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Garmin Software Version 0369.13 Cockpit Reference Guide

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1. OPSHN 3mh 268 M n 10000FT TOD within 1 minute 136 975 lt OPSHN 233 3 0NM 10000FT 136 975 FSHER Er S SNH 10000FT PYNON Er 113m 10000F7 a C ee o Approach KCOS RNAV 35Rors LPV nity d HABLUE iof z21 S SNH 30001 A titu FALUR 251 S NA 8600r1 CURRENT WHV PROFILE ACTIVE WA WET TOOOGFT at OPSHN 3rH VS TGT 796FPH FPA 30 N VS REQ FPH TIHE TOTOO 7 30 _ Eio pan flv oe FT Vertical i n FT 1000rr M Deviation Ha Indicator Required 80nH a l VIEH WAV PROF CNCL VNV YNV amp VDI Figure 7 35 Adjusting the Descent S Indicator 11800 RVSI c Press the ENT Key 1 aiman Figure 7 37 VDI amp RVSI Upon Reaching Top of Descent TOD 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 15 SECTION 7 NAVIGATION 16 Upon reaching TOD a descent vertical speed is established which places the VSI pointer in line with the RVSI as shown in Figure 7 38 Keep Vertical Align Actual Deviation Pointer Vertical Speed Centered with Required Vertical Speed Figure 7 38 VDI amp RVSI Showing Correctly Established Descent 17 When the aircraft is one minute from the bottom of descent BOD this will be annunciated as shown in Figure 7 39 Upon reaching the OPSHN offset waypoint three miles before OPSHN the aircraft will be at 10 000 feet 136 975 ee 10600 10500 Figure 7 39 Approaching Bottom of Descent BOD a
2. 12 9 MFD amp PFD Message AdVISOFI S c scscesseesesseeseesees 12 9 Database Message AdVISOFES c sscsseseeseseereesen 12 10 GMA 1347 Message Advisories ccsscestecseesteeseeseeen 12 12 GIA 63 Message Advisories c scesscesseseeseesesseeen 12 12 GIA 63W Message Advisories n u 12 15 GEA 71 Message Advisories sesiis 12 17 GTX 33 Message Advisories 12 18 GRS 77 Message Advisories 12 18 GMU 44 Message Advisories scesseesesesseesesseean 12 19 GDL 69A Message Advisories cesceseeseesessesseeen 12 19 GDC 74A Message Advisories 12 19 Miscellaneous Message Advisories 12 19 C2 ieee nfo er Index 1 Garmin G1000 Cockpit Reference Guide for the DA40 40F TABLE OF CONTENTS Blank Page iV Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 1 SYSTEM OVERVIEW The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the complete system are found in the G1000 Pilots Guide 190 00592 03 SECTION 1 SYSTEM OVERVIEW This guide gives the pilot abbreviated operating instructions for the Primary Flight Display PFD Multi Function Display MFD and the GMA 1347 Audio Panel System A NOTE The pilot should read and thoroughly understand t
3. 9 Turn the small FMS Knob to select MSL or AGL 10 Press the ENT Key The cursor is placed in the VNV offset distance field 11 Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to 12 Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the COURSE field 13 Turn the small FMS Knob to enter the desired course to the waypoint 14 Press the ENT Key to highlight ACTIVATE 15 Press the ENT again to activate the Direct to Garmin G1000 Cockpit Reference Guide for the DA40 40F Select a Direct to Destination to a Flight Plan Waypoint 1 While navigating an active flight plan press the Direct to 2 Key 2 Turn the small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7 8 __DIRECT TO KMIA MIAMI FL OFFSET SNH KIXD pe k ee KSLN lOVATL inf DIGBE ACTIVATE Figure 7 8 Flight Plan Waypoint List PFD 3 Turn the large FMS Knob to select the desired waypoint 4 Press the ENT Key The cursor is now displayed on ACTIVATE 5 Press ENT again to activate a Direct to Select a Direct to Destination to a Nearest Airport 1 Press the Direct to J Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 8 The list is only populated when navigating a flight plan N A a RIAMT FL
4. Displays the active Flight Plan Page for creating and editing the active flight plan or for accessing stored flight plans 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 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW 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 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 PROC Key Selects approaches departures and arrivals from the flight plan If
5. FUEL CALCULATOR GALLONS REMAIN 40 0 428 446 GALLONS USED 0 0 Fuel Totalizer Stepney 3 01 Calculations RANGE NM 303 TOTAL TIME IN SERVICE Aircraft Total Ean Ter 0 8 HRS J Time in Service DEC FUEL INC FUEL RST FUEL Figure 3 3 EIS Display DA40F 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F I9 SECTION 3 ENGINE INDICATION SYSTEM EIS 3 3 ENGINE LEANING While viewing the EIS ENGINE Page press the LEAN Softkey As the mixture is leaned one of the cylinders exhaust temperature will peak This is indicated by Ist being displayed below the first cylinder to peak See Figure 3 4 The A Peak temperature is the difference between the peak temperature and the present temperature Continuing to lean the mixture will cause each cylinder to peak until the last of the cylinders peaks This is indicated by Last being displayed below the last peaking cylinder as shown in Figure 3 5 Pressing the ENGINE Softkey returns the MFD to de fault operation NAV2 110 60 EIS ENGINE 123 800 TEMPERATURE ELECTRICAL 1604 1604 Cylinder Peak EGT F AMPS 1568 1586 Ho Temperature 1700 1600 MAN IN HG 1500 24 3 Ist Cylinder 1400 eee 0 Peak N FUEL 1300 7 i a ip 25 s di Di Rey ee Indicates Difference DN a D ne Present and GPH PSI me Peak Temperature 4 CHT F He e k of the First Peaked 17 9 25 0 ee O Cylinder FUEL CALCULATOR 500 GALLONS REMAIN 40
6. TAWS INHB will be annunciated in the lower right of portion of the screen Enable TAWS If TAWS has been inhibited from the TAWS Page press the INHIBIT Softkey The TAWS INHB annunciation will be removed Manual System Test A system test is automatically performed at power up After successful 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 verify proper operation of the aural and visual annunciations of the system perform the following steps 1 While the TAWS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS Page When all is in working order TAWS System Test OK will be heard Garmin G1000 Cockpit Reference Guide for the DA40 40F 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 on the TAWS Page as a yellow or red X Imminent Terrain Impac
7. a LOW ALT Low Altitude annunciation may appear if the current aircraft altitude is at least 164 feet below the prescribed altitude at the FAF The annunciation initially flashes After a few seconds the flashing stops and the annunciation is displayed as shown in Figure 2 10 Low Altitude Annunciation Figure 2 10 Low Altitude on GPS Approach Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 5 SECTION 2 FLIGHT INSTRUMENTS 2 6 2 4 VERTICAL DEVIATION GLIDEPATH GLIDESLOPE INDICATOR The Vertical Deviation and Required Vertical Speed Indicators appear when vertical guidance is being given prior to executing an approach see Figure 2 11 In systems that are WAAS enabled the Glidepath Indicator appears at a point prior to the FAF when executing an LPV LNAV VNAYV or LNAV V approach see Figure 2 12 VNAV Target Altitude Vertical Deviation Indicator Required Vertical Speed 13000 P 12900 Figure 2 11 Vertical Deviation Indications Garmin G1000 Cockpit Reference Guide for the DA40 40F Glidepath Indicator 29 921N Figure 2 12 Glidepath Indicator The Glideslope Indicator appears when an ILS is tuned in the active NAV receiver field see Figure 2 13 Marker Beacon Annunciation Glideslope Indicator Figure 2 13 Glideslope Indicator 190 00324 07 Rev A 2 5 MARKER BEACON ANNUNCIATIONS Inner Marker T Altimeter Outer Marker Middle Marker Figure
8. 10 16 12 5 12 6 TAWS B 10 10 TAWS system test 10 12 Terrain 10 9 10 10 10 14 10 16 11 2 12 11 TOD 7 15 7 18 Top of Descent 7 15 Tornado 10 5 Traffic advisory 10 7 10 8 10 16 Traffic map page 10 7 10 8 10 9 10 14 Transponder 4 4 INDEX Transponder standby mode 4 5 Transponder Status bar 4 5 Trim 6 1 Trim Manual Electric 6 21 Tropical storms 10 5 TX 4 3 U Unlighted obstacle 10 14 V VDI 7 15 7 16 Vertical Descent Indicator 7 15 Vertical Deviation 2 6 Vertical deviation guidance 1 10 1 11 Vertical navigation 1 10 1 11 Vertical Navigation flight control 6 10 6 14 Vertical Path Tracking Mode 6 10 6 11 6 28 Vertical speed 1 4 2 7 Vertical Speed Bug 2 7 Vertical speed guidance 1 10 1 11 Vertical Speed Mode 6 7 Vertical Speed Reference 6 7 Vertical track 12 8 VHF 4 1 VNAV 1 11 12 21 VNAV Target Altitude 6 10 6 13 VNAV Target Altitude Capture Mode 6 13 VNV 1 10 1 11 7 1 7 4 7 15 VOL PUSH ID 4 2 VOL PUSH SQ 4 2 4 3 Volume squelch 5 3 VS 1 4 VSI 7 16 Vspeeds 2 3 W WAAS 2 6 6 23 7 5 12 15 WAAS precision approach 6 31 WARN 2 11 2 12 Warning 12 1 12 2 Weather data link page 10 4 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F Index 3 INDEX Index 4 Weather product symbol 10 5 Weather product symbols 10 6 Weather warnings 10 5 Wind direction 10 5 Wind speed 10 5 Wings level 6 16 6 17 X XPDR Softkey 4 4 Garmi
9. 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 190 00324 07 Rev A 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 scale 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 Ro
10. 45 2 ey i ie rF all 4 eae Ch oa al j ia a Me su 99 1 J nE Pa 1U Figure 7 22 Turn on to Active Leg 7 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 At SLN Victor Airway 244 V244 will be intercepted Turn prompts will be displayed in the PFD Navigation Status Box as seen in Figure 7 23 136 975 E Ve r i das T Too Baos L bee T E a s Sea il ae 7 wth Se amp a A acA ba q f UF 1an 1 ra h a 50 aS ee oo Figure 7 23 Turn to Intercept V244 9 As seen in Figure 7 24 V244 is now the active flight plan leg 136 975 ACTIVE FLIGHT PLAN KHKC KCOS FPL ACTIVE FLIGHT PLAN NORTH UP ee te TFR NO DATA TEE Enroute TOR Airway V4 SUN SLN Arw V244 LA4 HYS LAA K n Airwoy TBE 7 JL KOOS 322 Arrival KOOS TBE DBRY 1 ALL CURRENT VNV PROFILE ACTIVE VNV WPT VS TGT tennan gt f Vv DEV 1006t ial 1000F t f Moo J JON CNEL VNV Figure 7 24 V244 Now Active Leg 190 00324 07 Rev A SECTION 7 NAVIGATION 10 At Lamar VOR LAA V263 will be intercepted See oe eT Figure 7 25 PSN cA H NH gt NORTH UP ir fas V4 SLN E y VZ44LAA fis ULUS 322 o T EAREN Arrival KCOS TBEDBRY1 ALL TBE a7 n LOCATION CURRENT VNV PROFILE sane ERG 2B DIS 10114 ACTIVE UNV WPT at V5 TOT FPH FPA i Q FP OT TERRAIN VS REQ M TIME
11. Knob to activate the cursor 2 Turn the large FMS Knob to highlight the desired flight plan 3 Press the INVERT Softkey Invert and activate stored flight plan will be displayed 4 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F _ SECTION 8 FLIGHT PLANNING 8 17 COPY A FLIGHT PLAN 1 From the Flight Plan Catalog press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the flight plan to be copied 3 Press the COPY Softkey 4 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 8 18 DELETE A FLIGHT PLAN 1 From the Flight Plan Catalog Page press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the flight plan to be deleted 3 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 8 19 GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the Joystick
12. N CEN USA m NORTH UP Figure 7 5 Recently Entered Waypoints List MFD Turn the small FMS Knob to the right to display the RECENT waypoints as shown in Figure 7 5 Turn the large FMS Knob to select the desired airport Press the ENT Key The cursor is now displayed on ACTIVATE Press ENT again to activate a Direct to Re center the CDI to the Destination Waypoint Press the Direct to J 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 Active Direct to 1 2 3 4 5 6 1 8 190 00324 07 Rev A Press the Direct to 39 Key Turn the large FMS Knob to highlight the VNV altitude field Enter the desired altitude Press the ENT Key The option to select MSL or AGL is now displayed Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor now highlights the VNV offset field Enter the desired the offset distance Press the ENT Key SECTION 7 NAVIGATION 9 Turn the large FMS Knob to place the cursor in the COURSE field 10 Enter the desired course 11 Press the ENT Key The cursor now highlights ACTIVATE 12 Press the ENT Key again to begin navigation using the selected destination altitude constraint and course Canceling Direct to Navigation 1 2 3 Press the Direct to E Key Press the M
13. NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the 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 Aeronautical 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 or 1044 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 Repair
14. P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Turn the FMS Knobs to enter the identitier 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 identitier 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 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 SECTION 8 FLIGHT PLANNING NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the act
15. Pu ae OPSHN erences Bip toii FSHER 352 1000061 PY NOM 352 11 S0H RFT Approoch KOOS RMAY 35Rors LPW HABUK lof B21 5 00 S000F1 FALUR 261 S NH B600 CEGIX fof 351 6 0NH Sa 20 7 ee oe f i ES M ol FPL ACTIVE FLIGHT PLAN 116 408 cong An Af aia A200 aa A z a s i pz 4 Zu 7 TFR KMKC KOOS i E A Pe FPL ACTIVE FLIGHT PLAN NORTH UP eon HILLS Se ACTIVE FLIGHT PLAN TFR KMKC KCOS NO DATA DTK DIS ALT TBE INOA pT RSENS F Arrival KCOS TBE DBRY 1 ALL GPSHN JNM OPSHN CURRENT WHY PROFILE ACTIVE Vi WPT VS TGT VS REG FPH TIHE TO BoD FSHER ees L PYNON 352 0 7 10000FT Approach KCOS RNAV SSRors LPY HABUK iaf 021 5 SNN s000 FALUR 261 SC NH 8600 CEGIX fof 351 GO 700m RHSSR map 351 SINH TERRAIN rt rt M SSS S n CNL NY 3 CURRENT VNV PROFILE Figure 7 41 Tracking the OPSHN to FSHER Leg al Sn oe VS REQ 471FPM TIME TO TOD 0057 V DEV 7T50FT TERRAIN 20 The flight continues through the arrival procedure ar to PYNON see Figure 7 42 At a point 31 nautical ices g i g UE 1 SONN miles from the destination airport the phase of e PAF GEL E flight scaling for the CDI will change to Terminal prs 3nm ers 351 136 975 gt Mode and is annunciated by displaying TERM on M EEE the HSI There will be a descent to HABUK in the next leg Note the TOD point on the map Annunciations for the upcoming turn and descent as well as the V
16. and their projected track at various time intervals The display is updated every 12 minutes Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs or SIGMETs Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that 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 10 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 e SIGMETs AIRMETs e METARs e City Forecast e Surface Analysis speed and direction at a selected altitude from the ground up to 42 000 feet in 3 000 foot increments After pressing the WIND Soitkey 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 awarenes
17. 1 8 VNAV Altitudes Bar which further illustrates vertical navigation in more detail 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 11 SECTION 1 SYSTEM OVERVIEW 1 6 BACKLIGHTING y When system power is turned off all manual backlighting settings will return to the factory default must be manually unmuted once the aircraft is outside the applicable speed range Refer to the Additional Features section of the G1000 Pilots Guide on 1 8 DATABASE UPDATES A the backlight for the PFD The G1000 System uses Secure Digital SD cards l to load and store various types of data For basic flight 1 Press the MENU Key on the PFD to display the PFD operations SD cards are required for database storage Setup Menu Window as well as Jeppesen aviation and ChartView database 2 Press the small FMS Knob to activate the cursor updates PFD DSPL gt AUTO is now highlighted The following procedures pertain to updating the 3 Turn the small FMS Knob to display the G1000 system with SD cards as outlined in Appendix B of selection window the G1000 Diamond DA40 40F Pilots Guide 4 Turn the FMS Knob to select MANUAL then press Jeppesen Aviation Database the ENT Key 5 With the intensity value now highlighted turn NOTE After the aviation database is installed the small FMS Knob to select the desired the card may be removed after loading the backlighting update to each LRU 6 Turn the large FMS
18. 1709 1498 1588 1600 1500 1400 1300 1 2 3 4 FUEL CALCULATOR GALLONS REMAIN 42 9 GALLONS USED 7 1 E uel Totalizer qg 15 ENDURANCE 3 31 Calculations RANGE NM 352 o o TOTAL TIME IN SERVICE i L FUEL QTY R FUEL QTY Aircraft Total GAL GAL AES AA 157 2 HRS Time in Service AN EC FUEL INC FUEL RST FUEL Figure 3 2 EIS Display DA40 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 3 2 DA40F ENGINE DISPLAY SECTION 3 ENGINE INDICATION SYSTEM EIS The following softkeys allow for adjustment of the remaining fuel quantity Pressing the ENGINE Softkey displays the EIS ENGINE Page as shown in Figure 3 3 Fuel used GALLONS USED endurance and range RANGE NM are all calculated based on the last manual adjustment of the fuel remaining GALLONS REMAIN Measured fuel quantity hasno effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining EIS ENGINE DEC FUEL Allows the pilot to decrease the gallons of fuel remaining GALLONS REMAIN in l gallon increments INC FUEL Allows the pilot to increase the gallons of fuel remaining in 1 gallon increments RST FUEL Resets the fuel remaining to 40 gallons 123 800 TEMPERATURE EGT F 1700 1600 1500 1400 QO CHT F OIL PSI 5008 400 5 8 L FUEL QTY R FUEL QTY GAL GAL 1652 1616 1634 1652 1 2 3 4 410 392
19. 25 13 UP ies Figure 2 31 Timer Status Prompts Change the Generic Timer 1 2 3 190 00324 07 Rev A Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it must be reset manually Press the CLR Key or the TMR REF Softkey to remove the window SECTION 2 FLIGHT INSTRUMENTS Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 13 SECTION 2 FLIGHT INSTRUMENTS Blank Page 2 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS The Engine Instrument Display is displayed on the lett side of the MFD Manifold Pressure Gauge RPM Gauge RPM 3666 y 2300 FUEL FLOW Ga Fuel Flow 25 Indicator Fuel Pressure Bain Yo Indicator optional Cylinder Head Temperature nl Oil Temperature OIL_TEMP eee Indicator v OIL PRES Oil Pressure AE Indicator AMPS Ammeter VOLTS Fuel Quantity fj y E Voltmeter Indicator scale is 0 25 with FUEL QTY GAL extended range nai sg fuel tanks 0 20 A as with standard tanks DA40
20. Airport nm Figure 10 18 PDA Alerting 190 00324 07 Rev A SECTION 10 HAZARD AVOIDANCE Excessive Descent Rate Alert EDR The purpose of the Excessive Descent Rate alert is to provide suitable alerts when the aircraft is determined to be closing descending upon terrain at an excessive speed Figure 10 19 displays the correlation between height above terrain and descent rate resulting in the two EDR alerts EDR alerts have two levels of severity caution sink rate and warning pull up 6000 5500 5000 4500 4000 3500 3000 2500 2000 Height Above Terrain Feet 1500 8000 Descent Rate Figure 10 19 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 13 SECTION 10 HAZARD AVOIDANCE 10 14 Height Above Terrain Feet Height Above Terrain Feet Five Hundred Aural Alert Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map
