXM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select the displayed AUX XM Information Page 3 Press the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Press the CATGRY Softkey on the XM Radio Page 2 Press the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page press the CHNL Softkey 2 Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or
23. 3066000000 017 6 0 63 Terrain Awareness amp Warning System TAWS Display Optional 65 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN table of contents ADDITIONAL 5 67 Synthetic Vision 67 Terminal Procedure Charts 68 AOPA Airport Directory ssssssssssssssessssssessssssessssnsessssssessssnnsessssenessssseess 70 SiriusXM Radio Entertainment nnrir 71 Satellite Telephone amp SMS Messaging Service Optional 72 Electronic Checklists Optional 84 Electronic Stability and Protection ESP Optional 85 Auxiliary Video Optional s s A s s s l S s s s 87 ABNORMAL OPERATION A s Reversionary Mode cccccccssssssssssscsssssssesssssseesssssseesssssceesssssseesssnsceesnsnseeesnssscsesnsnensen Abnormal COM Operation
24. Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Standby Navigation database mismatch Comments The PFD and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFD and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch The PFD and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Airport Terrain database mismatch The PFD and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determin
25. Displaying auxiliary video 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select VIDEO and display the AUX VIDEO Page The video display softkeys shown below appear on the AUX VIDEO Page Control of the AUX VIDEO Page can also be accessed through the Page Menu Selecting video menu options 1 While viewing the AUX VIDEO Page press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key Once the ENT key is pressed on any option the page menu closes and returns to the AUX VIDEO Page Video Setup Video brightness contrast and saturation may be adjusted be selecting the setup function While viewing the setup function softkeys after 45 seconds of softkey inactivity the system reverts to the AUX VIDEO Page softkeys Adjusting the video settings 1 With the AUX VIDEO Page displayed press the SETUP Softkey 2 Press the BRIGHT or BRIGHT to adjust display brightness in five percent increments from 0 to 100 3 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 100 4 Press the SAT or SAT to adjust display saturation in five percent increments from 0 to 100 5 If desired return the display to the default settings by pressing the RESET Softkey 6 Press the BACK Softkey to return to the previous softkey level
26. Enable New Message Popups 3 Press the ENT Key The pop up alert will not be displayed when an incoming text message is received Reply to a Text Message While viewing the text message press the REPLY Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Reply To Message c Press the ENT Key Sending a Text Message 1 2 3 4 5 6 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Message c Press the ENT Key The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Enter the desired message using any combination of entry methods as described in step 2 Press the ENT Key Press the SEND Softkey to send the message immediately or press the SAVE Softkey to save the message in Outbox for sending at a later time Press the CANCEL Softkey
27. FMS Knob to select the desired diameter and route width of the request then press the ENT Key 6 Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the GFDS Data Link Page without requesting data During a GFDS Data Request the Request Status box initially displays Contacting GFDS Once a connection is established the Request Status Box displays Receiv ing Wx Data Time Remaining with an estimated data transfer time either minutes or seconds If desired the GFDS Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background GFDS Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area and Iridium signal strength 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 53 AEN 540 52 orpny uqax 93 Slu umnnsui Tuo2 AEN sb buluueld Wil uep ony s Mp 01d paezey suey uoljesadQ sainjea4 unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN The system retrieves all available Worldwide Weather produ
28. Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 65 ACN 540 52 olpny uqax 99 syuauuni su u102 AEN fila buluueld Wil uep ony s mp oold paezey SH V uones do sainjea4 Tunuuy qeuuouqy leuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below ai
29. Satellite Infrared Satellite IR SAT data depicts cloud top temperatures from satellite imagery Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes Displaying Cloud Tops information 1 Select the GFDS Weather Data Link Page 2 select the IR SAT Softkey To display the Infrared Satellite legend select the LEGEND Softkey when Infrared Satellite data is selected for display Data Link Lightning Lightning data shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has occurred within a two kilometer region Neither cloud to cloud nor the exact location of the lightning strike is displayed If the aircraft is also equipped with the L 3 WX 500 Stormscope only one lightning product may be enabled for display at a time 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 57 AEN 549 52 olpny uqax sia sjuawinaysu u102 AEN buluueld Wil s mp oold paezey su jy uonesado s n e 4 unuuy jewuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 58 A GARMIN Displaying Data Link Lightning information 1 2 Select the MAP Softkey for the PFD Inset Map select the INSET Softke
30. aoueplony paezey s m e q described in step 5 8 Press the ENT Key 9 Press the SAVE Softkey The new predefined message is now shown in the displayed list Pressing the CANCEL Softkey will delete the message without saving 10 11 Message Press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Stop Editing Predefined 12 Press the ENT Key 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 79 xipuaddy SH V uones do junuuy Jewuougy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 80 A GARMIN Send a Predefined Text Message 1 2 3 4 5 6 7 While viewing the AUX TEXT MESSAGING Page press the NEW Softkey The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey Press the ENT Key The cursor i
31. as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances including negligence shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has 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 November 2012 190 00324 11 Rev C Printed in the U S A amp GARMIN _ suing Cautions amp Notes 6 WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify
32. components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Recor of Revisions Part Number Change Summary 190 00324 00 Initial Release 190 00324 01 Reformat of manual Added NAV COM volume levels Added Flight Timer Added extended range fuel tanks Changed NAV1 and NAV2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposite sides 190 00324 02 A
33. highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 39 olpny uqax s q siu uin sul u02 AEN fija 52 AeN 540 buluueld nubi s mp old aoueplony paezey spay sainjea4 Tunuuy qeuuouqy yeuonippy xipuaddy x pul Nav Com XPDR Audio Procedures Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Procedures 00000 GARMIN 4 5 6 7 8 9 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the l
34. no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F s uawin jsu UATE 53 olpny 4uqax mio AeN ACN 540 52 SH lV uoesado s n e 4 aoueplony 2 buluue
35. preset channels 3 Press any one of the PS1 PS15 softkeys to assign a number to the active channel 4 Press the SET Softkey on the desired channel number to save the channel as a preset Adjusting Volume 1 On the XM Radio Page press the RADIO Softkey 2 Press the VOL Softkey to access the volume control softkeys 3 Press VOL or VOL softkeys to adjust the volume level 4 Press the MUTE Softkey to mute the radio audio SATELLITE TELEPHONE amp SMS MESSAGING SERVICE OPTIONAL Operation of these features in the cockpit is accomplished through the AUX TELEPHONE and the AUX TEXT MESSAGING SETUP Pages Registering With Garmin Flight Data Services A subscriber account must be established prior to using the Iridium Satellite System Before setting up an Iridium account obtain the serial number of the Iridium Transceiver GSR1 and the SYSTEM ID by viewing the AUX SYSTEM STATUS Page Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 72 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Disable Enable Iridium Transceiver Iridium telephone may be turned on or off by performing the following steps Additional Features To enable the Iridium telephone system 1 With the AUX TELEPHONE Page displayed select the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Enable Iridium Tran
36. signal is received TAWS TEST System Test pass TANS System Test OK 98 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Annunciations amp Alerts VOICE ALERTS Voice Alert Description Minimums minimums The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued TAS system Traffic Advisory System Played when the TAS system passes a pilot initiated self test Test Passed Traffic Advisory System Played when the TAS system fails a pilot initiated self test Test Failed Engaging Autopilot The ESP system is engaging the autopilot See the Additional Features section for more details Airspeed Issued when the autopilot is engaged and the airspeed trend vector drops below 65 knots MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFD
37. 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Flight Planning CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 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 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Tum the small FMS Knob to select LAT LON latitude and longitude 9 Pres
38. to return to the top level softkeys 2 buluueld APN 540 qwbl4 aoueplony paezey CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press 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 3 Press the CDI Softkey a third time to return to GPS SH lV uones do sainjea4 Tunuuy qeuuouqy yeuonippy xipuaddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 Tum a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Tum the small FMS Knob to display the UP DOWN window Turn the FMS Knob to sele
39. typically country code area code phone number by selecting the number softkeys on the MFD or turning the FMS Knobs The GSR 56 may be configured by an authorized repair facility to automatically enter a default county code when the dialing window is displayed To replace the default country code move the cursor to the first furthest left number in the dialing window and enter the desired country code 4 Press the ENT Key OK is highlighted 5 Press the ENT Key The system will begin calling the number When the phone is answered the connection is established To exit the call select the HANGUP Softkey Text Messaging SMS 76 Messages may be sent to an email address or text message capable cellular telephone Message length is limited to 160 characters including the email address The text messaging user interface is mainly through the AUX TEXT MESSAGING Page Viewing the Text Messaging Page 1 2 3 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select SATELLITE PHONE If necessary press the SMS Softkey to display the AUX TEXT MESSAGING Page Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Additional Features Message Symbol Description Received text message that has not been opened Received text message that has been opened Saved text message draft not sent System is sending text message Tex
40. uonesado Jeuuougy su jy unuuy 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 alert will remain until the next power cycle h 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 129 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts A Appendix 0808080880 GARMIN 12 Turn system power OFF 13 Remove the SD card from the top card slot of the MFD 14 Turn system power ON 15 Press the ENT Key to acknowledge the startup screen 16 Turn the large FMS Knob to select the AUX Page group on the MFD 17 Turn the small FMS Knob to select the System Status Page 18 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by the AHRS GRS If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure GRS MV DB Update Available Update from 2005 to 20
41. 10 OK GRS Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS Mag Var Database STARTING UPLOAD 0 0 Uploading Database to GRS When the upload is complete the system is ready for use 130 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN A Access code 48 Activate a flight plan 20 Active Channel 71 Active database 128 Active Navigation Database 128 ADF 11 12 90 122 AHRS 111 112 Airport Signs 67 68 Airways 125 ALT 62 Altitude mode 62 Altitude volume 62 AOPAs Airport Directory 70 AP 95 Audio panel controls NAV1 NAV2 12 Autopilot 95 Auxiliary video 87 Barometric Altitude Minimums 3 Barometric pressure 122 C CDI 1 12 115 Cell 43 44 Cell mode 44 Channel Presets 72 ChartView 68 69 Checklists 84 85 CLD TOP Softkey 57 Clearance player 13 Clearance Recorder 13 Code selection softkeys 12 COM 12 13 89 Index D DB Mismatch 126 129 DCLTR Softkey 68 Dead Reckoning 90 Declutter 90 119 126 Direct to 19 DME 11 12 DR mode 90 91 92 E Edit a flight plan 35 Electronic checklists 84 85 Emergency checklist 85 Enable Terrain 64 65 Endurance 6 7 ESP 85 F FD 95 Flight Director 15 Flight 11 Flight path marker 6
