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Garmin Software Version 0321.19 Cockpit Reference Guide

1. 26 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A Table of Contents GARMIN Insert a Waypoint in the Active Flight Plan V V l 27 Enter an Airway in a Flight Plan Invert An Active Flight 667 55 Remove a Departure Arrival Approach or Airway from a Flight Plan 28 Store a Flight Pleas z n 29 Edit a Stored Flight Plan 29 Delete a Waypoint from the Flight 7 29 Invert and Activate a Stored Flight 30 Delete a Flight Plan Graphical Flight Plan Creation URULEDURE Load and Activate a Departure Procedure Activate A Departure Leg ou cccccsescssssssssssssessssssssssssssssesssssseesssssssesssssseessssnseessssnseeen Load An Arrival 6
2. Activate An Arrival Leg 0 cccccssussssssssssssssesssssssesssssssseesssssessssssseessssnseessssnssesssseeesen Load and or Activate an Approach Procedure 34 Activate An Approach in the Active Flight 35 Activate a Vector to Final Approach Fix s si s s si s s 36 Activate A Missed Approach in the Active Flight 77 556 36 HAZARD ss 37 Customizing the Hazard Displays on the Navigation Map 37 STORMSCOPE Optional s s s s s s s s s is XM Weather Traffic Systems oE A RERE Terrain And Obstacle Proximity Terrain SVS naa a sine antlnill eiiialliadian Terrain Awareness amp Warning System TAWS Display Optional 44 ADDITIONAL Synthetic VISION Terminal Procedure Charts XM Radio Entertainment ABNORMAL OPERATION 53 Reversionary Mode ccccccsssss
3. 5 5 DA40 Engine 5 dices 6 DA40F Engine Display 0 ccccccccsssssssesccsssscssssssscesssssesssssssesssssscessessessnniseeesennseessens 7 Engine Leaning ise 3s s n d d n A th 8 NAV COM TRANSPONDERI AUDIO PANEL 1 ADF Tuning 1 DME Tuning 5 0 1 Enter a Transponder Code ccccccsussssssssscssssesccsssssseesssnscessssssceesssssceesssnsteesnsnsceesssnseen 1 Selecting a COM Radio 2 Selecting a NAV Radio s s s s s ss s s sss s sssss s sssss s ssssl 2 NAV COM Tuning Ueyn ten aster ARALAR S Ada daa ae 2 Digital Clearance Recorder and Player 2 Intercom System ICS Isolation 3 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM 5 Fl
4. PFD MFD MFD Alert Type TAWS Page Aural Message Pop Up Alert Annunciation Reduced Required TERRAIN OBSTACLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead OBSTACLE ti Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN TOO LOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb ETERRRINI F varsa Don t sink Rate Caution NCR or or n Low Terrain TAWS SYSTEM STATUS ANNUNCIATIONS PFD MFD TAWS Page TAWS System Test Fail TAWS FAIL TAWS Alerting is disabled TAWS INHB TAWS N A No GPS position or excessively degraded GPS signal System Test in progress System Test pass TAWS System Test 190 00324 09 Rev A TAWS TEST Aural Message TANS System Failure TAWS Not Available TANS Available will be heard when sufficient GPS signal is re established one Ok Garmin G1000 Cockpit Reference Guide for the DA40 40F s m ie q UED OAV s mp old buluueld ACN 540 52 404 513 5149 011115 paezey Wila wio gt Aen 346
5. 2 s m ipuonippy uones do Jewuouqy SM V unuuy xipuaddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 32 A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the 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 Procedures 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 desired waypoint within the departure 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIV
6. PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be serviced 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 PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced 62 Garmin G1000 Cockpit Refe rence Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts MFD 8 PFD MESSAGE ADVISORIES CONT Message Comments MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced 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 na
7. 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 aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black Enable Disable Aviation Data 1 While the TAWS Page is displayed press the MENU Key 2 Tum the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit Inhibit TAWS While the TAWS Page is displayed press the INHIBIT Softkey Or 1 Press the MENU Key 2 Tum the small FMS Knob to select Inhibit TAVVS 3 Press the ENT Key 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 ARN Sd9 52 olpny uqax 93 5149 001115 u102 AEN 3461 wld s mp old paezey su jy uonesado s n e 4 Junuuy jewuouqy 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
8. Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG 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 GTX 33 MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder 72 Garmin 61000 Cockpit Reference G
9. Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Warning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTION Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN CAUTION TERRAIN Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRAIN CAUTION OBSTACLE Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRAIN 1 cautton oBSTACLE Caution Obstacle Caution 101 Obstacle TERRAIN SVS SYSTEM STATUS ANNUNCIATIONS Alert Type System Test fail Terrain Alerting is disabled No GPS position or excessively degraded GPS signal PFD MFD TERRAIN SVS Page Annunciation TER FAIL TER N A System Test in progress TER TEST System Test pass Terrain System Test OK 190 00324 09 Rev A Terrain System Terrain System Available will be heard when sufficient GPS signal is re established Aural Message Terrain System Failure one ot Available None Garmin G1000 Cockpit Reference Guide for the DA40 40F 9 s m ie q 2 ACN 540 52 444 513 5149 011115 2 wy wio gt AeN 346 uones do euuougy 5 x pul Additional Hazard Flight Nav Com
10. Traffic Displaying SVS Terrain 1 Press the PFD So 2 Press the SYN VI ftkey S Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page Displaying Pathvvays 1 Press the PFD So 2 Press the SYN VI ftkey S Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY Softkey 5 Press the BACK Softkey to return to the previous page 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 xipuaddy SHV uones do s mie q 2 ACN 5420 404 sia s u u nnsul junuuy jeunouqy a 2 Wil u102 AEN fia 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 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 ava
11. 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Tum the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field 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 returns to normal operation e 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN 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 PILOT Selected radios pilot copilot passengers music radios pilot Selected radios pilot OFF ON passengers music Selected CREW ON ON radios pilot copilot 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F Sel
12. 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan s mp old Buruuejd ACN Sd9 nubi 3 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point 4 Press the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and 513 syu wnysuj uu02 AEN 346 444 52 paezey s m ie q uonesado jeuuouqy so on 5 To change the user waypoint name follow the procedure for modifying a user waypoint 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 31 su jy unuuy xipuaddy x pul GARMIN Flight Planning s u uin sul fil 59 olpny dddX ui0 gt AeN 52 AeN 542 Huiuue d s Blank Page 6 2 4
13. 7 To remove the window press the CLR Key or the TMR REF Softkey 444 wi0 gt AeN S24V DISPLAYING WIND DATA ACN 540 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 buluueld 2 CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy paezey xipuaddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F amp GARMIN Flight Instruments ie olpny dddX uio gt AeN s24v AeN Sd5 Buruuejd bila Blank Page 6 2 4 puezey s n ze 4 ipuonippy uones do Jewuouqy SM V unuuy xipuaddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A GARMIN Engine Indication System ENGINE INDICATION SYSTEM Fuel Pressure is only available on certified aircraft Fuel Quantit Indicator scale is 0 25 with extended range fuel tanks 0 20 with standard tanks 190 00324 09 Rev A A RPM 330 FUEL FLOW GPH RPM x 2300 FUEL FLOW GP
14. Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service 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 G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative 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 A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 68 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments G S1 SERVICE G S1 needs service Return unit for repair 1 and or receiver 2 The receiver may still be G S2 SERVICE G S2 needs service Return unit for repair available The G1000 system should be serviced when possible A failure has been detected in glideslope receiver GIA 63W MESSAGE ADVISORIES Message GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d Comments
15. 47 T TA 62 TAF 39 TAS 41 62 73 Index 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Garmin nternational Inc 1200 Fast 151st Street Olathe KS 66062 U 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2004 2008 Garmin Ltd or its subsidiaries 190 00324 09 Rev A
16. ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Left fuel quantity is less than 3 gallons Right fuel quantity is less than 3 gallons l On board voltage is below 24 V ange Aural Tone Pitot heat is inoperative Pitot heat is off ALERT MESSAGE Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative MFD FAN FAIL The cooling fan for the MFD is inoperative None GIA FAN FAIL The cooling fan for the GIAs is inoperative 57 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F s m uep ony sainparold buluueld ACN Sd5 52 olpny uqax 513 s u uin sul p ezeH 346 yeuonippv uones do Jewiouqy 5 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Append Index Annunciations amp Alerts A FCS ALERTS Roll Failure MET Switch Stuck or Pitch Trim Axis Control Failure A GARMIN Pitch axis control failure AP is inoperative PTCH PTRM_ If an 0 ROLL Roll axis control failure AP is inoperative nunciated when AP is engaged take control e aircraft and disengage the autopilot If nunciated when AP is not engaged move each the MET switch separately to check if a switch is causing the annunciation System Failure AFCS AP and MET are unavailable FD may still be 58 El
17. Avoidance GARMIN Enable TAWS While the TAWS Page is displayed press the INHIBIT Softkey Or 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS 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 46 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN A SYNTHETIC VISION Additional Features DDITIONAL FEATURES Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 Integrated Flight Deck System SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilot s 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 Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensional Airport Signs e Runway Display
18. COM1 RMT 1 remote transfer key is stuck COM2 RMT 2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced with other NAVS LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase of flight 70 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message GPS NAV LOST Loss of GPS navigation Insufficient satellites Comments 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 WAAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair
19. INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Press the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Press the COPY Softkey A Copy to flight plan 82 confirmation window is displayed 30 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN FlightPlaming 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Press the DELETE Softkey A Delete flight plan 4 confirmation window is displayed
20. Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 83 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F saunqea4 aoueplony Buluueld APN 5640 2 olpny uqax sia syu wnysu Jeuonippy paezey T TR wio gt AeN 4613 euuougy suey unuuy E EF Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index Appendix MFD SOFTKEY MAP E a rs ENGINE LEAN DEC FUEL INC FUEL RST FUEL MAP TRAFFIC TOPO 84 A GARMIN SHVV CHRT CHKLIST optional optional Default softkey is dependant on Press the BACK Softkey on this the selection made level to return to the top softkey level in the map setup options optional optional optional TRAFFIC TERRAIN AIRWAYS STRMSCP NEXRAD XMLTNG BACK TOPO D ES onnm 7 AIRWY ON AIRWAY HI The DONE Softkey changes to UNDO when the checklist item is already checked ENGINE DONE EXIT EMERGCY S O D O MFD Softkeys Displays EIS Engine Page Selects the hottest cylinder and shows A PEAK for that cylinder Press to decrease remainingfuel quantity in 1 gallon increments Press to increas
21. 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN vVlarnings Cautions amp Notes NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California 5 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A amp Notes GARMIN Blank Page Garmin G1000 Coc
22. 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 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 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 913 s u uinnsu olpny qqax wi0 gt AeN ACN 540 52 su jy uoresado s n e 4 aoueplony 4 junuuy leuuouqy leuonippv xipuaddy x pul 346 paezey Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun GPS Nav AFCS EIS Procedures Append
23. 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 Tum the large FMS Knob until the Map Page group is selected 2 Tum the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Avoidance XM WEATHER OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM
24. 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 00 low to operate correctly Allow units to warm up to GIA2 COOLING GIA2 temperature operating temperature 00 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 temperature 66 Garmin 61000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN GIA 63 MESSAGE ADVISORIES CONT Annunciations amp Alerts Message Comments GIA1 SERVICE GIA1 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a pair l i problem in the unit The G1000 system should GIA2 SERVICE GIA2 needs service Return the unit for repair MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software MANIFEST GIA2 software mismatch installed The G1000 system should be serviced communication halted COM1 TEMP COMI over temp The system has detected an over temperature Reducing transmitter power condition in COM1 and or COM2 The transmit COM2 TEMP COM2 over temp ter is operating a
25. flight plan contains procedures that have been manually edited This alert is issued only after an aviation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 15 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F s m ie q uepI ony s mp old buluueld ACN 540 92 404 sia s u u nn sul paezey wy wio gt AeN 346 uonesado jewuouqy 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Abnormal Operation Sopena Eed Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts
26. 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 d a b c 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 waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 27 oipny YddX 93 S u umnnsul 161 523 s mp old Buruuejd ACN Sd9 nubi su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy paezey xipuaddy xe pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index A Flight Planning 0080880 ARMIN ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 4 5 6 7 Pr
