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Garmin DA40F User's Manual

1. 10 10 Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC 10 10 Imminent Terrain Impact ITI and Imminent DOSTAG C1NDACEHIO viciszeaisscannmersnanasinansean 10 10 Premature Descent Alert PDA scn 10 10 Excessive Descent Rate Alert EDR ou 10 10 Negative Climb Rate After TakeotfAlert NCR 10 11 Five Hundred Aural Alert ccscssssssesssssessseseeenes 10 11 Displaying Terrain and Obstacles on the NAVIGATION Mapica ii 10 11 POP DAT eaaa 10 12 TAWS Alerts SUMMAN dscrmssamenssanvenscnnoeascisseniaanes 10 13 Alert AUNMGIELIONS zeccs naaistonaciatansaee see dacruvasoissont 10 14 SECTION 11 ABNORMAL OPERATION 11 1 11 1 Reversionary Mode 0 cccccccsee cea 11 1 11 2 Abnormal COM Operation 0 0 0 0 00 11 2 11 3 Unusual Attitudes cscs 11 2 11 4 Hazard Displays with Loss of GPS Position 11 2 SECTION 12 ANNUNCIATIONS amp ALERTS 12 1 12 1 Alert Level Definitions 0 0 0 0 c ce 12 2 12 2 Aircraft Alerts ccc cesses teases 12 3 WARNING AIGNS ssccicistcatlincaincoeorieescansitatentimai 12 3 CAUTION PCTS lt 2 2 ssisiicnsaseuiveseseesspucvcssenrenanaucsians 12 3 Message Advisory Alerts c ssssssssesssesssessesseesneeen 12 3 12 3 AECS AlOUtS i ssssicciaicatissarassrinaacniehakoruncatnacene 12 4 System Status Annunciation 12 4 12 4 TAWS ALERTS 0 ccc eeteeteteeenees 12 5 TAWS System Status
2. XPOR IDENT TMR REF NRST AL Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL Approach Mode GPS VAPP or LOC The Approach mode acquires and tracks the selected navigation receiver on the HSI GPS VOR or LOC This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach The Approach mode provides greater sensitivity for VOR tracking than Navigation mode and allows the autopilot to fly an ILS approach with a glideslope NOTE While using Approach mode the Glideslope mode is automatically armed when LOC mode is selected on the HSI Approach Mode is active newt 111 398 114 18 SoC wer Flight Director command bars indicating descent on localizer glideslope path LOC2 is the active navigation receiver on the HSI If the CDI is not centered deviation gt 1 dot when the Approach mode is selected the mode is automatically armed The armed annunciation appears in white to the left of the active roll axis mode See the Example Procedures Using AFCS section for more information Go Around GA Go Around mode maintains a wings level 7 degree nose up attitude for instances where the pilot wishes to execute a missed approach or go around Figure 6 14 depicts the Go Around mode on the PFD Glideslope is active 118 208 136 975 121 358 cons OOMZ Figure 6 18 Approach Mode Garmin G1000 Cockpit Reference G
3. FLIGHT PLANNING already stored in memory by number Turn the large FMS Knob to highlight the LEG field and turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 will display an active flight plan If an active flight plan is selected REM will be an available option to display planning data for the remainder of the flight plan NOTE The Page Mode must be set to MANUAL to perform the following steps 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 Turn the FMS Knobs to enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings Turn the FMS Knobs to 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 on board field Turn the FMS Knobs to modify the fuel on board Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made in GAL REM on the EIS System Page The flashing cursor moves to the calibrated airspeed field Turn the FMS Knobs to enter a calibrated airspeed Press the ENT K
4. Information Window GPS Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window ADF Displays ADF waypoint frequency in the BRG1 Information Window OFF Removes the BRG1 Information Window 360 HSI Press to display the 360 compass rose ARC HSI Press to display the 140 viewable arc indicator for the corresponding source and displaying the the appropriate information NAV2 Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window GPS Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window ADF Displays ADF waypoint frequency in the BRG2 Information Window OFF Removes the BRG2 Information Window Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW STD BARO Press to set the barometric pressure to in the U S A refer to ICAO standards for VFR 29 92 inches of mercury 1013 hPa by pressing codes in other countries the METRIC Softkey CODE Press to display transponder code selection BACK Press to return to the previous level soltkeys 0 7 softkeys 0 through 7 Press numbers to enter code ALERTS Press to display the Alerts Window noo ND Press the BACK Softkey to return to the top level softkeys A Press the BACK Softkey to return to the top level softkeys DAND D Figure 1 5 PFD Softkey Flow Chart 3 OBS Press to sel
5. 10 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 11 ABNORMAL OPERATION 11 1 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 Minimal navigation capability is available on the reversionary mode display LEA i SECTION 11 ABNORMAL OPERATION Reversionary display mode can also be manually activated by the pilot if the system fails to detect a display problem The reversionary mode is activated manually by pressing the red DISPLAY BACKUP button on the bottom of the audio panel GMA 1347 Pressing the red DISPLAY BACKUP button again deactivates reversionary mode A NOTE The Diamond DA40 Airplane Flight Manual and Flight Manual Supplement always takes precedence over the information found in this section Normal MFD Display MFD in Reversionary Mode Figure 11 1 G1000 Reversionary Mode Failed PFD Garmin G1000 Cockpit Reference Guide for the DA40 40F 11 1 SECTION 11 ABNORMAL OPERATION 11 2 11 2 ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a dual display failure the emergency frequency 121 5
6. Box above the Altimeter Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in 6 seconds if the current rate of vertical speed is maintained Barometric Setting Box To set barometric pressure turn the BARO Knob to select the desired setting Altitude Alerting Within 1000 ft K 4000 Within 200 ft Deviation of 200 ft Figure 2 8 Altitude Alerting Visual Annunciations Visual annunciations appear in the Selected Altitude Box Whenever the Selected Altitude is changed the Altitude Alerter is reset The Altitude Alerter is independent of the Automatic Flight Control System An aural tone is heard when the aircraft is within 1000 feet of acquiring the selected altitude or when deviating beyond 200 feet of the acquired selected altitude Barometric Minimum Descent Altitude The desired barometric minimum descent altitude MDA or Decision Height DH can be set in the Timer References Window Visual annunciations alert the pilot when approaching the MDA e When the aircraft altitude descends to within 2500 feet of the MDA setting the Barometric Minimum Box appears with the altitude in light blue text The bug appears on the tape in light blue once in range e When the aircraft passes through 100 feet of the MDA the bug and text turn white e Once the aircraft descends past the MDA the bug and text turn yellow and the aural alert Minimums Minimums is gener
7. GEA1 CONFIG GEA1 configuration The GEA 71 configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GEA1 software mismatch Communication halted BACKUP PATH EIS using backup The GEA 71 is using a backup communication path The G1000 system should be data path serviced when possible The GEA 71 has incorrect sottware installed The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Message Advisories Alerts Window Message Comments o XPDR1 CONFIG XPDR1 contig error The transponder configuration settings do not match those of backup configuration Config service req d memory The G1000 system should be serviced MANIFEST GTX1 software mismatch The transponder has incorrect software installed The G1000 system should be Communication halted serviced BACKUP PATH XPDR1 using backup The 1 transponder is using a backup communications path The G1000 system data path should be serviced when possible GRS 77 Message Advisories Alerts Window Message Comments S AHRS1 TAS AHRS1 not receiving The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS airspeed relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup The
8. amp TRANSPONDER SECTION 4 NAV COM AND TRANSPONDER The NAV COM controls and frequency boxes are located on the Primary Flight Display and the Multi Function Display in the same locations NAV COM Controls NAV Frequency Box COM Frequency Box Controls navi 113 25 118 98 weTKSTL prs 199 095 mre 095 133 000 com NAVZ 110 90 124 388 J20 COMZ j CRS 4 BARO PUSH CAS CTA Z 650A RANGE E SN PIE RA ILEI COI ADF DME XPOR IDENT TMR REF NAST Figure 4 1 G1000 VHF NAV COM Interface PFD Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 1 SECTION 4 NAV COM amp TRANSPONDER Standby NAV Selected NAV Selected COM Standby COM Frequency Field Frequency Frequency Frequency Field nav1 189 98 gt 110 60 Cv TSI 180 Figure 4 2 Frequency Fields Tuning Box Active NAV Active COM Tuning Box Frequency Field Frequency Field 135 108 CoM 3 608 121 900 conz Frequency Transfer Arrow Tuning Box Figure 4 3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH ID Knob SQ Knob Frequency Transfer Key Dual NAV Dual COM Knob Knob Turn to tune in desired frequencies e Press to change tuning box positions Figure 4 4 NAV COM Controls 4 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 1 RADIO STATUS INDICATIONS RX When a COM signal is received a white RX appears by the active COM frequency during signal
9. by CWS in white until the CWS button is released Control Wheel Steering a ROL CHS PIT ALTO Figure 6 8 CWS Annunciation SECTION 6 AUTOMATIC FLIGHT CONTROL 6 4 LOSS OF DATA In general a flashing yellow mode annunciation indicates either the loss of sensor data AHRS ADC or GIA or loss of navigation data VOR LOC or GPS required to compute commands When such a loss occurs the system automatically reverts to the default mode for the affected axis wings level ROL for roll axis PIT for pitch axis The flashing annunciation stops when the pilot presses the affected mode button or selects another mode for the axis If no pilot action is taken the flashing annunciation stops after ten seconds OR Te he Figure 6 9 Loss of VOR Signal 6 5 PITCH AXIS MODES Mode annunciations for active pitch axis modes are shown in green during normal operation Note the Go Around button is not located on the MFD Annunciation PIT AT Altitude Hold ALT nnnnn Fr FIC Fight Level Change FLC nmn xr Glideslope vertical com ponent of Approach GA GoAround The default pitch axis mode is Pitch Hold PIT When no other pitch axis modes are selected this is the active pitch axis mode when the autopilot and or flight director is engaged ALT VS FLC APR GA Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 3 SECTION 6 AUTOMATIC FLIGHT CONTROL Pitch Hold Mode PIT 1 Press the
10. 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 GPS source system should be serviced when possible AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving any or any useful GPS information Check AFMS limita any GPS information tions The G1000 system should be serviced AHRS1 GPS AHRS1 not receiving The 1 AHRS is not receiving backup GPS information The G1000 system should be backup GPS information serviced AHRS1 GPS AHRS1 operating The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be exclusively in no GPS mode serviced MANIFEST GRS1 software mismatch Communication halted BACKUP PATH AHRS1 using backup The 1 AHRS is using a backup communications data path The G1000 system data path should be serviced when possible AHRS1 SRVC AHRS1 Magnetic tield The 1 AHRS earth magnetic field model is out of date Update magnetic field model model needs update when practical GEO LIMITS AHRS1 too far North The aircraft is outside geographical limits for approved AHRS operation Heading is South no magnetic compass flagged as invalid The AHRS has incorrect software installed The G1000 system should be serviced 12 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Message Advisories Alerts Window Message Comments HDG FAULT AHRS1 magnetometer A fault has occurred in the
11. 6 9 Heading indication 2 6 2 7 Heading Select 1 3 1 4 6 9 6 10 Heading Select Mode 6 10 Headset s 5 2 Hijack code 4 5 Horizontal situation indicator 2 5 2 6 Index 1 INDEX HSI 2 5 Hurricanes 10 3 ICAO 4 5 ID 4 3 IDENT function 4 5 Imminent Terrain Impact 10 10 Impact point 10 10 INC FUEL 3 3 Inhibit 10 9 Inhibit TAWS 10 9 INTEG 2 8 Interrogations 4 5 IOI 10 10 10 13 12 5 ITI 10 10 K Key s 1 4 L Lean engine 3 2 Lighted obstacle 10 11 Load approach 8 5 Load a VOR frequency 7 8 Load departure 8 4 Load the frequency for a controlling agency 7 10 Load the nearest ARTCC frequency 7 9 Loss of communication code 4 5 Manual Electric Trim 6 1 MAP 7 1 Map panning 10 3 Marker beacon 2 5 messages 12 1 Message advisories 12 2 12 9 12 17 MET 6 1 6 3 12 4 METAR 10 1 10 3 MFD 1 1 4 4 Military interceptor operations code 4 5 Missed Approach 6 19 Mistrim 12 4 MKR MUTE 5 2 5 4 Mode selection softkeys 4 5 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 2 NAV2 5 2 Navigation 7 1 Navigation Mode 6 11 Navigation status window 2 2 NAV Frequency Window 4 1 NCR 10 11 Nearest Airports Page 7 3 7 5 7 7 7 8 7 9 8 1 Nearest ARTCC amp FSS frequencies 7 9 Negative Climb Rate After Takeoff 10 11 NEXRAD 10 2 0 OBS 2 8 Obstacles 10 11 12 10 12 11 12 12 Operation 5 2 Optional NAV radios 4 3 overspeed 6 2 P Page group icon 1 8 PDA 10 1
12. ANNUNCIAtIONS sssi 12 6 12 5 G1000 System Annunciations 0 0008 12 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F TABLE OF CONTENTS 12 6 G1000 System Message Advisories 12 8 MFD amp PFD Message AdVISOTI S c scscecseesesseesresees 12 9 Database Message AdVISOFES c sscsseseseseeseesen 12 10 GMA 1347 Message Advisories s s s 12 11 GIA 63 Message Advisories c sscesseesssesseesessesseeen 12 11 GEA 71 Message Advisories scessecsceseeseesteeseeseen 12 13 GTX 33 Message Advisories 12 14 GRS 77 Message AVISOLGS scesecsceseessesteeseeseen 12 14 GMU 44 Message Advisories scessseceesseesessesseeen 12 15 GDL 69 Message Advisories 12 15 GDC 74A Message Advisories 12 15 Miscellaneous Message AdVISOFGS c ssseeseerees 12 15 INDER caa Index 1 IV Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi The purpose of this Cockpit Reference Guide is to Function Display MFD and the GMA 1347 Audio Panel provide the pilot a resource with which to find operating System instructions on the major features of the G1000 system ee more easily It is not intended to be a comprehensive A NOTE The pilot should read and thoroughly operating guide Complete operating procedures for the understand the Diam
13. CAUTION Alerts Single Aural Tone Message Advisory Alerts 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 3 SECTION 12 ANNUNCIATIONS amp ALERTS 12 3 AFCS ALERTS System Status Annunciation wv 113 00 110 90 IDD ufr pis ore T 1118 700 cons naV 118 99 I 32 r System Status Annunciation The following alert annunciations appear in the AFCS System Status Annunciation on the PFD Figure 12 5 AFCS System Status Annunciation Condition Annunciation Description o Pitch Failure PTCH Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative AP TRIM Switch Stuck PTRM If annunciated when AP is engaged a failure has occurred in the pitch trim system If or Pitch Trim Axis annunciated when AP is not engaged a failed or stuck switch is causing the annunciation Control Failure System Failure AFCS AP and manual electric trim AP TRIM are unavailable FD may still be available Elevator Mistrim Up TCI C A condition has developed causing the pitch servo to provide a sustained force in the nose up direction Elevator Mistrim IFI FE A condition has developed causing the pitch servo to provide a sustained force in the nose D
14. Key to accept Press the FMS Knob to remove the flashing Cursor VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key FLIGHT PLAN KIXD KSTL DTK DIS KIXD KSTL 0877 512 1NH Approoch ILS 30R 2 MOODS inf 127 19 0NH Figure 8 2 Active Flight Plan Window on the PFD ae F Figure 8 3 Active Flight Plan Window on the MFD ACTIVATE A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Figure 8 4 Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and press the ACTIVE Softkey 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 4 ACTIVATE A FLIGHT PLAN LEG 1 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired destination waypoint 2 Press the ACT LEG Softkey using MFD only OR 3 Press the MENU Key select the Activate Leg option trom the page menu and press the ENT Key This step must be used when activating a leg from the PFD 4 With Activate highlighted press the ENT Key KIAH Course 236 from KOJC to KIAB ACTIVATE or CANCEL Figure 8 5 Activate Flight Plan Leg Confi
15. MORE WX Press the MORE WX Softkey to display the following group of softkeys for additional weather control Map SECTION 10 HAZARD AVOIDANCE SFC Pressing the SFC Softkey for Surface Analysis shows current or forecast conditions Forecasts are available for intervals of Current 12 24 36 and 48 hours Press the softkey corresponding to the desired forecast The closest city forecast information is displayed in the legend The display is updated every 12 minutes FRZ LVL Press the FRZ LVL Softkey to display contour lines for freezing levels The display is updated every 12 minutes WIND Press the WIND Softkey to show wind speed and direction at a selected altitude from the ground up to 42 000 feet in 3 000 foot increments After pressing the WIND Softkey press the softkey corresponding to the desired winds aloft altitude The display is updated every 12 minutes COUNTY Pressing the COUNTY Softkey provides specific public awareness and protection weather warnings for Tornado Severe Thunderstorm and Flood conditions provided by the National Weather Service NWS The display is updated every 5 minutes CYCLONE Pressing the CYCLONE Softkey shows the current location of cyclones hurricanes and tropical storms and their projected track at various time intervals The display is updated every 12 minutes Panning Information Weather Data Link Page 1 2 Push in the Joystick to display the panning
16. Navigation c ccseesseesseseessesees 7 2 7 3 Airport Information 0 0 cece 7 3 Select the Airport Information Page 7 3 Enter a Waypoint Facility Name or City Location 7 3 Access RUNWAY Information 1 3 Access Frequency Information 1 3 7 4 Intersection Information 0 0 cce 7 4 Select the Intersection Information Page sceseseen 7 4 Access Information on an Intersection 1 4 7 5 NDB Information 0 0 0ccccccc esses 7 4 Select the NDB Information PaQe csscesecseeseeeeseen 7 4 View Information on a Specific NDB seescesseesveeseeee 7 4 7 6 VOR Information 0 00 0ccccccceseeseeeeeen 7 5 Select the VOR Information Page cssesesecsesseseeen 7 5 Access Information on a VOR sess 1 5 7 7 User Waypoint Information Page 7 5 7 8 Nearest Airports ccs essere 7 5 Nearest Airport Information on the MFD uu 7 5 Select the Nearest Airports Page sessessessessesseeee 7 5 Access Information on a Specific Airport 1 5 Access Runway Information for the Selected AIDOT opui e S ETE 7 6 Quickly Tune the COM Transceiver to a Nearby Aport FEGUONGY sei a EEO 1 6 Nearest Airports Information on the PFD 7 6 View Information on a Specific Airport in the List 7 6 Load an Airport COM Frequency into the FCIVE COM orainean E E ER 1 6 7 9 Nearest Intersections ccccsssseseseees l 1 Select the Nearest Int
17. OBSTACLE PULP YATE UP Obstacle Obstacle Pull Up Pull Up Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Reduced Required Obstacle Clearance Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead aanze Reduced Required Terrain Clearance Caution RTC Imminent Terrain Impact Caution ITI Imminent Obstacle Impact Caution IOI Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Too Low Terrain Five Hundred Don t Sink or Too Low Terrain Premature Descent Alert Caution PDA Altitude Callout 500 Excessive Descent Rate Caution EDR Negative Climb Rate Caution NCR Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 13 SECTION 10 HAZARD AVOIDANCE The following system status annunciations may also be issued PFD MFD TAWS Alert Type Page si Aural Message fo Pop Up Alert Annunciation TAWS System Test Fail AWS FA TAWS System Failure No GPS position or excessively degraded TAWS Not Available GPS signal TAWS Availble will be heard when sufficient GPS signal is re established Alert Annunciations mC BA TERRAIN 100F1 100 r i Figure 10 20 Alert Annunciation on the PFD Alert Annunciation Figure 10 19 Alert Annunciation on the TAWS Page
18. Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the third rectangular page icon Access Information on a Specific NDB 1 With the Nearest NDB Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired NDB The remaining information on the Nearest NDB Page pertains to the selected NDB 3 Press the FMS Knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 7 NAVIGATION 7 11 NEAREST VOR Select the Nearest VOR Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fourth rectangular page icon 136 975 ORTH UP eal TABNH 87 GHH TENA TESNH 1121H TIENA TINH THFORHATTON ec PENDLETON PENDLETON OF fies HIGH ALTITUDE 20E kN FREQUENCY eer 114 re Figure 7 13 Nearest VOR Page View Information on the Nearest VOR 1 With the Nearest VOR Page displayed press the VOR Softkey to place the cursor in the NEAREST VOR Box 2 Turn either FMS Knob to select a VOR 3 Press the FMS Knob to remove the flashing Cursor Select and Load a VOR Frequency 1 With the Nearest VOR Page displayed press the FREQ Softkey to highlight the VOR frequency in the FREQUENCY field 2 Press the ENT Key The selected VOR frequency is placed in the NAV standby trequency field 3 Press the F
19. SETUP GROUP Troffic Map Weother On Troff Cie All Traffic Aviation x Land L TSONH mwrr av LOW SANM Figure 10 3 Map Setup Group List 10 2 r TPD SECTION 10 HAZARD XM WEATHER OPTIONAL WARNING XM Weather is not intended to be used for hazardous weather penetration Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Press the MAP Softkey 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 IAP NAVIGATION MAP AINNEAPOLTS TERRAIN Figure 10 4 Navigation Map Page Displaying NEXRAD Weather Displaying METAR and TAF information on the Airport Information Page Display METAR and TAF text on the Airport Information Page 1 2 Turn the large FMS Knob to select the WPT Page Group Turn the small FMS Knob to select the Airport Information Page Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 1 SECTION 10 HAZARD AVOIDANCE 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes NORTH UP AIRPORT WU KMSP PUBLIC MINNEAPOLIS ST PAUL INTL MINNEAPOLIS MN METAR 10000FT FEW Text 1S600FT BROKEN i r AR WEN IDEW POTH ALTIMETER 29 721N _ TAP Text WX Softkey Figure 10 5 METAR and TAF Text Displayed on the Airport Weather In
20. The inactive alerts can be removed from the Alerts Window by pressing the flashing ALERTS Softkey ALERTS Softkey Annunciation When the Alerting System issues an alert the ALERTS Softkey is used as a flashing annunciation to accompany an alert During the alert the ALERTS Softkey assumes a new label consistent with alert level WARNING CAUTION or ADVISORY Pressing the softkey annunciation acknowledges that the pilot is aware of the alert The softkey then returns to the previous ALERTS label The pilot can then press the ALERTS Softkey again to view alert text messages System Annunciations Typically a large red X appears in a window when a related LRU fails or detects invalid data Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 1 SECTION 12 ANNUNCIATIONS amp ALERTS e Audio Alerting System The G1000 system issues audio alert tones when specific system conditions WARNI NG are met See the Alert Levels Definitions section for more information Figure 12 2 WARNING Softkey Annunciation 12 1 ALERT LEVEL DEFINITIONS The G1000 Alerting System as installed in Diamond DA40 aircraft uses three alert levels WARNING This level of alert requires immediate pilot attention A warning alert is accompanied by an annunciation in the Annunciation Window Warning text appearing in the Annunciation Window is RED A warning alert is also accompanied by a flashing WARNING Softkey annunciation as shown i
21. User Waypoint Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the desired field and turn the small FMS Knob to make changes Press the ENT Key to accept the changes Press the FMS Knob to remove the flashing Cursor Delete a User Waypoint 1 Select the User Waypoint Information Page and press MENU to display the User Waypoint Information Page Options or press the DELETE Softkey Turn the large FMS Knob to select Delete User Waypoint and press the ENT Key The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 1 SECTION 8 FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 8 2 1 With the Navigation Map Page displayed push the Joystick to activate the panning function The map pointer is displayed at the present aircraft position Move the Joystick to place the pointer at the desired position Press the ENT Key The User Waypoint Information Page is now displayed with the captured position Turn the FMS Knobs to select a waypoint name Press the ENT Key to accept the selected 8 3 name The first reference waypoint field is highlighted If desired turn the FMS Knobs to enter the identifier of the reference waypoint and the radial and distance to the reference waypoint Press the ENT
22. VNAV Aircraft is approaching VNAV profile Prepare to climb or descend to meet VNAV profile profile ire AE Ag tE Aircraft is approaching target altitude Prepare to level aircraft LOCKED FPL Cannot navigate locked This occurs when the pilot attempts to activate a stored flight plan that contains flight plan locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint muha 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 Special use airspace is ahead of aircraft The aircraft will penetrate the airspace than 10 minutes within 10 minutes than 2 nm not be smooth Prepare for steep turns ahead and expect noticeable course deviations active proach when required 12 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont Alerts Window Message Comments S SLCT AUTOSEQ Select auto The system notities the pilot to select auto sequence mode Press the OBS Sottkey to sequence mode deactivate the OBS mode SLCT FREQ Select appropriate The system notifies the pilot to load the approach frequency for the appropriate NAV frequency tor approach receiver Select the correct frequency for the a
23. WARNINGS CAUTIONS amp NOTES A 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 Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE All references to the Diamond DA40 aircraft equally apply to the Diamond DA4OF aircraft unless otherwise noted NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at Wwww garmin com prop65 Garmin G1000 Cockpit Reference Guide for the DA40 40F RECORD OF REVISIONS Part Number Change Summary 190 00324 00 Initial Release 90 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 90 00324 02 Added WX 500 Stormscope
24. bars are removed from the display Figure 6 2 Command Bars 6 1 MODE ANNUNCIATIONS Mode annunciations are displayed on the PFD Figure 6 3 shows the AFCS Status Box Modes associated with aircraft movement about the roll axis are displayed on the left side Modes associated with aircraft movement about the pitch axis are displayed on the right Armed modes are displayed in white and active modes are displayed in green Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Active Mode Mode Reference Armed Mode Autopilot Status Active Mode Armed Mode Roll Axis Modes Pitch Axis Modes AFCS Status Box nav 113 88 118 9B Trx0 wer DIS DTK TRX 33 000 118 788 com awe 110 90 11x07 735 325 Donz System Status Annuciation v Selected Altitude see Annunciations amp Alerts T E Box Aircraft Attitude Symbol Flight Director Command Bars CDI Ty MSMR GUE ALERTS Figure 6 3 PFD AFCS Display 6 3 AP ENGAGEMENT DISENGAGEMENT When the AP Key is pressed the system engages the autopilot If the flight director is not already active it is also engaged when the AP Key is pressed Autopilot engagement is displayed in the Autopilot Status Field of the AFCS Status Box Autopilot engagement PFI 6 2 OVERSPEED PROTECTION An overspeed annunciation flashing inverse video is displayed above the airspeed tape Figure 6 4 Overspeed Annunciation is indicated by a green AP When
25. error exists PFD1 DB ERR PFD1 basemap database error exists MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crossfill is off version mismatch Xtalk is off Install correct aviation database version in both displays DB MISMATCH Aviation database The PFD and MFD have different aviation database types installed Americas Euro type mismatch Xtalk is off pean etc Crosstill is off Install correct aviation database type in both displays DB MISMATCH Basemap database The PFD and MFD have different basemap database versions installed Crosstill is version mismatch Xtalk is off off Install correct basemap database version in both displays The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the ter rain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If pro
26. is used available procedures for the departure and or arrival airport are automatically suggested If a flight plan is not used the desired airport and the desired procedure may be selected This key selects IFR departure procedures DPs arrival procedures STARs and approaches IAPs from the database and loads them into the active flight plan Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW 16 ENT Key Accepts a menu selection or data entry This key is used to approve an operation or complete data entry It is also used to confirm selections and information entries 17 Dual ALT Knob Sets the selected altitude in the box located above the Altimeter The large knob selects the thousands while the small knob selects the hundreds Altitude Select is used by the Automatic Flight Control System in certain modes in addition to the standard G1000 Altitude Alerter function 18 AP Key Engages disengages the autopilot and flight director Pressing the AP Key activates the flight director and engages the autopilot in the default pitch axis and roll axis modes Pressing the AP Key again disengages the autopilot and deactivates the flight director 19 FD Key Activates deactivates the flight director only Pressing the FD Key turns on the flight director in the default pitch axis and roll axis modes Pressing the FD key again deactivates the flight director and removes the command bars unless th
27. less than one dot the flight director changes from Heading Select to During climb out the autopilot continues to fly the enn oan Navigation Mode and the green annunciation aircraft in Heading Select Mode Airway V107 to Panoche VOR flash Iot bedi VORTAC PXN should now be intercepted LOE Mae E O E Sige intercept the Selected Course 1 Tune the VOR frequency and activate Heading Select Mode J VOR JAP ALT 70007 a Use the CDI Softkey to set the HSI mode to 3 The autopilot continues the turn until the aircraft VOR is established on the Selected Course b Use the CRS Knob to set the Selected Course to 116 Note that at this point the flight director is still in Heading Select Mode and the autopilot continues to fly 070 HDG Mode VOR Armed 4 Panoche VORTAC PXN Figure 6 21 Intercepting a VOR Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 15 SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a GPS Flight Plan If the NAV Key is not pressed within 10 seconds of the HSI mode change the flight 1 Enter Panoche VORTAC PXN and Clovis VORTAC director will roll the wings level and enter Roll CZQ into the GPS flight plan in preparation to Hold Mode intercept this leg 3 Once the flight plan leg is intercepted the 2 Transition trom VOR to GPS Navigation Mode autopilot continues to track GPS guidance to the a Use the CDI Softkey to put the HSI in GPS end of the flight plan m
28. presen Ispldyed on screen cpa eth ae of topography presently ri ha on screen Aircraft altitude pane oh of topography eleva Ground elevation tion uh dis at present aircraft played on screen position Figure 10 10 Topography Scale Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Height is less than Height is less than Height is greater than Height is greater than 1000 AGL 1000 AGL 1000 AGL 1000 AGL Figure 10 11 Obstacle Symbols Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 7 SECTION 10 HAZARD 10 5 TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south A NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation z Displaying Terrain on the TAWS Page a S a VIEW Figure 10 12 TAWS Page 360 View 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS Page 3 If desired 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 Figure 10 13 TAWS Pa
29. reception e TX When a COM radio is transmitting a white TX indication appears to the right of the corresponding COM frequency ID When the Morse code identifier is ON for a NAV radio a white ID indication appears to the lett of the corresponding active NAV frequency The Morse code identifier can be heard if the corresponding NAV radio is selected on the audio panel 118 6808 com TX CON2 121 980 Figure 4 5 Radio Status Indications 4 2 VOLUME VOLUME is displayed in place of the associated radio name i e COMI or NAV2 for two seconds after the volume level is last changed The percentage of maximum volume is displayed in place of the standby frequency selected by the tuning box COM1 135 675 35 VOLUM Figure 4 6 COM Volume Level 4 3 AUTOMATIC SQUELCH Automatic squelch can be disabled for a COM radio by pressing the COM Knob to place the tuning box on the desired COMS standby frequency then by pressing the VOL PUSH SQ Knob 4 4 QUICKLY ACTIVATING 121 500 MHZ Pressing and holding the COM Frequency Transfer SECTION 4 NAV COM amp TRANSPONDER Key for approximately two 2 seconds automatically tunes the selected COM radio to the emergency frequency 4 5 OPTIONAL NAV RADIOS The ADF DME Tuning Window is displayed by pressing the ADF DME Softkey if no ADF is installed the softkey will be labeled DME ADF Radio optional Tune the ADF 1 From the tuning window tur
30. serviced GMA1 CONFIG GMA1 configuration The audio panel configuration settings do not match backup configuration memory error Contig service req d The G1000 system should be serviced MANIFEST GMA1 software The audio panel has incorrect software installed The G1000 system should be mismatch Communication halted serviced GMA1 SERVICE GMA1 needs The audio panel self test has detected a problem in the unit Certain audio functions service Return unit for repair may still be available and the audio panel may still be usable The G1000 system should be serviced when possible BACKUP PATH Audio panel 1 using The 1 audio panel is using a backup communication path The G1000 system backup data path should be serviced when possible GIA 63 Message Advisories Alerts Window Message Comments S GIA1 CONFIG GIA1 configuration error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration GIA2 CONFIG GIA2 configuration memory The G1000 system should be serviced error Config service req d GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to GIA2 COOLING GIA2 temperature warm up to operating temperature too low GIA1 COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 GIA2 COOLING GIA2 over system should be serviced tempera
31. software serviced mismatch Communication halted PFD1 COOLING PFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming MFD1 COOLING MFD1 has poor the display If problem persists the G1000 system should be serviced cooling Reducing power usage PFD1 KEY KEYSTK Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by press MFD1 KEY KEYSTK Key is stuck ing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration The PFD configuration module backup memory has failed The G1000 system should module is inoperative be serviced PFD1 VOLTAGE PFD1 has low volt age Reducing power usage MFD1 VOLTAGE MFD1 has low volt age Reducing power usage The PFD1 voltage is low The G1000 system should be serviced The MFD1 voltage is low The G1000 system should be serviced Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Alerts Window Message Comments o MFD1 DB ERR MFD1 aviation database error exists The MFD and or PFD detected a failure in the aviation database Attempt to reload PFD1 DB ERR PFD aviation the aviation database It problem persists the G1000 system should be serviced database error exists MFD1 DB ERR MFD1 basemap database
32. the DA40 40F SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated navi113 25 118 98 ve DIS RK 133 000 com NAV 116 98 124 308 COH E lann E 7000 Bone Rini ow 6760 Fs aaa Tini 6504 4 he Thi Ne STH 3 INSET FD CDI ADF DME XPDR TENT TMR REF RRT ALERTS O NAV Frequency Box E Turn Rate Indicator 2 Airspeed Indicator Barometric Setting Box G True Airspeed Box Vertical Speed Indicator Heading Box Altimeter Horizontal Situation Indicator 13 Altitude Reference Box 6 Outside Air Temperature Box COM Frequency Box 7 System Time Box 15 Navigation Status Box Transponder Status Box Slip Skid Indicator Attitude Indicator Figure 2 1 Default PFD Information Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 1 SECTION 2 FLIGHT INSTRUMENTS navi 108 00 RE 136 975 118 000 com NAV 117 95 136 975 COH BACKUP PATH Airdoto using Backus doto poth BACKUP PATHAR ate aa T dota path 1799 5 d yo AS ON ADF fxr R cl 06 3246 INSET PFD COI ADF DME XPOR IDENT THR REF NRST CALITO Traffic Annunciation 71 Alerts Window Selected Heading Box Selected Course Box Inset Map C Annunciation Window BRGI Information Window Vertical Deviation Glideslope Indicator DME Information Window Marker Beacon
33. 0 PFD 1 1 4 1 4 4 PIT 6 3 pitch axis modes 6 3 Pitch hold 1 4 6 1 6 3 6 4 6 8 Pitch Hold Mode 6 3 PLAY key 5 4 Premature Descent Alert 10 10 PROC key 1 3 Red pointer 2 3 Remove departure arrival or approach 8 5 Replies 4 5 Reversionary mode 11 1 ROC 10 10 10 13 12 5 Roll Axis Modes 6 2 6 9 Roll Hold 6 9 RST FUEL 3 3 RTC 10 10 RX indicator 4 3 R indication 4 5 S Selected vertical speed 2 5 Severe thunderstorm 10 3 SIGMET 10 3 Slip Skid indicator 2 3 Softkey function MFD 1 4 1 7 Speed ranges 2 3 Squelch 5 3 Store Flight Plan 8 5 System annunciations 12 1 12 6 System message advisories 12 8 T TAS 12 14 TAWS 10 8 10 14 12 5 12 6 TAWS B 10 8 TAWS system test 10 10 Terrain 10 6 10 8 10 12 10 14 11 2 12 10 Tornado 10 3 Traffic advisory 10 14 Traffic map page 10 5 10 6 10 7 10 11 Transponder 4 5 Transponder Status bar 4 5 Trim 6 1 Garmin G1000 Cockpit Reference Guide for the DA40 40F Tropical storms 10 3 TX 4 3 U Unlighted obstacle 10 11 V Vertical Deviation Glideslope indicator 2 5 Vertical navigation profile 8 8 Vertical speed 1 4 2 5 6 3 6 6 Vertical Speed Bug 2 5 Vertical Speed Mode 6 6 VFR code 4 5 VHF 4 1 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 3 VS 1 4 6 3 6 6 Vspeeds 2 3 W WARN 2 8 Warning 12 1 12 2 Weather data link page 10 2 Weather product symbol 10 4 Weather product symbols 10 4 Weather w
34. 0 40F SECTION 7 NAVIGATION The following discussions pertain to the Multi Function Display unless otherwise indicated 7 1 NAVIGATION MAP PAGE Select the MAP Page Group 1 TRAFFIC Turn the large FMS Knob until MAP is highlighted in the Page Group Box in the lower right of the MFD display Turn the small FMS Knob to select the first MAP page indicated by a solid rectangular icon Press the MAP Softkey to display softkeys for the available information which may be displayed on the map WARNING The map display should only be used for situational awareness Any map display indication should be compared with approved navigation sources Figure 7 1 Navigation Map Page SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION Direct to Navigation from the MFD DIRECT TH Identifier aA r Symbol Facility Name MIAMI INTL City MIAMI FL Flight Plan Field Erer Nearest Airport Map Orientation Map of the Selected Waypoint Map Range Bearing Region Distance Latitude Longitude o Activate Field ourse Figure 7 2 MFD Direct to Window Enter a Direct to Destination 1 Press the Direct to G39 Key 2 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 3 Repeat step 2 to spell out the rest of the waypoint identifier 4 Press the ENT Key to confirm the identifier The
35. 00 MHz automatically becomes the active frequency to the pilot through the pilot headset 11 3 UNUSUAL ATTITUDES The PFD will declutter when the aircraft enters an unusual attitude Only the basic primary functions will be displayed in these situations Red extreme pitch warning chevrons pointing toward the horizon are displayed starting at 50 degrees above and 30 degrees below the horizon line Figure 11 2 Extreme Pitch Indication 11 4 HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page will be removed until GPS position is again established The icons in the lower right of the screen indicating the selected functions for display will show an X as shown in Figure 11 3 BUUUOU Figure 11 3 Loss of Hazard Functions with Loss of GPS Position Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS NOTE The Airplane Flight Manual Supplement supersedes information found in this document System Annunciation Red X Annunciation Window GDC1 FAIL GDC1 is inoperative ALTERNATOR Alternator failed Battery is only elec source Alerts Window DOOR OPEN Canopy and or rear door is not closed and locked PITOT OFF Pitot heat is off peor 1200 ALT cl 004653 66 46 ALERTS Softkey Annunciation Figure 12 1 G1000 Alerting System The G1000 Alerting Syst