42. 13 s uaunysu puezey ubiu wio gt AeN ubiu euonippv uones do 1euuouqy m x pul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Features Annunciations amp Alerts A GARMIN PFD MFD MED Alert Type 1 TAWS B Page Aural Message 7 Pop Up Alert Annunciation Reduced Required TERRAIN OBSTACLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC OO osrin o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead OBSTACLE Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN TOO LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SKRE Sink Rate Rate Caution EDR Negative Cimb ETERRAINI varsa Don t sink Rate Caution NCR or or nu TAWS SYSTEM STATUS ANNUNCIATIONS Abnormal Operation Index Appendix PFD MFD TAWS B Page TAWS System Test Fail 5 FAIL TAWS Alerting is disabled TAWS INH No GPS position or excessively TAWS N A degraded GPS signal System Test in progress Aural Message TANS System Failure TAWS Not Available TANS Available will be heard when sufficient GPS
43. 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Press the available softkeys to select the desired XM weather product 4 Press 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 45 ACN 540 52 olpny uqax 99 syuauuni su wio gt AeN buluueld nubi aoueploay s mp oold paezey spay uolesadoQ sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Map Panning Information Weather Data Link Page 1 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressin
44. 6 Use the FMS Knob or the ENT Key to scroll through the PIREP text 7 Press the FMS Knob or the CLR Key to close the PIREP text window and return to the GFDS Weather Data Link Page To display the PIREP or AIREP legend select the LEGEND Softkey when PIREPs or AIREPs are selected for display The PIREP color is determined by the type routine or urgent 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 59 sub olpny qqax 59 wi0 gt AeN 52 APN 540 buluueld Wil aoueploay s mp oold paezey SH V uones do sainjea4 unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index A Hazard Avoidanes GARMIN Winds Aloft Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3 000 foot increments up to 42 000 feet MSL Displaying Winds Aloft data 1 2 3 4 Select the GFDS Weather Data Link Page Select the MORE WX Softkey Select the WIND Softkey Select the desired altitude level SFC surface up to 42 000 feet Select the NEXT or PREV Softkey to cycle through the altitude softkeys The WIND Softkey label changes to reflect the altitude selected To display the Winds Aloft legend select the LEGE
45. 7 Flight plan import export messages 117 FliteCharts 68 69 Frequency Transfer 12 Fuel remaining 6 7 Fuel used 6 7 H Horizon heading 67 Inhibit 64 66 Inhibit TAWS 66 Inhibit Terrain 64 Inset Map 119 120 IOI 96 97 98 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F ndex 1 sainjea4 aoueplony 2 buluueld ACN 540 S24Y olpny uqax sia s tin sul leuonippv 2 Wil Tuo2 NeN wb uonesado Jewuougqy su jy unuuy 1221 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Eee Appendix Index Iridium 72 73 Iridium satellite network 73 J Jeppesen 69 L Lightning 43 44 120 Loading Updated Databases 126 M Magnetic Field Variation Database Update 130 Map panning 46 Message advisories 99 117 MET 95 METAR 45 Minimums 99 Mistrim 95 Mixture 8 9 MKR MUTE 13 Mode 5 123 Mode selection softkeys 12 Multi Function Display MFD Softkeys 124 N NAV 12 NAV1 1 12 NAV2 1 12 Navigation database 21 22 NEXRAD 45 120 125 NEXRAD Softkey 56 0 OBS 2 Obstacles 103 108 Overspeed Protection 16 Index 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F A GARMIN P Pathvvays 67 68 PIREP 59 Power up page 84 Predefined message 79 Profile Vievv 125 R Register 48 Reversionary mode 89 ROC 96 9
46. 7 98 5 68 SBAS 16 41 65 66 91 108 109 Secure Digital SD card 84 SMS 72 Standby Navigation Database 129 Store Flight Plan 35 Stormscope lightning data 43 44 120 Strike 43 Strike mode 44 SVS 67 116 Synchronization 127 SYNC Status 129 Synthetic Vision System 67 System ID 48 T TA 99 TAF 45 58 TAS 62 99 111 TAVVS 65 66 96 97 98 TAWS B 65 Telephone 72 73 75 76 78 80 Terrain 63 65 103 120 125 Terrain SVS 63 64 65 Text message 76 77 79 80 190 00324 11 Rev C A GARMIN TFR 46 60 Timer 113 Topographical data 120 125 Traffic 43 61 125 Traffic Advisory 61 99 Traffic map page 61 62 63 Transponder 11 12 123 124 V vertical path guidance 23 Vertical speed guidance 22 Vertical track 99 Video 87 VNV 19 90 115 Vspeed 2 W Waypoint Selection Submenu 31 32 Weather data link page 45 Wind data 122 Winds Aloft 60 WIND Softkey 60 X XM lightning 120 125 XM weather 45 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F Index Index 3 sainjea4 aoueplony 2 buluueld ACN 540 S24Y olpny uqax sia s tin sul leuonippv p EzeH wold Tuo2 NeN wb uonesado Jewuougqy su jy unuuy GARMIN Index S u u nnsul fila 593 WO gt AeN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 Jeuolippy uone
47. Abort approach due to loss of GPS navigation TRUE APR True north approach Change hdg reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to MAGNETIC GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 SERVICE NAV2 needs service NAV2 RMT XFR NAV2 remote transfer key is stuck A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or rec
48. Alerts Operation Features Index Hazard Avoidance 0 GARMIN Enabling Automatic GFDS Data Requests 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With GFDS Weather Request highlighted press the ENT Key 4 Choose the desired weather coverage options 5 Turn the large FMS Knob to select the UPDATE RATE setting Then turn the small FMS Knob to highlight the desired automatic update frequency OFF 5 Min 10 Min 15 Min 20 Min 25 Min 30 Min 45 Min or 60 Min then press the ENT Key 6 The SEND REQ button is highlighted and a countdown timer is displayed in the REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate GFDS Data Request Or Press the FMS Knob to return to the GFDS Weather Data Link Page WORLDWIDE WEATHER PRODUCTS Precipitation Precipitation data is not real time The lapsed time between collection processing and dissemination of radar images can be significant and may not reflect the current radar synopsis Due to the inherent delays and the relative age of the data it should be used for long range planning purposes only NOTE Precipitation data cannot be displayed on the Navigation Map Page at the same time as terrain Displaying Precipitation Weather Information 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the GFDS Weather Data Link Page
49. C will not arm or capture Key Captures and tracks a Navigation Backcourse localizer signal for backcourse BC approaches Approach GPS Glidepath mode automatically armed if GPS vertical guidance is available 7 and tracks the APR selected navigation source Approach VOR GPS VOR LOC Key VAPP Approach LOC Glideslope Loc Mode automatically armed Disengages the autopilot and GA Go Around commands a constant pitch GA Switch angle and wings level Activated Autopilot engages and only by commands wings level the ESP a function 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 913 siu umnnsu olpnv qqax Wi0 gt AeN ARN SdD So4V SH lV uones do sainjea4 aoueplony 2 buluueld junuuy Jewuouqy Jeuonippy xipuaddy x pul qwbil4 nu paezey GARMIN AFCS s USWUNJ sU fila 593 Tu102 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey saunjea4 Jeuolippy uones do pulouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 18 A GARMIN GPS Navigation GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to E Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If
50. DA40 40F 23 olpny uqax s q siu uin sul 52 b sH ly uonesdo saunyea4 aoueplony saunpa20Jd unuuy euuouqy Jeuonippy paezey xipuaddy x pul nb mio AeN m m GARMIN GPS Navigation s USWUNJ sU fila 59 Tu102 AEN s24v Sd5 buluueld Blank Page soinpsd01d aoueplony puezey saunjea4 euonippv uones do pulouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 24 GARMI N 88 HilghtPlanning FLIGHT PLANNING TRIP PLANNING 1 Tum the large FMS Knob to select the AUX page group 2 Tum the small FMS Knob to select the first rectangular page icon 3 The current PAGE MODE is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey 4 For Direct to planning a Press the WPTS Softkey and verify 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
51. Directory database error exists PFD1 DB ERR PFD1 Airport Directory database error exists The MFD and or PFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced TERRAIN DSP PFD1 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFD and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on Garmin G1000
52. ERENCE 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 2 ACN 540 nubi 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 29 Sia siu uinnsu wio gt AeN olpny uqax 52 aoueplony paezey spay sainjea4 unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N Or a b o d Or a b o d Or a b o d Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the des
53. ETAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right CYCLONE WARNING The age of the displayed data is shown at the right L Vi AIREP The age of the displayed data is shown at the right m Sm PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow izi TURBULENCE The age of the displayed data is shown at the right The raluu la Bill altitude selection is shown at the bottom gil ICING POTENTIAL The age of the displayed data is shown at the right 6000FT The altitude selection is shown at the bottom No Status Icon TFR Depicted as an area outlined in yellow 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 47 EN 540 s24v olpny uqax sia siu umnsul Tuo2 AEN sub buluueld ni aoueplony s mp oold paezey sualy uonesado saunq
54. FW RNAY 17LePs RIVET inf 259 18 84 4 0 4 Sma Lig DRAAK 176 33mm 2000rr Blue Text INWOD 1767 2324 Sma Lig MENOL faf 176 3 9MM RW17L 5 3NM z g Small White Text 99 FT 1 8NM with Altitude POLKE Restriction Bar S L M Cross AT or ABOVE 5 000 fi PAGO Cross AT 2 300 ft cinsli Cross AT or BELOW 3 000 ft 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 21 sia siu uinnsu 3 olpny uqax uo2 AEN SH lV uones do sainjea4 2 buluueld Tunuuy qeuuouqy yeuonippy paezey n xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS AFCS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desire
55. G1000 Integrated Flight Deck Cockpit Reference Guide DA40 Diamond Star Diamond DA40 FP Diamond Star A GARMIN Copyright 2004 2009 2011 2012 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0321 23 or later for the Diamond DA40 inform Garmi and DA4OF Some differences in operation may be observed when comparing the tion in this manual to earlier or later software versions fed 5 International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmi nAT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmi South n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park ampton 5040 9 U K Tel 44 0870 8501241 Fax 4410870 8501251 Garm n Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 or af m ter 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 witho down othe or
56. IN SSS ppeerndix APPENDIX s tin sul sub PFD SOFTKEY MAP 59 optional GS 7 Gore Gee eT RY ST RTS 77 um m 7 mmu mu olpny uqax uo2 AEN CD NAV2 gt A vn Top Level PFD Softkeys a optional FE 7 HE HU HFH WwW P 39 optional optional a s optional optional a PL rme optional OFF fxteno FRAFFIC TOPO_ TERRAIN Bravo NEXRAD Par cTNG WETAR 2 DS ES NHuNHE Hu oO Press the BACK Softkey to return to the top level softkeys gt oa 5 a D gt Inset Map Softkeys zE 52 os CAE Level 1 Level2 Level 3 Description uonesado Jeuuougy INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan su jy unuuy gt 5 m x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 119 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix Level 1 Level 2 Level 3 Description WX LGND Displ
57. IN View Messages Sorted by Message Type While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TYPE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Type c Press the ENT Key The sorting selection is indicated at the bottom center of the list window View Messages Sorted by Address While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the ADDRESS Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Address c Press the ENT Key The sorting selection is indicated at the bottom center of the list window Viewing The Content of a Text Message 1 2 3 4 5 While viewing the AUX TEXT MESSAGING Page select the desired message box Press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Press the VIEW Softkey Or Press the ENT Key Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on View Selected Message c Press the ENT Key To close the text message press the CLOSE Softkey Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Close Message c Press the ENT Key Mark Se
58. 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 INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 34 1 2 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on 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 Press the EDIT Softkey Turn the