21. CRS Knob to set the Selected Course to 255 Note that at this point the flight director i is still in Heading Select Mode and the autopilot continues to fly 290 Salina VOR SLN Figure 6 31 Intercepting a VOR Radial 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 25 SECTION 6 AUTOMATIC FLIGHT CONTROL Flying a Flight Plan GPS Course A NOTE Changing the navigation source cancels Navigation Mode and causes the flight director to revert back to Roll Hold Mode wings rolled level As the aircraft approaches the Salina VOR GPS is used to navigate the next leg airway V244 Flying a GPS flight plan 1 Transition from VOR to GPS Navigation Mode a Press the CDI Softkey until GPS is the selected navigation source b Press the NAV Key to activate GPS Navigation Mode The autopilot guides the aircraft along the active flight plan leg 27 Hays VOR HYS SL 2 Following the flight plan the autopilot continues to steer the aircraft under GPS guidance Note that in GPS Navigation Mode course changes defined by the flight plan are automatically made without pilot action required V4 SLN gt V244 LAA irvay V263 TBE CURRENT VNV PROFILE ACTIVE UNV WPT VS TGT TERRAIN ve tae a O FT 100r7 Figure 6 32 Transition to GPS Flight Plan 6 26 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Descent While flyi
22. 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 KTSD P PUBLIC HEH CENTURY ADRCENTER OLATHE KS DEPARTURE HIEF3 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 9 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 5 6 NOTE If any portion of an arrival procedure is the active leg of a flight plan the existing arrival procedure must be deleted before changing to a different arrival procedure Press the PROC Key Turn the large FMS Knob to highlight SELECT ARRIVAL Press the ENT Key If a flight plan is active the destination airport will be displayed as the default A list of available arrivals 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 Arrival
23. L PL GEA 71 Engine O D j Airframe Unit Or OIL TEMP GIA 63 Integrated ll eres Avionics Unit OT Fae AMPS A RA VOLTS FUEL TY GAL 0 fala XPOR FATE ENGINE C A GDC 74A Air Data Computer Figure 12 6 G1000 System Failure Annunciations 12 7 OTHER G1000 AURAL ALERTS Traffic Traffic not available The Traffic Information Service TIS system has issued a Traffic Advisory alert The aircraft is outside the Tratfic Information Service TIS coverage area 12 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F DOMT DOM GIA 63 Integrated Avionics Units GDC 74A Air Data Computer GRS 77 AHRS O X GMU 44 Magnetometer GIA 63 Integrated Avionics Units ALERTS GTX 33 Transponder Or GIA 63 Integrated Avionics Units 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS 12 8 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 A 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 to a message Always use sound pilot judg
24. NOTE Pressing the HDG Knob synchronizes the Selected Heading to the current heading The Selected Heading is adjusted using the HDG Knob on either display Pressing the CWS Button and hand flying the aircraft does not change the Selected Heading The autopilot guides the aircraft back to the Selected Heading upon release of the CWS Button Heading Select Mode Active navi 111 98 114 18 Suc HAVZ 118 98 153c Command Bars Track Selected Heading Selected Heading Turns are commanded in the same direction as Selected Heading Bug movement even if the bug is turned more than 180 from the present heading e g a 270 turn to the right However Selected Heading changes of more than 340 at a time result in turn reversals Pitch Hold Mode Active CAR 136 975 con 975 COM T Selected Heading Bug R LEL 5 56 43PH Figure 6 21 Heading Select Mode Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Navigation Mode GPS VOR LOC BC NOTE The selected navigation receiver must have a valid VOR or LOC signal or active GPS course for the flight director to enter Navigation Mode Pressing the NAV Key selects Navigation Mode Navigation Mode acquires and tracks the selected navigation source on the HSI GPS VOR LOC The flight director follows GPS roll steering commands when GPS is the selected navigation source When the HSI is coupled to VOR or LOC the flight director creates r
25. SECTION 3 ENGINE INDICATION SYSTEM EIS es RPM 3000 aie y 2330 TAS ELOY Gt Fuel Flow Indicator Cylinder Head Iemperature Indicator OIL TEMP Oil Temperature bA Indicator OIL PRES Oil Pressure a aes Indicator AMPS P Ae Ammeter F 86 VOLTS m A Voltmeter FUEL QTY GAL Fuel Quantity 8 DA40F Figure 3 1 Engine Instrument Display on the MFD 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 3 ENGINE INDICATION SYSTEM EIS 3 2 3 1 DA40 ENGINE DISPLAY The following softkeys allow for adjustment of the remaining fuel quantity DEC FUEL Allows the pilot to decrease the gallons of fuel remaining GALLONS REMAIN in l gallon increments INC FUEL Allows the pilot to increase the gallons of fuel remaining in 1 gallon increments RST FUEL Resets the fuel remaining to 40 gallons in aircraft with standard fuel tanks Resets the fuel remaining to 50 gallons in aircraft with extended range fuel tanks Pressing the ENGINE Softkey displays the EIS ENGINE Page as shown in Figure 3 2 Fuel used GALLONS USED endurance and range RANGE NM are all calculated based on the last manual adjustment of the fuel remaining GALLONS REMAIN Measured fuel quantity hasno effect on fuel calculations Fuel calculations are based on sensed fuel flow and the last manual adjustment of the fuel remaining EIS ENGINE 123 800 TEMPERATURE 1526 1526 EGT F
26. Situation Indicator 360 2 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 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 Thien Rate Standard Tur Mee rend Vector Rate Tick Mark Fo rate gt 4 deg sec Turn Rate Trend Vector standard rate Figure 2 20 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 SECTION 2 FLIGHT INSTRUMENTS Figure 2 21 Course Pointer Course Deviation Indicator CDI The CDI scale automatically adjusts to the current phase of flight as seen in Figure 2 22 Scaling may be selected manually from the MFD System Setup Page Flight Phase Automatic CDI Full scale Deflection Approach LNAV 1 0 nm decreasing to 350 feet depending on variables see Figure Approach LNAV V 2 23 Approach LNAV 1 0 nm decreasing to a specitied VNAV WAAS only course width then 0 3 nm Approach
27. TO TOD T V DEV FT 100r i fenti Figure 7 26 Direct To OPSHN 30nnf NOL VNV Figure 7 25 HYS to LAA Leg Active ACTIVATE d Turn the large FMS Knob to place the cursor in the VNV altitude field as shown in Figure 7 27 11 ATC grants clearance to proceed direct to OPSHN intersection to begin the arrival procedure and E issues a crossing altitude restriction of 10 000 feet at OPSHN a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to select OPSHN in the flight plan list c Press the Direct to E Key The Direct to Window is now displayed as shown in Figure 7 26 i LOCATION 260 DIS 101 ACTIVATE Figure 7 27 Enter VNV Altitude e An altitude of 10 000 feet is entered as requested by ATC 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 11 SECTION 7 NAVIGATION 7 12 f Press the ENT Key The cursor is now displayed in the VNV offset field as shown in Figure 7 28 DIRECT T WN GGR8FT a HAR NORTH UP as SH 15H LOCATION j ERG 260 DIS 161NK 257 ACTIVATE Figure 7 28 Enter VNV Offset Distance g Enter the offset or distance from the waypoint at which the selected altitude will be reached In this case three miles prior to OPSHN is entered In other words the G1000 will give vertical guidance so the aircraft will arrive at an altitude of 10 000 feet three miles pri
28. WAAS capable or WAAS is not available the LPV approach will not be displayed in the list of available approaches Selecting the LNAV approach for runway 35R will give vertical guidance up to the IAF Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A b SELECT APPROACH should be highlighted as shown in Figure 7 30 PROCEDURES SELECT ARRIVAL SELECT DEPARTURE LOADED APPROACH ARRIVAL KCOS TBE DBRY 1 ALL DEPARTURE KMEC ALL WLOCT SLN Press the PROC key to view the previous page Figure 7 30 Procedures Window c Press the ENT Key A list of available approaches for the destination airport will be displayed as in Figure 7 31 AIRPORT KETS COLORADO SPRINGS CO APPROACH CHANNEL s CHANNEL 97799 10 W5A APPROACH RNAV 3SRePs LPW IRI mikit NDE 35L maar y wot wlhe RHJSR mop 351 5 144 B35SrT 38 Bdrm MOGAL mohp HOLD 50 BEN LOAD oR ACTIVATE Figure 7 31 List of Available Approaches 190 00324 07 Rev A SECTION 7 NAVIGATION d Turn either FMS Knob to select the LPV approach for 35R as shown in Figure 7 31 e Press the ENT Key A list of available transitions for the selected approach is displayed as shown on Figure 7 32 AIRPORT KCOS b PUBLIC CITY OF COLORADO SPRINGS COLORADO SPRINGS CO APPROACH CHANNEL CHANNEL 97799 I0 W35A RNAV 35Rops LPV TRANSITION HABUK lof VECTORS iouenc HI
29. a flight plan 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 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 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 AP Key Engages disengages the Autopilot and Flight Director Pressing the AP Key activates the Flight Director and engages the Autopilot in the Garmin G1000 Cockpit Reference Guide for the DA40 40F detault pitch axis and roll axis modes Pressing the AP Key again disengages the autopilot and deactivates the Flight Director 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 the Autopilot is en
30. becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition The flight director automatically arms Vertical Path Tracking allowing upcoming descent legs to be captured and subsequently tracked Altitude Reference In This Case Equal To VNAV Altitude Target AFT ALT VPTH Flash up to 10 sec Indicating Automatic Transition M E Figure 6 14 VNAV Altitude Capture Changing the VNAV Target Altitude NOTE Pressing the CWS Button while in VNAV Target Altitude Capture Mode does not cancel the mode Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL Changing the current VNAV Target Altitude while VNAV Target Altitude Capture Mode is active causes the B NOTE Glidepath Mode is available only in flight director to revert to Pitch Hold Mode Vertical Path installations with GIA 63W Integrated Avionics Tracking and the appropriate altitude capture mode are Units and WAAS is currently available armed in preparation to capture the new VNAV Target Altitude or the Selected Altitude depending on which altitude is to be intercepted first VNAV target altitudes can be changed while editing the active flight plan see the GPS Navigation Section for Glidepath mode is used to track the WAAS based glidepath Arming Glidepath Mode annunciated in white as GP requires e Approach supportin
31. 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 COM1 wv wv 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 over 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 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 ll y MKR HI SENS MUTE Figure 5 4 Marker Beacon 5 3 NAV RADIO AUDIO SELECTION Pressing DME AD
32. depending on variables see Figure LPV WAAS only 2 24 Missed Approach 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 9 SECTION 2 FLIGHT INSTRUMENTS Cc 2 O co S E E z E 2 z Z ai A gt 2 f v O n A z Refer to accompanying N 8 5 x approach CDI scaling figures 5 5 5 3 i a 5 5 z aa E Missed O Departure Terminal a Oceanic if gt 200 nm S Terminal Approach ADOrOack Fe from nearest airport Se pp O Drawing not to scale Figure 2 22 Phases of Flight CDI Scaling Q 5 CDI scale is set to the smaller of 0 3 nm 5 8 or an angle set by the system 8 D D D QA Q 3 Ss 8 z 7 3 op Ag T angle based ro n angle set 5 5 on database 8 A by system O information 3 e T i A FAF Landing FA Threshold A O CDI scale varies if Vectors To Final is activated CDI scald tane eee cine Drawing not to scale Drawing not to scale o Figure 2 23 Typical LNAV and LNAV V Approach CDI Scaling Figure 2 24 Typical LNAV VNAV and LPV Approach CDI Scaling WAAS Systems Only 2 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Bearing Pointers and Information Windows Pressing the PFD Softkey provides access to the BRG1 and BRG2 Softkeys The BRG1 pointer is a single line pointer The BRG2 pointer is a double line pointer Press the BRG1 or BRG2 Softkey to cycle through selec
33. displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle l T proximity will now be displayed on the map Altitude Loss Feet Pop up Aler ts ae 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 HAP NAVIGATION MAF 118 008 0 500 1000 1500 2000 2500 3000 3500 4000 Sink Rate Feet Per Minute Figure 10 20 Negative Climb Rate The purpose of the aural alert message Five hundred is to provide an advisory alert to the pilot 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 Figure 10 22 Alert Pop Up the CLR Key to remain on the Navigation Map Page Unlighted Obstacle Lighted Obstacle Unlighted Obstacle Lighted Obstacle Potential Impact Points 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 21 TAWS Symbols Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Press the ENT Key to display the TAWS Page or press SECTION 10 HAZARD AVOIDANCE TAWS Alerts Summary The following table shows the possible TAWS alert types with corresponding annunciations and aural messages PFD MF
34. following alert annunciations appear in the AFCS System Status Annunciation on the PFD Figure 12 5 AFCS System Status Annunciation 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 E Acondition has developed causing the pitch servo to provide a sustained force in the nose up direction Elevator Mistrim fe E A condition has developed causing the pitch servo to provide a sustained force in the nose Down down direction Aileron Mistrim Left AT A condition has developed causing the roll servo to provide a sustained left force Aileron Mistrim Right P ATI ay A condition has developed causing the roll servo to provide a sustained right force Preflight Test Performing preflight system test Upon completion of the test the aural alert will be heard Preflight system test has failed 12 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS 12 5 TAWS ALERTS Annunciations appear
35. independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING XM We
36. level softkeys Lo We Wes i W s IE e JE 7 Jf menr i ekse Back ffars nnnnnnianienienrnaAn w Press the IDENT or BACK Softkey to return to the top level softkeys Figure 1 5 XPDR Transponder Softkeys 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW IDENT Press to provide special aircraft position identification to Air Traffic Control ATC TMR REF Press to display the Timer References Window NRST Press to display the Nearest Airports Window ALERTS Press to display the Alerts Window 1 3 MFD SOFTKEYS ENGINE Pressing this softkey makes available the Engine Page iw m O TI C m MAP options INC FUEL wy n MAP Pressing this softkey enables the following softkeys 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 AIRWAYS Pressing this softkey displays removes airways information The default is dependent on map setup option selected Pressing cycles through all airways displayed AIRWY ON low altitude airways only AIRWY LO and high altitude airways only AIRWY HI A optional optional Default softkey is dependant on Press the BACK Softkey on this the selection made level to return to
37. modify the aircraft attitude Q e with the CWS Button or NOSE UP NOSE DN keys result in reversion to Pitch and Roll Hold modes Go Around Mode Active Autopilot Disconnect Annunciation Flashes Yellow 5 sec Command Bars Indicate Climb Roll Modes Roll Hold default mode Holds the current aircraft roll attitude or rolls the wings level depending on the commanded bank angle Heading Select Captures and tracks the Selected Heading Navigation GPS VOR LOC Captures and tracks the selected navigation source Approach GPS VAPP LOC BC Captures and tracks the selected navigation source with greater sensitivity for approach Go Around Commands a constant pitch angle and wings level while in the air 118 200 136 975 con 136 975 coM2 2000 299211 Figure 6 19 Go Around Mode 6 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Table 6 2 relates each roll mode to its respective control RM ALTS and annunciation Refer to the pitch modes section for Figure 6 20 Roll Hold Mode Annunciation information regarding Go Around Mode The CWS Button does not change lateral references Bank Angle Flight Director Response for Heading Select Navigation Backcourse or Approach Rolls wings level modes The autopilot guides the aircraft back to the 5545598 aeea arid Selected Heading Course upon release of the CWS aoe aaa gt 22 Ta
38. next TOD is reached Vertical Path Tracking becomes active may require acknowledgment to allow descent path capture _ GPS AP ALTV 5 As the aircraft nears the VNV Target Altitude the flight director transitions to VNV Target Altitude Capture Mode indicated by the green ALTV annunciation flashing for up to 10 seconds _ GPS AP ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft at the vertical waypoint ALT Mode Selected Altitude HABUK A Figure 6 35 Non path Descent 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 29 SECTION 6 AUTOMATIC FLIGHT CONTROL Approach KCOS Flying an ILS approach 1 Transition trom GPS Navigation Mode to Heading Select Mode 8 a Select the Runway 35L ILS approach for KCOS and select VECTORS for the transition Load and activate the approach in the flight plan b Use the HDG Knob to set the Selected Heading after getting vectors from ATC c Press the HDG Key The autopilot turns the aircraft to the desired heading d Use Heading Select Mode to comply with ATC vectors as requested 2 Arm LOC Approach and Glideslope modes apo SD lddv 207 PETEY PON AVN Sd5 a Ensure the appropriate localizer frequency is tuned b Press the APR Key when cleared f
39. on the PFD and MFD Pop up alerts appear only on the MFD PFD MFD TAWS Alert Type Page Be Map nage ao 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 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 or Obstacle Obstacle Pull Up Pull Up Reduced Required Terrain Clearance Caution Caution Terrain Caution Terrain RTC or Terrain Ahead Terrain Ahead Aural Message Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Reduced Required Obstacle Clearance Caution Obstacle Caution Obstacle Caution ROC or Obstacle Ahead Obstacle Ahead Imminent Obstacle Impact Caution IOI Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Premature Descent Alert Caution PDA Altitude Callout 500 Five Hundred Excessive Descent Rate Cauti
40. power usage 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 9 SECTION 12 ANNUNCIATIONS amp ALERTS MFD amp PFD Message Advisories Cont PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck CNFG MODULE PFD1 configuration The PFD1 configuration module backup memory has failed The G1000 system module is inoperative should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage MFD1 VOLTAGE MFD1 has low voltage Reducing power usage A key is stuck on the PFD and or MFD bezel Attempt to tree the stuck key by pressing it several times The G1000 system should be serviced if the problem persists The PFD and or MFD voltage is low The G1000 system should be serviced Database Message Advisories MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists MFD1 DB ERR MFD1 basemap database 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 The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced The MFD and or PFD detected a