36. 00 feet above or below for a climb the target altitude white arc an APPR TRG ALT Approaching Target Altitude message is provided The VSR readout on the Navigation Map Page is blanked out at this point SECTION 8 FLIGHT PLANNING ALERTS APPR VPROF Ea aane man T kA profile MFD FAN FAIL The cooling fan PFD FAN FAIL The cooling fan for the MFD is inoperative for the PFD is inoperative Figure 8 17 Approaching VNAV Profile Message PFD ALERTS APPR TRG ALTE target altitude MFD FAN FAIL The cooling fan for the MFD is inoperative PFD FAN FAIL The cooling fan for the PFD is inoperative Figure 8 18 Approaching Target Altitude Message PFD To display map data on the Vertical Navigation Map Page press the MAP Softkey Press the TOPO TERRAIN or LING Softkey Press the same softkey to remove the displayed data from the Vertical Navigation Page VNAV Page Menu Options The VNAV messages are not enabled until the VNAV Messages On option is enabled from the VNAV Page Menu Options To display the page menu press the MENU Key with the VNAV Page displayed The VNAV Page Options Menu also allows the pilot to restore VNAV page defaults Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 9 SECTION 8 FLIGHT PLANNING Blank Page 8 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activa
37. 1 With the G1000 System OFF insert the aviation database update SD card into the top card slot of the PFD Label of SD card facing left 2 Turn the G1000 System ON This prompt is displayed on the upper left corner of the PFD SECTION 1 SYSTEM OVERVIEW DO YOU WANT TQ UPDATE THE AVIATION DATABASE PRESS CLR FOR NO AND ENT FOR YES YOU HAVE 3 SECONDS BEFORE NO IS RETURNED Figure 1 9 Database Update Prompt 3 Press the ENT Key to confirm the database updated This prompt is displayed DO YOU WANT TQ UPDATE THE AVIATION DATABASE PRESS CLR FOR NO AND ENT FOR YES YOU HAVE 3 SECONDS BEFORE NO IS RETURNED UPDATING AVIATION DATABASE UPDATED Ne LES ITSUCLESSKULLCY Figure 1 10 Database Update Confirmation 4 After the update completes the PFD starts in normal mode Remove the aviation database update SD card trom the PFD 5 Turn the G1000 System OFF 6 Repeat steps 1 through 4 for the MFD The MFD and PFD aviation databases are now updated 7 Verify that the correct update cycle is loaded during startup of the MFD Terrain and Obstacle Database Updates A 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 A NOTE Obstacles 200 and higher are included in the obstacle database It is very important to note that not all obstacles are necessa
38. 124 6 8NM VFR 122 700 RNWY 2440FT 210 10 2N ILS 123 000 RNWY 57 0 FT 150 11 4NM ILS 133 000 RNwWY 7339FT LCL por 2345 ON LCL 01 38 18 IDENT THR REF NRST CAUTION Figure 4 10 Nearest Airports Window PFD Press the NRST Softkey to display the Nearest Airports Window Turn the FMS Knobs to highlight the desired frequency Press the ENT Key to place the frequency in the standby field of the active COM Press the Frequency Transfer Key to place the frequency in the active field NAV frequencies are entered automatically in the NAV active frequency field upon approach loading or approach activation Auto tuning on the MFD Auto tuning on the MFD is done in much the same way as on the PFD Use the FMS Knobs to select the desired frequency on any of the information pages Pressing the ENT Key then loads the selected frequency in the tuning box as a standby frequency Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 4 NAV COM amp TRANSPONDER 47 TRANSPONDER Following is a list of important codes e 1200 VFR code in the U S please refer to the Mode Selection ICAO standards for VFR codes in other countries The STBY ON and ALT Softkeys can be accessed by e 7000 VER code commonly used in Europe please pressing the XPDR Softkey refer to the ICAO standards e 7500 Hijack code Ground Mode Automatic e 7600 Loss of communication code e 7700 Emergency code GN
39. AP or FD Key PIT will be displayed in green in the Active Mode Field of the AFCS Status Box The system will maintain or give command bar direction for a constant pitch attitude pitch reterence depending on which key is pressed Pitch Hold mode is active nev1 113 88 118 98 ITXD wer NAW 118 98 ITxD Flight Director command bars maintain desired pitch reference 2 Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode Field to the right of the PIT annunciation 3 Pitch attitude can be adjusted in 0 5 degree increments by pressing the NOSE UP NOSE DN Keys 4 Aircraft pitch may also be changed by pressing and holding the CWS button to manually establish the desired pitch using the control stick When the CWS button is released the current pitch angle will be maintained 5 If desired enter an altitude in the Selected Altitude Box by turning the ALT Knob As the selected altitude is reached ALT will flash in green for 10 seconds in the Acitve Mode Field after which the annunciation stops flashing This signals the altitude capture is complete and the selected altitude will be maintained Altitude Hold mode is armed 118 708 con 123 8808 DOM2 Figure 6 10 Pitch Hold Mode If only the flight director is engaged pitch and roll commands are given to manually maintain the selected altitude 6 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F Altitude Ho
40. AREST AIRPORTS field The first airport in the nearest airports list is highlighted 2 Press the FMS Knob then turn the large FMS Knob to highlight the desired airport Garmin G1000 Cockpit Reference Guide for the DA40 40F i SECTION 7 NAVIGATION 1 6 3 Press the FMS Knob to remove the flashing Cursor Access Runway Information for the Selected Airport 1 2 3 With the Nearest Airports Page displayed press the RNWY Softkey to place the cursor in the RUNWAYS field Turn the small FMS Knob to select the desired runway Press the FMS Knob to remove the flashing Cursor Quickly Tune the COM Transceiver to a Nearby Airport Frequency 1 With the Nearest Airports Page displayed press the FREQ Softkey to place the cursor in the FREQUENCIES field Turn either FMS Knob to select the desired frequency Press the ENT Key The selected frequency is placed in the COM standby frequency tuning field Press the Frequency Transfer Key to place the frequency in the active field Press the FMS Knob to remove the flashing Cursor Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol Identifier USS E aer 9 3NM VER MULTICOM 122 900 RNWY 3500FT Runway Length KIDA 261 9 5NM ILS TOWER 118 560 RNWY 9 1FT KRXE 4 gt 352 20 11NM YOR UNICON 122 800 RNWY 4200FT Primary COM Frequency Figure 7 10 Nearest Airports Window Press the NRST Softke
41. Activate field is highlighted 5 Press the ENT Key to activate Select a Direct to Destination to a Flight Plan Waypoint or Nearest Airport 1 While navigating an active flight plan press the Direct to GE Key 2 Turn the large FMS Knob to highlight the FPL NRST WAYPOINT field Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 1 SECTION 7 NAVIGATION 7 2 3 4 5 Turn the small FMS Knob to display a list of waypoints or airports Continue turning the small FMS Knob to scroll through the list and highlight the desired waypoint or airport Press the ENT Key to confirm the selection Press ENT again to activate a Direct to Re center the CDI to the Destination Waypoint Press the Direct to E Key followed by pressing the ENT Key twice If a missed approach point MAP is the current destination the approach will be canceled Manually Define the Direct to Course 1 Press the Direct to Key and enter a waypoint as discussed in previous steps or to edit the active direct to Turn the large FMS Knob to highlight the COURSE field Turn the FMS Knobs to select the desired course and press the ENT Key Press the ENT Key again to begin navigation using the selected destination and course Canceling Direct to Navigation 1 2 3 Press the Direct to G39 Key Press the MENU Key to display the Direct to options menu With Cancel Direct To NAV highlig
42. Added XM Weather Added ADF DME Added bearing pointers Added fixed pitch propeller engine parameters Updated fixed pitch propeller engine parameters Added reference to DA4OF on Copyright page and in Warnings Cautions and Notes 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 Date of Revision Affected Pages 7 06 i Index 4 Production Release Garmin G1000 Cockpit Reference Guide for the DA40 40F RR 1 90 00324 03 Added diesel engine parameters Rev A RECORD OF REVISIONS Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW 0 0000000000 1 1 1 1 PFD MFD Controls 0 00 0 0 ccccccccseesceeeeseen 1 2 1 2 PFD SOT OVS ss asissccissentavadicihihrsuaaodanaseon 1 4 1 3 MPD Softkeys oc ccesceseeseeseeseesean 1 7 1 4 MFD Page Groups 1 8 1 5 Backlighting 0 0 ccccc cscs testes 1 8 1 6 XM Radio Automatic Muting 0 0 0 0 1 9 1 7 Database Updates sees 1 9 Aviation Database Update c sccsesesseesessesseesseerees 1 9 Terrain and Obstacle Database Updates 1 9 SECTION 2 FLIGHT INSTRUMENTS 000000 2 1 2 1 Airspeed Indicator esses 2 3 speed INGICATION disseran 2 3 SEIRE E A T TA 2 3 Airspe d Trend VEctOT sirosisi
43. Ahead Terrain Ahead Imminent Terrain Impact Caution ITI TERRAIN Terrain Ahead Terrain Ahead Caution Terrain Caution Terrain Reduced Required Obstacle Clearance TERRAIN Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Altitude Callout 500 Fenced RTC or or TERRAIN AHEAD TERRAIN TERRAIN AHED or or CAUTION TERRAIN TERRAIN CAUTION OBSTACLE or OBSTACLE AHEAD Imminent Obstacle Impact Caution IOI OBSTACLE AHEAD Obstacle Ahead Obstacle Ahead or CAUTION OBSTACLE TERRAIN TOO LOW TERRAIN Excessive Descent Rate Caution EDR TERRAIN Sink Rate DONTSE or TOO LOW TERRAIN Negative Climb Rate Caution NCR Don t Sink or Too Low Terrain Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS TAWS System Status Annunciations PFD MFD TAWS MFD Alert Type Page Annunciation Pop Up Alert TAWS System Test Fail AWS FAT TAWS System Failure No GPS position or excessively degraded TAWS N A None TAWS Not Available GPS signal TAWS Availble will be heard when sufficient GPS signal is re established System Test in progress AWS TES None System Test pass None TAWS System Test OK 12 5 G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red Aural Messag
44. Annunciation BRG2 Information Window Figure 2 2 Additional PFD Information O00000 Desired Track to Distance to Next Waypoint Next Waypoint Next Waypoint Current Track Figure 2 3 PFD Navigation Status Box 2 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 1 AIRSPEED INDICATOR Airspeed Trend ector Vspeed References Speed Ranges low end yellow band Actual Airspeed not displayed and other low end speed ranges differ on EASA certified aircraft Figure 2 4 Airspeed Indicator True Airspeed Box i Speed Indication The indicated airspeed is displayed inside the black pointer The pointer will become red upon reaching Vne Figure 2 5 Red Pointer at Vne Speed Ranges The color coded speed range strip denotes flaps operating range normal operating range and never exceed speed Vne A red range is also present for low speed awareness Refer to the Airplane Flight Manual AFM for airspeed limitations and indicator markings Airspeed Trend Vector The end of the trend vector displays approximately what the airspeed will be in 6 seconds if the current rate of acceleration deceleration is maintained SECTION 2 FLIGHT INSTRUMENTS Vspeed References Vspeed References are turned on or off in the Timer References Window Press the TMR REF Softkey to display the widow When active ON the Vspeeds are displayed at their respective locations to the right of the airspeed scal
45. Audio panel 4 3 5 1 Audio panel controls ADF 5 2 DME 5 2 NAV1 5 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F NAV2 5 2 Auto tuning 4 4 Automatic squelch 4 3 Autopilot 6 1 6 2 6 3 6 5 6 10 6 12 6 13 Aviation database 1 9 Backcourse 6 11 Barometric setting 2 4 Base reflectivity 10 2 BKSP Softkey 4 5 BRG1 2 7 BRG2 2 7 C Caution 12 1 12 2 CDI 2 7 12 17 Cell movement 10 3 CLR key 1 3 Codes important 4 5 Code selection 4 5 CODE Softkey 4 5 COM Frequency Window 4 1 COM knob 4 3 Controls 1 2 4 1 Control Wheel Steering 6 1 6 3 Create a new flight plan 8 3 8 4 Create a new user waypoint 8 1 CWS 6 1 6 3 6 9 Cyclones 10 3 Cylinder Select 3 2 CYL SLCT 3 2 D DEC FUEL 3 3 Departures 9 1 Direct to 7 1 DME 1 6 4 4 Dual CDU failure 11 2 INDEX E Edit a flight plan 8 5 EDR 10 10 Emergency code 4 5 Engine display 3 1 ENGINE Softkey 3 1 Engine system 3 3 Excessive Descent Rate 10 10 F FD 1 4 12 4 Five Hundred Aural Alert 10 11 FLC 1 4 6 3 6 7 Flight director 6 1 6 4 6 6 6 10 Flight ID 4 5 Flight level change 1 4 6 3 6 7 6 11 6 16 Flight Plan Catalog 9 1 9 2 FLTA 10 10 Forward Looking Terrain Avoidance 10 10 FPL key 1 3 Freezing level 10 3 Frequency toggle key 1 3 4 3 G GA 6 1 6 3 6 8 6 9 6 12 Glideslope 6 3 6 8 6 9 6 12 GMA 1347 1 1 Go Around 6 1 6 3 6 8 6 9 6 12 6 19 HDG key 6 10 Heading hold
46. D WPT Softkey To change the user waypoint name follow the procedure for modifying a user waypoint TRIP PLANNING Turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the first rectangular page icon The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey Garmin G1000 Cockpit Reference Guide for the DA40 40F Starting WPT Ending WPT Figure 8 15 Trip Planning Page For Direct to planning press the WPTS Softkey and verify that the starting waypoint field indicates P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display PPOS Press the ENT Key and the flashing cursor moves to the ending waypoint field Turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR For point to point planning turn the FMS Knobs to enter the identifier of the starting waypoint Once the waypoints identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again turn the FMS Knobs to enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint OR For flight plan leg planning press the FPL Softkey at the bottom of the display and turn the small FMS Knob to select the desired flight plan SECTION 8
47. D is displayed when the aircraft is on the ground l e 7111 Military interceptor operations code CL NEVER ENTER THIS CODE 7 e 0000 Code for military use in the U S Figure 4 11 Ground Mode Flight ID Reporting Reply Status If so configured the Flight ID may be entered in the When the transponder sends replies to interrogations Timer Reterence Window an R indication appears momentarily in the reply status REFERENCES field TIMER 0 00 00 UP START GLIDE TOKT ON Vr BSKT ON Ux B4KkT ON Figure 4 12 Reply Indication Vy BEKT 4 ON Code Selection FLIGHT ID AIR265 Flight ID 1 Press the XPDR Softkey to display the transponder Mode Selection softkeys Figure 4 13 Timer References Window 2 Press the CODE Softkey to display the transponder Code Selection softkeys which includes the digit softkeys 3 Press the appropriate digit softkeys to enter the code in the four digit code field of the Transponder Status Box Five seconds after the fourth digit has been entered the transponder code becomes activated When entering a code press the BKSP Softkey as needed to back up and change code digits Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 5 SECTION 4 NAV COM amp TRANSPONDER Blank Page 4 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL al COM1 MIC COMI Transce
48. EPARTURE See the Procedures section for a discussion on loading and activating departure procedures 8 9 LOAD AN ARRIVAL See the Procedures section for a discussion on loading and activating arrival procedures Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 10 LOAD AN APPROACH See the Procedures section for a discussion on loading and activating approach procedures 8 11 REMOVE A DEPARTURE ARRIVAL OR APPROACH FROM A FLIGHT PLAN With the Active or Stored Flight Plan Page displayed press the FMS Knob to activate the Cursor Turn the large FMS Knob to highlight the title for the approach departure or arrival to be deleted Titles appear in white directly above the procedure s waypoints Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure STORE A NEWLY CREATED FLIGHT PLAN After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan Figure 8 13 Store Flight Plan Confirmation EDIT A STORED FLIGHT PLAN Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page SECTION 8 FLIGHT PLANNING Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and
49. GMU 44 Heading is flagged as invalid The AHRS uses fault has occurred GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch Communication halted GDL 69 Message Advisories Alerts Window Message Comments S O GDL69 CONFIG GDL 69 configura GDL 69 configuration settings do not match those of backup configuration memory tion error Contig service req d 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 The GMU 44 has incorrect sottware installed The G1000 system should be serviced GDC 74A Message Advisories Alerts Window Message Comments S O GDC1 CONFIG GDC1 configuration GDC 74A configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch Communication halted serviced BACKUP PATH ADC1 using backup The GDC 74A is using a backup communications data path The G1000 system data path should be serviced when possible Miscellaneous Message Advisories Alerts Window Message Comments S O FPL WPT LOCK Flight plan waypoint Upon power up the G1000 system detects that a stored flight plan waypoint is is locked locked This occurs when an aviatio
50. Height and apply full power to execute a missed approach The flight director Command Bars establish a nose up climb to follow Note that when the GA button is pushed the autopilot disconnects and the AP annunciation flashes yellow for five seconds Flashes for five seconds GAAP ALT 2 Start the climb to the prescribed altitude in the published Missed Approach Procedure a Press the AP Key to re engage the autopilot b Set the HSI to GPS mode c Press the NAV Key to have the autopilot fly to the hold a GPS JAP ALT d Select the SUSP Softkey to resume sequencing approach legs to the Missed Approach Hold Point MAHP The autopilot flies direct to Clovis VORTAC according to the loaded approach see Figure 6 25 3 Use the ALT Knob to set a Selected Altitude to hold The CWS button may be used to set a new pitch attitude As the Selected Altitude is captured Altitude Hold Mode becomes active and the autopilot maintains the Selected Altitude SECTION 6 AUTOMATIC FLIGHT CONTROL 4 To use the autopilot to fly the hold in Heading Select Mode set the Selected Heading using the HDG Knob and press the HDG Key Use the HDG Knob guide the aircraft tor the remainder of the hold S G T Z tea fy Figure 6 25 Go Around Missed Approach Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 19 SECTION 6 AUTOMATIC FLIGHT CONTROL Blank Page 6 20 Garmin G1000 Cockpit Reference Guide for the DA4
51. M1 RMT XFR COM1 remote transfer key is stuck The system has detected an over temperature condition in COM1 and or COM2 The transmitter will operate at reduced power If the problem persists the G1000 system should be serviced The COM1 and or COM2 transfer switch is stuck in the enabled or pressed posi COM RMT XER COND tion Press the transter switch again to cycle its operation If the problem persists acai puu the G1000 system should be serviced transfer key is stuck RAIM UNAVAIL RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available trom FAF to MAP waypoints Monitoring RAIM from the FAF to the MAP waypoints RAIM UNAVAIL RAIM is not GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity available Monitoring RAIM for the current phase of flight POSN ERROR RAIM has determined When a RAIM position error is detected GPS is flagged and the system no longer GPS position is in error provides GPS based guidance 12 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Alerts Window Message DGRD GPS ACC GPS position z accuracy degraded amp RAIM unavailable GPS position accuracy has been degraded and RAIM is not available GPS1 FAIL GPS1 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver
52. MS Knob to remove the flashing Cursor Figure 7 14 Nearest User Waypoints Page Select the Nearest User Waypoint Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the fifth rectangular page icon Select a Nearest User Waypoint 1 With the Nearest User Waypoint Page displayed press the FMS Knob to activate the cursor It any previously entered User Waypoints are within 200 nm these will be displayed with the closest listed first 2 Turn either FMS Knob to select the desired waypoint The remaining information on the Nearest User Waypoint Page pertains to the selected Nearest User Waypoint Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 7 NAVIGATION 3 Press the FMS Knob to remove the flashing 7 144 NEAREST AIRSPACES cursor 136 975 NORTH UP 7 13 NEAREST FREQUENCIES i 136 975 ADA reas t uP oe Tia te i NEAREST ARTCC e P De Figure 7 16 Nearest Airspaces Page Select the Nearest Airspaces Page PINE a Mealeshsrequcnclee tage 1 Turn the large FMS Knob to select the NRST Select the Nearest Frequencies Page page group 2 Turn the small FMS Knob to select the seventh 1 Turn the large FMS Knob to select the NRST rectangular page icon page group 2 Turn the small FMS Knob to select the sixth Airspace Alerts Box rectangular page icon Ifthe projected course takes the aircraft inside an ath Ah