59. ND Softkey when Winds Aloft is selected for display Displaying TFR Data 1 Select the Weather Data Link GFDS Page or Navigation Map Page 2 Press the RANGE Knob and pan the map pointer over a TFR to highlight it The system displays TFR summary information above the map 3 Press the ENT Key The system displays a pop up menu 4 If necessary tum the FMS Knob to select Review Airspaces and press the ENT Key The system displays the TFR Information window Figure 6 91 5 Press the FMS Knob or the CLR Key to remove the TFR Information window TRAFFIC SYSTEMS 60 WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured MUTE and ALT MODE softkeys are displayed Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Hazard Avoidance Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation O Traffic Advisory TA dosing rate distance and ver
60. Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 71 2 Puluueld AeN SdD S4V olpny uqax sia siu u nnsul Tu102 AEN 346 aoueplony paezey xipuaddy SH V uones do sainjea4 unuuy jeunouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features oo GARMIN Entering a Channel Directly 1 While on the XM Radio Page press the CHNL Softkey 2 Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted 3 Press the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active press the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the
61. RS 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 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F A Wamings Santions Netes_ 0 GARMINM 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
62. RU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 101 sainjeay aoueplony 2 buluueld AN 540 S04V olpny uqax 913 s u wnysu puezey 346 wio gt AeN 3461 euonippv uones do 1euuouqy 7 Ea x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations 8 Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists Comments The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 Airport
63. S 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 52 AN 540 wold s snp oold DISPLAYING WIND DATA 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data to the left of the HSI 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey aoueplony paezey saunqea4 jeuonippy CHANGING HSI FORMAT uonesado Jewuougqy 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 xipuaddy SH lV junuuy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 3 GARMIN Flight Instruments E A olpny uddX Tu102 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 Jeuolippy uones do pulouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F A GARMIN ENGINE INDICATION SYSTEM Fuel Pressure is only available on EASA certified aircraft Fuel Quantit Indicator scale is 0 25 with extended range fuel tanks 0 20 with standard tanks 190 00324 11 Rev C RPM x 2300 FUEL FLOW GPH v FUEL PRES v OIL TEMP OIL PRES V
64. T COM2 software mismatch communication halted 1 and or 2 software mismatch The G1000 system should be serviced MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted NAV1 and or NAV2 software mismatch The G1000 system should be serviced COM1 CONFIG COM1 config error Config service req d COM2 CONFIG COM config error Config service req d COM1 and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power 108 Garmin G1000 Cockpit Reference Guide for the DA40 40F The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced 190 00324 11 Rev C A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM needs service Return unit for repair Comments The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible COM1 PTT 1 push to talk key is stuck COM2 PTT 2 push to talk key is st
65. Terrain System Available will be heard when sufficient GPS Signal is received one Terrain System Test OK 190 00324 11 Rev C A GARMIN Annunciations amp Alerts TAWS ALERTS PFD MFD MED Alert Type TAWS B Page Aural Message Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up 2 Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up tena Oe 3 Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 0 Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain utente 5 i Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Impact Caution ITI or Ahead TERRAIN a Caution Terrain Caution Terrain 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 97 s m p q aoueplony 2 buluueld AN 540 s d olpny qqax 9
66. Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO F NAL 3 Press the ENT Key 4 final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch 42 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C 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
67. age Advisories 3 Flight Plan Import Export Messages 7 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F il Table of Contents GARMIN TELEHUU oe Aten 119 PFD Softkey Map cccccccssssssssssssssssssesssssssssvsssssssssssvsssssesssssvsssssessssssssecessssnssseessassanses 119 MED Softkey 124 Loading Updated Databases s s s s s s s s s s ssil 126 Index 1 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING mal ca m a g 2 o a 59 Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG olpny uqax wi0 gt AeN 1 Select the PFD Softkey to display the second level softkeys 2 Select the STD BARO Softkey 52 CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey
68. al Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Expiration Weather Product Symbol Time Minutes Pilot Weather Report B 90 Continuous PIREPs Temporary Flight Restrictions TFRs no product image 60 Continuous Terminal Aerodrome Reports TAFs no product image 60 Continuous The composite precipitation image is updated every 3 minutes but individual radar sites may take between 3 and 10 minutes to provide new data Setting Up and Customizing the GFDS Weather Data Link Page 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With Weather Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON OFF range settings etc 7 Press the ENT Key to select an option 8 Press the FMS Knob or CLR Key to return to the GFDS Weather Data Link Page with the changed settings On aircraft equipped with both GFDS and XM WX Satellite Weather services customizing the display settings for the corresponding weather products shown in following table will result in identical settings for b
69. all 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 8 9 10 11 a b o Or a b o d Or a b 4 Or a b o d When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference wayp
70. alled The G1000 system should be serviced The 1 transponder should be serviced when possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 111 saunqea4 2 Bu
71. ansponder replies to interrogations ALT Selects Mode C Altitude Reporting Mode aoueplony paezey transponder replies to identification and altitude interrogations GND Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations saunqea4 jeuonippy uonesado jewuougy VFR Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 gt 5 3 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 123 Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix CCUG ARMIN Level 1 Level2 Level 3 Description IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen TMR REF Displays Timer References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window MFD SOFTKEY MAP TEsene 1 DCR 1 SHWCHRT D optional optional Default softkey is dependant on the selection made in the map setup optio
72. arge FMS Knob to highlight the desired waypoint altitude c Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 40 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN LOAD AND OR ACTIVATE AN APPROACH PROCEDURE Procedures 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 1 Press the PROC Key 2 Tum 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 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
73. ayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD _ Displays NEXRAD weather and coverage or information on the Navigation Map optional Displays Worldwide Weather precipitation on the PRECIP Navigation Map optional XM LTNG Displays XM lightning information on the or Navigation Map optional DL LTNG _ Displays Worldwide Weather lightning information on the Navigation Map optional METAR Displays METAR flags on airport symbols shown 190 00324 11 Rev C on the Navigation Map optional Garmin G1000 Cockpit Reference Guide for the DA40 40F sainjea4 aoueplony 2 buluueld ACN 540 S24V olpny uqax Sia syuawny suj leuonippv 2 nf swio AeN qb uonesado jewuougy su jy unuuy ies bz Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix 000 GARMIN Level 1 Level 2 Description LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG PROFILE and or METAR softkeys are selected BACK Returns to top level softkeys DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Dec
74. ayed 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 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 91 5149 011 15 UATE seunpa20Jd Puluueld NEN Sd9 5247 oipny 4ddX sia n l Tuo2 AEN aoueplony paezey saunyee4 euonippv xipuaddy suey yunuuy x pul Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Annun Appendix Alerts Index Abnormal Operation ss 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 e Navigation Status Box fields except Active Leg TAS and DIK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD e T
75. aypoint Defined by Radials from Other Waypoints 0 27 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 29 Delete a User Waypoint 0 ccccccssssssssesscsssssssssssssesssssssesssssssesssssseessssnseesssssseesnnnseen Create a Flight Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 5 33 Enter an Airway in a Flight Plan Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 34 Store a Flight Plan s s sss sss s s sss isss s sinin 35 Edit a Stored Flight Plan 5 6 35 Delete a Waypoint from the Flight 7 35 Invert and Activate a Stored Flight 665 36 Copy a Flight Delete a Flight Graphical Flight Plan 7 5
76. aypoint in the flight plan 3 default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point 4 Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on 5 To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD NOTE See the Annunciations amp Alerts section for flight plan export message descriptions 1 Insert the SD card into the top card slot on the MFD 2 Press the FPL Key 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 the large FMS Knob to highlight the flight plan to be exported 6 Press the EXPORT Softkey 7 Press the ENT Key to confirm the export 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 37 olpny uqax 59 s tin sul wio gt AeN 346 3 52 2 ACN 540 nubi aoueplony paezey spay sainjea4 Tunuuy qeuuouqy leuonippy xipuaddy x pul GARMIN Flight Planning S u u nnsu
77. ays icon and age on the Inset Map for the selected weather products optional TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft NEXRAD Displays NEXRAD weather and coverage information on the Inset Map optional PRECIP Displays Worldwide Weather precipitation on the Inset Map optional XM LING Displays XM lightning information on the r Inset Map optional DL LTNG Displays Worldwide Weather lightning information on the Inset Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optional 120 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Appendix me Ezs 1 8 eo e OR ENT RST ERTS 1 1 o gt s n r m x 59 Select the BACK Softkey to return to the top level softkeys olpny uqax uo2 AEN z coo z nn wn mn lt a 1 nnoAnN A buluueld Esse ALERTS Es nN Ic na A L L L Lenox Aerts naw L L sex 1 F EY HSM NU VS PFD Configuration Softkeys s snp old
78. azard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features 1 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 necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while
79. be serviced GFDS Comm Error 6 A communications error has occurred It this error persists the system should be serviced GFDS Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the data request GFDS Comm Error 8 A server error has occurred or invalid data received GFDS Login Invalid There is a problem with the GFDS registration Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 for assistance 54 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Hazard Avoidance Temporarily Inop Weather Request Description Status Message GFDS Server The GFDS weather data server is temporarily out of service but is expected to return to service in less than 30 minutes GFDS Server Inop The GFDS weather data server will be out of service for at least 30 minutes Invalid Coverage Area The weather data request coverage area does not contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled checked and contains required criteria then re send the data request No GFDS Subscription The system is not be currently subscribed to GFDS or the access code is incorrect Verify the access code Contact Garmin Flight Data Services at 1 866 739 5687 in the United Stat
80. calculate and display the aircrafts current estimated position 90 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Abnormal Operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure Also the CDI deviation bar is removed from the display 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 information displ
81. cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 2 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 2 3 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Nav Com XPDR Audio Panel DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing the PLAY Key once plays the latest recorded memory block then r
82. ckpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN 5 Press the FMS Knob or the CLR Key to return to the GFDS Weather Data Link Page Or Hazard Avoidance 1 Select the Weather Information Page a Turn the large FMS Knob to select the Waypoint Page Group b Select the WX Softkey to select the Weather Information Page 2 Press the FMS Knob to display the cursor 3 Use the FMS Knob to enter the desired airport and press the ENT Key 4 Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text Note that the METAR text must be completely scrolled through before scrolling through the TAF text To display the METAR legend on the GFDS Weather Data Link Page select the LEGEND Softkey when METARs are selected for display PIREPs Pilot Weather Reports PIREPs describe in flight weather encountered by pilots A PIREP may contain unforecast adverse weather conditions such as low in flight visibility icing conditions wind shear turbulence and type of aircraft flown PIREPs are issued as either Routine UA or Urgent UUA Displaying PIREP text 1 Select the GFDS Weather Data Link Page 2 Select the MORE WX Softkey 3 Select the PIREPS Softkey 4 Press the RANGE Knob and pan to the desired weather report A gray circle will appear around the weather report when it is selected 5 Press the ENT Key The PIREP text is first displayed in a decoded fashion then as raw text
83. ct UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 4 5 6 Press 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 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN __ Flight instruments TURN ALL VSPEED BUGS ON OR OFF mal m a g 2 o a 1 Select the TMR REF Softkey 2 Press the MENU Key 3 Tum the FMS Knob to highlight the desired option 4 Press the ENT Key Select the TMR REF Softkey to remove the window 59 SET BAROMETRIC MINIMUM DESCENT ALTITUDE olpny uqax u102 AEN 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FM
84. cts within the selected coverage area during an initial GFDS Data Request regardless of which products if any are currently enabled for display On subsequent requests previously retrieved textual data such as METARs and TAFS is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request If the system cannot complete a GFDS weather data request one or more messages will appear in the request status window as shown in the following table Weather Request Status Message Auto requests inhibited Send manual request to reset Description The system has disabled automatic weather data requests due to excessive errors Automatic weather data requests have stopped Send a manual weather data request to resume automatic updates Auto update retry Seconds The system will attempt another automatic weather data request after an error occurred during the previous request Timer counts down until the next automatic request occurs GFDS Comm Error 2 A communications error has occurred with the GIA The system should be serviced GFDS Comm Error 4 This occurs if multiple automatic weather data requests have recently failed or the GDL 59 or a GIA is off line GFDS Comm Error 5 The Iridium or GFDS networks are not accessible Check Iridium signal strength If this error persists the G1000H should
85. culated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to XXXx Stormscope has failed The G1000 system should be serviced MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER lt message gt Message criteria entered by the user PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card 2 is inva
86. d altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude GPS Navigation White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance Small Text Altitude is not designated Altitude is designated The system cannot to be used in determining for use in giving vertical use this altitude in vertical flight path flight path guidance determining vertical 22 guidance Altitude has been retrieved from the navigation databas
87. dded WX 500 Stormscope Added XM Weather Added ADF DME Added bearing pointers Added fixed pitch propeller engine parameters Updated fixed pitch propeller engine parameters Added reference to DA40F on Copyright page and in Warnings Cautions and Notes 190 00324 03 Added diesel engine parameters 190 00324 04 Added fuel pressure gauge for the DA40 190 00324 05 Added GFC 700 Automatic Flight Control System Added GDU 6 10 software parameters Updated G1000 System Messages Removed diesel engine parameters 190 00324 06 Added TAWS Added XM Muting Added configurable low airspeed ranges 190 00324 07 190 00324 08 Added Stormscope Added TAS600 Added Airways WAAS VNAV amp Charts Added new engine display Added database loading instructions Updated G1000 System Messages Added other GDU 8 02 parameters Reformatted manual Added GDU 8 20 parameters 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F RR 1 Record of Revisions Ss GARMIN Part Number Change Summary 190 00324 09 Added Synthetic Vision feature and GDU 9 01 parameters 190 00324 10 Added GDU 9 14 parameters Added flight plan import export Updated procedure for entering User Waypoints Updated XM weather products Updated Terrain SVS and TAWS annunciations 190 00324 11 Added GDU 12 01 parameters Rev A Added MV DB update procedure Added Profile View Added GFDS weather Ad
88. ded ESP Added Aux Video Added Iridium Phone Info Added Electronic Checklists Updated XM WX satellite weather product symbols Updated SiriusXM product references Added database loading procedures B Updated Caution Annunciations PERI Date of Revision Affected Pages November 2012 123 24 Added VNAV Note RR 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN of contents FLIGHT NSTRUMENTAL a 1 Selecting the Altimeter Barometric Pressure 1 Selecting Standard Barometric Pressure 29 92 in 0 1 Change Altimeter Barometric Pressure Setting 1 Change Navigation Sources 1 Enable Disable OBS Mode While Navigating with 6 5 2 wa E 2 Configure Vspeed Bugs 2 Turn All Vspeed Bugs On or Off o ccccsssssssssssssssssessssssssssssssssssssssssessssssssviscssssssssenees 3 Set Barometric Minimum Descent
89. ded on the Aux Video page are for supplemental use only 88 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMI N Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Diamond DA40 40F Pilot s Operating Handbook POH always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established MAP BOOOUO Loss of Hazard Functions with Loss of GPS Position 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 89 uep ony s np d01d Puluueld ARN 540 52 44 sia s3u u nsul puezey 3461 Wo gt AeN ubiu saunqea4 jeuonippy xipuaddy suey junuuy x pul Flight Instrumen
90. dure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F s m p q aoueplony saanpa20Jd buluueld AN 540 s d olpny qqax 913 s u wunysu puezey 346 wio gt AeN ubiu Jewuougy fa x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx STRMSCP FAIL Stormscope has failed The position of the selected waypoint xxx is not cal
91. e A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Contig service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced 110 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN GTX 33 MESSAGE ADVISORIES Annunciations amp Alerts Message XPDR1 CONFIG XPDR1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted XPDR1 SRVC XPDR1 needs service Return unit for repair The transponder has incorrect software inst
92. e and is provided as a reference Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database Garmin G1000 Cockpit Reference Guide for the DA40 40F flight path guidance 190 00324 11 Rev C GARMIN cs navigation NOTE Making course changes greater than 90 during a descent with vertical guidance may cause excessive and rapid movement of the vertical deviation indicator and SVS Pathways The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent BOD Due to tum anticipation guidance turn smoothing distance to the BOD can be affected by course changes greater than approximately 5 degrees Ground speed can be affected by factors such as shifts in wind direction aircraft power management pitch angle and course changes Abrupt and or substantial changes to either the distance to the BOD ground speed or both can cause similarly abrupt substantial changes in vertical path guidance Because of turn smoothing changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the
93. e data link weather products e g XM WX Satellite Weather GFDS Worldwide Weather or FIS B for hazardous weather penetration Weather information provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F A Wamings Cautions amp Notei GARMIN V ARNING NEXRAD vveather 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 vveather data should not be used for short range vveather avoidance 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 WARNING The Garmin G1000 as installed in the Diamond DA40 40F 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 safet
94. e ground and the current GPS time Weather products are updated continuously or refreshed at specific intervals defined in the Refresh Rate column in the following table If for any reason a weather product is not refreshed within the defined Expiration Time intervals the data is considered expired and is removed from the display The age of the expired product is replaced by dashes If more than half of the expiration time has elapsed the color of the product age readout changes to yellow The refresh rate represents the interval at which the GFDS servers make available the most current known weather data It does not necessarily represent the rate at which new content is received from weather sources Expiration Weather Product Symbol Time eM Rate Minutes Minutes Radar Precipitation 30 U S Canada 3 PRECIP Europe 15 Infrared Satellite IR SAT o 30 Data Link Lightning Er DL LTNG 30 Continuous SIGMETs AIRMETs SIGMET SIGIAIR AIRMET 60 Continuous Meteorological Aerodrome Report y METAR 90 Continuous Winds Aloft WIND 60 Continuous 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 49 AeN 549 S24Y olpny uqax sia sjuawinaysuy u102 AEN Yubilu buluueld Wil 2 4 paezey SH V uones do sainjea4 unuuy jewuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnorm
95. e the gallons of fuel remaining GALLONS REMAIN in 1 gallon increments INC FUEL Allows the pilot to increase the gallons of fuel remaining in 1 gallon increments RST FUEL Resets the fuel remaining to 40 gallons in aircraft with standard fuel tanks Resets the fuel remaining to 50 gallons in aircraft with extended range fuel tanks EIS ENGINE 123 888 y TEMPERATURE ELECTRICAL EGT F 149 AHPS 08 49 1700 y 1600 1500 x 3 4 7494 750 FUEL CALCULATOR GALLONS REMAIN 2 Fuel Total Time in DEC FEL INC FUEL RST FUEL Service EIS Display DA40 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN ___Engine indication system DA40F ENGINE DISPLAY Pressing the ENGINE Softkey displays the EIS ENGINE Page s u u nnsu UATE Fuel used GALLONS USED endurance and range RANGE NM are all calculat ed based on the last manual adjustment of the fuel remaining GALLONS REMAIN Measured fuel quantity has no effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining 52 Fo 524 The following softkeys allow for adjustment of the remaining fuel quantity DEC FUEL Allows the pilot to decrease the gallons of fuel remaining 2 GALLONS REMAIN in 1 gallon increments il INC FUEL Allows the pilot to increase the gallons of fuel remaining in 1 gallon incremen
96. e versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F s m p q aoueplony 2 buluueld AN 540 s d olpny uqax 913 syu wunysu puezey 346 wio gt AeN ubiu euonippv uones do 1euuouqy m x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Pee Annunciations amp Alerts A GARMIN GMA 1347 MESSAGE ADVISORIES Message GMA1 FAIL GMA is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMA1 config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMA1 software mismatch communication halted The audio panel has incorrect software installed The G1000 system should be serviced GMA1 SERVICE GMA1 needs service Return unit for repair The audio panel self test has detected a problem in the unit Certain audio functions may still be avail able and the audio panel may still be usable The G1000 system should be serviced
97. ea4 junuuy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN WORLDWIDE WEATHER OPTIONAL NOTE Garmin Flight Data Services Worldwide Weather provides information for avoiding hazardous weather Do not utilize Worldwide Weather informa tion to penetrate hazardous weather Weather data are provided when the pilot initiates either a manual or automatic GFDS data request on the GFDS Weather Data Link Page on the MFD No weather data is displayed until the first GFDS Weather Data Request is made Registering with Garmin Flight Data Services A subscriber account must be established prior to receiving Worldwide Weather products Contact Garmin Flight Data Services at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 After a subscriber account has been established the system must be registered for data link features such as reporting services or GFDS Worldwide Weather Registration is accomplished by entering the required access code This process is only performed when initially setting up the system for GFDS services Registering the system for data link services 1 With the aircraft outside and having a clear view of the sky turn the large FMS Knob on the MFD to select the AUX page group