27. of the following methods to enter the reference waypoint a Turn the small FMS Knob to the left to display a list of flight plan waypoints This list is populated only when there is an active flight plan b Turn the large FMS Knob to select the desired waypoint c Press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST waypoints to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 7 After pressing the ENT Key the cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 8 Press the ENT Key 9 cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 10 Press the ENT Key The cursor is now placed for entering another reference waypoint if desired 11 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the la
28. penetration Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN vVlarnings Cautions amp Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING 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 safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accur
29. AL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 33 ACN 540 S24V olpny xqax s z siu uini sul wio gt Aen 346 ni s snp old su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy puezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMI N 4 Turn the large FMS Knob to highlight the desired arrival 5 Press the ENT Key A list of transitions is displayed for the selected arrival 6 Turn either FMS Knob to select the desired transition 7 Press the ENT Key A list of runways may be displayed for the selected arrival 8 Turn the large FMS Knob to highlight the desired runway 9 Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival becomes part of the active flight plan 12 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 large 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 ARRIVA
30. CTIVATE VECTOR TO HNAL Press the ENT Key The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 36 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightnin
31. EST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 73 s mie q s mp old buluueld ACN 540 52 404 sia s u u nnsul paezey wy wio gt Aen 346 uones do euuouqy 5 x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Append Eed Index Annunciations amp Alerts GMU 44 MESSAGE ADVISORIES A GARMIN Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced GDL 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL soft
32. Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Appendix freee Index Annunciations amp Alerts A GARMIN TAWS ALERTS PFD MFD MED Alert Type TAWS 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 E Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up illik a 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 5 5 Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AFAD Terrain Ahead Terrain Impact Caution ITI or Ahead TERRAIN Caution Terrain Caution Terrain 60 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts
33. G 1000 Integrated Flight Deck Cockpit Reference Guide for the DA40 40F A GARMIN Copyright 2004 2008 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0321 18 or later for the Diamond DA40 and DA4OF Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the compl
34. GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE service Return NAV2 needs 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 transfer key is stuck NAV2 RMT XFR NAV2 remote 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 receiver 2 The G1000 system should be serviced 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F s mie q 2 ACN 540 52 04 sia s u u nn sul paezey wy wio gt AeN 346 uones do euuouqy aa 5 x pul Flight Instruments Additional Hazard Flight Nav Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Append Eed Index
35. H v l 25 FUEL PRES OIL TEMP OIL PRES Vv OIL TEMP Vv OIL PRES V AMPS Vv v 6 80 b A 80 VOLTS b A FUEL QTY GAL 8 FUEL QTY GAL e FRE 25 DA40 DA40F Engine Instrument Display on the MFD Garmin 61000 Cockpit Reference Guide for the DA40 40F siu uinnsu z Se Bo Fo a3 o su jy uoresado s n e 4 aoueplony 4 APN 5640 yi unuuy euuouqy Jeuonippy paezey xipuaddy x pul sub Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index amp Engine dication Syste 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 DEC FUEL Allows the pilot to decrease 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 f
36. HULULULLU Loss of Hazard Functions vvith Loss of GPS Position 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 93 s mp old buluueld ACN Sd9 52 404 513 5149 011115 paezey Wila wio gt Aen 346 s m ie q su jy unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Alerts Appendix 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 e Glideslope Glide e AFCS Annunciations PFD Setup Menu path and Vertical Flight director Com 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 e DME Information Nearest Airports 2 VNV Target Altitude Window Flight Plan e Wind Data Messages Selected Heading Box Procedures e Selected Course Box ADF DME Tuning e Transponder Status Barometric Minimum Box Descent Altitude Box Extrem
37. L LEG 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the arrival 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT APPROACH 34 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Uu 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 Procedures Press the ENT Key A list of available approaches for the destination airport 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 d
38. N As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity 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 56 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Qnnundations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Oil pressure is below 25 psi Fuel pressure is below 14 psi 1 0 psi on DA40F Fuel pressure is greater than 35 psi 8 psi on DA40F l Continuous Alternator failed Battery is only elec source Aural Tone Starter is engaged Canopy and or rear door is not closed and locked Autopilot automatic trim has failed KAP 140 equipped aircraft only CAUTION
39. 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 to return to the top level softkeys 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F su jy uoresado s n e 4 aoueplony s snp olq buluueld APN 540 yi olpny uqax 513 unuuy euuouqy Jeuonippy paezey Wija u102 AEN xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 2 3 Press the OBS Softkey to select OBS Mode Turn 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 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 2 3 Press the TMR REF Softkey th
40. RRIVAL APPROACH OR AIRWAY FROM A FLIGHT 1 28 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN rlstrtan ng Or for a stored flight plan a Press the FPL Key on the MFD and tum 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 2 Tum the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints 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 turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cur
41. Radio Service is approved only for weather avoidance not penetration Displaying XM Weather 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 Displaying Weather on the Weather Data Link Page 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 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 Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the repor
42. 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 the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished The flashing cursor moves to the calibrated airspeed field Enter a calibrated airspeed Press the ENT Key when finished CREATE A NEW USER WAYPOINT 24 1 2 3 4 5 6 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Press the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Use one