53. Manual System Test Phase of Flight Level Flight A system test is automatically performed at power up After sucessful completion of the test TAWS System Test OR will be heard The system test may also be initiated manually but only when the aircraft is on the ground To manually verity 508 T Approach 150 ft 100 ft 08 co 10 10 proper operation of the aural and visual annunciations of the system perform the following steps 1 While the TAWS Page is displayed press the During the final approach phase of flight RTC ROC ITIIOI alerts are automatically inhibited when the aircraft is below 200 feet AGL while within 0 5 nm of the approach MENU Key runway or is below 125 feet AGL while within 1 nm of the 2 Turn the small FMS Knob to select Test VOWS TAWS Premature Descent Alert PDA 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK will be heard Forward Looking Terrain Avoidance FLTA The Forward Looking Terrain Avoidance alert is composed of two sub functions Reduced Required Terrain Clearance RTC and Reduced Required Obstacle Clearance ROC This provides alerts when the aircraft flight path is above terrain and or obstacles yet is projected to come within minimum clearance values outlined in the following table When an RTC or ROC alert is issued a potential impact point is displayed o
54. PLAY Figure 5 8 Playback e Pressing PLAY once plays the latest recorded memory block then returns to normal operation Pressing MKR MUTE while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key will begin playing the next previously recorded block Ifa COM input signal is detected during while playing play is halted and the new COM input signal is recorded as the latest block 5 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL The GFC 700 AFCS is optional on the DA40 and DA40F In aircraft without the GFC 700 option refer to the operating instructions for the installed autopilot system for details In addition to the AFCS Automatic Flight Control System keys on the MFD as discussed in the System Overview section the following buttons and switches used by the AFCS are located in the cockpit separately from the PFD and MFD e AP DISC Autopilot Disconnect Button Located on the left and right control sticks pressing this button disengages the autopilot Pressing it also acknowledges an autopilot disconnect e CWS Control Wheel Steering Button Located on the left and right control sticks pressing and holding the CWS button disengages the control surface servos without disengaging the autopilot If the flight director has not been activated pressing t
55. PS Arm Capture Track GPS APR VOR Approach ILS Approach Arm Capture Track Glideslope pitch mode automatically armed Go Around Wings Level GA The detault roll axis mode is Roll Hold ROL When no other roll axis modes are selected this is the active roll axis mode when the autopilot and or flight director is engaged Roll Hold Mode ROL 1 Press the FD or AP Key If the aircraft bank angle is gt 6 degrees when the key is pressed Roll Hold mode is selected by default Roll attitude at the time of activation is maintained by the autopilot up to 22 It only the flight director is active command bars indicate the proper roll attitude L SECTION 6 AUTOMATIC FLIGHT CONTROL If the aircraft bank angle is lt 6 degrees when the key is pressed the aircraft will be maintained at wings level If only the flight director is active command bars give guidance to maintain wings level Roll Hold mode is annunciated by ROL ee R01 i ALT Figure 6 15 Roll Hold Mode A new heading can be established by pressing and holding the CWS button and manually turning the aircraft to the desired new heading Release the CWS button and the aircraft will maintain wings level at approximately the new heading but will not hold the heading The same practice applies to holding roll attitude Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 9 SECTION 6 AUTOMATIC FLIGHT CONTROL Heading S
56. S Knob to highlight Activate and press the ENT Key to activate the approach Selecting Load will add the procedure to the flight plan without immediately using it for navigation guidance Activate An Approach in the Active Flight Plan With the Navigation Map Page displayed press the PROC Key Turn the large FMS Knob to highlight ACTIVATE APPROACH Press the ENT Key The approach procedure is now active SECTION 9 PROCEDURES Garmin G1000 Cockpit Reference Guide for the DA40 40F 9 3 SECTION 9 PROCEDURES Blank Page 9 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE 10 1 CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 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 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select the Weather or Traffic group to customize the display of weather features Select Traffic to customize the display of traffic Press the small FMS Knob to return to the Navigation Map Page GPT IONS Measure Bearing Distance Press the FMS CRSA knob to return to bose poge Figure 10 1 Page Menu HAP SETUP STRHSCP LTNG n STRHSCP HODE Ce STRHSCP SHEL SRGNM NEXRAD DATA OFF 2Q QNH WH LTNG OFF 200 NH CELL HOVEHENT On Figure 10 2 Map Setup Menu MAP
57. Tk GARMIN G1 01010 Integrated Flight Deck Cockpit Reference Guide Diamond DA40 40F Copyright 2004 2006 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0369 11 or later for the Diamond DA40 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 Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey Hampshire 051 9DL 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 complete text of this copyri
58. also displayed If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Arrival field Turn the small FMS Knob to display a list of available arrivals Turn either FMS Knob to select the desired arrival and press the ENT Key Figure 9 3 Select Arrival Garmin G1000 Cockpit Reference Guide for the DA40 40F J SECTION 9 PROCEDURES 9 2 6 A second window is displayed listing available transitions for the arrival Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key Figure 9 4 Select Arrival Transition 7 Athird window is displayed listing the available runways Turn either FMS Knob to select the desired runway and press the ENT Key Figure 9 5 Select Arrival Runway 8 With LOAD highlighted press the ENT Key If a flight plan is active the selected arrival procedure is inserted after the destination airport and becomes part of the active flight plan If no flight plan is active when the arrival is loaded the arrival procedure will become the active flight plan 9 2 APPROACHES Not all approaches in the database are approved for GPS use When selecting an approach a GPS designation to the right of the procedure name indicates the procedure can be flown using the GPS receiver Some procedures will not have this designation meaning the GPS receiver can be u
59. an overspeed caution occurs reduce engine Autopilot Engaged power and or adjust the pitch reference to slow the xR ALT aircraft ai Figure 6 5 Autopilot Engaged Annunciation 6 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F Automatic Disengagement Automatic disengagement typically occurs due to a failure Automatic disengagement is annunciated by a flashing AP alternating red on white and white on red in the Autopilot Status Field Also the autopilot disconnect aural alert will be heard Both the annunciation and the aural alert will continue until acknowledged by pressing the AP DISC button or the AP TRIM ARM switch Automatic Disconnect ROL A ALT Figure 6 6 Automatic Disconnect Annunciation Manual Disengagement The autopilot may also be manually disengaged by pressing the AP DISC button the GA button the AP TRIM ARM switch or by pressing the AP Key on the MFD Manual disengagement is annunciated by a five second flashing yellow AP in the Autopilot Status Field and by a two second Autopilot disconnect aural alert Manual Disconnect J ROL JAP ALT Figure 6 7 Manual Disconnect Annunciation Control Wheel Steering Pressing and holding the CWS button disengages the servos from the flight control surfaces and allows manual manuevering of the aircraft At the same time the flight director is synchronized to the aircraft attitude during the maneuver The AP annunciation is temporarily replaced
60. arnings 10 3 Wind direction 10 3 Wind speed 10 3 X XPDR Softkey 4 5 INDEX Garmin G1000 Cockpit Reference Guide for the DA40 40F Index 3 INDEX Blank Page Index 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F ul Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 a E mn Garmin AT Inc 2345 Turner Road S Salem OR 97302 US y p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Unit 5 The Quadrangle Abbey Park Industrial Estate Romsey 051 9DL 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 190 00324 06 Rev A 2004 2006 Garmin Ltd or its subsidiaries
61. arrow Move the Joystick to place the panning arrow onAIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 3 SECTION 10 HAZARD AVOIDANCE Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that displays the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information Weather Products and Symbols Figure 10 7 depicts the symbol for each weather product read from left to right When a weather product is active the product symbol is displayed in the lower right of the screen e NEXRAD e Cloud Top Echo Top e XM Lightning e Cell Movement SIGMETs AIRMETs e METARs e City Forecast e Surface Analysis e Freezing Levels e Winds Aloft e County Warnings e Cyclone Warnings The XM Information Page in the AUX Page Group will display the weather products available for the current subscription A green box by the weather product means that it is available NOTE The DONE Softkey on the AUX XM INFORMATION Page is used to save the GDL 69 A activation data when the XM services are initially set up It is not used during
62. arts 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 The Jeppesen database used in the G1000 system must be updated regularly in order to ensure that its information remains current Updates are released every 28 days A database information packet is included in the G1000 package Pilots using an outdated database do so entirely at their own risk WARNING The basemap land and water data must not be used for navigation but rather only for non navigational situational awareness Any basemap indication should be compared with other navigation sources 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 69 is approved only for weather avoidance not penetration WARNING NEXRAD weather data is to be used for long range planning purpo
63. ated Alerting is inhibited while the aircraft is on the ground If the aircraft climbs after having reached the MDA once it reaches 50 feet above the MDA alerting is disabled Garmin G1000 Cockpit Reference Guide for the DA40 40F Within 100 ft Barometric Mini mum bug Barometric E Minimum Box Eana BARO MIN 3U 041N Figure 2 9 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2 4 MARKER BEACON ANNUNCIATIONS Marker Beacon Annunciation Vertical Deviation Glideslope Indicator Figure 2 10 Marker Beacon and Vertical Deviation SECTION 2 FLIGHT INSTRUMENTS 2 5 VERTICAL DEVIATION GLIDESLOPE INDICATOR The Vertical Deviation Glideslope Indicator appears when an ILS is tuned in the active NAV frequency field 2 6 VERTICAL SPEED INDICATOR Selected Vertical Speed Vertical Speed Bug Vertical Speed Pointer Figure 2 11 Vertical Speed Indicator The actual vertical speed is displayed inside the pointer When the Flight Director is placed in Vertical Speed Mode by pressing the VS Key the Vertical Speed Bug is displayed Press the NOSE UP or NOSE DN Key to adjust 2 7 HORIZONTAL SITUATION INDICATOR HSI The HSI compass can be displayed as a 360 rose or 140 arc by pressing the PFD Softkey followed by the 360 HSI or the ARC HSI Softkey Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 5 SECTION 2 FLIGHT INSTRUMENTS 2 6 O Turn Rate Indicator 2 Lateral Devia
64. blem persists The G1000 system should be serviced The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced DB MISMATCH Terrain database The PFD and MFD have different terrain database versions installed Crosstill is off version mismatch Xtalk is off Install correct terrain database version in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database types installed Crossfill is off type mismatch Xtalk is off Install correct terrain database type in both displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Crossfill is off version mismatch Xtalk is off Install correct obstacle database version in both displays 12 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Cont Alerts Window Message Comments S O DB MISMATCH Airport Terrain The PFD and MFD have different airport terrrain databases installed Crosstill is off database mismatch Xtalk is off Install correct airport terrain database in both displays GMA 1347 Message Advisories Alerts Window Message Comments S GMA1 FAIL GMAT is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be
65. d tracks the selected navigation receiver on the HSI e g GPS VOR or LOC GPS roll steering commands are followed when the HSI is in GPS mode and creates roll steering commands from the Selected Course and deviation when the HSI is in VOR LOC or BC backcourse modes Turning the CRS Knob moves the Course Pointer when in VOR LOC and OBS mode and displays the Selected Course Box The Selected Course is displayed in the box The box is displayed while the knob is turning and disappears three seconds after the knob stops turning Backcourse mode is automatically selected when the localizer front course is greater than 105 degrees from the aircraft heading NOTE When making a backcourse approach set Selected Course to the localizer front course Navigation Mode is active using GPS source Nat 113 68 WPT 117 95 Flight Director command bars indicating a left turn to track GPS course and a climb to intercept Selected Altitude CDI Figure 6 17 Navigation Mode SECTION 6 AUTOMATIC FLIGHT CONTROL Navigation Mode Armed If the CDI is not centered deviation gt 1 dot when the Navigation mode is selected the mode is automatically armed The armed annunciation appears in white to the left of the active roll axis mode See the Example Procedures Using AFCS section for more information Flight Level Change mode is active Altitude Hold is armed Selected Course GPS is active navigation receiver on the HSI
66. e A NOTE Upon power up of the G1000 system certain windows remain invalid as G1000 X is typically displayed on windows associated with the equipment begins to initialize All windows failed data The following section describes various system should be operational within one minute of annunciations Refer to the Airplane Flight Manual for power up Should any window continue to additional information regarding pilot responses to these remain flagged the G1000 system should be annunciations serviced by a Garmin authorized repair facility System Annunciation Commet Attitude and Heading Reterence System is aligning Display system is not receiving attitude information trom the AHRS 12 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS Display system is not receiving airspeed input trom air data computer Display is not receiving altitude input trom the air data computer Display is not receiving vertical speed input trom the air data computer GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded it GPS signals are not present see AFMS XPDR FALL Display is not receiving valid transponder intormation a A red X through any other display field such as engine instrumentation Other Various Red X Indications fields indicates that the field is not receivi
67. e To activate the Vspeed References display the Timer Reference Window and turn the large FMS Knob to place the cursor in the ON OFF field Turn the small FMS Knob to select ON or OFF 2 2 ATTITUDE INDICATOR The Slip Skid Indicator is located under the Roll Pointer and moves laterally away from the pointer to indicate lateral acceleration One Slip Skid indicator displacement is equal to one ball displacement when compared to a traditional slip skid indicator C1 Roll Pointer 2 Roll Scale 6 Aircraft Wing Tips 7 Pitch Scale 3 Horizon Line Slip Skid Indicator Aircraft Symbol E Sky Representation G Land Representation Roll Index Zero Figure 2 6 Attitude Indicator Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 gt SECTION 2 FLIGHT INSTRUMENTS 2 4 2 3 ALTIMETER Altitude Reference Z Aang Box Altitude Trend Current Altitude Vector Altitude Select Bug pa Barometric Setting 30 5IN Box Figure 2 7 Altimeter Altitude Select Bug The Altitude Select Bug is displayed at the selected altitude or if the selected altitude is beyond the altitudes currently displayed the bug is displayed at the top or bottom of the display whichever is closest to the selected altitude Set the Selected Altitude Bug Turn the ALT Knobs to set the Altitude Select Bug The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands This altitude also appears in the Selected Altitude
68. e Autopilot is engaged If the autopilot is engaged the FD Key is disabled 20 NAV Key Selects deselects the Navigation mode 21 ALT Key Selects deselects the Altitude Hold mode 22 VS Key Selects deselects the Vertical Speed mode 23 FLC Key Selects deselects the Flight Level Change mode 24 HDG Key Selects deselects the Heading Select mode 25 APR Key Selects deselects the Approach mode 26 27 NOSE UP NOSE DN Keys Controls the active pitch reference for the Pitch Hold Vertical Speed and Flight Level Change modes 1 2 PFD SOFTKEYS TERRAIN Softkey ON Softkey OFF optional nnonnnnnnnn op Figure 1 2 PFD Top Level Softkeys INSET Press to display the Inset Map in the lower left corner of the PFD OFF Press to remove the Inset Map DCLTR 3 Press momentarily to select the desired amount of map detail The declutter level appears adjacent to the DCLTR Softkey e No declutter All map features are visible Declutter 1 Declutters land data Declutter 2 Declutters land and SUA data e Declutter 3 Removes everything except the active flight plan TRAFFIC Press to display traffic on the inset map TOPO Press to display topographical data Q e coastlines terrain rivers lakes and elevation scale on the inset map TERRAIN Press to display terrain information on the inset map NEXRAD optional Press to display NEXRAD precipitation data
69. e Selected Altitude Press the VS Key The flight director is now activated if not already active and VS is displayed in green in the Active Mode Field and the Vertical Speed Bug will appear on the Vertical Speed Indicator Pitch commands are given to manually maintain vertical speed Press the AP Key to engage the autopilot for maintaining the current vertical speed Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode Field to the right of the VS annunciation The Vertical Soeed Bug can be adjusted in 100 fom increments by pressing the NOSE UP NOSE DN Keys to set the desired vertical speed The vertical speed setting will be displayed in the Selected Vertical Soeed Box and in the Vertical Speed Reference Field in the AFCS Status Box The Vertical Speed Box is located above the VSI when the aircraft is climbing and below the VSI when descending Vertical speed may also be changed by pressing and holding the CWS button to manually establish the desired vertical speed using the control stick When the CWS button is released the current vertical speed will be maintained A desired altitude may be entered in the Selected Altitude Box by turning the ALT Knob With Altitude Hold mode armed as the selected altitude is reached ALT will flash in green for 10 seconds in the Active Mode Field after which the annunciation stops flashing This signals the altitude capture is complete and
70. ead Select and Load the Nearest ARTCC FSS or Weather a M a a aia Pequenty e If the aircraft is within two nautical miles of an 1 With the Nearest Frequencies Page displayed airspace and the current course takes the aircraft press the ARTCC FSS or WX Softkey to place inside Ahead lt 2 nm is displayed the cursor in the appropriate field e If the aircraft is within two nautical miles of an 2 Turn the FMS Knobs to select the desired facility airspace and the current course will not take the aircraft inside Within 2 nm is displayed e Ifthe aircraft has entered an airspace Inside is displayed or frequency 3 Press the ENT Key to load the frequency into the COM frequency standby field 4 Press the FMS Knob to remove the flashing Cursor Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 9 SECTION 7 NAVIGATION View Additional Details for a Listed Airspace 1 With the Nearest Airspace Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to scroll through the list highlighting the desired airspace 3 Press the ALERTS Softkey to place the cursor in the AIRSPACE ALERTS field 4 Turn either FMS Knob to select the desired airspace 5 Press the FMS Knob to remove the flashing Cursor View and Quickly Load the Frequency for a Controlling Agency 1 With the Nearest Airspace Page displayed press the FREQ Softkey to place the cursor in FREQUENCIES