98. ecklist and select the desired checklist item Press the CLR Key or UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text Press the ENT Key GO TO NEXT CHECKLIST will be highlighted by the cursor Press the ENT Key to advance to the next checklist Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Additional Features Immediately Accessing Emergency Procedures 1 From any page on the MFD press the CHKLIST Softkey 2 Press the EMERGCY Softkey 3 Tum the FMS Knob to select the desired emergency checklist and press the ENT Key 4 Press the ENT Key or CHECK Softkey to check the selected emergency checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item olpny uqax 593 s u un sul Vuo2 AEN 3463 52 Press the CLR Key or UNCHECK Softkey to remove a check mark from an item 5 When all checklist items have been checked Checklist Fin
99. eiver 2 The G1000 system should be serviced 106 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN GIA 63 MESSAGE ADVISORIES Annunciations amp Alerts Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GIA 63W MESSAGE ADVISORIES CONT Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The G A1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high f problem persists the G1000 sys
100. em 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 truncated The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card 118 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C amp GARM
101. ent call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE Page al lowing additional call information to be viewed before answering Disabling incoming call alerts 1 With the AUX TELEPHONE Page displayed press the MENU Key on the MED to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable Incoming Call Alerts 3 Press the ENT Key The voice and pop up alert will not be displayed now when an incoming call is received Outgoing Calls Voice calls can be made from the cockpit through the Iridium Satellite Network To make a call 1 Press the TEL Key on the audio panel 2 select the DIAL Softkey on the MFD 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 15 s mp o4d Buluueld AeN 549 523 olpnyyuqax sia siu u nnsul Wfl Tu102 AEN 346 aoueplony paezey xipuaddy SH V uonesd do sainjea4 unuuy jeunouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN Or While viewing the AUX TELEPHONE Page a Press the or TEL Key on the audio panel b Press the MENU Key to display the Page Menu c Turn either FMS Knob to place the cursor on Dial a Phone Call d Press the ENT Key 3 Enter the desired number string
102. es Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts TERRAIN SVS ALERTS A GARMIN PFD MFD Alert Type TERRAIN SVS MFD Aural yP Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Warning Terrain Clearance Warning RTC Terrain Imminent Terrain Impact TERRAIN Warning Terrain Warning ITI Terrain Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Warning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN CAUTION TERRAN Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRATN 1 cautton OBSTACLE Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRATN 1 caurton oBSTACLE Caution Obstacle Caution 101 Obstacle TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS Alert Type System Test fail Terrain Alerting is disabled TER INH No GPS position or excessively degraded GPS signal System Test in progress System Test pass 96 Garmin G1000 Cockpit Reference Guide for the DA40 40F PFD MFD TERRAIN SVS Page Annunciation Terrain System Not Available
103. es or 913 397 8200 ext 1135 for assistance Reduce Request Area The GFDS weather data request area exceeds size limits Reduce weather coverage area and re send data request Request Cancelled The user has cancelled a GFDS weather data request Requested area too large Reduce coverage area The size of the GFDS weather data request has exceeded limits Reduce the size of the coverage area and try the weather data request again Request Failed Try Again Transfer Preempted The weather data request timed out Re send data request The data link is busy Retry request later Cancelling a GFDS Weather Data Request in Progress 1 Select the GFDS Weather Data Link Page 2 Press the MENU Key 3 With GFDS Data Request highlighted press the ENT Key 4 Turn the large FMS Knob to select CANCEL REQ and press the ENT Key The request status box indicates Request Cancelled 5 Press the FMS Knob to return to the GFDS Weather Data Link Page 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 55 ACN 540 S24V 404 99 siu umnnsul wio gt AeN T buluueld nubi s mp oold paezey SH V uones do sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix
104. eturns to normal operation Pressing the MKR MUTE Key while playing a memory block stops play e Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Com radios and music PILOT KEY COPLT KEY Pilot Hears Copilot Passenger ANNUNCIATOR ANNUNCIATOR Hears Hears Selected Selected Selected radios pilot radios pilot radios pilot OFF copilot copilot copilot passengers passengers passengers music music music ms 190 00324 11 Rev C Selected Selected COPILOT OFF ON radios pilot copilot radios pilot passengers passengers music music m Garmin 61000 Cockpit Reference Guide for the DA40 40F Copilot Copilot passengers passengers radios pilot music music Selected Selected Selected radios pilot radios pilot copilot copilot Passengers music siu umnnsu 59 523 olpny uqax M102 AEN uonesado sainqea4 aoueplony s mp oold 4 APN 5640 yunuuy Jeuuouqy Jeuonippy paezey xipuaddy x pul 3 nuru GARMIN Nav Com XPDR Audio Panel S u u nnsul fila 59 olpny uddX WO gt ACN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 Jeuolippy
105. ft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Tum the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey Or Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Hazard avoidance 1 While the Terrain SVS Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Enable Terrain 3 Press the ENT Key NOTE If Terrain SVS alerts are inhibited when the Final Approach is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B
106. g the ENT Key when panning over a TFR displays TFR specific information Displaying TFR Data 1 2 5 Select the Weather Data Link XM Page or Navigation Map Page Press the RANGE Knob and pan the map pointer over a TFR to highlight it The system displays TFR summary information above the map Press the ENT Key The system displays a pop up menu If necessary turn the FMS Knob to select Review Airspaces and press the ENT Key The system displays the TFR Information window Press the FMS Knob or the CLR Key to remove the TFR Information window XM WX Satellite Weather Products and Symbols Wx Product Status Icons Description US CN 101 NEXRAD Available for the US and Canada The age of the displayed data 211 each is shown at the right ECHO TOP The age of the displayed data is shown at the right Not om displayed when CLOUD TOP is displayed CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed 12m fry XM LIGHTNING The age of the displayed data is shown at the right gt a Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Hazard Avoidance Wx Product Status Icons Description CELL MOVEMENT The age of the displayed data is shown at the right SIGMET amp AIRMET The age of the displayed data for each is shown at the right M
107. ght plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F saunqee4 2 ACN 5649 2 olpny uqax sia syu unysu paezey nubi u102 NEN nubi euonippv uonesd do 1euuouqy 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Verify user modified procedures DB CHANGE Database changed Comments This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an navigation database update Verify that the user modified procedures in stored flight plan
108. he 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 Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing cursor moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press
109. ing displayed 9 Remove and reapply power to the system 10 11 12 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 Verify the correct database cycle information is shown for each database for each display 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F sainjea4 aoueplony 2 buluueld ACN 540 S24Y olpny uqax sia syuawny suj leuonippv p EZzeH wold Tuo2 NeN yb uonesado 1euuouqy su jy unuuy a k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix CCUG ARMIN Loading the Jeppesen Navigation Database as the Active Navigation Database The Jeppesen Navigation Database that is loaded to internal memory as the active database will be used by the system 1 2 3 4 5 6 7 8 9 10 11 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 W
110. ired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint 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 Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Tum the large FMS Knob to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 30 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN ri htrtanning 4 5 6 7 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Press the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A FLIGHT PLAN NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan
111. ished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text 6 Press the ENT Key GO TO NEXT CHECKLIST will be highlighted by the APN 540 buluueld Mb cursor 7 Press the ENT Key to advance to the next checklist 8 Press the RETURN Softkey to return to the previous checklist 9 Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed ELECTRONIC STABILITY AND PROTECTION ESP OPTIONAL The pilot can interrupt ESP by pressing and holding the Autopilot Disconnect AP DISC switch Upon releasing the or AP DISC switch ESP force will again be ap plied provided aircraft roll attitude is within engagement limits ESP can also be over ridden by overpowering the servos mechanical torque limit ESP can be enabled or disabled on the AUX SYSTEM SETUP 2 Page on the MED To enable or disable ESP 1 Turn the large FMS Knob to select the AUX Page Group 2 Tur the small FMS Knob to select the System Setup Page 3 If necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Page If the AUX SYSTEM SETUP 2 is already displayed proceed to step 4 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 85 xipuaddy SH V uones do sainyea4 aoueplony saunpadold junuuy jewuouqy Jeuonippy p EzeH x
112. ith the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD 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 PFD or MFD Apply power to the system and press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB Verify the correct active navigation database cycle information is shown for each display Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Appendix Loading the Jeppesen Navigation Database as the Standby Navigation Database The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Jeppesen Navigation Database to the bottom SD card prior to its effective date The Jeppesen Navigation Database is availab
113. ivate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Press the GO BACK Softkey to return to the previous page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options 4 Turn the small FMS Knob to choose between the On and Off Full Screen Options 5 Tum the small FMS Knob to choose between Day Auto and Night Options 6 In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 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 While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO
114. juuejd ACN SdD s24v olpny uqax sia s u un sul paezey nubi nubi euonippv uones do 1euuouqy x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS MAG DB AHRS magnetic model database version mismatch Comments The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced GSR 56 MESSAGE ADVISORIES Message Comments GSR1 FAIL GSR1 has failed A failure has been detected in the 1 GSR 56 The system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 sys
115. known Phone is disabled Phone is reserved for data transmission Calling other phone or incoming call from other phone Other phone is on hold Phones are connected Incoming Calls When viewing MFD pages other than the AUX TELEPHONE Page a pop up alert will be displayed The pop up alert may be inhibited at times such as during takeoff In addition to the pop up alert a ringing phone symbol will be displayed to the right of the MFD page title Also the voice alert Incoming Call will be heard on the selected cockpit audio 74 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Additional Features NOTE The Push to Talk switch is not utilized for telephone communication The microphone is active after selecting the ANSWER Softkey and stays active until the call is terminated Answering an incoming call 1 Press the TEL Key on the audio panel 2 select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page 1 Press the TEL Key on the audio panel 2 Press the MENU Key to display the Page Menu 3 Turn either FMS Knob to place the cursor on Answer Incoming Call 4 Press the ENT Key Selecting the IGNORE Softkey will extinguish the pop up window and leave the current call unanswered Selecting the IGNRE ALL Softkey will extinguish the pop up window for the current and all future incoming calls and leave the curr