41. 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 190 00324 07 Rev A 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 121 500 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 primary functions will be displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the air craft experiences unusual attitudes e Traffic Annunciations e Windows displayed in AFCS Annunciations the lower right corner Flight director Com of the PFD mand Bars Timer References e Inset Map Nearest Airports e Temperatures Flight Plan e DME Information Messages Window Procedures e Wind Data DME Tunin
42. serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch The GDL 69 has incorrect software installed The G1000 system should be communication halted serviced GDC 74A Message Advisories MANIFEST GDC1 software The GDC 74A has incorrect software installed The G1000 system should be mismatch communication halted serviced Miscellaneous Message Advisories 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 aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint trom the flight plan if it no longer exists in any database Or update the waypoint name identitier to reflect the new information FPL WPT MOVE Flight plan The system has detected that a waypoint coordinate has changed due to a new waypoint moved aviation database update Verity that stored flight plans contain correct waypoint locations 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 19 SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont TIMER EXPIRD Timer has expired The system n
43. system cannot use this altitude be used in determining vertical giving vertical speed and deviation in determining vertical speed and speed and deviation guidance guidance Altitude has been deviation guidance Altitude has been retrieved from retrieved trom the navigation the navigation database and is database or has been entered by provided as a reference the pilot and matches a published altitude in the navigation database Table 1 1 VNV Altitude Text Size and Color Refer to Figure 1 8 and Table 1 1 for more detail regarding the significance of text size and color 8 8 8 Some altitudes retrieved from the database have ACTIVE FLIGHT PLAN associated restrictions indicating to stay At At or Above KIXD KDFW or At or Below a specific altitude These restrictions are indicated using a bar above and or below the appropriate Large White altitude as shown in Figure 1 9 Text Large Light eism Stay AT or ABOVE 5 000 fi Approach KDFW RNAV 17Lops LPV Blue Text RIVET iof Mee MCE Small Light FANG Stay AT 2 300 ft KARLA 221 11 7NM 13 FT COVIE 221 9 0NM 12406FT LEMYN 220 8 0NN S39S GQFT DRAAK 176 3 3NM 2000 e INWOD 176 3 2MM 2go Small Light cisla Stay AT or BELOW 3 000 ft i Blue Subdued PHENOL faf 1 9 S Ni Text Figure 1 9 Altitude Restrictions RW1 L map 176 5 3NM Small White 99 FT 174 0 8NM Text with POLKE oe See Section 7 Navigation for a sample flight plan Figure
44. the GO BACK Softkey to return to the map FLIGHT PLAN LIST 1 KIXD KSN E 8 2 VIEWING THE ACTIVE FLIGHT PLAN Press the FPL Key Approoch ILS 30R MOODS iof 127 Figure 8 2 Active Flight Plan Window on the PFD Figure 8 4 Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan and press the ACTIVE Softkey 4 With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation 8 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A turn the large FMS Knob to highlight CANCEL and press the ENT Key 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 Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD 3 With Activate highlighted press the ENT Key KOJC KSLN ACTIVATE or CANCEL Figure 8 5 Activate Flight Plan Leg Confirmation 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 Press the FMS CRSA knob to return to bese poge Figure 8 6 Delete Flight Plan
45. the pointer the indicator for the corresponding source and displaying the appropriate information NAVI Displays NAV1 waypoint frequency or identifier and DME information in the BRG1 Information Window Garmin G1000 Cockpit Reference Guide for the DA40 40F GPS Displays GPS waypoint identifier and GPS distance information in the BRG1 Information Window ADF Displays ADF in the BRGI Information Window OFF Removes the BRG1 Information Window HSI FRMT Press to display the HSI formatting softkeys 360 HSI Press to display the HSI in a 360 degree format ARC HSI Press to display the HSI in an arc format BRG2 bearing Press to cycle through the following Nav sources making the pointer the indicator for the corresponding source and displaying the appropriate information NAV2 Displays NAV2 waypoint frequency or identifier and DME information in the BRG2 Information Window 190 00324 07 Rev A GPS Displays GPS waypoint identifier and GPS distance information in the BRG2 Information Window ADF Displays ADF in the BRG2 Information Window OFF Removes the BRG2 Information Window SECTION 1 SYSTEM OVERVIEW XPDR Press to display the transponder mode selection softkeys STBY Press to select Standby Mode ON Press to select Mode A ALT Press to select Altitude Reporting Mode GND Press to select Ground Mode VFR Press to automatically squawk 1200 only ALT UNI
46. 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 used 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 The G1000 GPS allows for flying LNAV LNAV VNAV WAAS only and LPV WAAS only approaches accord ing to the published chart The active approach type will be annunciated on the HSI as shown in the following table HSI DESCRIPTION ANNUNCIATION LNAV GPS approach using published LNAV minima LNAV V GPS approach using published LNAV minima Advisory vertical guidance is provided LNAV VNAV minima LPV minima WAAS systems only 190 00324 07 Rev A Load and or Activate an Approach Procedure 1 2 3 4 5 Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key If a flight plan is active the destination airport will be displayed as the default A list of available approaches 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 App
47. the small FMS Knob to select the first MAP Course age indicated by a solid rectangular icon paar J J Figure 7 2 MFD Direct to Window 136 975 30 cone a a Enter a Direct to Destination 1 Press the Direct to 8 Key 2 Enter the destination waypoint identifier 3 Press the ENT Key to contirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude contraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude AUE E AaRON MEE EOE 7 Press the ENT Key The option to select MSL or AGL is now displayed 8 Turn the small FMS Knob to select MSL or AGL 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 1 SECTION 7 NAVIGATION 9 Press the ENT Key The cursor is placed in the VNV offset distance field 10 Enter the desired target altitude offset trom the selected Direct to 11 Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the COURSE field 12 Enter the desired course to the waypoint 13 Press the ENT Key to highlight ACTIVATE 14 Press the ENT again to activate the Direct to Select a Direct to Destination to a Flight Plan Waypoint 1 While navigating an active flight plan press the Direct to 2 Key 2 Turn the
48. the top softkey level in the map setup optional optional optional re my n The DONE Softkey changes to UNDO when the checklist item is already checked 2 es es DD Figure 1 6 MFD Softkeys 1 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 1 SYSTEM OVERVIEW STRMSCP optional Pressing this softkey displays 1 4 MFD PAGE GROUPS removes Stormscope lightning data on the Navigation Map 1 Turn the large FMS Knob until the desired page NEXRAD optional Pressing this softkey displays group is selected removes precipitation data on the Navigation Map 2 Turn the small FMS Knob to select pages within the XM LING optional Pressing this softkey displays group See Figure 1 7 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 SHW CHRT Show Chart optional Pressing this softkey displays optional FliteCharts or ChartView charts CHKLIST checklist optional Pressing the CHKLIST Softkey displays the Checklist Page ENGINE Displays engine softkeys DONE Pressing this softkey checks off a checklist item If an item is already checked an UNDO Softkey will be displayed EXIT Press to exit the checklist EMERGCY Pressing this softkey displays the emergency checklist Nearest Group Au
49. 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 3 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 USRO01 USROO2 and so on Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 Ifthe 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 5 After placing the cursor at the desired point in the list of waypoints press the LD WPT Softkey 6 To change the user waypoint name follow the procedure for modifying a user waypoint 8 20 TRIP PLANNING 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the first rectangular page icon 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the page mode press the AUTO or MANUAL Softkey Starting WPT Ending WPT TA OTHER STATS DENSITY ALT TRUE AIRSPEED WIND DIRECTION WIND SPEED HEAD WIND Figure 8 22 Trip Planning Page 190 00324 07 Rev A 4 5 190 00324 07 Rev A 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
50. waypoint Once all waypoints have been entered press the FMS Knob to remove the cursor The new flight plan is now active Figure 8 12 Creating Flight Plan on the PFD 190 00324 07 Rev A SECTION 8 FLIGHT PLANNING 8 8 ENTER AN AIRWAY IN A FLIGHT 5 When the desired entry point is entered press the PLAN ENT Key 1 Press the FPL Key to display the active flight plan or display a stored flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the waypoint before which the airway will be entered Figure 8 15 Airway Entry Point Loaded 6 Turn the small FMS Knob to display the Waypoint Information Window WAYPOINT INFORHATION IDENT FACILITY CITY Figure 8 13 Airway Insertion Point 4 Turn the small FMS Knob to display the Waypoint Information Window and begin entering the desired airways entry point Way POINT INF ORHATION IDENT FACILITY CITY AnA LOCATION BRG HORTH UF DIS Press ENT to occept Figure 8 16 Display Waypoint Information Window LOCATION fil ERG W63 kj DIS 3304 yp Fress ENT to occept Figure 8 14 Load Airway Entry Point 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 5 SECTION 8 FLIGHT PLANNING 7 Press the LD AIRWY Softkey A list of available 12 With LOAD highlighted press the ENT Key airways is now displayed ENTRY ANY AIRWAY YE Wie p
51. 0 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 1 SECTION 10 HAZARD AVOIDANCE At a map range of less than 25 nm Stormscope MESSNER Ww STORNSCOPE 136 975 lightning data is not displayed but can still be present D The presence of Stormscope lightning data is indicated by the annunciation LTNG lt 25 nm in the upper right corner i com STRIKE RATE 1 HOG _ NORTH UP STRMSCP OE Aas Figure 10 5 Lightning Display Range Annunciation Select cell or strike as the Stormscope lightning mode 1 With the Weather Group selected press the ENT Figure 10 6 Stormscope Page Key The cursor flashes on STRMSCP LING 2 Turn the large FMS Knob to select STRMSCP Change the Stormscope lightning mode MODE between cell and strike 3 Turn the small FMS Knob to display the Cell Strike 1 Select the Stormscope Page window 2 Press the MODE Softkey The CELL and STRIKE 4 Turn either FMS Knob to select Cell or Strike Softkeys are displayed Press the CELL Softkey to Press the ENT Key display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page 5 Push the FMS Knob to return to the Navigation Map Page Clear Stormscope lightning data from the Navigation Map Page NOTE Cell mode uses a cluster
52. 0 Cockpit Reference Guide for the DA40 40F 12 11 SECTION 12 ANNUNCIATIONS amp ALERTS GMA 1347 Message Advisories GMA1 FAIL GMA1 is inoperative The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be serviced GMA1 CONFIG GMA1 contig error The audio panel configuration settings do not match backup configuration Contig service req d memory 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 service Return unit for repair functions may still be available and the audio panel may still be usable The G1000 system should be serviced when possible GIA 63 Message Advisories Message Comments S GIA1 CONFIG GIA1 contig error Contig service req d The GIA1 and or GIA2 contiguration settings do not match backup contiguration GIA2 CONFIG GIA2 config error memory The G1000 system should be serviced Contig service req d GIA1 CONFIG GIA1 audio contig error Contig service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 system GIA2 CONFIG GIA2 audio config should be serviced error Contig service req d GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too lo
53. 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL When the CDI has automatically switched from GPS to LOC during a LOC ILS approach GPS Navigation Mode remains active providing GPS steering guidance until the localizer signal is captured LOC Navigation Mode is armed in anticipation of localizer signal capture if the APR Key is not pressed prior to the automatic source switch If Navigation Mode is active and either of the following occur the flight director reverts to Roll Hold Mode wings rolled level e Different VOR is tuned while in VOR Navigation Mode VOR Navigation Mode reverts to armed e Navigation source is manually switched e Localizer signal is not captured by the final approach fix FAF while in LOC Navigation Mode Changing the Selected Course The Selected Course on the PFD is controlled using the CRS Knob Pressing the CWS Button and hand tlying the aircraft does not change the Selected Course while in Navigation Mode The autopilot guides the aircraft back to the Selected Course or GPS flight plan when the CWS Button is released Approach Mode GPS VAPP LOC NOTE The selected navigation receiver must have a Valid VOR or LOC signal or active GPS course for the flight director to enter Approach Mode Approach Mode is activated when the APR Key is pressed Approach Mode acquires and tracks the selected navigation receiver on the HSI GPS
54. 1 SECTION 2 FLIGHT INSTRUMENTS e SUSP Displayed when in OBS Mode indicating 2 9 WIND DATA GPS waypoint sequencing is suspended e DR Navigating using Dead Reckoning due to an error in the GPS solution When the window is selected for display but wind information is invalid or unavailable the window shows NO WIND DATA Wind data can be displayed in three different ways e Longitudinal and lateral components Option 1 Total wind direction and speed Option 2 e Total direction with head and crosswind speed components Option 3 Option 1 Option 2 Option 3 No Data NO WIND DATA Figure 2 30 Wind Data Window Displaying wind data Figure 2 29 GPS LOI GPS SUSP LOC1 and VOR2 1 Press the PFD Softkey a 2 Press the WIND Softkey to display wind data below Enable disable OBS Mode while navigating the Selected Heading with GPS 3 Press one of the OPTN softkeys to change how 1 Press the OBS Softkey to select OBS Mode wind data is displayed 2 Turn the CRS Knob to select the desired course 4 To remove the Wind Data Window press the OFF to from the waypoint Softkey 3 Press the OBS Softkey again to disable OBS Mode NOTE The OBS Softkey is only displayed when navigating an active leg using GPS 2 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 2 10 GENERIC TIMER REFERENCES 164 nO 40a Oe a ART REFERENCES TIMER 00 25 05 DN SUUM REFERENCES TIMER 00
55. 190 00324 07 Rev A 3 8 6 1 2 3 SECTION 8 FLIGHT PLANNING Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan 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 Press the FHS CRSA knob ta return to bose poge Figure 8 8 Invert Flight Plan Invert active flight plan CANCEL rr UK or Figure 8 9 Invert Flight Plan Confirmation Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 3 SECTION 8 FLIGHT PLANNING 8 7 CREATE A NEW FLIGHT PLAN Create a New Flight Plan Using the MFD 1 2 3 4 6 1 8 8 4 Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the NEW Softkey to display a blank flight plan page 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 th
56. 2 14 Marker Beacon Annunciations 2 6 VERTICAL SPEED INDICATOR Selected Vertical Speed Vertical Speed Bug Vertical Speed Pointer Figure 2 15 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 190 00324 07 Rev A SECTION 2 FLIGHT INSTRUMENTS 2 7 BAROMETRIC ALTITUDE MINIMUMS The desired barometric altitude minimums can be set in the Timer Reterences Window The altitude ranges from 0 to 16 000 feet in 10 foot increments The minimums are reset anytime the power is cycled MINIMUMS 4 BARO 1560FT Figure 2 16 Barometric Minimum Descent Altitude Settings Set the barometric altitude minimums 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the Minimums field Figure 2 16 3 Turn the small FMS Knob to select BARO OFF is selected by default Press the ENT Key or turn the large FMS Knob to highlight the next field 4 Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet 5 To remove the window press the CLR Key or the TMRIREF Softkey 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 a
57. 24 07 Rev A SECTION 7 NAVIGATION a Press the VNV PROF Softkey to place the cur 15 As seen in Figure 7 36 the aircraft is approaching sor in the target vertical speed field VS TGT as TOD Note the target vertical speed required to shown in Figure 7 35 reach the selected altitude The Vertical Deviation b At this point the descent vertical speed can be Indicator VDI and the Required Vertical Speed selected or the FPA can be selected Turn the Indicator RVSI are now displayed on the PFD as large FMS Knob to select the desired selection shown in Figure 7 37 field then turn the small FMS Knob to enter the FPL ACTIVE FLIGHT PLAN 136 975 desired value BETIE FLIGHT PLAN Note the information now displayed in the LAA D CURRENT VNV PROFILE box Also note the gt ipl Galea es ee offset waypoint and a gray circle labeled TOD Aerivol KCOS TBEDBRYIALL are now displayed on the map The gray circle sea O a aan iir marks the Top of Descent TOD In this example Ea Sa P A after passing the TOD point vertical guidance T an T ea will be provided that will result in a 3 0 degree FALUR 7 Som em FPA descent to an altitude of 10 000 feet at the e E offset waypoint vsToT B90FPH FPA 30 TERRAIN VS REG V DEV FPL ACTIVE FLIGHT PLAN EAH IE ACTIVE FLIGHT PLAN TFA KMKC KEOS HI DATA r SHH CHRT ee a Figure 7 36 Approaching Top of Descent TOD Arrival KCOS TBE DBRY 1 ALL
58. 324 04 Added fuel pressure gauge for the DA40 190 00324 05 Added GFC 700 Automatic Flight Control System Added GDU 6 10 software parameters Updated G1000 System Messages Removed diesel engine parameters 190 00324 06 Added TAWS Added XM Muting Added contigurable low airspeed ranges 190 00324 07 Added Stormscope Added TAS600 Added Airways WAAS VNAV amp Charts Added new engine display Added database loading instructions Updated G1000 System Messages Added other GDU 8 02 parameters 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F RR 1 RECORD OF REVISIONS Revision Date of Revision Affected Pages 5 07 Production Release RR 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 190 00324 07 Rev A Section 1 System Overview occ 1 1 1 1 PFD MFD Controls 0 00 00 0 c cccccscseesteeeesteen 1 2 1 2 PFD SOTKKEYS issvisisasccscicsssiciiscsintiacmonsimniennen 1 5 1 3 MFD Softkeys ssccoesenceccsmentionparenenee 1 8 1 4 MFD Page Groups 1 9 1 5 Vertical Navigation cece 1 10 1 6 Backlighting 0 0 0 ccc cscs ees 1 12 1 7 XM Radio Automatic Muting 00 1 12 1 8 Database Updates seca 1 12 Jeppesen Aviation Database cccesessesesereesen 12 Garmin Datahds Ssnan 1 13 Section 2 Flight Instruments 0 0 2 1 2 1 Airspeed Indicator 0 ccccccseseseeseeen 2 3 Speed NACAs EA 2 3 Speed RM Eanan e O 2 3 Air