71. ect OBS mode on the CDI when IDENT Press to provide special aircraft navigating by GPS only available with active leg position identification to Air Traffic Control CDI Press to change navigation mode on the CDI ATC between GPS VORI and VOR2 BKSP Press to remove numbers entered one ADF DME optional Press to display the ADF DME at a time Tuning Window BACK Press to return to the previous level XPDR Press to display the transponder mode softkeys selection softkeys IDENT Press to provide special aircraft position STBY Press to select standby mode identification to Air Traffic Control ATC ON Press to select mode A BACK Press to return to the previous level softkeys ALT Press to select altitude reporting mode ALERTS Press to display the Alerts Window VFR Press to automatically squawk 1200 only 1 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW IDENT Press to provide special aircraft position 1 3 MFD SOFTKEYS identification to Air Traffic Control ATC TMR REEF Press to display the Timer References ENGINE Pressing this softkey makes available Window the LEAN and SYSTEM Softkeys which in turn NRST Press to display the Nearest Airports access the Lean Display and the System Display Window respectively ALERTS Press to display the Alerts Window MAP Pressing this softkey enables the following A optional Press
72. ees Load and or Activate an Approach Procedure Activate An Approach in the Active Flight Plan SECTION 10 HAZARD AVOIDANCE 0000 10 1 Customizing the Hazard Displays on the Navigation Map 0 ccccccseseseeseesen 10 2 XM Weather Optional 0 0 Displaying METAR and TAF information on the Airport Information Page c sccscesesseseseeseseeseeseen Displaying Weather on the Weather Data Link Page NEXRAD LMINGUO MS cused a Map Panning Information Weather Data Link Page Weather Products and Symbols c ssssessecseesseesseen Weather Product Ag cssssssessssessessssssssseerneessen 10 3 Traffic Information Service TIS Displaying Traffic on the Traffic Map Page s0e Displaying Traffic on the Navigation Mapu TISAUGIO ACE ieoa nS 10 3 TABLE OF CONTENTS 10 4 Terrain And Obstacle Proximity 0 10 6 Displaying Terrain and Obstacles on the Terrain PRO MINAIEY PITO siita nnen cael sche iedaan ta we 10 6 Displaying Terrain and Obstacles on the Nava OM MaD a aces oie cases 10 7 10 5 Terrain Awareness amp Warning System TAWS Display Optional 0 0 0 0 cesses 10 8 Displaying Terrain on the TAWS Page scessesseseeen 10 8 Enable Disable Aviation Data cesseseeseeeaeeen 10 9 TANS IINMIDM ooien ir 10 9 Mangal system CST cts cactrostsscislvieeutndtuactimcanctash 10 10 Forward Looking Terrain Avoidance FLTA
73. elect Mode HDG 1 6 10 Flight Director command bars tracking Selected Heading elected Heading ox Turn the HDG Knob to move the heading bug on the HSI to the desired heading When the Knob is turned the Selected Heading Box will appear and remain for three seconds after the knob stops moving The selected heading will be displayed in the Selected Heading Box With the autopilot and or flight director engaged press the HDG Key HDG is now displayed in green in the Active Mode Field If the autopilot is engaged the aircraft will begin to turn toward the selected heading When the selected heading is reached the aircraft will maintain this heading If only the flight director is engaged manually maneuver the aircraft to the command bars to aquire the selected heading Heading Select mode NAVI 113 66 now2 108 08 117 95 PFD 06S CDI The heading may be adjusted by turning the HDG Knob and moving the heading bug to a new heading The aircraft will turn in the same direction the heading bug is moved However if the heading bug is moved more than 340 degrees at a time a turn reversal will be the result Altitude Hold mode is active XPOR Selected Heading Bug IDENT TMR REF NRST Figure 6 16 Heading Select Mode Garmin G1000 Cockpit Reference Guide for the DA40 40F Navigation Mode GPS VOR LOC or BC Pressing the NAV Key activates the Navigation Mode The Navigation mode acquires an
74. em conveys alerts to the pilot using a combination of the following items e Annunciation Window The Annunciation Window displays abbreviated annunciation text The Annunciation Window is located to the right of the Altimeter and Vertical Speed Indicator on the PFD display or the MFD if system is in reversionary mode Up to 12 DA40 annunciations can be displayed simultaneously A white horizontal line separates annunciations that are acknowledged SECTION 12 ANNUNCIATIONS amp ALERTS from annunciations that are not yet acknowledged Acknowledged annunciations are always above the line Annunciations are displayed in order of priority from top to bottom The highest priority annunciation is displayed at the top of the Annunciation Window Alerts Window The Alerts Window displays alert text messages Up to 64 prioritized alerts can be displayed in the Alerts Window Pressing the ALERTS Softkey displays the Alerts Window Pressing the ALERTS Softkey again removes the Alerts Window from the display When the Alerts Window is displayed the pilot may use the large FMS Knob to scroll through the alert list Higher priority alerts are displayed at the top of the window Lower priority alerts are displayed at the bottom of the window Active alerts are displayed in white text Alerts that have become inactive will change to gray text The ALERTS Softkey will flash if the state of a displayed alert changes or a new alert is displayed
75. er the speaker or headsets during marker beacon reception When the tone is active pressing the MKR MUTE Key once mutes the audio but does not affect the marker annunciator The audio returns when the next marker signal is received To turn off the marker beacon audio press the MKR MUTE Key once when there is no marker indication present or press twice when an indication is present The key annunciator will be extinguished when the marker beacon audio is turned off Outer Marker Annunciator Middle Marker Annunciator Inner Marker Annunciator Figure 5 3 Marker Beacon Annunciators on the PFD Marker Beacon Signal Sensitivity The HI SENS Key can be pressed for increased marker beacon signal sensitivity v v MKR HI MUTE SENS Figure 5 4 Marker Beacon 5 3 NAV RADIO AUDIO SELECTION Pressing DME ADF NAVI or NAV2 selects and deselects the radio source and activates the annunciator Selected audio can be heard over the headset and the speakers These four keys can be selected individually or together Figure 5 5 Navigation Radios Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 5 AUDIO PANEL 5 4 INTERCOM SYSTEM ICS ISOLATION 5 5 INTERCOM SQUELCH CONTROL Press the PILOT and or COPLT Key to select who is Select manual squelch for intercom audio by pressing isolated from hearing the NAV COM radios and music the MAN SQ Key to light the annunciator lecti in Table 5 1 Selec
76. erence Guide for the DA40 40F Figure 7 8 VOR Information Page Select the VOR Information Page 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the fourth rectangular page icon Access Information on a VOR 1 With the VOR Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the desired selection field identifier name or closest city 3 Turn the FMS Knobs to enter an identifier name or city and press the ENT Key 4 The FREQUENCY field is now highlighted If desired press the ENT Key to place the frequency in the NAV receiver standby field 5 Press the FMS Knob to remove the flashing cursor SECTION 7 NAVIGATION 7 7 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints 7 8 NEAREST AIRPORTS 17 95 prep 136 975 NORTH UP r ape NEAREST AIRPORTS gt 1 E rS f ae Oe 4 RW FREQ APR Figure 7 9 Nearest Airports Page Nearest Airport Information on the MFD Select the Nearest Airports Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the first rectangular page icon Access Information on a Specific Airport 1 With the Nearest Airports Page displayed press the APT Softkey to place the cursor in the NE
77. ersections Page 7 7 View Information on the Nearest Intersection 7 7 7 10 Nearest NDB 00 cece l 1 Select the Nearest NDB Page scssesseseseesessessean 7 7 Access Information on a Specific NDB l 1 DVL N arest VOR iocans 1 8 Select the Nearest VOR Page v ccscessessesseeseeseesesseean 1 8 View Information on the Nearest VOR 1 8 Select and Load a VOR Frequency stessesseesseesseesseeee 1 8 7 12 Nearest User Waypoint 0 0 cccceeeees 1 8 Select the Nearest User Waypoint Page 1 8 Select a Nearest User Waypoint eessesseseseeeeen 1 8 7 13 Nearest Frequencies 0 cccccccsseseseeseenees 19 Select the Nearest Frequencies Page cssessesesseeen 1 9 Select and Load the Nearest ARTCC FSS or MEEA GUEN CV oss esd scdubns cde daanacdetadeccdaesiteact 7 9 7 14 Nearest Airspace 7 9 Select the Nearest Airspaces Page 7 9 Airspace Alerts BOK csecsscotacnicsssntuontccniosisaamiess 7 9 View Additional Details for a Listed Airspace 7 10 View and Quickly Load the Frequency for a CORTON ING Agen saana 7 10 SECTION 8 FLIGHT PLANNING 0000000 8 1 8 1 User Defined Waypoints 0 0 cc ees 8 1 Select the User WPT Information Page c scseseseen 8 1 Create a New User Waypoint 8 1 Modity a User Waypoint sison ane 8 1 Delete a User Waypoint seesssesssssesessessessneessen 8 1 Create User Waypoints from the Navigation VAD ae saa teaduttens iit sadiledamracadailanersostine
78. eseseseesecsen 6 7 GEADA MOJEGA orraa nO nO nn MnO TET 6 8 EEI GS EEE E E 6 8 6 6 Roll Axis Modes cccccsssessessseesseessesnees 6 9 Roll Rold Mode ROL ssasctenarecsconmasnmanececunmerasvaress 6 9 Heading Select Mode HDG 6 10 Navigation Mode GPS VOR LOC or BC 6 11 Navigation Mode Armed 6 11 Garmin G1000 Cockpit Reference Guide for the DA40 40F TABLE OF CONTENTS Approach Mode GPS VAPP or LOC 6 12 GO POUR A endeaactanh co A 6 12 6 7 Example Procedures Using AFCG 6 13 DED AUG oaae OAA TO 6 14 Intercepting a VOR RAUIGI ica cttihdexcistiecctsitinxctamuayen 6 15 FIVING a GPS Flight PIAN 2os c2 ctovcevsneahexatoroaveuentannten 6 16 Flight Level Change Descent 6 17 ES ADDI OGC Is assscnsncctenatenauanacsnonimonsenanasnnas 6 18 Go Around Missed Approach 6 19 SECTION 7 NAVIGATION 7 1 7 4 Navigation Map Pag ccccceeeeceen 7 1 Select the MAP Page GIOUD csessessessessseeseesesseean 7 1 7 2 Direct to Navigation 0 0 cccc cscs 7 1 Direct to Navigation trom the MFD 7 1 Enter a Direct to Destination sssi Select a Direct to Destination to a Flight Plan Waypoint or Nearest Airport s s 1 1 Re center the CDI to the Destination Waypoint 7 2 Manually Define the Direct t0 Course vs 7 2 Canceling Direct to Navigation cesseesseesesseeseerees 1 2 Direct to Navigation from the PFD c scessessseseeeeeen 7 2 Cancelling Direct to
79. etting will be displayed in the Selected Airspeed Reference Flight Level Change mode is active Nav 113 68 nw2 108 08 117 95 SECTION 6 AUTOMATIC FLIGHT CONTROL Airspeed Box above the Airspeed Indicator and in the Airspeed Reference Field in the AFCS Status Box Airspeed may also be changed by pressing and holding the CWS button to manually establish the desired airspeed using the control stick When the CWS button is released the current airspeed will be maintained Adjust engine power to allow the autopilot to tly the aircraft at a pitch attitude which corresponds to the selected airspeed and the desired flight profile descent or climb With Altitude Hold mode armed as the selected altitude is reached ALT will flash in green for 10 seconds in the Acitve Mode Field after which the annunciation stops flashing This signals the altitude capture is complete and the selected altitude will be maintained If only the flight director is engaged pitch commands are given to manually maintain the selected altitude Altitude Hold mode is armed ekea oclected Altitude Figure 6 13 Flight Level Change Mode Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 7 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around Mode GA Pressing the GA button not located on the MFD engages the flight director in a wings level 7 degree pitch up attitude Go Around mode disengages the autopilot and arms Altitude H
80. ey when finished Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 SECTION 8 FLIGHT PLANNING 8 20 VERTICAL NAVIGATION VNAV PAGE 8 8 NOTE An active flight plan or Direct to must be entered in order to utilize VNAV NOTE VNAV is advisory only and cannot be coupled to the autopilot 4 20KT Create a Vertical Navigation Profile Press the FPL Key Turn the small FMS Knob to select the third page Icon Press the FMS Knob to activate the cursor With the TARGET POSITION distance field highlighted turn the FMS Knobs to select the desired distance for Top Of Climb or Bottom Of Descent from the VNAV profile endpoint The default distance is 4 nm DTK UP Press the ENT Key The cursor is now positioned over the Before and After field Turn the small FMS Knob to select whether the previously set distance is Before or After the endpoint Press the ENT Key The cursor is now placed over the VNAV profile endpoint field TARGET POSITION SNM KHDN TARGET ALTITUDE 3QGQFT Above WPT TARGET VERTICAL SPEED 400FPH STATUS VERTICAL SPEED REQUIRED Begin descent in 1 FPM 00 26 18 TARGET ALTITUDE LEGEND TOP OF DESCENT BOTTOM OF CLIMB TERRAIN 10 FT 100 FT a a i 2 NM 8 9 Figure 8 16 Vertical Navigation VNAV Page Turn the small FMS Knob to display a list possible VNAV profile endpoints When using a flight p
81. field 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key to load the frequency into the COM frequency standby field 4 Press the FMS Knob to remove the flashing cursor 7 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS Figure 8 1 User WPT Information Page Select the User WPT Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the fifth rectangular page icon Create a New User Waypoint 1 With the User Waypoint Information Page displayed press the NEW Softkey A waypoint is created at the current aircraft position Turn the small FMS Knob to enter first character of the waypoint name Turn the large FMS Knob to move the cursor to the next character field 8 SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered Press the ENT Key Press the ENT Key a again to accept the new waypoint identifier The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be defined by a reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial and distance from the reference waypoint Press the FMS Knob to remove the flashing Cursor Modify a User Waypoint With the
82. formation Page Displaying Weather on the Weather Data Link Page Select the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the fourth rectangular page icon 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 the FMS Knobs to scroll through the list Press the small FMS Knob or the ENT Softkey to return to the map ny o ICELL HOV SIG AIR HETAR LEGEND HORE WX Figure 10 6 Weather Data Link Page NEXRAD Press the NEXRAD Softkey to show NEXRAD weather and radar coverage information Areas where radar coverage is not available will be shown in grayish purple The display is updated every five minutes NEXRAD Limitations Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here e NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics hail vs rain etc e An individual NEXRAD site cannot depict high altitude storms at close ranges and has no information about storms directly over the site e The resolution of displayed NEXRAD data is 4 square kilometers Therefore when zoomed in on the display each square block is 2 kilometers on each side The intensity level reflected by the square will be the highest level sampled wi
83. g may be selected manually from the MFD System Setup Page See System Setup in the G1000 Pilots Guide for more details Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Sottkeys The BRGI Pointer is a single line pointer The BRG2 Pointer is a double line pointer DME Information Bearing 1 Window Pointer Bearing 2 Pointer N Bearing Bearing 2 Information Information Window Window Figure 2 16 HSI with Bearing Information SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source Waypoint Identifier OJSC 11 6 NH Je Bearing Pointer Source Icon Figure 2 17 BRG1 Information Window Distance to Bearing Source mi Waypoint i Identifier Bearing Pointer Icon Source Figure 2 18 BRG2 Information Window DME optional To display the DME Information Window press the PFD Softkey followed by the DME Softkey Figure 2 19 DME Information Window Navigation Source Change between navigation sources 1 Press the CDI Softkey to change from GPS to VOR1 LOC1 2 Press the CDI Softkey again to change trom VOR1 LOC1 to VOR2 LOC2 3 Press the CDI Softkey a third time to return to GPS Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 7 SECTION 2 FLIGHT INSTRUMENTS 2 8 When using GPS as the navigation source the following may appear NOTE The OBS Softkey is only displayed when ee navigating an active
84. ge ARC View 10 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE Terrain Obstacle Location Suggested Pilot Response Terrain Obstacle at or within 100 Initiate climb and or turn away from below or above aircraft altitude terrain obstacle Terrain Obstacle between 100 and Be aware of surroundings 1000 below current aircraft altitude Be prepared to take action Terrain Obstacle is more than 1000 No action required Black below aircraft altitude Potential Impact Point Projected Flight Path af 100 Threshold a Unlighted Obstacle Enable Disable Aviation Data TAWS Inhibit 1 While the TAWS Page is displayed press the Flying VFR into an area where unique terrain exists MENU Key could cause the system to annunciate a nuisance alert 2 Turn the small FMS Knob to select Show or binge is inhibited only FLTA and PDA alerts are Hide Aviation Data Inhibit TAWS 3 Press the ENT Key 1 While the TAWS Page is displayed press the MENU Key PAGE MENU p OPTIONS 2 Turn the small FMS Knob to select Inhibit Inhibit TAWS TAWS ak 3 Press the ENT Key Enable TAWS 1 While the TAWS Page is displayed press the Press the FMS CRSR knob to MENU Ke return to base page y 2 Turn the small FMS Knob to select Enable Figure 10 14 TAWS Page Menu TAWS 3 Press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 9 SECTION 10 HAZARD AVOIDANCE
85. ght 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 These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc July 2006 190 00324 06 Rev A Printed in the U S A Garmin G1000 Cockpit Reference Guide for the DA40 40F WARNINGS CAUTIONS amp NOTES 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 the sole source of obstacle and terrain avoidance information Always refer to current aeronautical ch
86. haracter of the identifier of the departure waypoint Turn the large FMS Knob to move the cursor to the next character field Repeat steps 4 and 5 until the desired identifier has been entered WAYPOINT INFORMATION IDENT FACILITY CITY NORTH UP Figure 8 11 Waypoint Info Window Press the ENT Key Repeat steps 3 through 5 to enter the identifier for each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Create a New Flight Plan Using the PFD 8 4 NOTE A flight plan cannot be entered using the PFD if another flight plan is active 8 8 NOTE After the first leg is entered using the PFD only it is immediately activated Press the FPL Key then press the FMS Knob to activate the cursor 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 2 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 2 through 4 to enter the identitier for each additional flight plan waypoint Once all waypoints have been entered press the FMS Knob remove the cursor The new flight plan is now active Figure 8 12 Creating Flight Plan on the PFD LOAD A D
87. he CWS button will activate the flight director in the default pitch and roll hold modes GA Go Around Button Located on the throttle lever the GA button disengages the autopilot and selects the Go Around wings level mode AP TRIM Autopilot Trim Switch Located on the left control stick this switch is used to operate manual electric pitch trim Moving both switches forward simultaneously trims the aircraft nose down Moving both switches aft simultaneously trims the aircraft nose up The left switch is the ARM contact and the right switch controls the up down trim Pressing the ARM switch disengages the autopilot if currently engaged If one side of the switch is active for more than three seconds without the other side SECTION 6 AUTOMATIC FLIGHT CONTROL also being active PTRM is displayed in the AFCS System Status Box on the PFD Pressing the ARM switch also acknowledges an autopilot disconnect Figure 6 1 AFCS Keys Pressing the FD Key activates only the flight director in the default Pitch Hold Roll modes without engaging the autopilot Pressing the AP Key activates the flight director and engages the autopilot When only the flight director is engaged pressing the FD Key removes the flight director Upon activation of the autopilot and or flight director command bars are displayed on the PFD If the attitude information being sent to the flight director becomes invalid or unavailable the command