116. l fila 59 WO gt AeN s24v AeN Sd5 buluueld 346 Blank Page 5 2 4 puezey saunjea4 Jeuolippy uones do pulouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 38 GARMIN 70 Procedures PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on 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 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE
117. 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Flight Planning 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MED it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD and tum the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location 6 Enter the changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page 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 Or for a stored flight plan a Press the FPL Key on the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor
118. ld unuuy qeuuouqy yeuonippy paezey n xipuaddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS 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 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 again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the f
119. le from Jeppesen seven days prior to its effective date NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of each PFD and the MFD 3 Turn the system ON A prompt 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 6 Again press any key to continue as instructed on the display 7 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 8 Press the ENT Key to acknowledge the startup screen 9 Turn the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page 11 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 sainjea4 aoueplony sainpadoid buluueld ACN 540 52 olpny uqax sia syuawny suj leuonippv 2 nf Tuo2 NeN qb
120. lected Message As Read 1 2 3 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Press the MRK READ Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Mark Selected Message As Read c Press the ENT Key The message symbol now indicates the message has been opened Mark All Messages As Read 1 2 3 4 While viewing the Inbox on the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Mark All New Messages As Read Press the ENT Key A confirmation window is displayed With cursor highlighting YES press the ENT Key The message symbols now indicate all the message have been opened Delete a Message 1 2 3 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Press the DELETE Softkey 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F Additional Features 83 2 Buluueld AeN 549 S4V olpny uqax sia s u u nnsul Tu102 AEN 3461 paezey xipuaddy SH V uones do sainjea4 unuuy jeunouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Av
121. lid 116 Garmin 61000 Cockpit Reference Guide for the DA40 40F The SD card in the bottom card slot of the PFD or MFD contains invalid data 190 00324 11 Rev C A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments CHECK CRS Database course for LOC1 LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS REGISTER GFDS Data services are inoperative register w GFDS Selected course for LOC2 differs from published localizer course by more than 10 degrees The system is not registered with Garmin Flight Data Services or its current registration data has failed authentication TRN AUD FAIL Trn Awareness audio source unavailable The audio source for terrain awareness is offline Check GIA1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req d Terrain audio alerts are not configured properly The system should be serviced FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight plan successfully imported Flight Plan Import Export Results Description File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified These waypoints have been saved to
122. light plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint On the MFD press the ACT LEG Softkey Or Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C 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 does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN VOM Yi BAKU aa T aroe White 221 9 NM 12400FT 23 LEMYN 220 g nu eae t Large Lig 2 Blue Text Approach KD
123. lutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the ac tive flight plan SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists LOADING UPDATED DATABASES N CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page 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 displays listed after it When an error 126 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Appe
124. n of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press 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 Press the GO BACK Softkey to return to the previous page 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 69 s mp o4d Buluueld AeN 549 S24V olpny uqax sia siu u nnsul nubi Tu102 AEN 346 aoueplony paezey s m xipuaddy SH V uones do junuuy Jewuougy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to act
125. ndix message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing 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 Tum the small FMS Knob to select the System Status Page 8 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete be
126. normal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 4 5 6 7 A GARMIN Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list IMPORT A FLIGHT PLAN FROM AN SD CARD 32 1 2 3 4 5 6 7 8 NOTE See the Annunciations amp Alerts section for flight plan import message descriptions Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the MFD to display the Active Flight Plan Page Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight plan Press the IMPORT Softkey If an empty flight plan is selected a list of
127. ns DCLTR 2 DCLTR 3 Press the BACK Softkey on this optional optional level to return to the top softkey level PRECIP DL LTNG oF oF optional optional optional TERRAIN AIRWAYS STRWSCP NEXRAD XMLTNG METAR LEGEND _ BACK Es EY ES w A Es EF A 7 AIRWAY HI The DONE Softkey changes to UNDO when the checklist item is already checked ENGINE DONE exir EMERGCY So A MFD Softkeys Level 1 Level 2 Description ENGINE Displays EIS Engine Page LEAN Selects the hottest cylinder and shows A PEAK for that cylinder DEC FUEL Press to decrease remaining fuel quantity in l gallon increments INC FUEL Press to increase remaining fuel quantity in l gallon increments 124 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Appendix Level 1 Level 2 Description RST FUEL Press to reset fuel to full MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map PROFILE Displays removes Profile Vievv on Navigation Map Page TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map ATRVVAYS Displays airvvays on the map eycles through the following AIRWAYS No airways are displ
128. nter clockwise to display a smaller area Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed press the MAP Softkey 3 Press the TRAFFIC Softkey Traffic is now displayed on the map Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Fasad Avoidance TERRAIN AND OBSTACLE PROXIMITY NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Displaying Terrain and Obstacles on the Terrain Proximity Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the last rectangular page icon If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Displaying Terrain and Obstacles on the Navigation Map 1 2 With the Navigation Map displayed press the MAP Softkey Press the TERRAIN Softkey Terrain and obstacle p
129. ntil the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Tum the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING OPTIONAL 1 Press the ADF DME or DME Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F s tin sul nubi 53 s24v olpny uqax M102 AEN sualy uonesado saunqee4 2 AeN 649 junuuy feuonippv paezey xipuaddy x pul Flight Instruments Abnormal Additional Hazard Flight Planning Annun Nav Com AFCS XPDR Audio EIS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Nav Com XPDR Audio Panel A GARMIN ENTER A TRANSPONDER CODE 1 2 3 Press the XPDR Softkey to display the transponder mode selection softkeys Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is
130. o the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 2 Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 2 Select the Stormscope Page Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR S
131. oach when the nav angle is set to AUTO s m p q aoueplony 2 buluueld AN 540 s d olpny uqax 913 syu wnysu puezey 34 wio gt AeN ubiu Jewuougy Ea x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ee Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair Comments A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperativ
132. ockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message ARSPC NEAR Airspace near less than 2 nm Comments Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active SLCT FREQ Select appropriate frequency for approach The system notifies the pilot that the loaded approach is not active Activate approach when required The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a proce
133. oftkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIM F s Avoidance XM WX SATELLITE WEATHER OPTIONAL WARNING Use of XM WX Satellite Weather for hazardous weather penetration is not recommended Weather information provided by SiriusXM Radio Service is approved only for weather avoidance not penetration Displaying XM WX on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Switching Between XM WX and GFDS Weather Sources 1 Tum the large FMS Knob on the MFD to select the MAP page group 2 Tum the small FMS Knob to select the desired Weather Data Link Page 3 Press the MENU Key 4 Turn the large FMS Knob to select Display XM Weather or Display GFDS Weather or choice dependent on current weather source and press the ENT Key Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Group
134. oidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Delete Selected Message c Press the ENT Key ELECTRONIC CHECKLISTS OPTIONAL The system accesses the checklists from an SD card inserted into the bezel slot If the SD card contains an invalid checklist file or no checklist the Power up Page messages display Checklist File Invalid or Checklist File N A not available and the CHKLIST Softkey is not available Accessing and Navigating Checklists 1 2 3 4 5 6 7 8 9 10 84 From any page on the MFD except EIS Pages press the CHKLIST Softkey Turn the large FMS Knob to select the GROUP field Turn the small FMS Knob to select the desired procedure and press the ENT Key Turn the large FMS Knob to select the CHECKLIST field Turn the FMS Knob to select the desired checklist and press the ENT Key The selected checklist item is indicated with white text surrounded by a white box Press the ENT Key or CHECK Softkey to check the selected checklist item The line item turns green and a checkmark is placed in the associated box The next line item is automatically selected for checking Either FMS Knob can be used to scroll through the ch
135. oint Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Flight Planning 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 CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 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 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Tum the small FMS Knob to select RAD DIS radial distance 9 Press the ENT Key 10 The cursor moves to the REF
136. oth services 50 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Hazard Avoidance XM WX Weather Product GFDS Worldwide Weather Product Next generation Radar Precipitation NEXRAD PRECIP Cloud Top Infrared Satellite CLD TOP IR SAT XM Lightning GFDS Lightning XM LTNG DL LTNG SIGMETs AIRMETs SIGMETS AIRMETs SIG AIR SIG AIR Meteorological Aerodrome Report METARs Meteorological Aerodrome Report METARs Winds Aloft Winds Aloft WIND WIND Pilot Weather Report Pilot Weather Report PIREPs PIREPs Temporary Flight Restriction TFR Temporary Flight Restriction TFR Restoring Default GFDS Weather Data Link Page Settings 1 2 3 4 5 Select the GFDS Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired default s to restore all or for selection and press ENT Key Switching Between GFDS and XM WX Weather Sources 1 Tum the large FMS Knob on the MFD to select the MAP page group 2 Tum the small FMS Knob to select the GFDS or XM WX Weather Data 190 00324 11 Rev C Link Page Garmin G1000 Cockpit Reference Guide for the DA40 40F ACN 540 52 404 s q s u umn sul u102 AEN buluueld nubi s mp oold paezey SH V uonesd do sainjea4 Tunuuy qeuuouqy Jeuonipp