43. The GIA1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced 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 system should be serviced G A1 SERVICE GIA1 needs GIA2 SERVICE GIA2 needs service Return the unit for repair service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 69 s mie q uepI ony s mp old ACN 540 92 444 513 5149 011115 2 wy wio gt Aen Ifid uones do euuouqy 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Abnormal Operation Append Ee I
44. active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings 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 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F s n e 4 aoueplony 4 APN 5640 yi olpny uqax 913 s u uinnsu Jeuonippy 2 T TR u102 AEN 4613 uones do jeuuouqy sH ly unuuy oe 651 Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Appendix Index Appendix BRG2 ALT UNIT METERS IN HPA STD BARO cor L rovel XPDR 82 A GARMIN Cycles the Bearing 2 Information Win dow through NAV2
45. acy 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A Warnings Cautions amp Notes GARMIN WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarm
46. aezey wy wio gt AeN 346 uones do euuouqy 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Abnormal Operation Faza Index Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT GPS NAV LOST Loss of GPS navigation Position error Message Comments GPS NAV LOST Loss of GPS naviga Loss of GPS navigation due to insufficient satel tion Insufficient satellites lites Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail f Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach 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 AUTO 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
47. age 6 2 4 puezey s n ze 4 ipuonippy uones do Jewuouqy SM V unuuy xipuaddy x pul 190 00324 09 Rev A 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 Z Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 sia s u uinnsu 444 W0 gt AeN sub 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 41 a buluueld nf 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 Gj 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Tur
48. av Com Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Abnormal Operation Azza k Index Annunciations amp Alerts A GARMIN GMA 1347 MESSAGE ADVISORIES Message GMAT FAIL GMA1 is inoperative The audio panel self test has detected a failure Comments 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 f 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 61000 system should be serviced when possible GIA 63 MESSAGE ADVISORIES Message GIA1 CONFIG GIA1 config error Config service 0 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 contig error Config service req d The GIA1 and or GIA2 have an error in the audio GIA2 CONFIG GIA2 audio config
49. base 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 MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced 64 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Chartview database error exists Comments The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a 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 Aviation database version mismatch Xtalk is of
50. ccsssssscsssssscesssssseesssssseesssnsceessssscessssnseeesssnsceesssnsceesssnateen 53 Abnormal COM Operation s s s s s s s s s atenn arenar rrt 53 Hazard Displays with Loss of GPS 5 53 Unusual Attitudes 2 scscsasdoucusdiisdsakunasusnndlusudandinelaininwaaie 54 Dead Reckoning c cccccscsssssssssssssescssssescsssssscccsssssceessssseessssssseesnsssceesnsceesnceesreessens 54 i Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Tibleof Contents ANNUNCIATIONS amp LL 57 WARNING Annunciation aerieni 57 CAUTION Annunciation 57 Alert Message ECS Alerts cee r G Terrain SVS Alerts na 59 Terrain SVS System Status 6 ss s s s si s si 59 TANS Alerts ia sedis at eed ret Seba Ada RUR SAZI dames 60 TAWS System Status Annunciations s s s s s s si s s si s s 61 Volce Alertsi ane Pastel teeth SA al ete oa SL tee uu 62 MFD amp PFD Message Advisories 62 Database Message Ad
51. e 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 desired 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 givin
52. e Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position 94 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Abnormal Operation NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure 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 WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become
53. e remaining fuel quantity in 1 gallon increments Press to reset fuel to full Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN DCLTR 3 SHVV CHRT CHKLIST 190 00324 09 Rev A TERRAIN AIRWAYS STRMSCP NEXRAD XM LING BACK Appendix Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map fea tures visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything ex cept the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists 85 Garm
54. ected radios pilot copilot passengers music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music Nav Com XPDR Audio Panel s u umnnsu 52 olpny 4aqax 93 smo AeN su jy uoresado s n e 4 4 APN 5640 junuuy leuuouqy leuonippv xipuaddy Wil 2 GARMIN Nav Com XPDR Audio Panel syu wun su sub 59 ipnv uqax u102 AEN SodV AeN Sd5 Buruuejd Blank Page 6 2 4 puezey sainjea4 Jeuolppy uonesado Jewuouqy SM V unuuy xipuaddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 14 A GARMIN 265 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 A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active
55. en 49 L Lightning 37 38 80 M Map panning 39 Message advisories 62 78 MET 58 METAR 39 Minimums 62 Mistrim 58 Mixture 8 9 MKR MUTE 12 Mode 83 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F Index ndex 1 saunqea4 aoueplony s snp olq buluueld APN 5640 2 olpny uqax 913 syu wnysu Jeuonippy paezey Wij wio gt AeN 4613 jeuuouqy su jy unuuy iz Ta Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts EA Appena A GARMIN Mode selection softkeys 11 TAVVS 44 45 46 59 60 61 Multi Function Display MFD TAVVS B 44 Softkeys 84 Terrain 42 43 44 65 80 84 85 Terrain SVS 43 44 N Timer 75 NACO 49 Topographical data 80 84 NAV 12 Traffic 37 41 84 NAV1 1 12 Traffic Advisory 62 NAV2 1 12 Traffic advisory 40 Navigation database 21 22 Traffic map page 41 42 NEXRAD 39 40 80 85 Transponder 11 82 83 0 V OBS 2 Vertical speed guidance 22 Obstacles 65 70 Vertical track 62 Overspeed Protection 16 VNV 19 54 77 Vspeed 2 P W Pathways 47 WAAS 70 R Weather data link page 39 Reversionary mode 53 Wind data 81 ROC 59 60 61 X 5 lightning 80 85 SafeTaxi 48 XM weather 39 Store Flight Plan 29 Stormscope lightning data 37 38 80 Strike 37 Strike mode 38 SVS 47 78 Synthetic Vision System
56. en turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS 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 09 Rev A A GARMIN Flight Instruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Tum the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS a 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key
57. ess 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 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 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 A
58. ete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin key NavData is a registered trademark of Jeppesen Inc Stormscope is a registered tradema of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc March 2008 190 00324 09 Rev A Printed in the U S A A Warnings Cautions amp Notes GARMIN WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G1000 Terrain Proximity 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 Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as t