59. 324 07 Rev A SECTION 10 HAZARD AVOIDANCE Traffic Advisory aircraft is 1200 TNA Mute above amp climbing moving in the Traffic out of Traffic Mode Status direction of the line range is older than 6 level sec resulting in Coast Mode patric update rt at same altitude Proximity Traffic 1200 above ight amp moving in the amp descending moving in the irection of the line direction of the line Figure 10 11 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 10 HAZARD AVOIDANCE 10 5 AVIDYNE TAS600 SERIES Refer to the Avidyne TAS600 Series Pilots Guide for a detailed discussion of the TAS system and an explanation of the aural alerts Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page OPERATING is displayed in the Traffic Mode field 3 Press the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOV
60. 6 400 GALLONS USED 9 4 19 15 300 ENDURANCE 215 RANGE NM 227 200 o o TOTAL TIME IN SERVICE L FUEL QTY R FUEL QTY GAL GAL 100 ope peter nin HRS a e ee PEC FUEL TNC FUEL RST FUEL Figure 3 4 Leaning to First Peak DA40 shown 3 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 3 ENGINE INDICATION SYSTEM EIS ETS ENGINE 123 800 TEMPERATURE ELECTRICAL Cy lin d er Pe ak 1609 1609 p EGT F AMPS A Temperature wea IS 1591 O M 1600 MAN IN HG 1500 24 3 Last Cylinder 1400 ee Peak CARBON HONOXTDE 1300 Indicates Difference 25 Ta _ Between Present and GPH PSI Peak Temperature o 7 a of the Last Peaked 16 8 25 0 Cylinder FUEL CALCULATOR GALLONS REMAIN 40 2 GALLONS USED 9 8 ENDURANCE 2 23 RANGE NM 239 i sae fe SERS TOTAL TIME IN SERVICE GAL GAL Tee ie yee a 8 HRS es a P DEC FUELJINC FUEL RST FUEL Figure 3 5 Leaning to Last Peak DA40 shown 19 15 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 3 5 SECTION 3 ENGINE INDICATION SYSTEM EIS Blank Page 3 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 4 NAV COM 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 Frequ
61. 90 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 17 SECTION 12 ANNUNCIATIONS amp ALERTS GTX 33 Message Advisories XPDR1 CONFIG XPDR1 config error The transponder configuration settings do not match those of backup Contig service req d configuration memory The G1000 system should be serviced MANIFEST GTX1 software The transponder has incorrect software installed The G1000 system should be mismatch communication halted serviced XPDRt SRVC g aii needs service The 1 transponder should be serviced when possible Return unit for repair XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder GRS 77 Message Advisories AHRS1 TAS AHRS1 not receiving airspeed AHRS1 GPS AHRS1 using backup GPS source AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information AHRS1 GPS AHRS1 operating exclusively in no GPS mode AHRS MAG DB AHRS magnetic model database version mismatch AHRS1 SRVC AHRS1 Magnetic field model needs update GEO LIMITS AHRS1 too far North South no magnetic compass MANIFEST GRS1 software mismatch communication halted Garmin G1000 Cockpit Reference Guide for the DA40 40F The 1 AHRS is not receiving true airspeed trom the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system shou
62. A GARMIN G1 01010 Integrated Flight Deck Cockpit Reference Guide Diamond DA40 40F SYSTEM OVERVIEW FLIGHT INSTRUMENTS ENGINE INDICATION SYSTEM NAV COM TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE Copyright 2004 2007 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0369 13 or later for the Diamond DA40 and DA4OF Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton 040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of any revision to this manual onto a
63. 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 tield 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 it 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 G MODE 4ADF gt voL 507 DME MODE NAY ENT TO TRANSFER XPDR 1200 STBY LCL 16 52 53 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 4 Change the DME tuning source 1 2 Turn the small FMS Knob to display the selection window Turn the FMS Knob to select the desired mode and press the ENT Key Figure 4 9 DME Selection Window 4 6 FREQUENCY AUTO TUNING Auto tuning on the PFD ADF DME IDENT THR REF _NRST_ CAUTION Figure 4 10 Nearest Airports Window PFD ADF DME TUNING 196 0 MODE4BFO voL 507 ie SNA Y 1 Figure 4 8 ADF DME Tuning Window From the tuning window turn the large FMS Knob to highlight the desired D
64. AV flight plan with at least one vertical waypoint or direct to with a vertical constraint has been activated Refer to the GPS Navigation Section for more information on VNAV flight plans The flight director may be armed for VNAV at any time but no target altitudes are captured during a climb The Command Bars provide vertical profile guidance based on specified altitudes entered manually or loaded from the database at waypoints in the active flight plan or vertical direct to The appropriate VNAV flight control modes are sequenced by the flight director to follow the path defined by the vertical profile Upon reaching the last waypoint in the VNAV flight plan the flight director transitions to Altitude Hold Mode and cancels any armed VNAV modes Garmin G1000 Cockpit Reference Guide for the DA40 40F Vertical Path Tracking Mode VPTH NOTE If another pitch mode key is pressed while Vertical Path Tracking Mode is selected Vertical Path Tracking Mode reverts to armed When a vertical profile VNAV flight plan is active and the VNV Key is pressed Vertical Path Tracking Mode is armed in preparation for descent path capture VPTH or V when Glidepath or Glideslope Mode is concurrently armed is annunciated in white in addition to previously armed modes If applicable the appropriate altitude capture mode is armed for capture of the next VNAV Target Altitude ALTV or the Selected Altitude ALTS whichever is greater fa P
65. Automatic Squelch eee 4 3 4 4 Quickly Activating 121 500 MHZ 4 3 4 5 Optional NAV Radios 0 ccccceeeeeeen 4 3 ADF Radio ODUON all sccssnnarnistxestenaaneehartdonnnxannieint 4 3 DME Radio optional ine tetanxasttainscisinnecictanaspuduoaseden 4 4 4 6 Frequency Auto tuning cccceceeen 4 4 Auto tunino on Me PED enana a 4 4 Autotuning onthe MPD iecrenisimininianisoniniii 4 4 4 7 Transponder 4 4 Mode SOIC CON aano 4 4 aE SEE 0 E E EE tor 4 5 Code selection esana a S 4 5 PIANE ID REDON nnen 4 6 Section 5 Audio Panel cscs 5 1 5 1 COM Radio Selection 5 2 5 2 Marker Beacon Receiver 0 ccccccceeeceen 5 2 Marker Beacon Signal Sensitivity c ssssesesseesseesseen 5 2 5 3 Nav Radio Audio Selection ccccee 5 2 5 4 Intercom System ICS Isolation 5 3 5 5 Intercom Squelch Control 0 0 0 cce 5 3 5 6 Digital Clearance Recorder and Player 5 4 Section 6 Automatic Flight Control 6 1 6 1 AFCS Controls 6 1 6 2 Flight Director Operation 5555511111111111 6 1 Activating the Flight Director 6 2 Command B eraan ene erecta eoeeecneaee 6 2 AFGI Stats BOX a schetonces tari oiei aiaia 6 3 6 3 Flight Director Modes 0 cccccsceceees 6 3 PITCH IOUCS eraon conse aiienr tenant seaide mizcelass etl mzda 6 3 CO LE Cie 3 osinon a men eae eS 6 16 6 4 Autopilot Oper
66. BANH ICURRENT WHW PROFILE ACTIVE Wh WPT _ __FT at VS TGT PH FRA V5 REQ FP T TERAAIN V5 REO FP H TIME TO TOD l V DEV FT j s 15r Figure 7 47 Descending to the Missed Approach Point Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 19 SECTION 7 NAVIGATION In this missed approach procedure the Tix immediately following the MAP in this case 6368FT is not part of the published procedure It is simply a fix that defines a leg which guides the aircraft along the runway centerline until the required altitude to make the first turn on the missed approach is exceeded In this case if the aircraft altitude is below the specitied altitude 6 368 feet after crossing the MAP a direct to will be established to this fix until an altitude of 6 368 feet reached After reaching 6 368 feet a direct to will be established to the published fix in this case MOGAL If the aircraft altitude is above the specitied altitude after crossing the MAP a direct to will be established to the published tix MOGAL to begin the missed approach procedure The altitude constraint value defaults to 400 feet AGL when the fix is not part of the published procedure In some missed approach procedures this altitude fix may be part of the published procedure For example the procedure dictates a climb to 5 500 feet then turn left and proceed to the Missed Approach Hold Point MAHP In this case the alti
67. Capture is analogous to Selected Altitude Capture Mode and is armed automatically after the VNV Key is pressed and the next VNAV Target Altitude is to be intercepted before the Selected Altitude The annunciation ALTV indicates that the VNAV Target Altitude is to be captured VNAV Target Altitudes are shown in the active flight plan or vertical direct to and can be entered manually or loaded from a database see the GPS Navigation Section for details At the same time as 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL TOD within 1 minute is annunciated in the Navigation Data Box the VNAV Target Altitude is displayed above the Vertical Speed Indicator see Figure 6 12 and the Vertical Track aural annunciation is issued VNAV Target Altitudes can be modified until VNAV Target Altitude Capture Mode becomes active As the aircraft nears the VNAV Target Altitude the flight director automatically transitions to VNAV Target Altitude Capture Mode with Altitude Hold Mode armed This automatic transition is indicated by the green ALTV annunciation flashing for up to ten seconds and the appearance of the white ALT annunciation The VNAV Target Altitude is shown as the Altitude Reference beside the ALTV annunciation At 50 ft from the VNAV Target Altitude the flight director automatically transitions from WNAV Target Altitude Capture to Altitude Hold Mode and tracks the level leg As Altitude Hold Mode
68. Confirmation 4 After the update completes the PFD starts in normal mode 5 Turn the G1000 System OFF and remove the SD card 6 Repeat steps 1 through 4 for the MFD The MFD and PFD databases are now updated Remove the SD card when finished 7 Verity that the correct update cycle is loaded during startup of the MFD Garmin Databases Since these databases are not stored internally in the MFD or PFD a Supplemental Data Card containing identical database versions must be kept in each display unit 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 190 00324 07 Rev A 1 2 3 4 5 SECTION 1 SYSTEM OVERVIEW Insert one SD card in the bottom card slot of the MFD and one in the bottom card slot of the PFD The SD card containing the ChartView or FliteCharts database must be inserted into the bottom slot on the MFD Apply power to the G1000 System View the MFD power up splash screen Check that the databases are initialized and displayed on the scrolling window of the splash screen When updating the terrain and FliteCharts databases an in progress message may be seen If this message is present wait for the system to finish loading before veritying the correct databases are initialized then proceed to step 3 DATABASE 7A Che
69. D 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 IOI PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up or OBSTACLE PULP TE 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 C
70. DA40 40F 1 29 SECTION 7 NAVIGATION Blank Page 7 30 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 8 FLIGHT PLANNING The following discussions pertain to the Multi Function Display unless otherwise indicated 8 1 USER DEFINED WAYPOINTS oer ee Figure 8 1 User WPT Information Page Select the User WPT Information Page 1 Turn the large FMS Knob to select the WPT page group 2 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 2 Turn the small FMS Knob to enter first character of the waypoint name 3 Turn the large FMS Knob to move the cursor to the next character field 190 00324 07 Rev A 5 6 1 SECTION 8 FLIGHT PLANNING Repeat steps 2 and 3 until the desired name is entered Press the ENT Key The cursor is now in the REFERENCE WAYPOINTS field If desired the waypoint can be moditied by changing the reference waypoint Turn the FMS Knobs to enter the position coordinates or the radial and distance trom the reference waypoint Press the FMS Knob to remove the flashing cursor Modify a User Waypoint 1 2 3 4 With the User Waypoint Information Page displayed press the FMS Knob to activate the cursor Turn the large FMS
71. DI and RVSI appear on the PFD as the flight progresses Figure 7 42 Approaching PYNO 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 17 SECTION 7 NAVIGATION 21 Upon passing PYNON the approach procedure will automatically become active The approach may be activated at any point to proceed directly to the IAF In this example the aircraft has progressed through the final waypoint of the arrival and the flight plan has automatically sequenced to the IAF as the active leg activating the approach procedure see Figure 7 43 FPL ACTIVE FLIGHT PLAN 136 975 R eS ACTIVE FLIGHT PLAN mmm TFR KMKC KOOS NO DATA vay uE DTK DIS OPSHN 3Nn ER ae A OPSHN Nn RRR FSHER EDA peee i PYNON cea o DS FT Approoch KCOS RNAV 3SRGPS LPV gt HABUK iof 021 5 2NM 3000 FALUR 261 5 NH A CEGIX fof 351 6 0 RH SR map 351 5 1NM 5368FT 348 U 4NN MOGAL sahp CURRENT VNV PROFILE ACTIVE UNV WEPT S OGeT at HABUK laf VS TGT 7S6FPH FPA VS REO 6Z7FPH T O TO TERRAIN VS REQ oz IME T 0 I V DEV 290FT 1001 1000F j i V244 f PUEE 30nn VIEH VNV PROF CNCL VNV VNY Figure 7 43 Approach Leg is Now Active To manually activate the approach procedure perform the following steps a Press the PROC Key b Turn the large FMS Knob to highlight ACTIVATE APPROACH as shown in Figure 7 44 PROCEDURES OPTIONS ACTIVATE VECTOR TO FINAL ACTIVATE APPROACH S
72. DISC Switch at the Decision height and land the aircraft e Use the GA Switch to execute a missed approach SECTION 6 AUTOMATIC FLIGHT CONTROL KCOS SPO d9 lddV Sd9 SPOIN AVN Sd9 Figure 6 37 LPV Approach to KCOS 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 31 SECTION 6 AUTOMATIC FLIGHT CONTROL 6 32 Go Around Missed Approach Flying a missed approach 1 Push the GA Switch at the Decision 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 Switch is pushed the missed approach is activated and the autopilot disconnects indicated by the AP annunciation flashing yellow for 5 seconds and the autopilot disconnect aural alert Flashes 5 sec _ GA AP ALTS 2 Start the climb to the prescribed altitude in the published Missed Approach Procedure in this case 10 000 ft a Press the AP Key to re engage the autopilot b If navigating an ILS approach press the CDI Softkey to select GPS as the navigation source This is not necessary when navigating a GPS approach c Press the SUSP Softkey to begin navigating to the Missed Approach Hold Point d Press the NAV Key to have the autopilot fly to the hold _ GPS AP ALTS 3 Use the ALT Knob to set a Selected Altitude to hold To hold the current airspeed during the climb press the FLC Ke
73. DRAKE FUE HABUK inf FALUR B N CEGIN fof G m RH35R mop Dim B3B3FT 348 0 O LOAD oR ACTIVATE Figure 7 32 List of Available Transitions f Turn either FMS Knob to select the desired transition In this case the Initial Approach Fix IAF at HABUK will be used g Press the ENT Key Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 13 SECTION 7 NAVIGATION 7 14 h With LOAD highlighted again press the ENT Key The selected approach is added to the flight plan as seen in Figure 7 33 FPL ACTIVE FLIGHT PLAN 136 975 a Or A ACTIVE FLIGHT PLAH KMKC KOOS ee ee Arrival ECOS TBE DBRY1 ALL OPSHN 3nn 260 663nh 10000FT OPSHN BF JOM F FSHER 37r ISMH FT ae ra PYNOHN el HABLUE iof B21 S SNH 30001 FALUR 251 S NA 86001 Aporooch KOOS RHAV 35Rors LPY CURRENT WNW PROFILE ACTIVE We WET TOOOGFT ot OPSHN Jhr VS TGT S5FPH FPA VS REG TERRAIN WS REC Y 100Fr gl 1000F _ Figure 7 33 Loaded Approach 13 Note the altitude constraints associated with each of the approach waypoints as seen in Figure 7 33 These altitudes are loaded from the database and are displayed as light blue text indicating these values are designated for use in computing vertical deviation guidance If it is desirable not to use the displayed altitude for calculating vertical deviation guidance perform the following a Press the FMS Knob t
74. E or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 5 Press the MUTE Softkey to mute TAS voice alerts Garmin G1000 Cockpit Reference Guide for the DA40 40F Traffic Advisory aircraft is 400 below is Out of Traffic Mode Altitude Mode climbing ange 136 975 Non Bearing Traffic system Proximity Traffic is unable to determine bearing 1000 above amp distance is 8 0 nm 1190 above descending and descending Figure 10 12 Traffic Map Page Displaying Traffic on the Navigation Map 1 Ensure the TAS system is operating With the Navigation Map displayed press the MAP Softkey 2 Press the TRAFFIC Softkey Traffic will now be displayed on the map see Figure 10 12 190 00324 07 Rev A SECTION 10 HAZARD 10 6 TERRAIN AND OBSTACLE PROXIMITY 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 is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 def
75. ELECT APPROACH SELECT ARRIVAL SELECT DEPARTURE Figure 7 44 Activate Missed Approach c Press the ENT Key to activate the approach 7 18 Garmin G1000 Cockpit Reference Guide for the DA40 40F 22 The IAF is the next waypoint At the TOD establish a descent vertical speed as previously discussed in Step 16 The aircraft altitude will be 9 000 feet upon reaching HABUK FPL ACTIVE FLIGHT PLAN 136 975 i R 5358FT nae ACTIVE FLIGHT PLAN a TFR KMKC KCOS NO DATA OPSHN 3n OPSHN FSHER PYNON en ere KCOS RNAV 35Roes LPV HABUK lof 251 1 7N ry FALUR 261 S ONH CEGIX fof 351 6 0NM RH SR aap 351 SINH GIGBFT 346 U 4NM MOGAL aahp CURRENT VNV PROFILE ACTIVE Viv WPT S QGeT at HABUK laf VS TGT 7S6FPH FPA VS REO FPH TIME TO BO TERRAIN VS REO bain IME B00 f v Dev SOFT 100Ff1 1000Ff7 m sj JONN VIEH VNY PROF CNOL VNV VNV amp K 10099 F a a 1 W y Q N a T ETES LELE U E Figure 7 45 Descending Turn to the Initial Approach Fix IAF 190 00324 07 Rev A 23 After crossing FALUR the next waypoint is the FAF The flight phase changes to LPV on the HSI indicating the current phase of flight is in Approach Mode and the approach type is LPV CDI scaling changes accordingly and is used much like a localizer when flying an ILS approach The RVSI is no longer displayed and the VDI changes to the Glidepath Indicator as shown in Figure 7 46 when the final approach course become