137. p notice and provided further that any unauthorized commerc revision hereto is strictly prohibited Garm and S used without the express permission of Garmin NavData is a registered trademark o of L 3 ut the express written permission of Garmin Garmin hereby grants permission to oad a single copy of this manual and of any revision to this manual onto a hard drive or electronic storage medium to be viewed for personal use provided that such electronic nted copy of this manual or revision must contain the complete text of this copyright al distribution of this manual or any in and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts afeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be f Jeppesen Inc Stormscope is a registered trademark Communications and SiriusXM is a registered trademark of SiriusXM Satellite Radio Inc Honeywell and Bendix King are registered trademarks of Honeywell International Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively expressly disclaim all warranties with respect to the AOPA information included in this data and fitness for a particular purpose The in express or implied including but not limited to the implied warranties of merchantability formation is provided
138. pendix Alerts Operation Features Index Hazard Avoidance GARMIN 62 Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional System Self Test 1 Set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert TAS System Test OK is heard If the self test fails the system reverts to Standby Mode and a voice alert TAS System Test Fail is heard Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Traffic Map Page OPERATING is displayed in the Traffic Mode field 3 Select the NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger area or rotate cou
139. perative ROLL Roll axis control failure AP is inoperative f annunciated when AP is engaged take control e aircraft and disengage the autopilot If nunciated when AP is not engaged move each of the MET switch separately to check if a switch is causing the annunciation A condition has developed causing the pitch rvo to provide a s rvo to provide a s apply nose down ot disconnect ustained force Be prepared apply nose up control wheel force upon topilot disconnect ndition has developed causing the pitch ustained force Be prepared control wheel force upon A condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits auepiony Buluueld APN 540 52 olpnyyuqax sia paezey nubi uo2 AEN Wia saunqea4 jeuonippy Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test PFT Performing preflight system test Upon completion the aural alert will be heard PFT Preflight system test has failed 1 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 95 uonesado Jeuuougy x pul Hazard Flight Nav Com Flight Features Avoidance Procedur
140. points to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 33 olpny uqax s q s uawin jsu Vuo2 AEN 3463 52 2 4 NEN 540 nubi aoueplony paezey spay uones do s m unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 4 5 6 7 A GARMIN Turn the small FMS Knob one click clockwise and press the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The
141. 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 Press 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 25 olpny uqax 59 934 15 Vuo2 AEN 3463 52 2 4 ARN 540 nubi aoueplony paezey spay uones do sainjea4 unuuy qeuuouqy yeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 26 5 6 7 8 9 10 11 12 13 A GARMIN d Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is 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 Turn t
142. pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Avoidance Appendix Alerts Operation Index Additional Features GARMIN 4 Press the FMS Knob to activate the cursor 5 Tum the large FMS Knob to place the cursor in the STABILITY amp PROTECTION field 6 Tur the small FMS Knob to select ENABLE or DISABLE 7 Press the FMS Knob to remove the cursor ESP is automatically enabled on system power up Roll Engagement Roll Limit Indicators are displayed on the roll scale at 45 right and left indicating where ESP will engage As roll attitude exceeds 45 ESP will engage and the on side Roll Limit Indicator will move to 30 The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases to within the desirable roll attitude range Once engaged ESP force will be applied between 30 and 75 The force increases as roll attitude increases and decreases as roll attitude decreases The applied force is intended to encourage pilot input that returns the airplane to a more normal roll at titude As roll attitude decreases ESP will disengage at 30 Pitch Engagement ESP engages at 15 nose up and 18 nose down Once ESP is engaged it will apply increasing opposing force between 15 and 20 nose up and between 18 and 23 nose down Maximum opposing fo
143. rack Indicator All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and Terrain Proximity TERRAIN SVS and TAWS are disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 92 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Alternator failed Battery is only elec source Canopy and or rear door is not closed and locked Fuel pressure is greater than 35 psi 8 psi on DA40F Fuel pressure is below 14 psi 1 0 psi on DA40F Oil pressure is below 25 psi Starter is engaged Repeating Aural Tone Autopilot automatic trim has failed None KAP 140 equipped aircraft only CAUTION ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Left fuel quantity is less than 3 gallons Right fuel quantity is less than 3 gallons On board voltage is below 24 V Pitot heat is inoperative Pitot heat is off The cooling fan for the GIAs is inoperative GIA1 over temperature GIA2 over temperature cooling
144. ration settings do not match backup configuration memory The G1000 system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFDs have different software versions installed The G1000 system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The 1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists The MFD and or PFD detected a failure in the na
145. rce is applied between 20 and 50 nose up and between 23 and 50 nose down ESP disengages when 50 is exceeded in a nose up or nose down attitude With ESP engaged and the aircraft in a nose up condition opposing force steadily decreases from 20 nose up to 10 nose up as aircraft pitch moves toward zero degrees ESP disengages at 10 nose up With ESP engaged and the aircraft in a nose down condition opposing force steadily decreases from 23 nose down to 13 nose down as aircraft pitch moves toward zero degrees ESP disengages at 13 nose down The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft There are no indications marking the pitch ESP engage and disengage limits in these nose up nose down conditions High Airspeed Protection Exceeding Vne will result in ESP applying force to raise the nose of the aircraft When the high airspeed condition is remedied ESP force is no longer applied 86 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Additional Features AUXILIARY VIDEO OPTIONAL There are four modes of operation of the optional auxiliary video display Full Screen Full Screen with Digital Zoom Split Screen with Map and Split Screen with Map and Digital Zoom
146. rcraft altitude Enable Disable Aviation Data 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key TAWS Inhibit Inhibit TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key Enable TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1 2 3 66 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 NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL A 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 A WARNING Do not use SVS runway depic
147. roximity will now be displayed on the map TERRAIN SVS NOTE Terrain SVS is only available when the Synthetic Vision System SVS option is installed and the TAWS option has not been installed NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 63 olpnyyaqax sia uo2 AEN 52 AeN 540 buluueld nubi s mp oold paezey SH V uones do sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 64 Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircra
148. rted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key 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 copied Press the COPY Softkey A Copy to flight plan 22 confirmation window is displayed With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 36 1 2 3 4 Press the FPL Key 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 deleted Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Flight Planning 5 Press the DELETE Softkey A Delete flight plan 4 confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a w
149. s do pulouqy suay unuuy 190 00324 11 Rev Garmin G1000 Cockpit Reference Guide for the DA40 40F Index 4 A GARMIN Garmin International Inc 1200 East 151st Street s o the KS 66062 USA 9 o 397 82827 in Europe pe Liberty l Cape Road Park utha No 68 Gach ond F su m asr g z 2004 2009 2011 2012 Garmin Ltd or its subsidiaries 190 00324 11 Rev
150. s 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 all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANE
151. s are correct and up to date Verify stored airways DB CHANGE Database changed This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint xxxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position 114 Garmin G1000 C
152. s now displayed in the MESSAGE field Press the PREDEFD Softkey The PREDEFINED MESSAGE MENU Window is displayed Press the ENT Key The predefined message text is inserted into the message field If desired the message can be edited by using the FMS Knobs Press the ENT Key Press the SEND Softkey to transmit the message Text Message Boxes Received text messages reside in the Inbox as Read or Unread messages The Outbox contains Sent and Unsent text messages Saved messages that are meant to be sent later are stored as Drafts Each text message box may be viewed separately or together in any combination Show Inbox Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the INBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Inbox Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Additional features Shovv Outbox Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the OUTBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Outbox Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom lef
153. s the ENT Key 2 4 ARN 540 nubi CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 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 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 27 sia syuawin4 su wio gt AeN 34 olpny uqax 52 aoueplony paezey SH lV uones do sainjea4 unuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 28 A GARMIN 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the sm
154. s with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The G1000 system should be serviced PFD1 CONFIG PFD1 config error Config service req d PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced The PFD and or MFD self test has detected a problem The G1000 system should be serviced 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 99 saunqea4 2 ACN 5649 2 olpny uqax sia siu un sul paezey nubi Wil Jeuuougy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix m Annunciations 8 Alerts A GARMIN MFD amp PFD MESSAGE ADVISORIES CONT Message Comments MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configu
155. shown aoueplony paezey Pressing the ENGINE Soltkey returns the MFD to default operation sualy uonesado saunqea4 junuuy Jeuuouqy xipuaddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 9 GARMIN Engine Indication System S u umnnsul sub Tu102 AEN s24v AeN Sd5 Blank Page buluueld 6 2 4 aoueplony puezey saunjea4 Jeuolippy uoeaado jewouqy suay unuuy x pu ddy x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR Audio Panel ENTER OR CHANGE FLIGHT ID 1 Press the TMR REF Softkey then turn the large FMS Knob to highlight the Flight ID field 2 Tum the small FMS Knob to enter the first character 3 Turn the large FMS Knob to select the next field 4 Tum 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 Tum 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 Tum the small FMS Knob to enter the desired number 5 Repeat steps 3 and 4 u
156. smission 3 Press the ENT Key To disable the Iridium telephone system 1 With the AUX TELEPHONE Page displayed select the MENU Key on the MED to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable Iridium Transmission 3 Press the ENT Key Telephone Communication The pilot or copilot can place and answer calls on the Iridium satellite network Control and monitoring of telephone functions are accomplished through the AUX TELEPHONE Page To view the Telephone Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select SATELLITE PHONE Internal Phone External Phone Description Phone is Idle Phone is ringing Phone has a dial tone off hook or connected to another phone 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 73 xipuaddy suey uoesado s n e 4 aoueplony 2 buluueld ACN 540 52 olpny uqax 513 siu un sul junuuy Jewuougy paezey ubiu wo gt AeN ubiu x pul Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Index Additional Features Internal Phone External Phone A GARMIN Description Phone dialed is busy Phone is dialing another phone Phone has failed Phone status not