59. evator Mistrim Up Elevator Mistrim Down Aileron Mistrim Left Aileron Mistrim Right Preflight Test A con ili app top ndition has developed causing the pitch vo to provide a sustained force Be prepared app control wheel force upon autopi ot disconnect y nose down ot disconnect dition has developed causing the pitch o to provide a sustained force Be prepared y Nose up control wheel force upon A condition has developed causing the roll servo top m x top Performing preflight system com Preflight system test has fa rovide a sustained left slip skid indicator is centered n maxi imum fuel imbalance i A condition has developed rovide a sustained righ slip skid indicator is center 4 0 C mum fuel imbalance kE ce Ensure the and observe any ts ausing the roll servo orce Ensure the ed and observe any im its test Upon pletion the aural alert will be heard Garmin G1000 Cockpit Reference Guide for the DA40 40F iled 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts TERRAIN SVS ALERTS PFD MFD Alert Type TERRAIN SVS MFD Aural yP Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN Waring Terrain Clearance Warning RTC Terrain Imminent Terrain Impact TERRAIN Warning Terrain Warning ITI Terrain
60. ey Turn the small FMS Knob to select Inhibit Terrain Press the ENT Key Enable Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey 1 2 3 Or While the Terrain SVS Page is displayed press the MENU Key Turn the small FMS Knob to select Enable Terrain Press the ENT Key NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL 44 NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK is heard Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN Hazard avoidance Display Terrain on the TAWS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS Page
61. f The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays DB MISMATCH Aviation database type mismatch Xtalk is off The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Install correct aviation database type in all displays DB MISMATCH Terrain database version mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays 190 00324 09 Rev A 65 Garmin G1000 Cockpit Reference Guide for the DA40 40F s m ie q UED OAV s mp old buluueld ACN 540 52 44 sia 5149 011115 2 wy wio gt Aen 346 uonesado jewouqy a 5 x pul Flight Instruments Additional Hazard Flight N
62. g Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old NE Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 With the Weather Group selected press the ENT Key The cursor flashes on STRMSCP LING 2 Tum the large FMS Knob to select STRMSCP MODE 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 37 s uawin ysu 3461 a AeN 540 5247 olpny uqax 5 u102 AEN buluueld Wil 2 2 uones do saunyea4 junuuy leuuouqy leuonippv xipuaddy xe 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 38 3 Turn the small FMS Knob to display the Cell Strike window 4 Turn either FMS Knob to select Cell or Strike Press the ENT Key 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 Press the MENU Key with the Navigation Map Page displayed 2 either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes
63. g 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 database 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 09 Rev A GARMI N slight Planning 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 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 Po
64. he 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN 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
65. he 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 aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not
66. hen finished to remove the Chart Setup Menu RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 2 3 Turn the large FMS Knob to select the Auxiliary Page Group Turn the small FMS Knob to select the displayed AUX XM Information Page 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 50 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Features 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 Press the FMS Knob to
67. highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 While on the XM Radio Page 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 preset channels 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F x pu ddy su jy uoresado s n e 4 aoueplony s snp od buluueld APN 5640 yi olpny uqax sia siu uinnsu junuuy Jewuouqy Jeuonippy puezey nufiu wio gt AeN fila x pul Nav Com XPDR Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN 52 3 Press any one of t
68. ight Director Activation 755 5 ED nen tania then Gia 2 22 6 Lateral 5 7 9 Direct to Navigation s s s s s s sss s s ssss s ss s s isss s ssis 9 Activate a Stored Flight Plan s s s s s s s s s s s l 20 Activate a Flight Plan Leg ccccccucssssssssssssssssssssssssssnessssnseessssvessssnnsessssvessssnenss 20 Stop Navigating a Flight 755 21 Vertical Navigation VNAV s s s s s s s s s s s s 21 FLIGHT PLANNING s s s s s sil 23 osas ss 23 Create a New User Waypoint 24 Delete a User Vlaypoint s s s s s sss s sss s sss s s s 25 Create a New Flight Plan 6
69. ight 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 KIXD KDFW KARLA COVIE LEMYN RIVET iaf DRAAK INWOD MENOL faf RW17L map 930FT ZA AL T BMK unla S aroe White 22177 9 NM 12400FT oxi 7h aa nan 1 Large Lig E iz Bluc Text Approach KDFW RNAY 111 6 5 LPY 259 18 5NM agg mall Lig 176 3 3MM Blue Text 176 3 2NM a Smal m ese Blue Subdued 176 3 9NM Text 176 5 3NM A Small White Text 174 8NM with Altitude Restriction Bar POLKE 190 00324 09 Rev A S L M Cross AT or ABOVE 5 000 fi VAC B Cross AT 2 300 ft Cinn 141 Cross AT or BELOW 3 000 ft Garmin G1000 Cockpit Reference Guide for the DA40 40F s uawin ysu sub m 5 44 Wi0 gt AeN 11 su jy uoresado s n e 4 aoueplony Huluuelg junuuy leuuouqy leuonippv 2 Wfil4 x pu ddy x pul Nav Com XPDR Audio GPS Nav AFCS Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures ar
70. ilability of SafeTaxi ChartView or FliteCharts in electronic form it is still advisable to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams aid in following ground control instructions by accurately displaying the aircraft position on the map in relation to taxiways ramps runways terminals and services This database is updated on a 56 day cycle 48 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Additional Features ChartView ChartView resemble
71. in environment disposal isp V ARNING Because of anomalies in the earth s magnetic field operating the G1000 within the following areas could result in loss of reliable attitude and heading indications North of 70 North latitude and south of 70 South latitude An area north of 65 North latitude between longitude 75 West and 120 West An area south of 55 South latitude between longitude 120 East and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules
72. in G1000 Cockpit Reference Guide for the DA40 40F sainqeay aoueplony 4 APN 540 yi olpny uqax sia syu wnysu Jeuonippy paezey T TR wio gt AeN 4613 Jeuuougy suealy unuuy E kea GARMIN Appendix s u uin sul sub 59 uio gt AeN 52 AeN 5492 Buruuejd bila Blank Page 6 2 4 puezey s n ze 4 ipuonippy uones do Jewuouqy su jy junuuy xipuaddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 86 A GARMIN A Activate a flight plan 20 Active Channel 50 ADF 11 12 54 81 82 AHRS 73 74 Airport Signs 47 48 Airways 85 AP 58 Audio panel controls NAV1 NAV2 12 Autopilot 58 Barometric Altitude Minimums 3 Barometric pressure 82 C CDI 1 12 76 Cell 37 38 Cell mode 38 Channel Presets 51 ChartView 48 49 Clearance player 12 Clearance Recorder 12 Code selection softkeys 11 COM 12 53 D DCLIR Softkey 48 Dead Reckoning 54 Dedutter 54 79 85 Direct to 19 DME 11 12 DR mode 54 55 56 E Edit a flight plan 29 Enable Terrain 44 Endurance 6 7 F FD 58 Flight Director 15 Flight path marker 47 FliteCharts 48 49 Frequency Transfer 12 Fuel remaining 6 7 Fuel used 6 7 H Horizon heading 47 Inhibit 44 45 Inhibit TAVVS 45 Inhibit Terrain 44 Inset Map 79 80 IOI 59 60 61 J Jeppes
73. increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function is not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 55 oIpny YddX 99 siu u n sul WO gt AeN S24V aoueplony s mp oold APN 540 2 s m e q euonippv sual junuuy xipuaddy x pul 346 Nav Com XPDR Audio Hazard Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMI
74. ining in 1 gallon increments RST FUEL Resets the fuel remaining to 40 gallons ACN 540 S24V buluueld Wil EIS ENGINE 123 800 TEMPERATURE ELECTRICAL ae 1552 1616 1634 1652 40 7 1700 Y 1500 1500 1400 1300 1 r 7 4 aoueplony 2 s m ie q OIL PSI lt EA FLOW GPH SF 75 0 13 2 FUEL CALCULATOR 4 z GALLONS REMAIN 400 5 GALLONS USED 09 Fuel 25 ENDURANCE 3 01 Totalizer RANGE NH 303 Calculations su jy unuuy TOTAL TIME IN SERVICE Aircraft 0 0 HRS Total Time in Service y l L FUEL QTY GAL DEC FUEL INC FUEL RST FUEL xipuaddy EIS Display DA40F x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A Engine Indication System GARMIN ENGINE LEANING While viewing the EIS ENGINE Page press the LEAN Softkey 2 2 s SE 25 TE 2 As the mixture is leaned one of the cylinders 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 gs 123 808 _ Cylinder Peak Temperature y 4 VOLTS HAN IN HG PH 5 28 0 2 24 3 I 1st Cylinder 5 si Peak OIL i s R nu rie ndicates 2 Se M Difference 410 410 11 Betwee
75. irection of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 35 S24V olpny qadx 59 siu unnsul Huo2 AEN ACN 540 buluueld su jy uoresado s n e 4 aoueplony junuuy leuuouqy jeuonppy xipuaddy x pul 346 puezey Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures 0000002 GARMIN ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight A
76. ition with alternate navigation sources TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced STRMSCP FAIL Stormscope has failed Stormscope has failed The G1000 system should be serviced 190 00324 09 Rev A 77 Garmin 61000 Cockpit Reference Guide for the DA40 40F s m ie q uepI ony s mp old buluueld ACN 540 92 04 sia s u u nn sul paezey Wila wio gt AeN 346 uones do euuouqy 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Appendix K Index Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message FAILED PATH A data path has failed Comments A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles SVS SVS DISABLED Out of available terrain region The GDU 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 Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Te
77. ix 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 777 displayed in the Selected Altitude ALTS Armed window Altitude Hold x ALT Key ALT nnnnn rr 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 airspeed in IAS while the aircraft is dimbing descending to the Selected PEN S nn Altitude VNAV Captures and tracks the VNAV flight VNV Ke VPTH GDU 1044 only path VNAV Target Altitude 1 AFCS armed to capture the altitude Armed GDU 1044 displayed in the VNAV Target a ALTV only Altitude window Glidepath WAAS only Cap ures and tracks the WAAS GP glidepath on approach ibn Captures and tracks the ILS Glideslope j GS glideslope on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA Switch and wings level in the air 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 Alti
78. kpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Fesord f 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 Added 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 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F RR 1 A Record of Revision
79. me Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G1000 system should be serviced PFD1 VOLTAGE 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 aviation database error exists database error exists PFD1 DB ERR PFD1 aviation The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists The MFD and or PFD detected a failure in the basemap database 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 63 s m ie q UED OAV s mp old buluueld ACN 540 52 04 sia s u u nnsul paezey wy wio gt AeN 346 uones do euuouqy 5 x pul Addi
80. n Present 5 5 Peak FUEL CALCULATOR GALLONS REHAIN 40 6 mperature of e irst Peaked GALLONS USED 9 4 Cyl d va p A ENDURANCE 215 y inder g RANGE NH 227 L TOTAL TIME IN SERVICE L FUEL GAL GAL 0 0 HRS Procedures Hazard Avoidance 7 FC 1717 TECFELIM FUELTRST FUEL Leaning to First Peak DA40 shown Annun Abnormal Additional Alerts Operation Features Appendix Index Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A 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 c 58 ox x 2 a 123 808 R Cylinder Pcah ELECTRICAL emperature z ZS 58 HAN IN HG RPH 5 oY 24 3 wi Last Cylinder to 2 f 5 N A PEA Indicates Difference z Ve 418 410 g Between Present 194 75 0 16 a 3 and Peak z FUEL CALCULATOR Temperature of ALLE A 40 2 iy the Last Peaked uSED 38 ENDURANCE 2 23 Cy linder RANGE NH 239 TOTAL TIME E 0 0 HRS buluueld wil DEC FUEL INC FUEL RST FUEL s mp old Leaning to Last Peak DA40 shown aoueplony paezey Pressing the ENGINE Softkey returns the MFD to default operation su jy uoresado s n e 4 junuuy leuuouqy leuonippv xi
81. n 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 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F uoleiado soinjeo4 s mp old jewouqy feuonippy xipuaddy 2 unuuy 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 P
82. ndex Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted Comments A GIA mismatch has been detected where only one is WAAS capable MANIFEST 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 COM1 TEMP 1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE 1 needs service Return unit for repair COM2 SERVICE 2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 1 and or 2 may still be usable The G1000 system should be serviced when possible COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its Operation f the problem persists the G1000 system should be serviced
83. onder mode selection softkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry s u uinnsu 52 olpny 4aqax 53 smo AeN uonesado saunqea4 aoueplony s snp olq buluueld APN 5640 paezey jewuouqy su jy unuuy 3461 3 Press the digit softkeys to enter the code in the code field VVhen entering the code the next key in sequence must be pressed vvithin 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F xipuaddy x pul Flight Instruments Nav Com AFCS XPDR Audi Abnormal Additional Hazard Flight Planning Annun GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN 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 Press the CDI Softkey to select NAV1 VOR1 LOC1 or NAV2 VOR2 LOC2 2 Pressing the NAV1 NAV2 DME or ADF Key on the audio panel selects and deselects the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING
84. ons 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message PTK FAIL Parallel track unavailable bad geometry Comments 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 procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx The selected waypoint xxxx does not use the WGS 84 datum Cross check pos
85. 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 a non n Ev rs mu Press the BACK Softkey to return to the top level softkeys ETT T 7 Tom Tser Tose Yaram STBY ON Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys Displays transponder mode selection softkeys Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations Garmin 61000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN ALT GND VFR CODE 0 7 BKSP IDENT TMR REF NRST ALERTS Appendix Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position
86. ory TA Bs closing rate distance and vertical separation meet TA criteria 26 9 Traffic Advisory Off Scale Annun Alerts Traffic Symbol Description Traffic Information Service TIS Appendix NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use Index 40 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Hazard Avoidance 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 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 Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page G