76. ENT Key 7 22 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 7 NAVIGATION Access Runway Information 7 5 INTERSECTION INFORMATION 1 With the Airport Information Page displayed press Select the Intersection Information Page the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor on the 1 Turn the large FMS Knob to select the WPT page RUNWAYS identifier field ser 2 Turn the small FMS Knob to select the second rectangular page icon 3 Turn the small FMS Knob in the direction of the green arrow to display the next runway for the selected airport Continue turning the small FMS Knob to select the desired runway 4 To remove the flashing cursor press the FMS Knob Access Frequency Information 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to move the cursor to the Frequencies box 3 Turn either FMS Knob to scroll through the list placing the cursor on the desired frequency If a listed trequency has sector or altitude restrictions the frequency is preceded by an info i designation Figure 7 57 Intersection Information Page Press the ENT Key to view the information The following may be displayed with the frequency Access Information on an Intersection e TX transmit only 1 With the Intersection Information Page displayed e RX rece
77. ENU Key to display the Direct to options menu With Cancel Direct To NAV highlighted press the ENT Key If a flight plan is still active the G1000 resumes navigating the flight plan along the closest leg PAGE MENU OPTIONS Concel Direct To NAV Clear Vertical Constraints Press the FMS CRSR knob to return to bese poge Figure 7 6 Canceling Direct to Navigation Direct to Navigation from the PFD WPT Symbol DIRECT TO Identifier ae ie WPT Location Facility Name 3 VNV Target Altitude aaa OFFSET 5MM Offset Distance Bearing to WPT GAIA DIS 1074N4 Distance from WPT Course to Selected WPT AR ACTIVATE Figure 7 7 PFD Direct to Window Garmin G1000 Cockpit Reference Guide for the DA40 40F i SECTION 7 NAVIGATION Enter a Direct to Destination 1 Press the Direct to Key E 2 Turn the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude contraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the VNV altitude field 7 Turn the small FMS Knob to enter the desired VNV altitude 8 Press the ENT Key The option to select MSL or AGL is now displayed
78. F 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 190 00324 07 Rev A 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 Selection 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 gt CREW OW 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 5 3 S
79. FSS frequencies 7 28 Negative Climb Rate After Takeoff 10 13 NEXRAD 1 9 10 4 Non path descent 6 12 6 29 6 30 0 OBS 2 12 Obstacles 10 14 12 11 12 15 Operation 5 2 Optional NAV radios 4 3 Overspeed protection autopilot 6 33 P Page group icon 1 9 PDA 10 13 PFD 1 1 4 1 4 4 Pitch hold 1 4 Pitch Hold Mode PIT 6 5 Pitch modes flight director 6 3 6 9 Pitch Reference 6 5 PLAY Key 5 4 Premature Descent Alert 10 13 Procedures GFC 700 6 23 6 34 PROC Key 1 4 Red pointer 2 3 Remove departure arrival or approach 8 6 Replies 4 5 Required Vertical Speed 2 6 7 15 Required Vertical Speed Indicator 7 15 Reversionary mode 11 1 ROC 10 12 10 15 12 5 Roll Axis Modes 6 2 190 00324 07 Rev A Roll Hold Mode ROL 6 17 Roll modes flight director 6 16 6 19 Roll Reference 6 17 RTC 10 12 RVSI 7 15 7 16 RX indicator 4 3 R indication 4 5 S Secure Digital SD card 1 12 Selected Altitude 6 6 6 10 6 13 Selected Altitude Capture Mode 6 6 6 10 6 13 Selected Course 6 20 Selected Heading 6 18 Selected vertical speed 2 7 Servos 6 21 Severe thunderstorm 10 5 SIGMET 10 5 Slip Skid indicator 2 3 Softkey function MFD 1 5 1 8 Speed ranges 2 3 SQ 1 3 Squelch 5 3 STBY Softkey 4 5 Store Flight Plan 8 7 Stormscope lightning data 1 5 1 9 10 2 Strike 10 2 Strike mode 10 2 System annunciations 12 1 12 6 System message advisories 12 9 T TAS 10 8 12 18 TAWS 10 10 10 12 10 14
80. Figure 7 19 V4 is Loaded in the Flight Plan 5 V4 will now be made the active leg of the flight plan l GPS rg a a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight SLN The TO waypoint of the leg is selected in order to activate the leg c Press the ACT LEG Softkey The confirmation window is now displayed as in Figure 7 20 Note the TOP to SLN leg is actually part of V4 Figure 7 21 V4 Now Active Leg TOP gt SLN ACTIVATE ummm Or 01m Figure 7 20 Confirm Active Leg d Verity the displayed leg is the desired leg and press the ENT Key Note in Figure 7 21 the magenta arrow in the flight plan window and magenta line on the map indicating V4 is now the active flight plan leg 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 9 SECTION 7 NAVIGATION 6 The aircraft continues on heading 290 When 2 0 nm trom the intercept the XTK will disappear trom the HSI and the CDI will be positioned on the last dot indicating a 2 0 nm distance from the centerline of the next course 7 As the CDI approaches center the aircraft turns onto the active leg as seen in Figure 7 22 136 975 ACTIVE FLIGHT PLAN FPL ACTIVE FLIGHT PLAN MCI TIFTC Enroute TOP Airvoy V4 SLN SLN Airway 244 LAA 7 rez X FA ENEN 16SNH CURRENT VNV PROFILE ACTIVE VNV WPT VS TGT TERRAIN i 100F7 ef 1000r7 Mi Lal Fa La CNCL VNV Y EA
81. Flight ID field 3 Turn the small FMS Knob to enter the desired first character 4 Turn the large FMS knob to place the cursor in the next desired field 5 Turn the small FMS Knob to enter the next desired character 6 Repeat steps 4 and 5 until the desired Flight ID is entered 7 Press the ENT Key updating will be displayed as the Flight ID is loaded into the system 4 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 5 AUDIO PANEL SECTION 5 AUDIO PANEL COM1 MIC COMI Transceiver Audio Transmitters J COM 3 is unavailable COM3 MIC is unavailable Oy 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 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 5 1 SECTION 5 AUDIO PANEL 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
82. GPS system while the G1000 provides vertical guidance through descents A lateral flight plan LNAV would be navigated in much the same way but would not include vertical guidance when the final approach course is active The example is a flight plan from KMKC to KCOS filed using the TIFTO2 departure various Victor Airways and the DBRY1 arrival with the transition at TBE Enroute altitude will be 12 000 feet An LPV WAAS approach will be selected for runway 35R A missed approach will be executed at the Missed Approach Point MAP A few enroute changes are demonstrated NOTE If the loaded arrival procedure has published altitudes contained in the navigation database these are for turbojet aircraft only Accept or change these values as desired to meet the requirements of the clearance 1 Prior to departure the TIFTO2 departure the airways and the DBRY 1 arrival at KCOS are loaded See the Procedures section for loading departures and arrivals Note the magenta arrow in Figure 7 11 indicating the active departure leg After takeoff ATC assigns a heading of 240 Garmin G1000 Cockpit Reference Guide for the DA40 40F i SECTION 7 NAVIGATION 2 Figure 7 11 shows the aircraft on the assigned 3 heading of 240 TERM Terminal is the current CDI flight phase displayed on the HSI indicating 1 0 nm CDI scaling 136 975 ACTIVE FLIGHT PLAN KMKC KCOS FPL ACTIVE FLIGHT PLAN NORTH UP DTK DE Dep
83. Go Around in air GA Switch ALTS is armed automatically when PIT VS FLC or GA is active and under VPTH when the Selected Altitude is to be captured instead of the VNAV Target Altitude ALTV is armed automatically under VPTH when the VNAV Target Altitude is to be captured instead of the Selected Altitude Table 6 1 Flight Director Pitch Modes 6 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Pitch Hold Mode PIT When the flight director is activated the FD Key is pressed Pitch Hold Mode is selected by default Pitch Hold Mode is indicated as the active pitch mode by the green annunciation PIT This mode may be used for climb or descent to the Selected Altitude shown above the Altimeter since Selected Altitude Capture Mode is automatically armed when the mode is activated In Pitch Hold Mode the flight director maintains a constant pitch attitude the pitch reference The pitch reference is set to the aircraft attitude at the moment of mode selection If the aircraft pitch attitude exceeds the flight director pitch command limitations the flight director commands a pitch angle equal to the nose up down limit Pitch Hold Mode Active nev1 1 13 08 118 98 ee wv215 98 118 9010 ROL PIT ALTS Command Bars Maintain Desired Pitch Reference SECTION 6 AUTOMATIC FLIGHT CONTROL Changing the Pitch Reference When operating in Pitch Hold Mode the pitch reference can be a
84. Heading Box Altimeter Horizontal Situation Indicator 13 Selected Altitude 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 1 SECTION 2 FLIGHT INSTRUMENTS Nava 117 95 naz 108 00 117 95 W thas fa TRAFFIC oe _ e ee i a ral ey INSET Traffic Annunciation 2 Vspeed References G Selected Heading Box Wind Data Window G Inset Map 6 BRGI Information Window T DME Information Window BRG2 Information Window 136 975 128 109 cont 136 975 DOH F BARO HIN Z494IH ester T FLIGHT PLAN GILRO KSIC DIS PATYI NH HIVAK fof r HH SUNNE mohp 6 8NH dp HOD FF A ANH i JBL GPS PDE R ILC ADF DHE XPDR IDENT THR REF NRST Flight Plan Window Le W F 19 07 57 10 Barometric Minimums Box Annunciation Window Selected Altitude Bug 13 Selected Course Box Barometric Minimums Bug 15 Glidesope Indicator Marker Beacon Annunciation Figure 2 2 Additional PFD Information Flight Plan Messages Indications Distance to Next Waypoint Bearing to Next Waypoint DIS BRG Figure 2 3 PFD Navigation Status Box 2 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A
85. Knob to highlight MFD DSPL 1 7 gt AUTO and repeat steps 3 through 5 PFD SETUP MENU AUTO AUTO 23 474 wet PFD DSPL gt MFD DSPL Figure 1 10 PFD Setup Menu Window XM RADIO AUTOMATIC MUTING XM Radio audio will be automatically muted when the Updating the Jeppesen aviation database 1 With the G1000 System OFF insert the SD card containing the aviation database update into the top card slot of the PFD to be updated Label of SD card facing left 2 Turn the G1000 System ON A prompt similar to the following is displayed in the upper left corner of the PFD DO YOU WANT TO UPDATE THE AVIATION DATABASE FROM TO WORLDWIDE WORLDWIDE 0584 0605 13 APR 2006 11 MAY 2006 11 MAY 2006 48 JUN 2006 NO WILL BE ASSUMED IN 8 SECONDS Figure 1 11 Database Update Prompt aircraft groundspeed exceeds approximately 30 kts and the airspeed is less than approximately 80 kts The audio 1 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 3 Press the ENT Key to start the database update A prompt similar to the following is displayed DO YOU WANT TO UPDATE THE AVIATION DATABASE FROM TO WORLDWIDE WORLDWIDE 0584 0605 13 APR 2006 11 MAY 2006 11 MAY 2006 48 JUN 2006 REGION CYCLE NO WILL BE ASSUMED IN 8 SECONDS UPDATING AVIATION DATABASE PLEASE WAIT UPDATED TOP ILES SULEESSFULL I PRESS ANY KEY TO CONTINUE CONTINUING IN 8 SECONDS Figure 1 12 Database Update
86. 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 2 Select the User Waypoint Information Page and press the DELETE Softkey 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 SECTION 8 FLIGHT PLANNING Create User Waypoints from the Navigation Map Page 1 With the Navigation Map Page displayed push the Joystick to activate the panning function The target pointer is displayed at the present aircraft position 2 Move the Joystick to place the pointer at the desired position 3 Press the ENT Key The User Waypoint Information Page is now displayed with the captured position FP E 4 Turn the FMS Knobs to select a waypoint name Figure 8 3 Active Flight Plan Page on the MFD 5 Press the ENT Key to accept the selected name The first reference waypoint field is highlighted 8 3 ACTIVATE A STORED FLIGHT PLAN 6 If desired turn the FMS Knobs to enter the identifier of the reference waypoint and the radial and 1 Press the FPL Key and turn the small FMS Knob to distance to the reference waypoint Press the ENT display the Flight Plan Catalog Page Key to accept 7 Press the FMS Knob to remove the flashing cursor or press
87. MAL OPERATION will be disabled Additionally the accuracy of all nearest information airports airspaces and waypoints will be questionable Finally airspace alerts will continue to function but with degraded accuracy 11 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 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 System 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 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS from annunciations that are not yet acknowledged Acknowledged annunciations are always above the li
88. ME source NEAREST AIRPORTS 124 6 8NM 122 700 RNWY 244QFT 210 10 2N 123 000 RNWY 57 FT 150 11 4NM 133 000 RNWY 7339FT Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 Press the NRST Softkey to display the Nearest Airports Window 2 Turn the FMS Knobs to highlight the desired frequency 3 Press the ENT Key to place the frequency in the standby field of the active COM 4 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 4 7 TRANSPONDER Mode Selection The STBY ON ALT GND VFR CODE and IDENT Softkeys can be accessed by pressing the XPDR Softkey Ground Mode Automatic or Manual GND is displayed when the aircraft is on the ground or when the GND Softkey is pressed The transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely address Mode S interrogations xPOR ENT __ _BACK _ ADVISORY Figure 4 11 Ground Mode 190 00324 07 Rev A Standby Mode Manual Press the STBY Softkey In Standb
89. ONTROL descent The flight director maintains the current altitude until either engine power or the Airspeed Reference are adjusted and does not allow the aircraft to climb or descend away from the Selected Altitude Changing the Airspeed Reference The Airspeed Reference shown in both the AFCS Status Box and above the Airspeed Indicator may be adjusted e Using the NOSE UP NOSE DN Keys By pressing the CWS Button hand tflying the aircraft to a new airspeed then releasing the CWS Button to establish the new Airspeed Reference Flight Level Change Airspeed Altitude Hold Mode Active Reference Mode Armed NAVI 113 80 aE a A nav2108 08 117 95 Airspeed Reference 3120K1 Airspeed Reference Bug Tae of Figure 6 9 Flight Level Change Mode 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 9 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Navigation Modes VPTH ALTV NOTE Pressing the CWS Button while Vertical Path Tracking Mode is active does not cancel the mode The autopilot guides the aircraft back to the descent path upon release of the CWS Button NOTE VNAV flight director pitch modes are available only in conjunction with GPS roll modes A NOTE The Selected Altitude takes precedence over any other vertical constraints Vertical Navigation VNAV flight control is available for enroute terminal cruise and descent operations when VNAV has been enabled and a VN
90. S ALT 3000er VPI Akt ALTS GP V Figure 6 10 Vertical Path Tracking Armed Annunciations Prior to descent path interception the Selected Altitude must be set below the current aircraft altitude by at least 75 ft For the flight director to transition from Altitude Hold to Vertical Path Tracking Mode acknowledgment is required within five minutes of descent path capture by Pressing the VNV Key e Adjusting the Selected Altitude If acknowledgment is not received within one minute of descent path interception the white VPTH annunciation starts to flash Flashing continues until acknowledged or the descent path is intercepted If the descent is not confirmed by the time of interception Vertical Path Tracking Mode remains armed and the descent is not captured 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL In conjunction with the TOD top of descent within 1 minute annunciation in the Navigation Data Box VNAV indications VNAV Target Altitude vertical deviation and vertical speed required appear on the PFDs in magenta Figure 6 11 Vertical Path Tracking Armed Flashing Altitude Hold Mode Active Indicates Acknowledgment Required 136 975 118 000 com VPTH 136 975 COM VNAV Target Altitude Selected Altitude Below VNAV Target Vertical Deviation Indicator cH 6000 es Required Vertical a 7 Speed Bug Enroute Phase of Flight HSI Set to GPS Figure 6 11 Vert
91. S Knob to remove the flashing cursor Access Runway Information for the Selected Airport 1 With the Nearest Airports Page displayed press the RNWY Softkey to place the cursor in the RUNWAYS field 2 Turn the small FMS Knob to select the desired runway 3 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 2 Turn either FMS Knob to select the desired frequency 3 Press the ENT Key The selected frequency is placed in the COM standby frequency field 4 Press the Frequency Transfer Key to place the frequency in the active field 5 Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 25 SECTION 7 NAVIGATION Nearest Airports Information on the PFD Bearing TO Distance Airport Symbol NEAREST JAIRPORTS E Identifier JU56 E eE eN VER I MULTICOM 122 900 RNWY 3500FT KIDA 261 95nNM ILS TOWER 118 5600 RNWY ss i KRXE 352 20 1NM UNICOM 122 800 RNWY Runway Length 4200FT Primary COM Frequency Figure 7 61 Nearest Airports Window Press the NRST Softkey to display the PFD Nearest Airports Window View Information on a Specific Airport in the List 1 With the Nearest Airports Window displayed turn either FMS Knob to place the cur
92. SE DN keys or push the CWS Button while hand flying the aircraft to adjust the commanded airspeed while maintaining the same power or reduce power to allow descent in Flight Level Change Mode while the autopilot maintains the current airspeed As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft Cruise Altitude of 12 000 MSL rg ALT Mode 2 ALT Mode Figure 6 33 FLC Descent 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 27 SECTION 6 AUTOMATIC FLIGHT CONTROL Vertical Path Tracking descent to VNV Target Altitude 1 Select coupled VNAV a Press the VNV Key to arm Vertical Path Tracking Mode The white annunciation VPTH appears J GPS AP VPTH b Using the ALT Knob set the Selected Altitude at least 75 feet below the flight plan s VNV Target Altitude of 10 000 feet This altitude was entered in the flight plan as a component of an offset waypoint trom OPSHN intersection as indicated in the example flight plan in Section 7 GPS Navigation If the Selected Altitude is not adequately adjusted below the VNV Target Altitude the flight direc
93. SECTION 12 ANNUNCIATIONS amp ALERTS This annunciation will only be seen when the autopilot is engaged The Other Various Red X Indications annunciation indicates an AHRS monitor has detected an abnormal flight parameter possibly caused by strong turbulence In this case the situation should correct itself within a few seconds If there is an actual failure a red X will soon appear over the Attitude Indicator 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 Display is not receiving valid transponder information A red X through any other display field such as engine instrumentation fields indicates that the field is not receiving valid data 190 00324 07 Rev A 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 nawe MAN iy L 1n y l a i ATTITUDE p TE RPA 7990 S A A A Sow P 1G aR FUEL FLOW GPH L