88. he Flight Plan Catalog press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be copied Press the COPY Softkey A Copy to flight plan confirmation window is displayed With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be deleted Press the DELETE Softkey A Delete flight plan confirmation window is displayed With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION Press the FPL Key to display the Active Flight Plan Page 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 Press the LD WPT Softkey The selected waypoint will be inserted at the end of the flight plan The default user waypoint naming is USROOO USROO1 USROO2 and so on If the selected waypoint is to be placed elsewhere in the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor After placing the cursor at the desired point in the list of waypoints press the L
89. heading bug with the compass lubber line Selected Heading provides the heading reference to the Flight Director while operating in Heading Select mode 5 Joystick Changes the map range distance top to bottom of map display when rotated Activates the map pointer when pressed 6 CRS BARO Knob The large knob sets the altimeter barometric pressure and the small knob adjusts the course The course is only adjustable when the HSI is in VORI VOR2 or OBS SUSP mode Pressing this knob centers the CDI on the currently selected VOR Selected Course provides course reference to the Flight Director when operating in Navigation and Approach modes 7 Dual COM Knob Tunes the MHz large knob and kHz small knob standby frequencies for the COM transceiver Pressing this knob switches the tuning cursor light blue box between the COM and COM2 fields 8 COM Frequency Transfer Key Switches the standby and active COM frequencies Pressing and holding this key for two seconds automatically tunes the emergency frequency 121 5 MHz in the active frequency field 9 COM VOL SQ Knob Controls COM audio level Pressing this knob turns the COM automatic squelch ON and OFF Audio volume level is shown in the field as a SECTION 1 SYSTEM OVERVIEW percentage 10 Direct to Key Allows the user to enter a destination waypoint and establish a direct course to the selected destination specified by the identifier chosen from the ac
90. hted press the ENT Key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest leg PAGE MENU OPT TONS Cancel Direct To NAV Press the FMS CRSR knob to return to bose page Figure 7 3 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol Identifier WPT Location Facility Name Flight Plan WPT Nearest WPT Bearing to WPT N 43 36 44 Lat Lon Distance from WPT wees Course to Selected WPT ACTIVATE Figure 7 4 PFD Direct to Window Press the Direct to Key E Turn the large FMS Knob to place the cursor in the desired selection field Turn the small FMS Knob to begin selecting the desired identifier location etc Press the ENT Key The cursor is now flashing on ACTIVATE Press the ENT Key again to activate Cancelling Direct to Navigation Press the Direct to GE Key Press the MENU Key to display the Options Window The cursor will be flashing on Cancel Direct to NAV Press the ENT Key to cancel the direct to Garmin G1000 Cockpit Reference Guide for the DA40 40F 136 975 Figure 7 5 Airport Information Page Select the Airport Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the first rectangular page icon Enter a Waypoint Facility Name or City Location With the Airport Information Page displayed press the FMS Knob to activa
91. irector in Vertical Speed Mode a Press the VS Key Altitude Hold Mode is armed automatically ee ROT ae ALT b Press the AP Key to engage the autopilot in Roll Hold and Vertical Soeed modes _ ROL JAP ALT S HDG Mode No me Selected Altitude of 7 000 MSL d me uei ode VSN 3 Activate Heading Select Mode while the autopilot is engaged in the climb a Use the HDG Knob to set the Selected Heading to 070 b Press the HDG Key The autopilot follows the Heading Bug on the HSI and turns the aircraft to the desired heading a HDG JAP ALT 4 As the aircraft climbs to the Selected Altitude the flight director changes from Vertical Speed to Altitude Hold Mode This active mode change is indicated by the green ALT annunciation flashing for ten seconds 5 Upon reaching the Selected Altitude the autopilot completes the capture process and levels the aircraft From this point the flight director continues to operate in Altitude Hold Mode 070 ALT Mode 5 Figure 6 20 Departure 6 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial c Press the NAV Key to arm Navigation Mode The white annunciation VOR appears to NOTE Changing the HSI mode cancels the left of the active roll mode Navigation Mode and causes the flight VOR HDG JAP ALT 7000rr7 director to revert to Roll Hold Mode 2 When the CDI shows
92. is GPS2 FAIL GPS2 is inoperative unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still GPS2 SERVICE GPS needs service be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still NAV2 SERVICE NAV2 needs service be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote os transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed NAV2 RMT XER NAV state Press the transter switch again to cycle its operation If the problem persists en eno the G1000 system should be serviced transter Key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 G S2 FAIL G S2 is inoperative system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service may still be available The G1000 system should be serviced when possible Return unit for repair GEA 71 Message Advisories Alerts Window Message Comments S O
93. iver Audio Transmitters E COM 3 is unavailable COM3 MIC is unavailable o Telephone Unavailable Passenger Address Speaker Marker Beacon Mute Marker Beacon Signal Sensitivity a Aircraft Navigation Radio Audio Aircraft Navigation Radio Audio ADF amp DME optional AUX 7 unavailable Manual Squelch Nau Recorded COM Audio Playback CREW PILOT con ICS Isolation ics ISOLATION PILOT O PASS VOL SO Volume Squelch VOL Annunciation SQ Annunciation Reversionary Mode DISPLAY BACKUP Figure 5 1 Audio Panel Controls Garmin G1000 Cockpit Reference Guide for the DA40 40F 5 1 SECTION 5 AUDIO PANEL Jz 5 1 COM RADIO SELECTION Pressing the COMI MIC or COM2 MIC Key selects the active transmitter i e microphone The associated receiver audio COMI or COM2 also becomes selected when the COM MIC Key is pressed To prevent deselecting the desired received audio when pressing another COM MIC Key press the already selected COMI or COM2 Key before pressing the other COM MIC Key Bn a wv COM1 MIC COM1 gt gt COM2 MIC COM2 Figure 5 2 Transceivers 5 2 MARKER BEACON RECEIVER The marker beacon receiver is always on Only the marker beacon audio can be turned off Figure 5 3 shows the marker beacon annunciators on the PFD When the MKR MUTE Key is pressed the key annunciator is lit and the audio tone can be heard ov
94. l Sisscisrotiisiainianiatsisrksisnaainan 4 4 4 6 Frequency Auto tuning 0 0ccccsssen 4 4 Auto tuning on the PFD sssri 4 4 A to tuning on the MFin 4 4 4 7 Transponder 4 5 Mode Selectie ovale ie eecee 4 5 Ground Mode AUtOMATIC ccecccscecesescssesesteseseeeee 4 5 ODI Sas A A A R E 4 5 CODE SEIO hotoke peen E 4 5 PIII RE DOT UNO canari 4 5 SECTION 5 AUDIO PANEL 0000 5 1 5 1 COM Radio Selection ccc 5 2 5 2 Marker Beacon Receiver ccccccceeeeen 5 2 Marker Beacon Signal Sensitivity c ssssesecsessseesseen 5 2 5 3 Nav Radio Audio Selection cccc 5 2 5 4 Intercom System ICS Isolation 5 3 5 5 Intercom Squelch Control 0 cccccces 5 3 5 6 Digital Clearance Recorder and Player 5 4 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 1 6 1 Mode Annunciations ccccsesseeeseeeees 6 1 6 2 Overspeed Protection ou 6 2 6 3 AP Engagement Disengagement 6 2 Automatic Disengagement ecssssessessssssseessnsseen 6 3 Manual Disengagement ccscesesessecsesseaseeseeren 6 3 Control Wheel Ste ring c scesessessecsessesseeseesessean 6 3 6 4 LOSS Of Data ccs 6 3 6 5 Pitch Axis Modes uu ccccsessessessseesseessessees 6 3 Pitch Hold Mode PIT o an 6 4 Altitude Hold Mode ALT enonisrirsinennioieiaisa 6 5 Vertical Speed Mode VS s s s 6 6 Flight Level Change Mode FLC c sess
95. lan the target reference waypoint itself can be specified from the waypoints contained in the flight plan By default the last waypoint in the flight plan is selected Highlight the desired waypoint Press the ENT Key 10 With the TARGET ALTITUDE field highlighted turn the small and large FMS Knobs to select Garmin G1000 Cockpit Reference Guide for the DA40 40F the target altitude It the selected altitude is above the current aircraft altitude a profiled climb is created If the selected altitude is below the current aircraft altitude a protiled descent will be created 11 Press the ENT Key The cursor is now placed in the TARGET VERTICAL SPEED field The default profile utilizes a 400 toot per minute descent rate 12 To change the vertical speed turn the FMS Knobs to enter the desired vertical speed Press the ENT Key when finished With the profile set the vertical speed required VSR is displayed Expect the following to occur when using the vertical navigation feature At one minute prior to reaching the Bottom Of Climb or Top Of Descent point gray arc the message APPR VPROF Approaching VNAV Profile is displayed as a PFD alert The descent or climb angle also locks to prevent changes in speed from altering the profile If selected the vertical speed required VSR readout on the default NAV and map pages shows the desired vertical speed to maintain the proper descent or climb angle At 5
96. ld Mode ALT 3 1 Press the ALT Key The flight director is activated if not already active and ALT is now displayed in green in the Active Mode Field with the current altitude displayed in the Altitude Reterence Field 2 Pitch commands will be given to manually maintain the current altitude Press the AP Key to engage the autopilot for maintaining the current altitude Altitude Hold mode is active newt 113 08 118 98 ITXD wer 118 98 ITXxD Flight Director command bars hold pitch attitude to maintain the altitude reference SECTION 6 AUTOMATIC FLIGHT CONTROL To change aircraft altitude press and hold the CWS button and manually maneuver to the desired altitude Upon reaching the desired altitude release the CWS button This new altitude is now displayed in the Altitude Reference Field The autopilot will now hold the aircraft at this altitude NOTE If the Selected Altitude is captured during CWS maneuvering the Flight Director altitude reference is not changed To adjust the altitude reference in this case the pilot must again press the CWS button after the Selected Altitude is captured Altitude Reference 118 788 com 123 808 COH2 Figure 6 11 Altitude Hold Mode Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Speed Mode VS 1 6 6 Flight Director command bars indicating a climb at the prescribed vertical speed to th
97. lder than 6 altitude level Teh amp moving debi moving in the is pressed a radar like 120 view is displayed ee resulting in in the direction of the line direction of the line Press the 360 Softkey to return to the 360 oast mode Figure 10 8 Traffic Map Page default display 4 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 JAP TERRAIN PROKIMTTY 136 975 20kT HOG LP 2 Press the TRAFFIC Softkey Traffic will now be displayed on the map TIS Audio Alert When a Traffic Advisory TA is displayed an audio alert Traffic is given Traffic Not Available will be heard whenever TIS service becomes unavailable Figure 10 9 Terrain Proximity Page Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE Color indication Displaying Terrain and Obstacles on the WARNING Terrain Obstacle at or within Navigation Map 100 below or above aircraft altitude 1 With the Navigation Map displayed press the CAUTION Terrain Obstacle between 100 MAP Softkey and 1000 below current aircraft altitude 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map Aircraft Altitude J oo Tiieshotd ELEV FT Maximum el MAX 181 dp raphy
98. leg using GPS e INTEG GPS information is either not present or is invalid for navigation use e WARN GPS detects a position error e SUSP Displayed when in OBS Mode indicating GPS waypoint sequencing is suspended Figure 2 20 GPS INTEG GPS SUSP LOC1 and VOR2 Enable disable OBS mode while navigating with GPS 1 Press the OBS Softkey to select OBS Mode 2 Turn the CRS Knob to select the desired course TO FROM the waypoint 3 Press the OBS Softkey again to return to normal operation Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 ENGINE DISPLAY In all cases green indicates normal operation yellow indicates caution and red indicates warning Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys which in turn provide access to the Lean Display and the System Display respectively Manifold Pressure Gauge RPM Gauge REN 3000 o 2320 Fuel Flow FUEL FLOW GPH Indicator LF CH Cylinder Head Lau Temperature Oil Temperature OIL TEMP Indicator Indicator y OIL PRES Oil Pressure FT Indicator AMPS Ammeter Fuel Quantity VOLTS Indicator scale Lm V Voltmeter is 0 25 with FUEL QTY GAL extended range R a fuel tanks A Figure 3 1 DA40 Default Engine Display SECTION 3 ENGINE INDICATION SYSTEM EIS we RPM Gauge RPM f 2310 e191 515 elon FUEL FLOW GPH Indicator Cylinder Head Temperature Indicat
99. lot s Guide documentation and the G1000 Flight Manual Supplement 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 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 Airman s Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo CAUTION The GDU 1040 PFD and GDU 1042 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F
100. ly RX receive only PT part time frequency Press the ENT Key to place the selected frequency in the standby tield of the COM or NAV Frequency Box To remove the cursor press the FMS Knob Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 3 SECTION 7 NAVIGATION 1 4 7 4 INTERSECTION INFORMATION Select the Intersection Information Page Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the second rectangular page icon 136 975 Figure 7 6 Intersection Information Page Access Information on an Intersection 1 With the Intersection Information Page displayed press the FMS Knob to activate the cursor Turn the FMS Knobs to enter a name for the identifier and press the ENT Key Press the FMS Knob to remove the flashing Cursor Figure 7 7 NDB Information Page Select the NDB Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to select the third rectangular page icon View Information on a Specific NDB 1 2 With the NDB Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired selection field identifier name or closest city Turn the FMS Knobs to enter an identifier name or city and press the ENT Key Press the FMS Knob to remove the flashing Cursor Garmin G1000 Cockpit Ref
101. mation From Peak for that cylinder to be displayed CHT Readout a Cylinder Head For Selected 4 Temperature Cylinder Bar Graph LERE aS Sa Sa a a a ao 1 Figure 3 4 DA40 LEAN Engine Display 3 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 ENGINE SYSTEM DISPLAY ae If desired use the DEC FUEL INC FUEL and RST y 29 10 3000 FUEL Softkeys to adjust the amount of fuel remaining for Staley totalizer calculations OILF 227 OIL PSI 63 0 NOTE Fuel calculations do not use the aircraft Information AMPS 44 fuel quantity indicators and are calculated from FFLOW GPH 8 0 the last time the fuel was reset FUEL CALC GAL REM 39 9 JE GAL USED 0 1 Fuel Calculation ENDUR Information RPM ne RANGE NM o 2210 SYSTEM OIL F 22 OIL PSI 63 0 System VOLTS 31 7 T AMPS 41 TTL TIME IN SVC Aircraft Total FFLOW GPH 0 0 Fuel Pressure 0000 8 HRS Time in Service Indi i E a he Figure 3 7 DA4OF Fixed Pitch Propeller DA40 SYSTEM Engine Display FUEL CALC GAL REM 39 9 GAL USED 0 1 Fuel Calculation ENDUR Information RANGE NM TTL TIME IN SVC Aircraft Total 000 0 HRS Time in Service Figure 3 6 DA40 SYSTEM Engine Display Garmin G1000 Cockpit Reference Guide for the DA40 40F 3 3 SECTION 3 ENGINE INDICATION SYSTEM EIS Blank Page 3 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 4 NAV COM
102. n Figure 12 2 Pressing the WARNING Softkey acknowledges the presence of the warning alert and stops the aural tone if applicable DYI SORY e CAUTION This level of alert indicates the Figure 12 4 ADVISORY Softkey existence of abnormal conditions on the aircraft Annunciation that may require pilot intervention A caution alert is accompanied by an annunciation in the Annunciation Window Caution text appearing in the Annunciation Window is YELLOW A caution alert is also accompanied by a flashing CAUTION Softkey annunciation as shown in Figure 12 3 Pressing the CAUTION Softkey acknowledges the presence of the caution alert Figure 12 3 CAUTION Softkey Annunciation e MESSAGE ADVISORY This level of alert provides general information to the pilot A message advisory alert does not issue annunciations in the Annunciation Window Instead message advisory alerts only issue a flashing ADVISORY Softkey annunciation as shown in Figure 12 4 Pressing the ADVISORY Softkey acknowledges the presence of the message advisory alert and displays the alert text message in the Alerts Window 12 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS 12 2 AIRCRAFT ALERTS The following alerts are configured specifically for the Diamond DA40 aircraft See the Flight Manual Supplement for information regarding pilot responses WARNING Alerts Alerts Window Message Continuous Aural Tone
103. n database update eliminates an obsolete way point The flight plan cannot tind the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database OR update the waypoint name identitier to reflect the new information Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 15 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont Alerts Window Message Comments S FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved aviation database update Verity that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired The system notifies the pilot that the timer has expired DB CHANGE Database changed This occurs when a stored flight plan contains procedures that have been manually Verity user moditied procedures edited This alert is issued only after an aviation database update Verity that the user moditied procedures in stored flight plans are correct and up to date FPL TRUNC Flight plan has been This occurs when a newly installed aviation database eliminates an obsolete ap truncated proach or arrival used by a stored flight plan The obsolete procedure is removed trom the flight plan Update flight plan with current arrival or approach APPR VPROF Approaching
104. n the TAWS Page as a yellow or red X Imminent Terrain Impact ITI and Imminent Obstacle Impact 101 This provides alerts when the aircraft is below the elevation of terrain in the aircrafts projected path ITI and IOI alerts are accompanied by a potential impact point displayed on the TAWS Page as a yellow or red X The alert is given when the projected vertical flight path is calculated to come within minimum clearance altitudes in the following table A Premature Descent Alert is issued when the system detects that the aircraft is significantly below the normal approach path to a runway The PDA alert mode functions only during descent to land PDA alerting begins when the aircraft is within 15 nm of the destination airport and ends when the aircraft is either 0 5 nm from the runway threshold OR is at an alti tude of 125 feet AGL while within 1 nm of the threshold During the final descent algorithms will set a threshold for alerting based on speed distance and other param eters Runway Threshold PDA Alerting Area 1 2 NM 5 NM 15 NM Figure 10 15 PDA Alerting Excessive Descent Rate Alert EDR The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined Garmin G1000 Cockpit Reference Guide for the DA40 40F to be closing descending upon terrain at an excessive speed Figure 10 16 displays the correlation between height above terrain and descent rate re