87. puaddy 190 00324 09 Rev A Garmin 61000 Cockpit Reference Guide for the DA40 40F GARMIN Engine Indication System s u uin sul fila olpny dddX ui0 gt AeN 52 AeN 542 Blank Page buluueld 6 2 4 2 sainjea4 euolppy uonesadg Jewuouqy su jy unuuy x pu ddy x pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 A GARMIN NAV COM TRANSPONDER AUDIO PANEL Nav Com XPDR Audio Panel 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 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 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 ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey to display the transp
88. ress 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 flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 20 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint 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 09 Rev A A GARMIN GPS Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the fl
89. rge FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 Tur the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 25 olpny qqax 53 5349 011115 361 52 s mp old Buruuejd ACN Sd9 nubi su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy paezey xipuaddy xe 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 A GARMIN CREATE A NEW FLIGHT PLAN 26 NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Using the MFD 1 Press the FPL Key 2 Turn the small FMS Knob to display the Flight Plan Catalog Page 3 Press the NEW Softkey to display a blank flight plan for the first empty storage location 4 Turn the small FMS Knob to display the Waypoint Information Window 5 Enter the identifier of the departure wa
90. roup ACN SdD S24V olpny xqax sia su uini sul wio gt Aen 164 buluueld s mp old paezey s m ie q 2 Turn the small FMS Knob to select the Traffic Page OPERATING is displayed in the Traffic Mode field 3 Press the ALT MODE Softkey to dhange 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 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 5 Press the MUTE Softkey to mute TAS voice alerts 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F uones do jeuuouqy su jy unuuy xipuaddy x pul A Hazard Avoidance GARMIN Displaying Traffic on the Navigation Map Flight Instruments 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 TERRAIN AND OBSTACLE PROXIMITY Nav Com XPDR Audio NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south AFCS Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group GPS Nav 2 Tum the small FMS Knob to select the last rectangular page icon 3 If de
91. rrain 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 78 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN Appendix APPENDIX syuawny suj 16114 PFD SOFTKEY MAP 993 optional Vaser E 1 CS Poe Ge ST fer ST ETS noes wv 7 uu m olpny qqax wi0 gt AeN CDI NAV2 S24V Top Level PFD Softkeys ACN 540 optional CS 7 V one Ge fer faner OT TG Al FE Hu HU HU E Hu Eu D optional optional optional 1572 ero 1257 E e TTesee ALERTS AA r s uu r buluueld 2 Press the BACK Softkey to return to the top level softkeys aoueplony paezey Inset Map Softkeys s mie q INSET Displays Inset Map in PFD lower left corner g OFF Removes Inset Map 2 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 o xe pul 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 19 Flight Instruments Ann
92. s GARMIN Part Number Change Summary 190 00324 09 Added Synthetic Vision feature and GDU 9 01 parameters fen Date of Revision Affected Pages March 2008 Production release RR 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Tibleof Contents FLIGHT INSTRUMENTS s ss s s s 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units VVv 1 Change Navigation Sources s s s s s ss s sss s sss s sssss n 1 Enable Disable OBS Mode While Navigating With 6 5 5 2 Generic TIME icena aaa DABUL eeu one 2 Configure Vspeed BUGS cccccccccssssssssssssssssssesssssssssvssssssssssssssssseessssvsssscesssssssssecesssssssssees 2 Set Barometric Minimum Descent Altitude 10er 3 Displaying Wind Data 7555 3 Changing HSI Format cccccccccsusssssssscsssssssccssssssecsssssessssnscessnssscessenaceesnssssessesneessens 3 ENGINE INDICATION 5 9
93. s the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of National Aeronautical Charting Office NACO terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 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 Press the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs 3 Press the GO BACK Softkey to return to the previous page View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the depar
94. sired 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 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 1007 below current aircraft altitude Flight Planning Hazard Avoidance Procedures Terrain Obstade between 100 and 1000 below current aircraft altitude Additional Features Terrain Obstacle is more than 1000 below aircraft altitude Black Abnormal Operation Displaying Terrain and Obstacles on the Navigation Map Annun Alerts 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Appendix Index 4 Garmin 61000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Avoidance TERRAIN SVS NOTE Terrain SVS is only available when the Synthetic Vision System SVS option is installed and the TAWS option has not been installed NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Display Terrain on the TERRAIN SVS Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to selec
95. sition 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 waypoints identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint c Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a 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 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 23 olpny qqax 93 S3u umnnsul WO gt AEN 161 523 s mp old Buruuejd ACN Sd9 nubi su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 6 7 8 9 A GARMIN
96. sor 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 29 olpny qqax 93 5349 001115 ub S24V s mp old Buruuejd ACN 540 nubi su jy uoresado s n e 4 aoueplony unuuy euuouqy Jeuonippy paezey 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 2 3 4 5 A GARMIN 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 large FMS Knob to highlight the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor
97. t Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 39 ARN Sd9 so4dV olpny qqax 93 5149 001 15 u102 AEN 3461 wld s mp old paezey SH ly uones do saunyea4 junuuy leunouqy leuonippv xipuaddy A Hazard Avoidance GARMIN Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Flight Instruments Echo Top Cloud Top and Echo Top Mutually Exclusive Cell Movement City Forecast Freezing Levels Cyclone Warnings Nav Com XPDR Audio Np wh a a Sih x gt q AFCS XM Lightning METARs Surface Analysis County VVarnings Cloud Top SIGMETs AIRMETs Winds Aloft GPS Nav TRAFFIC SYSTEMS e If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed e Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST Flight Planning and ALT MODE softkeys are displayed 1 Traffic Symbol Description 2 Non Threat Traffic 28 intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA 85 intruder is within 5 nm and less than 1200 vertical separation 5 O Taffic Advis