94. STBY LCL 2541p Figure 6 8 Vertical Speed Mode Changing the Vertical Soeed Reference The Vertical Speed Reference shown both in the AFCS Status Box and above below the Vertical Speed Indicator any be changed by e Using the NOSE UP NOSE DN Keys e By pressing the CWS Button hand flying the aircraft to attain a new Vertical Speed Reference then releasing the CWS Button Flight Level Change Mode FLC NOTE The Selected Altitude should be set before selecting Flight Level Change Mode 6 8 Garmin G1000 Cockpit Reference Guide for the DA40 40F Flight Level Change Mode is selected by pressing the FLC Key When Flight Level Change Mode is active the flight director continuously monitors Selected Altitude airspeed and altitude This mode acquires and maintains the Airspeed Reference while climbing or descending to the Selected Altitude shown above the Altimeter The Airspeed Reference is set to the current airspeed upon mode activation Flight Level Change Mode is indicated by an FLC annunciation beside the Airspeed Reference in the AFCS Status Box The Airspeed Reference is also displayed directly above the Airspeed Indicator along with a bug corresponding to the Airspeed Reference along the tape Engine power must be adjusted to allow the autopilot to fly the aircraft at a pitch attitude corresponding to the Airspeed Reference and the desired flight profile climb or 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT C
95. T Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as hectopacals STD BARO Press to set the barometric pressure to standard pressure BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window OBS Press to select OBS Mode on the CDI when navigating by GPS only available with active leg CDI Press to change navigation mode on the CDI between GPS VORI and VOR2 ADF DME optional Press to display the ADF DME Tuning Window optional in the U S A refer to ICAO standards for VFR codes in other countries CODE Press to display transponder code selection softkeys 0 7 0 through 7 Press numbers to enter code IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BKSP Press to remove numbers entered one at a time BACK Press to return to the previous level softkeys IDENT Press to provide special aircraft position identification to Air Traffic Control ATC BACK Press to return to the previous level softkeys ALERTS Press to display the Alerts Window nHnHenAnirnkin O Il sy on ar f eno ver J coo Licent __J _back_J aterrs Press the BACK Softkey to return to the top
96. VOR or LOC depending on the loaded approach This mode uses the selected navigation receiver deviation and desired course inputs to fly the approach Approach Mode provides greater sensitivity for signal tracking than Navigation Mode Pressing the APR Key when the CDI is greater than one dot arms the selected approach mode annunciated Garmin G1000 Cockpit Reference Guide for the DA40 40F in white to the left of the active roll mode If the selected navigation receiver is GPS pressing the APR Key arms GPS Approach Mode provided that a GPS approach has been loaded into the flight plan If the loaded approach provides WAAS based vertical guidance Glidepath Mode is also armed Figure 6 16 If GPS Approach Mode is selected while in GPS Navigation Mode capture can occur with crosstrack error of up to 2 nm GPS GPS e ALTS Figure 6 24 GPS Approach Mode Armed LOC Approach Mode allows the autopilot to fly a LOC ILS approach with a glideslope LOC Approach Mode is armed along with Glideslope Mode see Figure 6 17 when the APR Key is pressed and either of the following have been done e Navigation source is set to LOC A LOCALS approach is loaded into the flight plan and the corresponding localizer frequency tuned even if the selected navigation source is GPS Localizer capture is suppressed until the navigation source is changed to LOC It Approach Mode is active and either of the following occur the flight director rev
97. Vertical Speed Mode the flight director acquires and maintains a Vertical Speed Reference Current aircraft vertical speed to the nearest 100 fpm becomes the Vertical Speed Reference at the moment of Vertical Speed Mode activation Vertical Speed Mode does not consider the relative position of the Selected Altitude in relation to the current aircraft altitude at the time of mode activation so it is possible to use Vertical Speed Mode while not climbing descending to the Selected Altitude Vertical Speed Mode is activated by pressing the VS Key the VS annunciation appears in the AFCS Status Box to indicate the active pitch mode along with the Vertical Speed Reference to the right The Vertical Speed Reference is also displayed above the Vertical Speed Indicator A Vertical Speed Reference Bug corresponding to the Vertical Speed Reference is shown on the indicator 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 7 SECTION 6 AUTOMATIC FLIGHT CONTROL MAN Li 118 98 Itxp nav2i115 98 110 90 TIX Vertical Speed Mode Active Command Bars Indicate Climb to Attain Vertical Speed ya Selected Altitude Capture Referee H Aw and CON1 een ALTS 123 SHB md 135 325 conz ji _ _ Selected Altitude E Fag aa e Vertical Speed ac ER Reference E 1300 E Vertical Speed Reference Bug el 300 eee je l 1140 E TTWH 4 1000 M 900 2 r 29 731N xPOR 1200
98. a OFFSET SNH KIXD i Ds 1074NH 51K Figure 7 9 Nearest Airport List PFD 190 00324 07 Rev A 3 Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position as shown in Figure 7 9 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press ENT again to activate a Direct to Select a Direct to Destination to a Recently Entered Identifier 1 Press the Direct to GX Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 8 The list is only populated when navigating a flight plan 3 Turn the small FMS Knob to the right to display the RECENT waypoints as shown in Figure 7 10 OFFSET SHH DIS 1A74HH ACTIVATE Figure 7 10 Recently Entered Waypoints List PFD 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press ENT again to activate a Direct to Cancelling Direct to Navigation 1 Press the Direct to E88 Key 190 00324 07 Rev A SECTION 7 NAVIGATION 2 Press the MENU Key to display the Options Window The cursor will be tlashing on Cancel Direct to NAV 3 Press the ENT Key to cancel the direct to 7 3 NAVIGATING AN EXAMPLE FLIGHT PLAN The following discussion is an example of navigating a flight plan with the WAAS capable
99. aircraft symbol a Figure 6 3 Command Bars Mode Reference Armed Mode Pitch Axis Modes AFCS Status Box nav 113 88 gt 118 9B91z3 wer NANG 118 98 11x System Status Annunciation see Annunciations amp Alerts Aircraft Attitude Symbol Flight Director Command Bars Garmin G1000 Cockpit Reference Guide for the DA40 40F 118 708 com Selected Altitude Box DR IDEN PFD AFCS Display 190 00324 07 Rev A AFCS Status Box Flight director roll modes are shown on the left and pitch on the right Armed modes are annunciated in white and active in green Autopilot status is displayed in the center of the AFCS Status Box 6 3 FLIGHT DIRECTOR MODES Flight director modes are normally selected independently for the pitch and roll axes Unless otherwise specified all mode keys are alternate action i e press on press off In the absence of specific mode selection the flight director reverts to the default pitch and or roll mode s Armed modes are annunciated in white and active in green in the AFCS Status Box Under normal operation when the control for the active flight director mode is pressed the flight director reverts to the default mode s for the axis es Automatic transition from armed to active mode is indicated by the white armed mode annunciation moving to the green active mode field and flashing for ten seconds A flashing yellow mode annunciation and annunciator light indicate
100. an nunciation Autopilot Manually Disengaged a ROL O gt IT ALTS Figure 6 28 Manual Autopilot Disengagement Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 6 AUTOMATIC 6 5 EXAMPLE PROCEDURES USING AFCS A NOTE The diagrams in this section are for instruc tional purposes only and should not be used for navigation This section provides a scenario based set of procedures showing various GFC 700 AFCS modes used while following a previously entered flight plan The following example closely follows the example flight plan discussed in the GPS Navigation section Refer to the example in Section 7 GPS Navigation when studying the this example In this scenario the aircraft departs Charles B Wheeler Downtown Airport KMKC enroute to Colorado Springs Airport KCOS After departure the aircraft climbs to 12 000 ft and airway V4 is intercepted after following heading vectors of 240 and 290 assigned by ATC Airway V4 is flown to Salina VOR SLN using VOR navigation then airway V244 is flown using a GPS flight plan The ILS approach for runway 35L and LPV WAAS approach for runway 35R are shown and a missed approach is executed KCOS ey Salina VOR SLN Figure 6 29 Flight Plan Overview 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 23 SECTION 6 AUTOMATIC FLIGHT CONTROL De
101. ata 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 Winds Alor time the product time will change from light blue to amber Clouds Tops in color 10 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 10 4 Displaying Traffic on the Traffic Map Page TRAFFIC INFORMATION SERVICE TIS NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the second rectangular page icon 3 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Press the STANDBY Softkey to place the system in the Standby mode STANDBY will be displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area If data is not received for a period longer than 6 seconds the age of the present data will be displayed in the lower left of the screen along with the annunciation 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 190 00
102. ather 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 purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 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
103. ation 0 6 21 Engaging the AUtopilot scssccsssesssssssssessesseessean 6 21 Control Wheel Ste ring ccssccsscesssesseesecsessesseesneesees 6 21 Disengaging the AUtOpIIOt ccssessesssessesseeseeen 6 22 6 5 Example Procedures Using AFCG 6 23 Pepati CBeeaemaeeter eee ten tenee tea men ema te irerentre ers 6 24 Intercepting a VOR Radial ssssssssessssessessessesneeen 6 25 Flying a Flight Plan GPS COUrS ssssessessessesseeen 6 26 DES COMI E TEE E E E E E E E 6 27 Garmin G1000 Cockpit Reference Guide for the DA40 40F TABLE OF CONTENTS LNT 0 crs EAE T E E er 6 30 Go Around Missed Approach sssssessessessesseesseerees 6 32 6 6 AFCS Annunciations and Alerts 0 6 33 APCS Statis AlGIS ascs snorstessvermestaasatsnsnornteesvarenciared 6 33 Overs peed PROTECTION ranea 6 34 Section 7 NAVIGATION 7 1 7 4 Navigation Map Pag cccccesceeeceen 7 1 Select the MAP Page GIOUD cssessessesseesseeseesesseean 7 1 7 2 Direct to Navigation 0 0 ccc cee 7 1 Direct to Navigation trom the MFD 7 1 Direct to Navigation trom the PFD s 7 3 7 3 Navigating an Example Flight Plan 7 5 7 4 Airport Information 0 0 0 0 eee 7 21 Select the Airport Information Page 7 21 7 5 Intersection Information 0 0 cc 1 23 Select the Intersection Information Page 1 23 7 6 NDB Information 0 0 c cceee een 7 24 Sele
104. ault display Terrain Obstacle above or within 100 4 Rotate the Joystick clockwise to display a larger below or above aircraft altitude area or rotate counter clockwise to display a smaller l gt ace Terrain Obstacle between 100 and 1000 below current aircraft altitude Displaying Terrain and Obstacles on the Navigation Map Prga Miroraft Atitude _ 1 With the Navigation Map displayed press the MAP Softkey 2 Press the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map 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 13 Obstacle Symbols 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 9 SECTION 10 HAZARD 10 7 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 TERRAIN Displaying Terrain on the TAWS Page i Sei j 1 Turn the large FMS Knob to select the Map Page a 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 Softk
105. b 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 190 00324 07 Rev A SECTION 7 NAVIGATION NEAREST VO HRST m Ta HOATH LIP j ere 7 aa ra GA a Figure 7 64 Nearest VOR Page 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 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 frequency field Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 27 SECTION 7 NAVIGATION 3 Press the FMS Knob to remove the flashing cursor 7 13 NEAREST USER WAYPOINT INFORMATION QJ41 16 REFERENCE WAYPOINTS Figure 7 65 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 t
106. ble 6 3 Roll Hold Mode Responses Button Roll Hold Mode ROL Changing the Roll Reference NOTE If Roll Hold Mode is activated as a result The roll reference can be changed by pressing the CWS of a mode reversion the flight director rolls the Button establishing the desired bank angle then releasing wings level the CWS Button When the flight director is activated the FD or AP Key is pressed Roll Hold Mode is selected by default This mode is annunciated as ROL in the AFCS Status Box The current aircraft bank angle is held subject to the bank angle conditions listed in Table 6 3 Roll Mode Roll Hold default Heading Select HDG Key Navigation GPS Arm Capture Track GPS Langaton VOR Enroute Arm Capture Track NAV Key VOR Navigation LOC Arm Capture Track LOC No Glideslope Approach GPS Arm Capture Track GPS Approach VOR Arm Capture Track APR Key VAPP Approach ILS Arm Capture Track LOC Glideslope Mode automatically armed Go Around in air GA Switch Table 6 2 Roll Modes 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 17 SECTION 6 AUTOMATIC FLIGHT CONTROL Heading Select Mode HDG Heading Select Mode is activated by pressing HDG Key Heading Select Mode acquires and maintains the Selected Heading The Selected Heading is shown by a light blue bug on the HSI and in the box to the upper lett of the HSI Changing the Selected Heading
107. cal waypoint ALT Mode Selected Altitude set below VNAV Target Altitude Along track Offset 3 nm before OPSHN m 3 nm A Figure 6 34 VPTH Descent 6 28 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Non path descent using Flight Level Change Mode 1 Command a non path descent using Flight Level Change Mode a Using the ALT Knob set the Selected Altitude below the current aircraft altitude to an altitude in this case 9 400 feet at which to level off between VNV flight plan altitudes b Press the FLC Key before the planned TOD during an altitude hold while VPTH is armed The Airspeed Reference defaults to the current aircraft airspeed Vertical Path Tracking and Selected Altitude Capture Mode are armed automatically _ GPS TAP ALTS VPTH 2 Reduce power to allow descent in Flight Level Change Mode The autopilot maintains the Airspeed Reference 3 As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds Selected Altitude of 9 400 MSL OPSHN E 3 n A SECTION 6 AUTOMATIC FLIGHT CONTROL E GPS AP ALT _VPTH The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft J GPS AP VPTH 4 When the
108. cklist File N A Basemap Land 1 01 A gt SofeToxi Expires 28 SEP 2006 aw Terrain 2 04 a Airport Terrain 2 04 aN Obstacle Expires 28 SEP 2006 Aviation Expires 23 NOV 2006 FliteCharts Expires 11 MAY 2006 All map and terrain data provided is only to be used as a general reference to your surrounding und as an aid to situational awareness Press ENT or rightmost softkey to continue Figure 1 13 Power Up Splash Screen Window Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey At the MAP NAVIGATION MAP Page select the MAP Softkey and check to make sure that the TOPO and TERRAIN Softkeys are available not dimmed and other database features are functioning Power down the G1000 Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 13 SECTION 1 SYSTEM OVERVIEW Blank Page 1 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 2 FLIGHT INSTRUMENTS SECTION 2 FLIGHT INSTRUMENTS The following discussions pertain to the Primary Flight Display unless otherwise indicated navi113 25 110 90 ERG 133 000 con NAVE 118 98 124 300 COM Tann E sii E 7000 6504 ST ALERTS INSET F CDI ADF DME XPOR IDENT TMR REF NRST O NAV Frequency Box E Turn Rate Indicator 2 Airspeed Indicator Barometric Setting Box G True Airspeed Box Vertical Speed Indicator
109. ct the NDB Information Page ccscesecseseeseesees 7 24 7 7 VOR Information seen 7 24 Select the VOR Information Page c ccscesecseeseesesees 7 24 7 8 User Waypoint Information Page 7 25 7 9 Nearest Airports 0 c ccs 7 25 Nearest Airport Information on the MFD c e00 7 25 Nearest Airports Information on the PFD 1 26 7 10 Nearest Intersections c cscs 1 26 Select the Nearest Intersections Page 7 26 7 11 Nearest NDB 0 0 cece 1 21 Select the Nearest NDB Page sssssessessessesseaneerees 7 27 7 12 Nearest VOR cece 1 21 Select the Nearest VOR Page cessssessessessesseesneerees 7 27 7 13 Nearest User Waypoint 0 cccceseen 7 28 Select the Nearest User Waypoint Page 1 28 7 14 Nearest Frequencies c cccccseseseeeeen 1 28 Select the Nearest Frequencies Page 7 28 7 15 Nearest AirSpaCes c ccc 7 29 Select the Nearest Airspaces Page 7 29 Section 8 Flight Planning 8 1 8 1 User Defined Waypoints 11111111111111111111 8 1 Select the User WPT Information Page 8 1 Create User Waypoints from the Navigation Map Page 8 2 8 2 Viewing the Active Flight Plan 8 2 8 3 Activate a Stored Flight Plan 8 2 ii Garmin G1000 Cockpit Reference Guide for the DA40 40F 8 4 Activate a Flight Plan Leg 5555151111111 8 3 8 5 Stop Navigating a Flight P
110. ct the fourth rectangular page icon Access Information on a VOR 1 2 3 4 5 With the VOR 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 Enter an identifier name or city and press the ENT Key The FREQUENCY field is now highlighted If desired press the ENT Key to place the frequency in the NAV receiver standby field Press the FMS Knob to remove the flashing cursor 190 00324 07 Rev A 7 8 USER WAYPOINT INFORMATION PAGE See the Flight Planning section for a discussion on creating and modifying user defined waypoints 7 9 17 9 NEAREST AIRPORTS AnD rey Figure 7 60 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 Initially the closest airport to the aircraft s present position is displayed Access Information on a Specific Airport 1 With the Nearest Airports Page displayed press the APT Softkey to place the cursor in the NEAREST AIRPORTS field The first airport in the nearest airports list is highlighted 190 00324 07 Rev A 2 3 SECTION 7 NAVIGATION Press the FMS Knob then turn the large FMS Knob to highlight the desired airport Press the FM
111. dicated by a green ALT annunciation in the AFCS Status Box Altitude Hold Mode is automatically armed when the flight director is in Selected Altitude Capture Mode Selected Altitude Capture Mode automatically transitions to Altitude Hold Mode when the altitude error is less than 50 ft In this case the Selected Altitude becomes the flight director s Altitude Reference Changing the Altitude Reference NOTE Turning the ALT Knob while in Altitude Hold Mode changes the Selected Altitude but not the flight director s Altitude Reference and does not cancel the mode With the CWS Button depressed the aircraft can be hand flown to a new Altitude Reference When the CWS Button is released at the desired altitude the new altitude is established as the Altitude Reference 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL If the Selected Altitude is reached during CWS maneuvering the Altitude Reference is not changed To adjust the Altitude Reference in this case the CWS Button must be pressed again after the Selected Altitude is reached Altitude Hold Flight Director Mode Active Altitude Reference navil1 13 88 118 98 IIXD s 1 3 118 700 com nav2 119 98 118 90 TIXO OL ALT 1123 800 139 929 cone Selected Altitude Selected Altitude Bug 2 Command Bars Ho Pitch Attitude to Maintain Altitude Reference XPOR 1288 STBY LCL 2 33 06em Figure 6 7 Altitude Hold Mode Vertical Speed Mode VS In