105. n the large FMS Knob to highlight the ADF tuning field 2 Turn the small FMS Knob to enter the first digit 3 Turn the large FMS Knob to select the next desired digit field Turn the small FMS Knob to again select the desired digit 4 When the desired frequency is entered press the ENT Key to transfer the frequency into the active field 5 Turn the large FMS Knob to select the MODE field Turn the small FMS Knob to select ADF or BFO 6 Turn the large FMS Knob to select the volume field if desired Turn the small FMS Knob to adjust the ADF volume to the desired level 7 Press the FMS Knob to exit all the fields ADF DME TUNING ae 190 0 MODE 4 ADF gt VoL 507 DME MODE NAV ENT TO TRANSFER XPDR 1200 STBY j LCL 16 52 54 ADF DME XPDR IDENT TMR REF NRST WARNING Figure 4 7 ADF DME Tuning Window Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 3 SECTION 4 NAV COM amp TRANSPONDER DME Radio optional 4 6 ADF DME TUNING ADF 190 0 MODE4BFO gt voL 50 DME MODE MENA Figure 4 8 ADF DME Tuning Window Change the DME tuning source 1 2 4 4 From the tuning window turn the large FMS Knob to highlight the desired DME source 1 Turn the small FMS Knob to display the selection window Turn the FMS Knob to select 2 the desired mode and press the ENT Key 3 4 Figure 4 9 DME Selection Window FREQUENCY AUTO TUNING Auto tuning on the PFD NEAREST AIRPORTS
106. ng valid data Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 7 SECTION 12 ANNUNCIATIONS amp ALERTS A red X may be the result of an LRU or an LRU function failure The Figure 12 6 illustrates all possible flags and the responsible LRUs GIA 63 Integrated Avionics Units f GIA 63 Integrated Avionics Units at HU J GDC 4A Air Data N j Computer r 5 y F N P FUEL FLOW GPH E L cee N GRS 77 AHRS GEA 71 Engine CHT p OR i J GMU 44 Magnetometer Airframe Unit OR GIA 63 Integrated Avionics Unit OIL TEMP a A OIL PRES erT AMPS e A RA f T yp GIA 63 Integrated om Avionics Units FUEL QTY GAL ches ENGINE CDI OBS XPOR IDENT TMREREF NRST ALERTS GDC 744A Air Data GTX 33 Transponder Computer OR P GIA 63 Integrated Avionics Units Figure 12 6 G1000 System Failure Annunciations 12 6 G1000 SYSTEM MESSAGE ADVISORIES This section describes various G1000 system message advisories Certain messages are issued due to an LRU or an LRU function failure Such messages are normally accompanied by a corresponding red X annunciation as shown previously in the G1000 System Annunciation section NOTE This section provides information regarding G1000 message advisories that may be displayed by the system Knowledge of the aircraft systems flight conditions and other existing operational priorities must be considered when responding t
107. normal operation of the GDL 69 A and it should have no adverse effects if inadvertently selected during flight Refer to the GDL 69 69A XM Satellite Radio Activation Instructions 190 00355 04 Rev E or later for further information Weather Product Age The age for each of the enabled products is displayed on the right side of the display Times are based on Zulu time when the data was assembled on the ground not the time the data was received by the XM receiver When the age of a weather product has exceeded half of the expiration time the product time will change from light blue to amber in color a Echo Top Cloud Top and Echo Top Mutually Exclusive Figure 10 7 Weather Product Symbols Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE Weather Product Expires After 10 3 TRAFFIC INFORMATION SERVICE TIS innate JQ Wore atc fomation sence TIS i ont Ialric inrormation service IS ONLY SIGMETS AIRMETs OO available when the aircraft is within the service City Forecasts ss 0 volume of a TIS capable terminal radar site County Warnings o splay tf tf Cyclone Warnings oO Displaying Traffic on the Traffic Map Page Echo Tops 0 1 Turn the large FMS Knob to select the Map Freezing Levels a Page Group METARS a 2 Turn the small FMS Knob to select the second Lightning rectangular page icon NEXRAD 3 Press the OPERATE Softkey to begin displaying traffic TIS OPERATIING is displayed in
108. nseshiieni 8 2 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 8 4 Activate a Flight Plan Leg 0 8 3 8 5 Stop Navigating a Flight Plan 8 3 8 6 Invert Active Flight Plan ee 8 3 ii Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 7 Create a New Flight Plan 0 0 0 Create a New Flight Plan Using the MFD nsss Create a New Flight Plan Using the PFD uu 8 8 Load a Departure ou ccs 8 9 Load an AMV fcciisisecedtisecctiiiocestctaeccdionuseciecse 8 10 Load an Approach uses 8 11 Remove a Departure Arrival or Approach from a Flight Plan cece eee 8 12 Store a Newly Created Flight Plan 8 13 Edit a Stored Flight Plan 8 14 Delete a Waypoint from the Flight Plan 8 15 Invert and activate a Stored Flight Plan 8 16 Copy a Flight Plann cess 8 17 Delete a Flight Plan eee 8 18 Graphical Flight Plan Creation 0 8 19 Trip Planning 0 0 c cece 8 20 Vertical Navigation VNAV Page Create a Vertical Navigation Profile VNAV Page Menu Options cscsssssssesesen SECTION 9 PROCEDURES w 9 1 Arrivals and Departures Load and Activate a Departure Procedure c c00e Load and Activate an Arrival Procedure 9 2 Approaches ou ccccsscesstesssesseeseesesseeanees
109. o a message Always use sound pilot judgment The Aircraft Flight Manual takes precedence over any conflicting guidance found in this section 12 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories Message Comments S O DATA LOST Pilot stored data was The pilot profile data was lost System reverts to default pilot profile and settings lost Recheck settings The pilot may reconfigure the MFD amp PFD with preferred settings if desired XTALK ERROR A flight display The MFD and PFD are not communicating with each other The G1000 system should crosstalk error has occurred be serviced PFD1 SERVICE PFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be MFD1 SERVICE MFD1 needs serviced service Return unit for repair PFD1 CONFIG PFD1 configuration error Contig service req d The PFD and or MFD configuration settings do not match backup configuration MFD1 CONFIG MFD1 configuration memory The G1000 system should be serviced error Contig service req d SW MISMATCH GDU software The MFD and PFD have different software versions installed The G1000 system mismatch Xtalk is off should be serviced MANIFEST PFD1 software mismatch Communication halted The PFD and or MFD has incorrect software installed The G1000 system should be MANIFEST MFD1
110. ode This cancels VOR mode on the HSI and the flight director loses the VOR signal As a result the VOR annunciation flashes yellow Flashes for ten seconds then transitions to ROL b Press the NAV Key to activate GPS Navigation Mode to cause the autopilot to steer the aircraft toward the active flight plan leg 23 0 Clovis VORTAC CZQ Panoche VORTAC PXN Figure 6 22 Transition to GPS Flight Plan 6 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL Flight Level Change Descent 2 Reduce power to allow descent in Flight Level While flying the GPS leg from Panoche VORTAC to The autopilot maintains the Clovis VORTAC the aircraft is cleared to make a descent BOP ae to 3000 feet in preparation for the approach to KFAT 3 Upon capturing the Selected Altitude the flight 1 Enter Flight Level Change Mode director changes trom Flight Level Change to Altitude Hold Mode The annunciation ALT a Using the ALT Knob set the Selected Altitude flashes in green to indicate the altitude capture to 3000 feet After the capture is complete the autopilot holds b Press the FLC Key to activate Flight Level the aircraft level at the Selected Altitude Change Mode The annunciation FLC appears next to the Airspeed Reference ANNES CTSA ET S171 which defaults to the current aircraft airspeed 142 knots Altitude Hold Mode is armed automa
111. old Mode automatically Subsequent autopilot engagement is also allowed If the pitch attitude is changed manually e g with the CWS button or the NOSE UP NOSE DN Keys Pitch and Roll Hold modes will automatically be selected Glideslope GS A NOTE Pressing the CWS button while Glideslope Mode is active does not cancel the mode The autopilot guides the aircraft back to the glides lope upon release of the CWS button Glideslope Mode is only available when the flight di rector has been set for approach Glideslope Mode is au tomatically armed under the following conditions e Valid localizer frequency is tuned Horizontal Situation Indicator HSI is in LOC mode with valid deviation indication e Valid glideslope deviation APR Key is pressed Autopilot disconnect annunciation Go Around mode is ac flashes yellow for 5 seconds tive in both pitch axis amp roll axis modes NAN 114 10 SJC wer Flight Director command bars indicating climb COI Figure 6 14 Go Around Mode 118 200 121 358 com 136 975 COH2 dani IDENT 6 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 6 ROLL AXIS MODES Mode annunciations for active roll axis modes are shown in green during normal operation Key FD AP only Roll Hold Default Heading Select HDG VOR Enroute Arm Capture Track GPS Arm Capture Track GPS BC Arm Capture Track OC NAV LOC Arm Capture Track No Glideslope G
112. on the inset map XM LTNG optional Press to display the XM Radio lightning data on the inset map BACK Press to return to the previous level softkey configuration ALERTS Press to display the Alerts Window PFD Press to display the additional softkeys for additional configuration of the PFD METRIC Press to display the current and reference altitudes in meters in addition to feet Pressing the metric softkey also changes the barometric setting to hectopascals DFLTS Press to reset default settings on the PFD DME optional Press to display the DME Information Window BRG bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the the appropriate information Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW INSET optional optional oN GN GON TT E MmmnnMRnMnNn ND Press the BACK or OFF Softkey to return to the top level softkeys Figure 1 3 PFD Softkey Flow Chart 1 PFD tional nnMonMnononnnnnn D Press the DFLTS Softkey to change the PFD metric values to standard Press the STD BARO or BACK Softkey to return to the top level softkeys Figure 1 4 PFD Softkey Flow Chart 2 BRG2 bearing Press to cycle through the following Nav sources making the pointer the NAVI Displays NAV1 waypoint frequency or identifier and DME information in the BRG1
113. ond DA40 Aircraft Flight complete system are found in the G1000 Pilots Guide Manual Supplement AF MS for limitations 190 00592 02 procedures and operational information not contained in this Cockpit Reference Guide The Diamond DA40 Aircraft Flight Manual Supplement always takes precedence over the information found in this guide Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 1 SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS OQ Oo 0O oO s lt gt COM EMERG PUSH 1 2 CRS A4 BARO PUSH PUSH HDG SYNC CRS CTR RANGE A Figure 1 1 PFD MFD Controls OFLT ale F Mi S O PUSH CHSH MFD Only with optional GFC 700 1 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F PFD and MFD controls function the same with the exception of the dedicated Automatic Flight Control System AFCS keys located only on the MFD bezel 1 NAV VOL ID Knob Controls the NAV audio level Press to turn the Morse code identifier ON and OFF Volume level is shown in the field as a percentage 2 NAV Frequency Transfer Key Switches the standby and active NAV frequencies 3 Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV receiver Press to switch the tuning cursor light blue box between the NAV1 and NAV2 fields 4 Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the
114. or Oil Temperature Indicator Oil Pressure Indicator Ammeter Voltmeter Fuel Quantity Indicator Figure 3 2 DA4OF Fixed Pitch Propeller Default Engine Display Fuel Pressure Indicator Option DA40 only Located between the Fuel Flow and CHT Indicators and shows the fuel pressure in pounds per square inch e Green Normal Red Warning minimum and maximum Figure 3 3 Fuel Pressure Indicator Showing Warning Garmin G1000 Cockpit Reference Guide for the DA40 40F 3 1 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 LEAN ENGINE DISPLAY Cylinder Select The CYL SLCT Softkey can be utilized to obtain a information about a particular cylinder The CYL SLCT Softkey becomes disabled when a particular cylinder turns yellow or red until the temperature decreases and returns to normal or when the ASSIST Softkey is pressed Exhaust Gas Temperature Bar Graph EGT Readout Temperature EGT F 1653 For Selected JE Deviation APEAK 17 F Cylinder From Peak MAN IN w 24 4 Cylinder Head 219 yo f4 Temperature can FFLOW GPH 0 0 ra CHT F 453 Hollow Bar Figure 3 5 DA4OF Fixed Pitch Propeller Exhaust Gas ee Representing Peak LEAN Engine Display Temperature Bar Graph 46 i Pe iy SEED ESE Pressing the ASSIST Softkey causes the first cylinder Ginger EM bahia EGT that peaks to become highlighted and informati ylinder APEAK 54 F Deviation at peaks to become highlighted and infor
115. own down direction Aileron Mistrim Right ATI 4 condition has developed causing the roll servo to provide a sustained right force Preflight Test PFT Performing preflight system test Upon completion of the test the aural alert will be Preflight system test has Tailed Aileron Mistrim Lett AT A condition has developed causing the roll servo to provide a sustained left force 12 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 TAWS ALERTS Annunciations appear on the PFD and MFD Pop up alerts appear only on the MFD PFD MFD TAWS Alert Type Page Me Map nage T Pop Up Alert Annunciation Excessive Descent Rate Warning EDR PULL UP Pull Up Reduced Required Terrain Clearance Warn PULL UP Terrain Terrain Pull Up Pull Up ing RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up or or Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning 101 PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up OF or Obstacle Obstacle Pull Up Pull Up Aural Message Reduced Required Terrain Clearance Caution Caution Terrain Caution Terrain Terrain
116. pproach SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI approach to the correct NAV receiver NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check position waypoint for navigation Xxxx with alternate navigation sources TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data trom the traffic system The traffic device failed should be serviced Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 17 SECTION 12 ANNUNCIATIONS amp ALERTS Blank Page 12 18 Garmin G1000 Cockpit Reference Guide for the DA40 40F A Abnormal COM operation 11 2 Activate a flight plan 8 3 Active flight plan 8 2 ADF 1 5 4 3 ADVISORY 12 1 Advisory alerts 12 3 AFCS 1 3 6 1 6 4 6 6 6 7 6 9 6 11 6 12 6 13 12 4 Age 10 4 AHRS 12 14 Aircraft alerts 12 3 AIRMET 10 3 Airport frequency 7 6 Airport information 7 3 Airspace alerts 7 9 Airspeed indicator 2 3 Airspeed trend vector 2 3 Alerting System 12 1 Alerts 12 1 Alert levels 12 2 Alert Pop Up 10 12 Altitude Hold 1 4 Altitude hold 1 4 6 3 6 8 6 10 Altitude trend vector 2 4 ALT knob 1 4 Annunciations 12 1 AP 1 4 6 1 6 7 6 9 12 4 Approaches 9 2 Approach activation 4 4 Approach markers Signal augmentation 5 2 Approach Mode 6 12 AP disconnect 6 1 Arrivals 9 1 ASSIST 3 2 Attitude indicator 2 3 Audio alerting system 12 2
117. press the ENT Key Turn the large FMS Knob to place the cursor in the desired locations for entering changes Turn the FMS Knobs to make the desired changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the Cursor Turn the large FMS Knob to select the waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window Remove KCRQ OK or CANCEL Figure 8 14 Remove Waypoint Confirmation 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 5 SECTION 8 FLIGHT PLANNING 8 15 8 6 INVERT AND ACTIVATE A STORED FLIGHT PLAN From the Flight Plan Catalog Page press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Press the INVERT Softkey Invert and activate stored flight plan will be displayed With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN From t
118. rily charted and therefore may not be contained in the obstacle database Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW These databases are not stored internally in the MFD or PFD Supplemental Data Cards containing identical database versions must be kept in both displays to retain ae terrain and obstacle data A Supplemental Data Card i ilre should be inserted into the bottom card slot of the PFD eE and MFD Version 2 00 Copyright 2003 Garmin Ltd or its subs GARMIN CORPORATION 1995 2003 NOTE If the Supplemental Data Card is eee ee aati removed from the display the TOPO and TER as on aid to situational bina RAIN softkeys are not functional and are grayed out on the MFD Map Page US Obstocle Dotobose Version 2 48 Looyright 2H 1 Insert one card in the bottom card slot of the MFD and one in the bottom card slot of the PFD 2 Apply power to the G1000 System View the MFD power up splash screen Check that the Terrain and Obstacle databases are initialized and displayed on the scrolling window of the splash screen Figure 1 11 Power Up Splash Screen Window 3 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 4 Atthe MAP NAVIGATION MAP page select the MAP Softkey and check to make sure that the TOPO and TERRAIN softkeys are functional not grayed out 5 Power down the G1000 1 10 Garmin G1000 Cockpit Reference Guide for
119. rmation 8 5 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 Figure 8 6 Delete Flight Plan 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 8 7 SECTION 8 FLIGHT PLANNING the flight plan This will not delete the stored flight plan only the active flight plan Figure 8 7 Delete Flight Plan Confirmation INVERT ACTIVE FLIGHT PLAN From the Active Flight Plan Page press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan and 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 Figure 8 9 Invert Flight Plan Confirmation CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 3 SECTION 8 FLIGHT PLANNING 2 Press the NEW Softkey to display a blank flight plan window for the first empty storage location STORED FLIGHT PLAN Figure 8 10 Create FPL on MFD Turn the small FMS Knob to display the Waypoint Information Window Turn the small FMS Knob to enter the first c
120. ronienannnninoninan 2 3 Vspeed RETEreNCeS eaa a 2 3 2 2 Attitude Indicator 0 0 0 css 2 3 2 3 Altimeter cscs tessa 2 4 Altitude Select BUG arsson 2 4 Aetea VOC Ol a nvereiecctinecen 2 4 Barometric Setting BOX scin2 an erionacuanetevadencenavatuandnae 2 4 Aide ATIN ona 2 4 Barometric Minimum Descent Altitude csseseees 2 4 2 4 Marker Beacon Annunciations 2 5 2 5 Vertical Deviation Glideslope Indicator 2 5 2 6 Vertical Speed Indicator 0 cccees 2 5 2 7 Horizontal Situation Indicator HSI 2 5 COUE POINTE car orrn E N 2 6 Course Deviation Indicator CDI 2 7 Bearing Pointers and Information Windows 2 7 DME Opona seannsa 2 7 A VIOATON SOURCE T S 2 7 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 1 3 1 Engine Display 0 0 cccccse cesses 3 1 Fuel Pressure Indicator Option DA40 only 3 1 3 2 Lean Engine Display 0 0 ccccscceseeceen 3 2 ROET a A eat irea tes cuted naenemennerts 3 2 3 3 Engine System Display 0 cccccseseees 3 3 SECTION 4 NAV COM AND TRANSPONDER 4 1 4 1 Radio Status IndicationS 0 cccccseen 4 3 42 Nol M nouisinssiieeniiiceienineiiea 4 3 TABLE OF CONTENTS 4 3 Automatic Squelch cee 4 3 4 4 Quickly Activating 121 500 MHZ 4 3 4 5 Optional NAV Radios 0 0 cccceeeen 4 3 ADF RAGOLODUONAI artarena ienai 4 3 DMERadio Optiona
121. sed for supplemental navigation guidance only If the GPS receiver cannot be used for primary guidance the appropriate navigation receiver must be used for the selected approach e g VOR or ILS The final course segment of ILS approaches for example must be flown by tuning the Nav receiver to the proper frequency and selecting that Nav receiver on the CDI Load and or Activate an Approach Procedure 1 With the Navigation Map Page displayed press the FPL Key 2 Press the LD APR Softkey If a flight plan is active the destination airport will be displayed as the default A list of available approaches is also displayed 3 If no flight plan is active use the FMS Knobs to enter the identitier of the desired airport Press the ENT Key 4 Turn the large FMS Knob to highlight the Approach field Turn the small FMS Knob to display a list of available approaches Figure 9 6 Selecting an Approach Procedure Turn the FMS Knobs to highlight the desired approach Press the ENT Key Ul Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 The cursor will move to the TRANSITIONS field Turn the large FMS Knob to highlight the desired transition waypoint and press the ENT Key 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 Figure 9 7 Selecting an Approach Transition Turn the large FM