98. t reduced power If the problem Reducing transmitter power persists the G1000 system should be serviced COM1 SERVICE COMI needs service The system has detected a failure in 1 Return unit for repair and or COM2 COM1 and or COM2 may still be COM2 SERVICE COM2 needs service usable The 61000 system should be serviced Return unit for repair when possible COM1 PTT 1 push to talk key is The 1 and or 2 external push to talk stuck switch is stuck in the enable or pressed COM2 PTT COM2 push to talk key is position Press the PTT switch again to cycle its stuck operation If the problem persists the 61000 system should be serviced COM1 RMT XFR 1 remote The COM1 and or COM transfer switch is stuck transfer key is stuck in the enabled or pressed position Press the COM2 RMT XFR COM remote transfer switch again to cycle its operation If the transfer key is stuck problem persists the G1000 system should be serviced RAIM UNAVAIL RAIM is not available GPS satellite coverage is insufficient to perform from FAF to MAP waypoints Receiver Autonomous Integrity Monitoring RAIM from the FAF to the MAP waypoints LOI GPS integrity lost Crosscheck with bd other NAV Loss of GPS integrity monitoring 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 67 s n ze uepIony s mp old buluueld ACN 540 52 404 sia s u u nnsul p
99. t the Terrain SVS Page 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 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 1007 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 2 3 While the Terrain SVS Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key 43 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F ARN Sd9 52 olpny qqax 53 5149 011115 u102 AEN 3461 buluueld wld s mp old paezey su jy uonesado s n e 4 Junuuy jewuouqy xipuaddy Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Terrain SVS Inhibit Inhibit Terrain While the Terrain SVS Page is displayed press the INHIBIT Softkey 1 2 3 Or Press the MENU K
100. tional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Abnormal Operation Append Ee Index Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists Comments 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 database missing PFD1 DB ERR PFD1 terrain 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 LRU 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 data
101. 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 ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CD for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 76 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciati
102. tude Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A 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 iH Selected Heading Key we Navigation GPS GPS Navigation VOR Enroute Captures and tracks the a VOR Mode selected navigation source Navigation LOC Glideslope GPS VOR LOC NAV LOC 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 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 17 sia olpny qaax wi0 gt AeN ACN 540 su jy uoresado s n e 4 aoueplony 4 junuuy leuuouqy leuonippv xipuaddy x pul 3463 paezey GARMIN AFCS s tin sul sb 59 wi0 gt AeN s24v AeN Sd5 Buruuejd bila Blank P
103. ture 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 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 49 suj 346 3 xipuaddy SHV uonesado soinjeo4 UED OAV s mp old buluueld ACN Sd9 52 404 513 junuuy jeunouqy Lea 2 Wil u102 AEN 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 Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options In Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity Press the FMS Knob w
104. uel remaining to 40 gallons in aircraft with standard fuel tanks Resets the fuel remaining to 50 gallons in aircraft with extended range fuel tanks ETS ENGINE 123 888 TEMPERATURE ELECTRICAL 1526 1526 AMPS 1508 49 EST F 1490 1700 Y 1622 x 1 2 3 4 y 4 7 194 75 8 12 2 25 0 FUEL CALCULATOR GALLONS REMAIN 2 Fuel ERR GALLONS USED 7 li 5 X JS ol ENDURANCE k m cae 4 A a Calculations 1 1 Ai i SERV eS TOTAL TIME IN SERVICE ircraft GAL GAL 1 157 2 HRS Total Time in Service LEAN DEC FUEL INC FUEL RST FUEL EIS Display DA40 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN ____Engine Indication System DA40F ENGINE DISPLAY Pressing the ENGINE Softkey displays the EIS ENGINE Page s uawin ysu sub 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 z Be Bo 22 a3 o The following softkeys allow for adjustment of the remaining fuel quantity DEC FUEL Allows the pilot to decrease the gallons of fuel remaining GALLONS REMAIN in 1 gallon increments INC FUEL Allows the pilot to increase the gallons of fuel rema
105. uide for the DA40 40F 190 00324 09 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations 8 Alerts 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 The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced 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 GRS 77 MESSAGE ADVISORIES CONT Message Comments 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 MANIF
106. un Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Index A Appendix GARMIN TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map vvindovv 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 vveather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature vm ou rs a ee Ee Verir ae CS nn nnn Select the STD BARO or BACK Softkey to return to the top level softkeys PFD Configuration Softkeys 80 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN PFD SYN VIS DFLTS WIND DME BRGI HSI FRMT 190 00324 09 Rev A PATHWAY SYN TERR HRZN HDG APTSIGNS OPIN 1 OPTN 2 OPTN 3 OFF 360 HSI ARC HSI Appendix Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the
107. uonesado jewouqy 5 x pul Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Abnormal Operation Hiram Index Annunciations amp Alerts A GARMIN VOICE ALERTS Voice Alert Description Minimums minimums 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 MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings XTALK ERROR A flight display crosstalk error has occurred The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired The MFD and PFDs are not communicating with each other The G1000 system should be serviced
108. visories s s s s s s sss s ssss sss 63 GMA 1347 Message AdVISO IGS csccsccsssssccssssessesssssssessssscessssssceesssssceesssnscessnsnateen 66 GIA 63 Message Advisories s s ss s s s s sss s sss isss s ssss GIA 63W Message Advisories GEA 71 Message AdVISOLIES cscccccssssssssssssscesssssssesssssccesssssseesssnsceessssscessnsnsceesssnetsen GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories GDL 69A Message Advisories GDC 74A Message Advisories Miscellaneous Message AdViSOFIGS csccsccssesccsssescsssssessessssssessnssssessnsssseessseteen 75 APPENDIX D a iba PFD Softkey Map MFD Softkey Map INDEX ects Index 1 190 00324 09 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F A Table of Contents GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3
109. ware mismatch communication halted The GDL 69 has incorrect software installed The G1000 system 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 74 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored
110. ypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identifier for each additional flight plan waypoint 8 When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Using the PFD 1 2 3 4 5 6 7 NOTE If a flight plan is active an additional flight plan cannot be entered using the PFD Press the FPL Key Turn the small FMS Knob to display the Waypoint Information Page Turn the small FMS Knob to enter the first letter of the destination waypoint identifier Turn the large FMS Knob to the right to move the cursor to the next character position Repeat step 3 and 4 to spell out the rest of the waypoint identifier Press the ENT Key and the cursor is now ready for entering of the next flight plan waypoint Repeat steps 3 through 6 to enter the identifier for each additional flight plan waypoint Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 09 Rev A A GARMIN Flight Planning 8 Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the

Garmin Software Version 0321.19 Cockpit Reference Guide

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