112. djusted by e Using the NOSE UP NOSE DN Keys e Pressing the CWS Button hand flying the aircraft to establish a new pitch reference then releasing the CWS Button Selected Altitude Capture Mode Armed gt 118 708 com 123 800 135 325 conz Selected Altitude S ee E DS kar 1200 SHAY m E 1110 a 1000 yuu 29 13TH PIR 12060 STBY LOL 2 32 19FPH Figure 6 5 Pitch Hold Mode 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 5 SECTION 6 AUTOMATIC FLIGHT CONTROL Selected Altitude Capture Mode ALTS Selected Altitude Capture Mode arms automatically when the flight director is in Pitch Hold Vertical Speed Flight Level Change or Go Around Mode This mode is also armed automatically under Vertical Path Tracking Mode when the Selected Altitude is to be captured instead of the VNAV Target Altitude The white ALTS annunciation indicates Selected Altitude Capture Mode is armed see Figure 6 5 for example The ALT Knob is used to set the Selected Altitude shown above the Altimeter until Selected Altitude Capture Mode becomes active As the aircraft nears the Selected Altitude the flight director automatically transitions to Selected Altitude Capture Mode with Altitude Hold Mode armed Figure 6 7 This automatic transition is indicated by the green ALTS annunciation flashing for up to ten seconds and the appearance of the white ALT a
113. e 6 32 6 33 Go Around Mode GA 6 16 Heading indication 2 9 Heading Select 1 3 1 4 Heading Select Mode 6 18 Heading Select Mode HDG 6 24 Headset s 5 2 Horizontal situation indicator 2 8 HSI 2 8 Hurricanes 10 5 ID 1 3 4 3 4 6 IDENT function 4 6 ILS approach 6 30 Imminent Terrain Impact 10 12 Impact point 10 12 Inhibit 10 12 Interrogations 4 5 IOI 10 12 10 15 12 5 ITI 10 12 K Key s 1 4 L Lighted obstacle 10 14 Lightning 1 5 1 9 10 2 LNAV 2 6 7 5 12 16 Load approach 8 6 Load a VOR frequency 7 27 Load departure 8 6 Load the frequency for a controlling agency 7 29 Load the nearest ARTCC frequency 7 28 LOI 2 11 LOW ALT 2 5 Low Altitude 2 5 LPV 2 6 6 23 7 5 7 20 Manual Electric Trim 6 1 Manual Electric Trim MET 6 21 MAP 7 1 Map panning 10 5 Marker beacon 2 7 Messages 12 1 Message advisories 12 2 12 9 12 16 12 21 MET 6 1 12 4 METAR 10 3 10 5 Metric display 2 4 MFD 1 1 4 4 Minimums 12 8 Missed approach 6 32 Mistrim 12 4 Mixture 3 4 MKR MUTE 5 2 5 4 Mode S 4 4 Mode selection softkeys 4 5 4 6 Morse code identifier 4 3 Nav Com controls 4 1 NAV1 5 2 NAV2 5 2 Navigation 7 1 Navigation database 1 10 1 11 7 5 Navigation Mode 6 19 6 20 6 25 6 26 Navigation status window 2 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F NAV Frequency Window 4 1 NCR 10 13 Nearest Airports Page 7 21 7 25 7 29 8 1 Nearest ARTCC amp
114. e 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 190 00324 07 Rev A 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 turn the large FMS Knob to highlight the
115. e right enter the first character of the identitier of the departure airport Turning the knob to the left will access the FPL NRST and RECENT waypoint list Turn the large FMS Knob to move the cursor to the next character field Repeat steps 4 and 5 until the desired identitier has been entered WAYPOINT INFORHATION IDENT FACILITY CITY San NORTH UP Chi y Figure 8 11 Waypoint Info Window Press the ENT Key Repeat step number 3 4 and 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F Create a New Flight Plan Using the PFD 1 2 4 5 6 NOTE A flight plan cannot be entered using the PFD if another flight plan is active 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 departure airport 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 identifier for each additional flight plan
116. ed condition occurs the Airspeed Reference appears in a box above the Airspeed Indicator flashing a yellow MAXSPD annunciation Engine power should be reduced as pitch is adjusted by the autopilot to slow the aircraft The annunciation disappears when the overspeed condition is resolved nav1115 58 113 00 nav2 108 00 117 95 Airspeed Indicator Figure 6 40 Overspeed Annunciation 6 34 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 7 NAVIGATION SECTION 7 NAVIGATION 7 2 DIRECT TO NAVIGATION The majority of the following discussions pertain to Direct to Navigation from the MFD the Multi Function Display In discussions pertaining to the PFD the controls are located on the PFD Identifier eg Geographic p KMIA SE USA Region 7 14 NAVIGATION MAP PAGE Facility Name SRE City Sienai VNV Target Altitude TE ham T TRR E Offset o Selected WARNING The map display should only be VNV 3000F1 Sie Direct to used for situational awareness Any map display Target Altitude tee oe RST TORT OP Map Orientation indication should be compared with approved Tonite sea navigation sources Sed He seed ee Waypoint 3 peering KA Select the MAP Page Group aes ak eo Le Se ea pe gauai A 1 Turn the large FMS Knob until MAP is highlighted OY ies EEEE Map Range in the page group box in the lower right of the MFD Bearing LOA cca oe ee Direct to eer ACTIVATE Activate Field 2 Turn
117. ed when possible service Return unit for repair C OM1 PTT COM1 push to talk ke cie P y The COM1 and or COM2 external push to talk switch is stuck in the enable or e pressed position Press the PTT switch again to cycle its operation ne pup ee emigre ihe problem persists the G1000 system should be serviced COM1 RMT XFR COM1 remote Drees ie transfer key is stuck 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 a LanG 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 LOI GPS integrity lost Crosscheck os MO with other NAYS Loss of GPS integrity monitoring a aA peal J ea doa Loss of GPS navigation due to insufficient satellites tion Insufficient satellites 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 13 SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont comments SSS we bua peal 7 AEO Loss of GPS navigation due to position error navigation Position error ai ne pil p edie Loss of GPS navigation due to GPS failure navigation GPS fail APORTAR LOOLE Abort approach due to los
118. eet from the Selected Altitude the green ALT annunciation flashes for up to 10 seconds the autopilot transitions to Altitude Hold Mode and levels the aircraft ALT Selected Altitude of 12 000 MSL ALT Mode Figure 6 30 Departure Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Intercepting a VOR Radial d Press the NAV Key This arms VOR Navigation Mode and the white VOR annunciation appears During climb out the autopilot continues to fly the to the left of the active lateral mode aircraft in Heading Select Mode Airway V4 to Salina VOR SLN should now be intercepted Since the MOO enroute flight plan waypoints correspond to VORs flight director Navigation Mode using either VOR or GPS as the o 2 Once the flight director calculates the proper navigation source may be used In this scenario VOR capture point the flight director transitions trom Navigation Mode is used for navigation to the first VOR Heading Select to VOR Navigation Mode and the waypoint in the flight plan VOR annunciation flashes green The autopilot Intercepting a VOR radial begins turning to intercept the Selected Course 1 Arm VOR Navigation Mode J VOR AP ALT 12000r7 a Tune the VOR frequency b Press the CDI Softkey to set the navigation 3 The autopilot continues the turn until the aircraft source to VOR is established on the Selected Course c Use the
119. elect the seventh rectangular page icon Airspace Alerts Box e Ifthe projected course takes the aircraft inside an 190 00324 07 Rev A airspace within the next ten minutes Ahead is displayed If the aircraft is within two nautical miles of an airspace and the current course takes the aircraft inside Ahead lt 2 nm is displayed If the aircraft is within two nautical miles of an airspace and the current course will not take the aircraft inside Within 2 nm is displayed If the aircraft has entered an airspace Inside is displayed SECTION 7 NAVIGATION View Additional Details for a Listed Airspace 1 2 3 4 5 With the Nearest Airspace Page displayed press the FMS Knob to activate the cursor Turn either FMS Knob to scroll through the list highlighting the desired airspace Press the ALERTS Softkey to place the cursor in the AIRSPACE ALERTS field Turn either FMS Knob to select the desired airspace Press the FMS Knob to remove the flashing cursor View and Quickly Load the Frequency for a Controlling Agency 1 2 3 4 With the Nearest Airspace Page displayed press the FREQ Softkey to place the cursor in FREQUENCIES field Turn either FMS Knob to select the desired frequency Press the ENT Key to load the frequency into the COM frequency standby field Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the
120. elected radios Selected radios Passengers pilot copilot pilot copilot MUSIC 2 Table 5 1 ICS Isolation Modes SECTION 5 AUDIO PANEL 5 6 DIGITAL CLEARANCE RECORDER AND PLAYER Each reception of primary active COM audio is automatically recorded ina 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 PLAY Figure 5 8 Playback Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation e Pressing the MKR MUTE Key while playing a memory block stops play 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 If a COM input signal is detected 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 190 00324 07 Rev A 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 6 1 AFCS CONTROLS The following ded
121. ency Box COM Frequency Box Controls navi 113 29 110 90 Se KMCI RG 133 000 com NAV 116 98 COHZ jm CRS4 BARO li SSS a PUSH CAS CTA ey 14 1516 mmy ALERTS ae XP OE B CDI ADF DME XPOR IDENT TMR REF NRST Figure 4 1 G1000 VHF NAV COM Interface PFD 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 4 1 SECTION 4 NAV COM amp TRANSPONDER Selected COM Standby COM Standby NAV Selected NAV Frequency Field Frequency Field Frequency Frequency nav1189 98 gt e 118 588 con nav2 1 118 68 _ CKY WPT VOR INFORMATION 118 400 XAA comz Figure 4 2 Frequency Fields Actie COM Tuning Box Tuning Box Active NAV Frequency Field Frequency Field 135 100 COM1 A e 121 980 conz Frequency Transfer Arrow Tuning Box Figure 4 3 Frequency Transfer Arrow and Tuning Box NAV Controls COM Controls VOL PUSH VOL PUSH a ID Knob S9 Knob PUSH VOL sq Frequency Transfer Key 4 gt 1 COM EMERG 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 190 00324 07 Rev A 4 1 RADIO STATUS INDICATIONS RX When a COM signal is received a white RX appears by the active COM frequency during signal reception e TX When a COM radio is transmitting a whit
122. erts to Roll Hold Mode wings rolled level e Vectors to Final is activated e Navigation source is manually switched e Localizer signal is not captured by the final approach fix FAF while in LOC Navigation Mode Changing the Selected Course The Selected Course on the PFD is controlled using the CRS Knob Pressing the CWS Button and hand ilying the aircraft does not change the Selected Course while in Approach Mode The autopilot guides the aircraft back to the Selected Course or GPS flight plan when the CWS Button is released 190 00324 07 Rev A 6 4 AUTOPILOT OPERATION NOTE Refer to the AFM for specific instructions regarding emergency procedures The autopilot operates flight control surface servos to provide automatic flight control Pitch and roll com mands are provided to the servos based on the active flight director modes The autopilot uses pitch and roll rates to stabilize the aircraft attitude during upsets and flight director maneuvers Flight director commands are rate and attitude limited combined with pitch and roll damper control and sent to the pitch and roll servo mo tors Pitch autotrim provides trim commands to the pitch trim servo to relieve any sustained effort required by the pitch servo The pitch servo measures the output effort torque and provides this signal to the pitch trim servo The pitch trim servo commands the motor to reduce the average pitch servo effort When the autopilot is no
123. ey 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 15 TAWS Page 360 View Figure 10 16 TAWS Page ARC View 10 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 10 HAZARD AVOIDANCE Terrain Obstacle Location Terrain Obstacle above or within 100 below or above aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Black Terrain Obstacle is more than 1000 below aircraft altitude Potential Impact Point Projected Flight Path af Unlighted Obstacle Enable Disable Aviation Data 1 While the TAWS Page is displayed press the MENU Key Y PAGE MENU 2 Turn the small FMS Knob to select Show or Hide OPTIONS Aviation Data Inhibit TAWS 3 Press the ENT Key i Show Aviation Data Press the FMS CRSR knob to return to base page Figure 10 17 TAWS Page Menu 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 11 SECTION 10 HAZARD AVOIDANCE TAWS Inhibit Flying VFR into an area where unique terrain exists could cause the system to annunciate a nuisance alert When TAWS is inhibited only FLTA and PDA alerts are disabled Inhibit TAWS While the TAWS Page is displayed press the INHIBIT Softkey
124. f FULL TIHE RH SR aap FREQUENCIES 6368 1 ATIS MOGAL mahp CURRENT VNV PROFILE ACTIVE UNV WPT _____ VS TGT TERRAIN agar d fi _ NH WPT ocx re 0001 Figure 7 53 Airport Information Page Figure 7 49 Establishing the Holding Pattern Select the Airport Information Page 27 The aircraft maintains 10 000 feet while following 1 Turn the large FMS Knob to select the WPT page the magenta line through the hold as in Figure 7 ger _ 2 Turn the small FMS Knob to select the first B ts ee aan rectangular page icon Initially information for the wa RKC KEOS airport closest to the aircraft s present position is ese DOEDE _ fet displayed herons KS SMa eiin Select an Airport from the Database cst fof es 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 2 Enter the desired airport identifier HOGAL mahp CURRENT WHY PROFILE ACTIVE Vi WPT VS TGT TERRAIN VS REG Y DEV r1 I 1000F A 15m CHOL YKY Figure 7 50 Hold Established 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F l 21 SECTION 7 NAVIGATION Select an Airport from the Active Flight Plan Select a Recently Entered Airport Identifier 1 With the Airport Information Page displayed press 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor the FMS Knob to activate the cursor 2 Turn the small FMS Knob to
125. failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced 12 10 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS Database Message Advisories Cont MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists MFD1 DB ERR MFD1 SateTaxi database error exists PFD1 DB ERR PFD1 SafeTaxi database error exists MFD1 DB ERR MFD1 Chartview The MFD and or PFD detected a failure in the ChartView database optional database error exists feature Ensure that the data card is properly inserted Replace data card It problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts The MFD and or PFD detected a failure in the FliteCharts database optional database error exists feature Ensure that the data card is properly inserted Replace data card It problem 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 pr
126. 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F J SECTION 9 PROCEDURES AIRPORT STL gt PUBLIC AHBERT ST LOUIS INTL ST LOUIS MO ARRIVAL I Citin Figure 9 3 Select Arrival 7 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 8 A third window is displayed listing the available runways Turn either FMS Knob to select the desired runway and press the ENT Key IRMAT Figure 9 5 Select Arrival Runway 9 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F 9 2 APPROACHES NOTE If certain GPS parameters WAAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Not all approaches in the database are approved for GPS use When selecting an approach a GPS designation to the right of
127. g e Selected Heading Box Barometric Minimum e Selected Course Box Descent Altitude Box Transponder Status e Glideslope Glidepath Box and Vertical Deviation e System Time Indicators e PFD Setup Menu e Altimeter Barometric Setting e Selected Altitude e VNV Target Altitude Garmin G1000 Cockpit Reference Guide for the DA40 40F 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 STORMSCOPE OPERATION WITH LOSS OF HEADING INPUT It heading is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircratt 11 5 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 190 00324 07 Rev A 11 6 DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system will automatically revert to Dead Reckon
128. g WAAS vertical guidance is loaded into the flight plan Bee Expected availability of vertical guidance Glidepath Mode GP e GPS Approach Mode is armed after acquiring clearance for approach prior to intercepting the NOTE Pressing the CWS Button while Glidepath WAAS glidepath GPS is the selected navigation Mode is active does not cancel the mode The source and the APR Key is pressed see GPS autopilot guides the aircraft back to the glidepath Approach Mode upon release of the CWS Button GPS Approach Mode Active Glidepath Mode Active navi 10 98 114 18 suc 118 208 136 975 com navz 113 80 118 90 TsJc L 136 379 8 008 conz Glidepath Indicator Command Bars Indicate Descent on Glidepath LPV HSI Set to GPS a ctive YFIR ILT RIEL 8 4256PH Figure 6 15 Glidepath Mode 6 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL GPS AP ALTS GP Glideslope Mode is available for LOC ILS approaches Figure 6 16 Glidepath Mode Armed to capture and track the glideslope Glideslope Mode is armed when If vertical guidance becomes or is expected to become A valid localizer frequency is tuned unavailable and the approach downgrades Glidepath e LOC Approach Mode is armed the APR Key is Mode is disarmed When vertical guidance becomes pressed and either LOC is the selected navigation available again Glidepath Mode is automatically re armed source or a LOC ILS appr
129. gaged If the Autopilot is engaged the FD Key is disabled 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 HDG Key Selects deselects the Heading Select Mode 25 APR Key Selects deselects the Approach Mode VNV Key Selects deselects Vertical Navigation Mode NOSE UP NOSE DN Keys Controls the active pitch reference for the Pitch Hold Vertical Speed and Flight Level Change Modes 190 00324 07 Rev A SECTION 1 SYSTEM OVERVIEW 1 2 PFD SOFTKEYS TERRAIN Softkey ON Softkey OFF 190 00324 07 Rev A VOR1 on HS VOR2 on HS GPS on HSI nnna D Figure 1 2 PFD Top Level Softkeys ames c te T Press the BACK or OFF Softkey to return to the top level softkeys Figure 1 3 INSET 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 No declutter All map features are visible Declutter 1 Declutters land data Declutter 2 Declutters land and SUA data Declutter 3 Declutters large NAV data remaining removes everything except the active flight pla