157. t message has been sent System failed to send text message Predefined text message Viewing a Text Message When Received When viewing MFD pages other than the AUX TEXT MESSAGING Page a pop up alert will be displayed when a new text message is received Press the VIEW Softkey to view the message Pressing the IGNORE Softkey will extinguish the pop up window and leave the text message unopened Pressing the IGNR ALL Softkey will extinguish the pop window and ignore all future incoming text messages Pressing the SMS Softkey will display the AUX TEXT MESSAGING Page The pop up alerts may be enabled or disabled through the Page Menu 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 AeN 540 523 oipny 4ddX sia syuauinyysuy u102 AEN aoueplony paezey s m su jy unuuy x pu ddy x pul 34 nu Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 78 A GARMIN Enable Disable Incoming Text Message Pop Up Alerts 1 With the AUX TEXT MESSAGING Page displayed press the MENU Key on the MFD to display the Page Menu 2 Turn either FMS Knob to place the cursor on Disable New Message Popups or
158. t of the list window Show Draft Messages While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the DRAFTS Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Draft Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Arranging Text Messages The viewed messages may be listed according to the date time the message was sent or received the type of message read unread sent unsent etc or by message address View Messages Sorted by Message Date Time While viewing the AUX TEXT MESSAGING Page press the ARRANGE Softkey then press the TIME Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Date Time c Press the ENT Key The sorting selection is indicated at the bottom center of the list window 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 Buluueld AeN 549 S4V olpnyyuqax sia s u u nnsul Tu102 AEN 3461 aoueplony paezey xipuaddy SH V uones do sainjea4 unuuy jeunouqy leuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features 82 A GARM
159. taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing 68 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Additional Features 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 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 versio
160. tch communication halted IFEST GIA2 software mismatch The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced m N communication halted NIFEST GFC software mismatch munication halted ncorrect servo software is installed or gain set tings are incorrect COM1 TEMP 1 over temp Reducing transmitter power COM2 TEMP CON2 over temp Reducing transmitter power The system has detected an over temperature ondition in COM1 and or COM2 The transmit ter is operating at reduced power If the problem persists the G1000 system should be serviced 1 SERVICE 1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or 2 may still be usable The G1000 system should be serviced when possible COM1 PTT 1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM
161. tem should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The G A1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F saunqea4 2 Bujuuejd ACN SdD 2 olpny uqax sia siu umn su paezey nubi u102 AEN nubi euonippv uones do 1euuouqy 5 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted Comments A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect MANIFEST COM1 software mismatch communication halted MANIFES
162. tem should be serviced GDC 74A MESSAGE ADVISORIES Message Comments MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced ADC1 ALT EC ADC1 altitude error correction is unavailable ADC1 AS EC GDC1 software mismatch communication halted GDC1 is reporting that the altitude error correction is unavailable GDC1 is reporting that the airspeed error correction is unavailable 112 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN GDL 69A MESSAGE ADVISORIES Annunciations amp Alerts Message GDL69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an navigation database update eliminates an obsolete waypoint The fli
163. the A flight plan file stored on the SD card was successfully imported as a stored flight plan The file stored on the SD card did not contain a flight plan only user waypoints system user waypoints No flight plans stored in the system 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 export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 117 saunqea4 uepjoay 2 Gujuuejd ACN SdD 2 olpny uqax s q siu un sul paezey u102 AEN nubi euonippv uones do 1euuouqy m x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN Flight Plan Import Export Results Flight plan partially imported File contained user waypoints only Description 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 syst
164. 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 could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Do not us
165. 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 press the IMPORT Softkey Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Flight Planning Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b c d a b d e Enter the user waypoint identifier facility or city Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airport way
166. tical separation meet TA citeria Traffic Advisory Off Scale Traffic Symbol Traffic Information Service TIS Description NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Press the TNA MUTE Softkey to mute the Traffic Not Available aural alert if desired 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 61 ACN 540 S24V 404 99 siu umn sul u102 AEN buluueld nubi uep ony s mp oold paezey SH V uones do sainjea4 Tunuuy qeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Ap
167. tion as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing 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 Three dimensional Traffic Airport Signs e Runway Display Displaying SVS Terrain 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 67 2 Puluueld AeN 549 52 olpnyyuqax sia siu u nnsul 614 Tu102 AEN 3461 2 xipuaddy SH V uones do sainjea4 unuuy jeunouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning H
168. to delete the message Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C GARMIN Additional Features Predefined Text Messages Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message Create a Predefined Text Message 1 While viewing the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu 2 Tur either FMS Knob to select Edit Predefined Messages 3 Press the ENT Key The PREDEFINED MESSAGES view is now displayed 4 Press the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Predefined Message c Press the ENT Key The PREDEFINED SMS TEXT MESSAGE Window is now displayed 5 cursor is displayed in the TITLE field Enter the desired message title Entry can be accomplished through the FMS Knob and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by pressing the NUMBERS Softkey Press the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by pressing the SYMBOLS Softkey 6 Press the ENT Key The cursor is now displayed in the MESSAGE field 7 Enter the desired message using any combination of entry methods as 2 4 ARN 540 52 olpny gqax sia syuawin4su Tuo2 AEN sub
169. ts RST FUEL Resets the fuel remaining to 40 gallons buluueld Wil EIS ENGINE 123 888 TEMPERATURE ELECTRICAL k r F 1652 1616 aes 1634 1652 40 7 1700 7 0 1500 VoL i 1500 1400 1300 1 7 4 aoueplony saunpa20Jd paezey saunyea4 yeuonippyv 2 un 410 392 OIL PSI FUEL FLOW GPH 13 2 so FUEL CALCULATOR GALLONS REMAIN 400 Fuel 4 428 446 400 niz a GALLONS USED 00 i i y 300 ENDURANCE 3 01 lota izer rs RANGE NH 303 Calculations 200 ri a y TOTA h VICI gt L FUEL R FUEL TOTAL TIME IN SERVICE Aircraft GAL GAL 100 mane 0 0 HRS lotal Time in TE FOL RT FET R Jewuouqy su jy unuuy x pu ddy EIS Display DA40F x pul 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 Engine indication System GARMIN ENGINE LEANING While viewing the EIS ENGINE Page press the LEAN Softkey 2 o SE 2s iz 2 2 As the mixture is leaned one of the eylinder5 exhaust temperature will peak This is indicated by Ist being displayed below the first cylinder to peak as seen in the first figure The A Peak temperature is the difference between the peak temperature and 25 the present temperature 25 123 800 Cylinder Peak ELECTRICAL Temperature xi ui y HAN IN HG PM 51 8 24 3 Ist Cylinder un Peak r 2 X k ie 32 PPM
170. ts Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes e Traffic Annunciations System Time Glideslope Glide e AFCS Annunciations 9 PFD Setup Menu path and Vertical Flight director Com e Windows displayed in Deviation Indicators mand Bars the lower right corner Altimeter Barometric Inset Map of the PFD Setting e Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status Barometric Minimum Box Descent Altitude Box Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to
171. uck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT 1 remote transfer key is stuck COM2 RMT 2 remote transfer key is stuck The COM1 and or 2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums TRUE APR True north approach Change HDG reference to TRUE 190 00324 11 Rev C Garmin G1000 Cockpit Reference Guide for the DA40 40F Displayed after passing the first waypoint of a true north appr
172. vigation database Attempt to reload the navigation database If problem persists the G1000 system should be serviced 100 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists Comments The MFD and or PFD detected a failure in the basemap database MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another L
173. when possible GIA 63 MESSAGE ADVISORIES Message GIA1 CONFIG GIA1 config error Config service req d Comments The G A1 and or GIA2 configuration settings do GIA2 CONFIG GIA2 config error Config service req d not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio GIA2 CONFIG GIA2 audio contig error Config service req d configuration The G1000 system should be serviced GIA1 COOLING GIA1 temperature The GIA1 and or GIA2 temperature is too low too low to operate correctly Allow units to warm up to GIA2 COOLING GIA2 temperature operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be GIA2 COOLING GIA2 over sarar temperature 104 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 11 Rev C A GARMIN Annunciations amp Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments GIA1 SERVICE GIA1 needs service Return the unit for repair 1 Return the unit for repair GIA2 SERVICE GIA2 needs service The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced MANIFEST GIA1 software misma
174. y This step is not necessary on the GFDS Weather Data Link Page Select the DL LTNG Softkey To display the Data Link Lightning legend on the Weather Data Link Page select the LEGEND Softkey when Data Link Lightning is selected for display SIGMETs and AIRMETs The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the GFDS data request Displaying SIGMETs and AIRMETs 1 2 3 4 Select the GFDS Weather Data Link Page Select the SIG AIR Softkey To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon Press the ENT key To display the SIGMET and AIRMET legend select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display METARs and TAFs NOTE METAR information is only displayed vvithin the installed navigation database service area METAR and TAF text are displayed on the WPT Weather Information Page TAF information is displayed in its raw form when it is available DisptayiING METAR anp TAF Text 1 2 3 4 On the GFDS Weather Data Link Page select the METAR Softkey Press the RANGE Knob and pan to the desired airport Press the ENT Key The Weather Information Page is shown with METAR and TAF text Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text METAR text must be completely scrolled through before scrolling through the TAF text Garmin G1000 Co
175. y xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 52 3 4 A GARMIN Press the MENU Key Turn the large FMS Knob to select Display GFDS Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Legends for Displayed GFDS Weather Products 1 2 3 4 Select the GFDS Weather Data Link Page Select the LEGEND Softkey to display the legends for the displayed weather products Or a Press the MENU Key b Select Weather Legend and press the ENT Key Turn the FMS Knob to scroll through the legends if more are available than fit in the window To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Setting Up and Customizing Weather Data for the Navigation Map Page 1 2 3 4 5 6 7 8 Select the Navigation Map Page Press the MENU Key With Map Setup highlighted press the ENT Key Turn the small FMS Knob to select the Weather Group and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to scroll through options for each product ON OFF range settings Press the ENT Key to select an option
176. y 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 the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Diamond DA40 40F Pilot s Operating Handbook POH 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 DA40 40F 190 00324 11 Rev C amp GARMIN 7 Cautions amp Notes V ARNING 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 mile

Download Pdf Manuals

Related Search

Related Contents

Tageslichtlampe Daylight lamp Lampe à lumière du jour  EKA Manuale Di Installazione ITA-ENG  LevelOne Smart Mobile USB Storage  Benutzerhandbuch - XProtect Smart Client  Pyrit 10A, 12A, 15A active 2 way full  MANUAL DE INSTALACION DEL VISUALCONT  TABLE OF CONTENTS  平成 19 年度 級管工事学科試験 問題B  Woods Equipment 1009 User's Manual  Belvoir High School Parent Portal User Guide for Parents and Carers  

Copyright © All rights reserved. Failed to retrieve file