122. ses 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F WARNINGS CAUTIONS amp NOTES WARNING The Garmin G1000 as installed in the Diamond DA40 aircraft has a very high degree of functional integrity However the pilot must recognize that providing monitoring and or self test capability for all conceivable system failures is not practical Although unlikely it may be possible for erroneous operation to occur without a fault indication shown by the G1000 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pi
123. sulting in the two EDR alerts EDR alerts have two levels of severity caution sink rate and warning pull up 5000 4500 4000 3500 3000 2500 2000 1500 Height Above Terrain Feet 6000 8000 Descent Rate FPM Figure 10 16 Excessive Descent Rate Negative Climb Rate After Takeoff Alert NCR The purpose of the Negative Climb Rate After Takeoff alert is to provide suitable alerts to the pilot when the system determines that the aircraft is losing altitude closing upon terrain after takeoff The aural message Don t Sink is given for NCR alerts accompanied by an annunciation and a pop up terrain alert on the display Unlighted Obstacle Height is less than 1000 AGL Lighted Obstacle Height is less than 1000 AGL 1000 AGL Unlighted Obstacle Height is greater than SECTION 10 HAZARD AVOIDANCE Five Hundred Aural Alert The purpose of the aural alert message Five hundred is to provide an advisory alert to the aircrew that the aircraft is five hundred feet above terrain When the aircraft descends within 500 feet of terrain the aural message Five hundred is heard There are no display annunciations or pop up alerts that accompany the aural message Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle pro
124. te a Departure Procedure 1 2 With the Navigation Map Page displayed press the FPL Key Press the LD DP Softkey If a flight plan is active the departure airport will be displayed as the default A list of available departures is also displayed If no flight plan is active use the FMS Knobs to enter the identifier of the desired airport Press the ENT Key Turn the large FMS Knob to highlight the Departure field Turn the small FMS Knob to display a list of available departures Turn either FMS Knob to select the desired departure and press the ENT Key AIRPORT KTD RAL PUBLIC NEW CENTURY ATRCENTER DEPARTURE Figure 9 1 Select Departure A list of runways may be displayed for the departure Turn either FMS Knob to select the desired runway and press the ENT Key A list of available transitions is displayed for the departure Turn either FMS Knob to highlight the desired transition waypoint and press the ENT Key 8 SECTION 9 PROCEDURES DEPARTURE CHIEFS RUNWAY ALL TRANSITION CATTS Figure 9 2 Select Departure Transition With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active Load and Activate an Arrival Procedure 1 2 With the Navigation Map Page displayed press the FPL Key Press the LD STAR Softkey If a flight plan is active the destination airport will be displayed as the default A list of available arrivals is
125. te the cursor Turn the large FMS Knob to select the facility name or location city field Turn the small FMS Knob to select the desired first character Turn the large FMS Knob to select the next character field Repeat steps 3 and 4 until the facility name or location is selected then press the ENT Key If there are duplicate names in the database 6 SECTION 7 NAVIGATION a list is displayed from which to choose the desired location To remove the flashing cursor press the FMS Knob Access Runway Information With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to place the cursor on the RUNWAYS identifier field Turn the small FMS Knob to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway To remove the flashing cursor press the FMS Knob Access Frequency Information 1 2 3 5 With the Airport Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS Knob to move the cursor to the Frequencies Box Turn either FMS Knob to scroll through the list placing the cursor on the desired frequency It a listed frequency has sector or altitude restrictions the frequency is preceded by an info i designation Press the ENT Key to view the information The following may be displayed with the frequency TX transmit on
126. the T a Traffic Mode field Ual 4 Press the STANDBY Softkey to place the system Surface Analysis oo in the Standby mode TIS STANDBY will be TR displayed in the Traffic Mode field Winds Aloft oO 5 Rotate the Joystick clockwise to display a larger Ts iP area or rotate counter clockwise to display a Clouds Tops a smaller area If data is not received fora period longer than 6 seconds the age of the present data will be displayed in the lower left of of the screen along with the annuciation that the system has entered Coast mode The system will maintain the traffic display up to 60 seconds until the next data reception If no data is received after 60 seconds traffic will be removed from the display Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 5 SECTION 10 HAZARD AVOIDANCE 10 6 paffemode ieie Aton areas 400 above fic outoy 10 4 TERRAIN AND OBSTACLE PROXIMITY ng moving in the direction o range 136 975 A NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the last rectangular page icon 3 If desired press the VIEW Softkey to access the ARC and 360 Softkeys When the ARC Softkey Last data update Proximity Traffic at same Traffic 1600 above amp Ota te A is o
127. the BACK Softkey on this level to return to the top softkey level 7 rs Press to return to the top softkey level optional optional gt Rare A SH a D A rs Ae A nD Press the ENGINE or BACK Softkey on any level to return to the default page level The DONE Softkey changes to UNDO when the checklist SYSTEM evi sicr ASSIST item is already checked ry fy ry NANN D D mw A A CLR nm n ry Figure 1 6 MFD Softkeys Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 7 SECTION 1 SYSTEM OVERVIEW TRAFFIC Pressing this softkey displays removes Traffic on the Navigation Map TOPO Pressing this softkey displays or removes topographic information on the Navigation Map TERRAIN Pressing this softkey displays removes terrain and obstacle data on the Navigation Map NEXRAD optional Pressing this softkey displays removes precipitation data on the Navigation Map XM LING optional Pressing this softkey displays removes XM Radio lightning data on the Navigation Map BACK Pressing this softkey displays the ENGINE and MAP top level softkeys DCLTR declutter Pressing this softkey removes map information in three levels 1 4 MFD PAGE GROUPS 1 Turn the large FMS Knob until the desired page group is selected 2 Turn the small FMS Knob to select pages within the group See Figure 1 7 Nearest Group Auxiliary Page Group Waypoint Page Group Map Page Group 1 5 BACKLIGHTING When s
128. the selected altitude will be maintained If only the flight director is engaged pitch and roll commands are given to manually maintain the selected altitude Vertical Speed Reference Vertical Speed mode is active Nav 118 98 ITXD wer nov2 115 98 118 98 ITxXD PFD 06S CDI XPOR Figure 6 12 Vertical Speed Hold Mode Altitude Hold is Armed en Selected Altitude Selected Vertical Spee Vertical Speed Reference Bug K coo SIBY 2542 IDENT THR REF NRST ALERTS Garmin G1000 Cockpit Reference Guide for the DA40 40F Flight Level Change Mode FLC 1 Selected Airspeed Airspeed Reference Bug Select the desired altitude by turning the ALT Knob to set the altitude in the Altitude Select Box This altitude must be selected first because Flight Level Change mode will only fly toward a selected altitude Press the FLC Key The flight director is activated if not already active and FLC is now displayed in green in the Active Mode Field and the Airspeed Bug will appear on the Airspeed Indicator Pitch commands are given to manually maintain airspeed Press the AP Key to engage the autopilot for maintaining the current airspeed Altitude Hold mode is automatically armed with ALT displayed white in the Armed Mode Field to the right of the FLC annunciation The Airspeed Bug can be adjusted in 1 knot increments by pressing the NOSE UP NOSE DN Keys to set the desired airspeed The airspeed s
129. thin the square area 10 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F ECHO TOP Press the ECHO TOP Softkey to show the location elevation and direction the highest radar echo This may not indicate the top of a storm or clouds only the highest radar return echo ECHO TOPS cannot be displayed along with NEXRAD and CLOUD TOPS When ECHO TOPS is activated NEXRAD and CLOUD TOPS are removed Refer to the Legend for a description of the ECHO TOPS coding The display is updated every 7 5 minutes CLD TOP Press the CLD TOP Softkey to show the cloud top altitude determined from satellite imagery The display is updated every 15 minutes LING Pressing the LING Softkey shows the location of cloud to ground lightning strikes The display is updated every five minutes NOTE Strikes depicted represent cloud to ground strikes within a 2 kilometer radius of the actual strike location Therefore the exact location of the strike is not displayed CELL MOV Pressing the CELL MOV Softkey shows storm cell movement by displaying an arrow pointing in the direction of predicted movement The display is updated every 12 minutes SIG AIR Pressing the SIG AIR Softkey shows SIGMET and AIRMET information The display is updated every 12 minutes METAR Press the METAR Softkey to graphically display METARs METARS are shown as colored flags at airports providing METAR reports The display is updated every 12 minutes
130. tically _ GPS AP TALT Cruise Altitude of 7 000 MSL 3 NNN Selected Altitude of 3 000 MSL ALT Hold Mode Figure 6 23 FLC Descent Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 17 SECTION 6 AUTOMATIC FLIGHT CONTROL ILS Approach 3 In preparation for approach tune the localizer 7 a frequency and select LOC mode on the HSI 1 Transition trom GPS Navigation Mode to Heading Select Mode a Load the Runway 29R ILS approach for KFAT into the Flight Plan 4 Press the APR Key when cleared for approach to arm the Approach Mode LOC and GS appear in the armed roll and pitch mode fields respectively b Select Vectors to Final for the transition The autopilot and flight director determine when c Set the Selected Heading after getting vectors to begin the turn to intercept the final approach from ATC and press the HDG Key The autopilot course turns the aircraft to the desired heading LOC HDG IAP ALT 3000r GS HDG JAP ALT 300077 5 The autopilot flies the ILS Approach At the 2 Use Heading Select Mode to comply with ATC Decision Height there are two options push the vectors as requested AP DISC switch and land the aircraft or use the GA button to execute a missed approach refer to the following procedure Figure 6 24 ILS Approach to KFAT 6 18 Garmin G1000 Cockpit Reference Guide for the DA40 40F Go Around Missed Approach 1 Push the GA button at the Decision
131. tion Scale G Navigation Source Aircraft Symbol G Course Deviation Indicator 6 Rotating Compass Rose Q OBS Mode TO FROM Indicator C Heading Bug 10 Course Pointer Flight Phase 12 Turn Rate and Heading Trend Vector Heading Lubber Line Figure 2 12 Horizontal Situation Indicator 360 Turn Rate Indicator and Heading Trend Vector Tick marks to the left and right of the lubber line denote halt standard and standard turn rates A magenta turn rate trend vector shows the current turn rate The end of the trend vector gives the heading predicted in six seconds based on the present turn rate At rates greater than 4 deg sec an arrowhead appears at the end of the magenta trend vector and the prediction is no longer valid Half Standard Turn Rate Tick Mark Tiri Rae Standard Turn Trend Vector Rate Tick Mark rate gt 4 fA deg sec Turn Rate Trend Vector standard rate Figure 2 14 Standard Rate Turn Indication Course Pointer The Course Pointer is a single line arrow GPS VORI and LOC1 or double line arrow VOR2 and LOC2 which points in the direction of the set course Lateral Deviation Course Deviation Scale TO FROM Indicator Figure 2 15 Arc CDI and Compass Rose CDI Garmin G1000 Cockpit Reference Guide for the DA40 40F Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight enroute 5 0 nm terminal area 1 0 nm or approach 0 3 nm Scalin
132. tion scenarios are addressed in Table 5 Pressing the small VOLU SQ Knob now switches CREW between volume and squelch adjustment by lighting VOL PILOT COPLT or SQ respectively ICS ISOLATION wv Figure 5 6 ICS Isolation MAN PLAY Y CREW wv PILOT COPLT ICS ISOLATION PILOT O PASS Figure 5 7 Volume Squelch Control PILOT KEY COPLT KEY Pilot Hears Conilot Hears Passenger ANNUNCIATOR ANNUNCIATOR p Hears Selected radios Selected radios Selected radios pilot copilot pilot copilot pilot copilot passengers passengers passengers MUSIC 1 MUSIC 1 MUSIC 2 Selected radios copilot l aa lot Passengers passengers P MUSIC 1 MUSIC 2 PILOT Selected radios Selected radios pilot passengers Copilot pilot passengers MUSIC 1 MUSIC 2 COPILOT Selected radios Selected radios Passengers pilot copilot pilot copilot MUSIC 2 Table 5 1 ICS Isolation Modes Garmin G1000 Cockpit Reference Guide for the DA40 40F 5 3 SECTION 5 AUDIO PANEL 5 6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded in a memory block When the next transmission is received it is recorded in the next memory block and so on Once the 2 5 minutes of recording time has been reached the recorder begins recording over the stored memory blocks starting from the oldest block Powering off the unit automatically clears all recorded blocks v v MAN SQ
133. tive route or taken from the map pointer position 11 FPL Key Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans 12 CLR Key DFLT MAP Erases information cancels an entry or removes page menus To display the Navigation Map Page immediately press and hold CLR MFD only 13 Dual FMS Knob Used to select the page to be viewed only on the MFD The large knob selects a page group MAP WPT AUX NRST while the small knob selects a specific page within the page group Pressing the small knob turns the selection cursor ON and OFF When the cursor is ON data may be entered in the different fields using the small and large knobs The large knob is used to move the cursor on the page while the small knob is used to select individual characters for the highlighted cursor location When the G1000 displays a list that is too long for the display screen a scroll bar appears along the right side of the display indicating the availability of additional items within the selected category Press the small FMS Knob to activate the cursor and turn the large FMS Knob to scroll through the list 14 MENU Key Displays a context sensitive list of options This list allows the user to access additional features or to make setting changes that relate to certain pages 15 PROC Key Selects approaches departures and arrivals from the flight plan If a flight plan
134. ture Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Alerts Window Message Comments S GIA1 SERVICE GIA1 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 GIA2 SERVICE GIA2 needs service system should be serviced Return the unit for repair HW MISMATCH GIA hardware There is a hardware mismatch between GIA1 and GIA2 The G1000 system should mismatch Communication halted be serviced MANIFEST GIA1 software mismatch Communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should MANIFEST GIA2 software mismatch be serviced Communication halted COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power COM1 SERVICE COM1 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may COM2 SERVICE COM 2 needs still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk ke a i j The COM1 and or COM2 external push to talk switch is stuck in the enable or COM2 PTT COM oushttotalk k pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced CO
135. uide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL 6 7 EXAMPLE PROCEDURES USING AFCS NOTE The diagrams in the following examples This section provides a scenario based set of procedures are for instructional purposes only and may not showing various autopilot modes used during a flight In be used for navigation this scenario the aircraft departs Reid Hillview Airport KRHV from runway 13L enroute to Fresno Yosemite International Airport KFAT Climb to an altitude of 7 000 feet MSL and fly a heading of 070 degrees to intercept airway V107 Fly airway V107 to Panoche VORTAC PXN using VOR navigation then fly airway V230 using a GPS flight plan Prior to reaching Clovis VORTAC CZQ descend to 3 000 feet and load the ILS approach to R29R at KFAT Fly the ILS approach and execute a missed approach KRHV 3 _ 23 0 X Clovis VORTAC o CZQ Panoche i VORTAC a Gv PXN Figure 6 19 Flight Plan Overview Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 13 SECTION 6 AUTOMATIC FLIGHT CONTROL Departure Climb to the selected altitude and fly an assigned heading 1 Upon takeoff set the Selected Altitude to 7000 feet using the ALT Knob To have the autopilot capture this altitude use Pitch Hold Vertical Speed or Flight Level Change Mode In this example Vertical Soeed Mode is used 2 Upon reaching the desired vertical speed of 1000 fom enable the flight d
136. ximity will now be displayed on the map Lighted Obstacle Height is greater than 1000 AGL Potential Impact Points Figure 10 17 TAWS Symbols Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 11 SECTION 10 HAZARD AVOIDANCE Pop up Alerts When the Navigation Map Page is displayed and a terrain or obstacle alert is issued a pop up window is displayed with the appropriate alert 176 80 Figure 10 18 Alert Pop Up Press the ENT Key to display the TAWS Page or press the CLR Key to remain on the Navigation Map Page 10 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages PFD MFD TAWS Alert Type Page sie Aural Message ae Pop Up Alert Reduced Required Terrain Clearance Warn PULL UP TERRAIN PULL UP Terrain Terrain Pull Up Pull Up ing RTC or or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact Warning ITI PULL UP Terrain Ahead Pull Up Terrain Ahead Pull Up OF or TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Reduced Required Obstacle Clearance PULL UP Obstacle Obstacle Pull Up Pull Up Warning ROC or or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact Warning 101 PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up or
137. y to display the PFD Nearest Airports Window View Information on a Specific Airport in the List 1 2 3 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport identifier Press the ENT Key to display airport information Press the ENT Key again cursor is on BACK to return to the list Load an Airport COM Frequency into the Active COM 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cursor on the desired airport frequency Press the ENT Key and the selected frequency will be placed in the COM standby frequency field Press the Frequency Transfer Key to make the frequency the active frequency Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 9 EA anlai 136 975 NORTH UP wae ane eE E ARENI I 5 K Tey Figure 7 11 Nearest Intersections Page Select the Nearest Intersections Page 1 Turn the large FMS Knob to select the NRST page group 2 Turn the small FMS Knob to select the second rectangular page icon View Information on the Nearest Intersection 1 With the Nearest Intersections Page displayed press the FMS Knob to activate the cursor 2 Turn either FMS Knob to select the desired intersection 3 Press the FMS Knob to remove the flashing Cursor SECTION 7 NAVIGATION 7 10 NEAREST NDB 136 975 NEAREST NDE Figure 7 12 Nearest NDB Page Select the Nearest NDB
138. ystem power is turned off all manual backlighting settings will return to the factory default settings Manually adjust the backlight for the PFD and MFD Press the MENU Key on the PFD to display the PFD Setup Menu Window Press the small FMS Knob to activate the cursor PFD DSPL gt AUTO is now highlighted Turn the small FMS Knob to display the selection window Turn the FMS Knob to select MANUAL then press the ENT Key With the intensity value now highlighted turn the small FMS Knob to select the desired backlighting Number of Pages in Current Group Figure 1 7 Page Group Icon Selected Page Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 Turn the large FMS Knob to highlight MFD DSPL gt AUTO and repeat steps 3 through 5 PFD SETUP MENU AUTO PFD DSPL MFD DSPL 23 474 a f Figure 1 8 PFD Setup Menu Window 1 6 XM RADIO AUTOMATIC MUTING XM Radio audio will be automatically muted when the aircraft groundspeed exceeds approximately 30 kts and the airspeed is less than approximately 80 kts The audio must be manually unmuted once the aircraft is outside the applicable speed range Refer to the Additional Features section of the G1000 Pilots Guide 1 7 DATABASE UPDATES Aviation Database Update NOTE The display downloads the aviation database and stores it internally The aviation database SD card is not required to remain in the display after the update

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