130. gation Wap Pagie n 10 1 OOE PaE nsina 10 2 10 3 XM Weather Optional 00 0 10 3 Displaying METAR and TAF information on the Airport Information Page ssssssessessessesseseessen 10 3 Displaying Weather on the Weather Data Link Page 10 4 Map Panning Information Weather Data Link Page 10 5 Weather Products and Symbols sssssesesseeseesseen 10 5 Weather Produ AgS ixsccnsesscissnsrnenarensoenumies 10 6 190 00324 07 Rev A 190 00324 07 Rev A 10 4 Traffic Information Service TIS 10 7 Displaying Traffic on the Traffic Map Page 10 7 Displaying Traffic on the Navigation Map 10 7 To AULO ACH ainainen 10 7 10 5 Avidyne TAS600 Series 0 0 0 10 8 Displaying Traffic on the Traffic Map Page 10 8 Displaying Traffic on the Navigation Mapu 10 8 10 6 Terrain And Obstacle Proximity 0 10 9 Displaying Terrain and Obstacles on the Terrain PROM IMILY Pagen a 10 9 Displaying Terrain and Obstacles on the Navigation MaDi ARANE 10 9 10 7 Terrain Awareness amp Warning System TAWS Display Optional 0 cc seen 10 10 Displaying Terrain on the TAWS Page c scseseeses 10 10 Enable Disable Aviation Data csccseseeseseeeesen 10 11 TEANO Ree ee ER ST 10 12 Manual System Testenia aean 10 12 Forward Looking Terrain Avoidance FLTA 10 12 Premature Descent Alert PDA cn 10 13 Excessive Descent Rate Alert EDR ov 10 13 Negative Cli
131. ge 12 22 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A A Abnormal COM operation 11 2 Activate a flight plan 8 3 Active flight plan 8 2 ADF 1 6 1 7 4 3 ADVISORY 12 1 Advisory alerts 12 3 AFCS 1 3 6 1 6 2 6 23 12 4 Age 10 6 AHRS 12 18 12 19 Aircraft alerts 12 3 AIRMET 10 5 Airport frequency 7 25 Airport information 7 21 Airspace alerts 7 29 Airspeed indicator 2 3 Airspeed Reference 6 8 Airspeed trend vector 2 3 Airways 8 5 Alerting System 12 1 Alerts 12 1 Alert levels 12 2 Alert Pop Up 10 14 ALT 1 4 1 7 2 4 6 4 6 6 6 13 7 19 Altitude alerting 2 4 Altitude constraints 1 10 7 12 Altitude hold 1 4 Altitude Hold Mode 6 6 Altitude Reference 6 6 6 13 Altitude restrictions 1 11 Altitude trend vector 2 4 ALT Knob 1 4 Annunciations 12 1 AP 1 4 6 1 12 4 Approach ILS 6 30 Missed 6 32 WAAS 6 31 Approaches 9 2 Approach activation 4 4 Approach markers Signal augmentation 5 2 Approach Mode 6 20 6 30 190 00324 07 Rev A Approach Mode AFCS 6 31 AP disconnect 6 1 AP DISC Switch 6 33 Arrivals 9 1 Attitude indicator 2 3 Audio alerting system 12 2 Audio panel 4 3 5 1 Audio panel controls ADF 5 2 DME 5 2 NAV1 5 2 NAV2 5 2 Aural alerts 12 8 Auto tuning 4 4 Automatic Flight Control System AFCS Status Annunciations 6 33 Status Box 6 2 Automatic squelch 4 3 Autopilot 6 1 6 21 6 22 Autopilot disconnect 6 16 6 22 Base reflectivity 10 4 BRG1 2 11 BRG2 2 11 C Cautio
132. ght director is synchronized to the aircraft attitude during the maneuver The AP annunciation is temporarily replaced by CWS in white for the duration of CWS maneuvers In most scenarios releasing the CWS Button reengages the autopilot with a new reference Refer to the flight director modes section for CWS behavior in each mode Control Wheel Steering a ROL ICHS PIT ALTS Figure 6 26 CWS Annunciation Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 6 AUTOMATIC FLIGHT CONTROL 6 22 Disengaging the Autopilot Automatic disengagement occurs due to e System failure e Inability to compute default flight director modes FD also disengages automatically e Invalid sensor data Automatic autopilot disengagement is indicated by a flashing red AP annunciation and by the autopilot disconnect aural alert which continue until acknowledged by pushing the AP DISC or MET Switch Autopilot Automatically Disengaged a ALTS Figure 6 27 Automatic Autopilot Disengagement The autopilot is manually disengaged by pushing the AP DISC Switch GA Switch MET ARM Switch or the AP Key on the MFD Manual disengagement is indicated by a five second flashing yellow AP annunciation and a two second autopilot disconnect aural alert After manual disengagement the autopilot disconnect aural alert may be cancelled by pushing the MET ARM or AP DISC Switch AP DISC Switch also cancels the flashing AP
133. 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 copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SateTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc Stormscope is a registered trademark of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc May 2007 190 00324 07 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
134. he Diamond DA40 Aircraft Flight Manual Supplement AFMS for limitations 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW 1 1 PFD MFD CONTROLS O OO Oo 0O oO PUSH 1 2 CRS A4 BARO PUSH PUSH HDG SYNC CRS CTR RANGE A Figure 1 1 PFD MFD Controls 000 PUSH C HSAH 0O000OG MFD Only with optional GFC 700 1 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 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 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 Transfers the standby and active NAV frequencies G Dual NAV Knob Tunes the MHz large knob and kHz small knob standby frequencies for the NAV receiver Press to switch the tuning box light blue box between the NAVI and NAV2 fields 4 Heading Knob Turn to manually select a heading on the HSI When pressed it synchronizes the heading bug with the compass lubber line Selected Heading provides the heading refe
135. he fifth rectangular page icon Select a Nearest User Waypoint 1 2 1 28 With the Nearest User Waypoint Page displayed press the FMS Knob to activate the cursor If any previously entered User Waypoints are within 200 nm these will be displayed with the closest listed first 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 3 Press the FMS Knob to remove the flashing 1 2 cursor 7 14 NEAREST FREQUENCIES Figure 7 66 Nearest Frequencies Page Select the Nearest Frequencies Page Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to select the sixth rectangular page icon Select and Load the Nearest ARTCC FSS or Weather Frequency 1 2 3 4 With the Nearest Frequencies Page displayed press the ARTCC FSS or WX Softkey to place the cursor in the appropriate field Turn the FMS Knobs to select the desired facility or frequency Press the ENT Key to load the frequency into the COM frequency standby field Press the FMS Knob to remove the flashing cursor 190 00324 07 Rev A VERTICAL LIHITS JE0OFT mel Figure 7 67 Nearest Airspaces Page Select the Nearest Airspaces Page 1 2 Turn the large FMS Knob to select the NRST page group Turn the small FMS Knob to s
136. hould 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 NAV2 SERVICE NAV2 needs service still be available The G1000 system should be serviced Return unit for repair NAV1 RMT XFR NAV1 remote transter key is stuck NAV2 RMT XFR NAV2 remote transter key is stuck G S1 FAIL G S1 is inoperative has been detected in glideslope receiver 1 and or receiver 2 The G S2 FAIL G S2 is inoperative G1000 system should be serviced G S1 SERVICE G S1 needs service a Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The 3 receiver may still be available The G1000 system should be serviced when G S2 SERVICE G S2 needs service possible Return unit for repair GEA 71 Message Advisories GEA1 CONFIG GEA1 configuration The GEA1 configuration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be serviced MANIFEST GEA1 software The 1 GEA 71 has incorrect sottware installed The G1000 system should be The remote NAV1 and or NAV2 transter switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced mismatch communication halted serviced 1
137. iations 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 in 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 ackno
138. ical Path Capture 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 11 SECTION 6 AUTOMATIC FLIGHT CONTROL When a descent leg is captured Figure 6 12 Vertical Path Tracking becomes active and tracks the descent pro file An altitude capture mode ALTS or ALTV is armed as appropriate Vertical Path Tracking Active navi 1A8 88 lt 117 95 nav2 108 00 117 95 HSI Set to GPS VNAV Target Altitude Capture Armed erg 232 136 975 118 000 com ALTV 136 375 10 008 CONE VNAV Target r 1000 Altitude Vertical Deviation Indicator Required Vertical Speed Bug Terminal Phase of Flight YPOR Figure 6 12 Vertical Path Tracking Mode Automatic Pitch Hold Reversion Several situations can occur while Vertical Path Tracking Mode is active which cause the flight director to revert to Pitch Hold Mode Vertical Path Tracking and the appropriate altitude capture modes are armed for possible descent profile recapture if the vertical deviation e Exceeds 200 ft during an overspeed condition e Experiences a discontinuity exceeding 200 ft due to a flight plan change e Becomes invalid due to excessive cross track error track angle error e Cannot be computed for a leg type such as a hold or procedure turn The following circumstances cause mode reversion without arming Vertical Path Tracking Mode Navigation source manually changed from GPS CNCL VNV Soitkey selected
139. icated AFCS keys are located on the bezels of the MFD Figure 6 1 AFCS Keys 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 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL surface servos without disengaging the autopilot If the flight director has not been activated pressing the 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 autop
140. igation due to position error navigation Position error ne mel ar i oa Loss of GPS navigation due to GPS failure navigation GPS fail 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 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced The COM1 and or COM2 transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced PB ORT A Leo Or Gh Do Abort approach due to loss of GPS navigation Abort approach PR DAORA DE epi Use LNAV minima when approach is downgraded downgraded TRUE APR True north approach Displayed atter passing the first waypoint of a true north approach when the nav Change hdg reference to TRUE angle is set to AUTO 12 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may GPS2 SERVICE GPS2 needs service still be available The G1000 system s
141. ilot if currently engaged If one side of the switch is active for more than three seconds without the other side also being active PTRM is displayed in the AFCS System Status Box on the PFD Pressing the ARM switch also acknowledges an autopilot disconnect 6 2 FLIGHT DIRECTOR OPERATION With the flight director activated the aircraft can be hand flown to follow the path shown by the Command Bars Maximum commanded pitch 20 15 and bank 22 angles vertical acceleration and roll rate are limited to values established during AFCS certification The flight director also provides commands to the autopilot Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 1 SECTION 6 AUTOMATIC FLIGHT CONTROL Activating the Flight Director Pressing the FD or AP Key when the flight director is not active activates the flight director in default pitch roll modes Pushing the GA Switch or any flight director mode key activates the flight director in the respective mode s The flight director may be turned off by pressing the FD Key Active Mode Armed Mode Autopilot Status Roll Axis Modes Active Mode GPS ROLD AP m ALTS VPTH e a Command Bars Upon activation of the flight director Command Bars are displayed on the PFD as a single cue If the attitude information sent to the flight director becomes invalid or unavailable the Command Bars are removed from the display The Command Bars do not override the
142. ing DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode will only function in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution will produce a NO GPS POSITION annunciation on the map and the G1000 will stop navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in Figure 11 4 In addition DR will be prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in Figure 11 4 Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert message will appear on the PFD Normal navigation using GPS WAAS source data will resume automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of accurately tracking your estimated position and consequently the system may display a path that is different than the actua
143. ing program to N 1 Press the MENU Key with the Navigation Map Page n clusters of electrical activity that indicate displayed 2 Turn either FMS Knob to highlight the Clear Change the viewing mode between 360 and 120 Stormscope Lightning field and press the ENT 1 Select the Stormscope Page 2 Press the VIEW Softkey The 360 and ARC Softkeys Stormscope Page are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to 1 Turn the large FMS Knob until the Map Page group display a 120 viewing area s selected Press the CLEAR Softkey to remove all Stormscope 2 Turn the small FMS Knob until the Stormscope Page lightning data from the display is selected 10 2 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 10 HAZARD AVOIDANCE 10 3 XM WEATHER OPTIONAL Displaying METAR and TAF information on the lt Airport Information Page WARNING XM Weather is not intended to be used for hazardous weather penetration Display METAR and TAF text on the Airport Weather information provided by XM Radio Information Page Service is approved only for weather avoidance not penetration 1 Turn the large FMS Knob to select the WPT Page SEE Group 1 Press the MAP Softkey 2 Turn the small FMS Knob to select the Airport 2 Press the NEXRAD or XM LTNG Softkey to display Information Page the desired weather Press the applicable softkey 3 Press the WX S
144. irth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A RECORD OF REVISIONS Part Number iit Summary 190 00324 00 UU Release 190 00324 01 ey of manual Added NAV COM volume levels Added Flight Timer Added extended range fuel tanks Changed NAV1 and NAV2 on the PFD to VOR or LOC Moved altitude and airspeed trend vectors to opposite sides 190 00324 02 Added WX 500 Stormscope Added XM Weather Added ADF DME Added bearing pointers Added fixed pitch propeller engine parameters Updated fixed pitch propeller engine parameters Added reference to DA4OF on Copyright page and in Warnings Cautions and Notes 190 00324 03 Added diesel engine parameters Rev A 190 00
145. ish purple The display is updated every five minutes Garmin G1000 Cockpit Reference Guide for the DA40 40F NEXRAD Limitations Certain limitations exist regarding the NEXRAD radar displays Some but not all are listed here NEXRAD base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics hail vs rain etc An individual NEXRAD site cannot depict high altitude storms at close ranges and has no information about storms directly over the site 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 within the square area 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 u
146. ive only press the FMS Knob to activate the cursor e PT part time frequency 2 Enter an intersection identifier and press the ENT 4 Press the ENT Key to place the selected frequency Key in the standby field of the COM or NAV box 3 Press the FMS Knob to remove the flashing 5 To remove the cursor press the FMS Knob cursor 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 23 SECTION 7 NAVIGATION 7 6 7 24 NDB INFORMATION Pipro HOATH UP s ITKE Hre Mg Fa Fa i LEI Figure 7 58 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 3 4 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 Enter an identifier name or city and press the ENT Key If there are duplicate identifiers in the database a list is displayed trom which to choose the desired location Press the FMS Knob to remove the flashing cursor Garmin G1000 Cockpit Reference Guide for the DA40 40F Figure 7 59 VOR Information Page Select the VOR Information Page 1 2 Turn the large FMS Knob to select the WPT page group Turn the small FMS Knob to sele
147. l movement of the aircratt Estimated position information displayed by the G1000 190 00324 07 Rev A SECTION 11 ABNORMAL OPERATION through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS Mode due to the lack of satellite measurements needed to determine a position Changes in wind speed and or wind direction will compound the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Figure 11 4 Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data will be computed based upon an estimated position and will be displayed as yellow text on the display to denote degraded navigation source information This data includes the following e Navigation Status Box fields except Active Leg TAS and DTK e GPS Bearing Pointer e Wind data and pointers in the Wind Data Box on the PFD and MFD Track Bug e All Bearing Pointer Distances e Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will not couple to GPS and both TAWS and Terrain Proximity Garmin G1000 Cockpit Reference Guide for the DA40 40F 11 3 SECTION 11 ABNOR
148. l servo providing sustained force in the indicated direction Aileron Mistrim Left Elevator Mistrim Down Pitch servo providing sustained force in the indicated direction Elevator Mistrim Up Pitch Trim Failure _PTRM If AP engaged take control of the aircraft and disengage AP or stuck MET Switch If AP disengaged move MET switches separately to unstick Roll Failure ROLL Roll axis control Roll axis control failure AP inoperative AP Roll axis control failure AP inoperative Pitch Failure PTCH Pitch axis control failure AP inoperative System Failure l ese AP and MET are unavailable FD may still be available Performing preflight system test aural alert sounds at completion Do not press the AP DISC Switch during servo power up and preflight system tests as this may cause the preflight system test to fail or never Preflight Test to start if servos fail their power up tests Power must be cycled to the servos to remedy the situation Preflight system test failed aural alert sounds at failure Table 6 4 AFCS Status Field Alerts 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 33 SECTION 6 AUTOMATIC FLIGHT CONTROL Overspeed Protection Overspeed protection is provided in situations where the flight director cannot acquire and maintain the vertical Mode Reference for the selected vertical mode without exceeding the certified maximum autopilot airspeed When an autopilot overspe
149. lan 8 3 8 6 Invert Active Flight Plan 8 3 8 7 Create a New Flight Plan 0 0 8 4 Create a New Flight Plan Using the MFD uu 8 4 Create a New Flight Plan Using the PFD uo 8 4 8 8 Enter an Airway in a Flight Plan 8 5 8 9 Load a Departure ou ccs 8 6 8 10 Load an Arrival ccs ees 8 6 8 11 Load an Approach ou cscs 8 6 8 12 Remove a Departure Arrival Approach or Airway from a Flight Plan ccceceeeeen 8 6 8 13 Store a Flight Plamen 8 7 8 14 Edit a Stored Flight Plan 8 7 8 15 Delete a Waypoint from the Flight Plan 8 7 8 16 Invert and Activate a Stored Flight Plan 8 7 8 17 Copy a Flight Plan oo cesses 8 8 8 18 Delete a Flight Plan ou seen 8 8 8 19 Graphical Flight Plan Creation 8 8 8 20 Trip Planning 8 8 Section 9 Procedures 0 00 0 9 1 9 1 Arrivals and Departures 551555111111111111 9 1 Load and Activate a Departure Procedure c c0 9 1 Load and Activate An Arrival Procedure 9 1 9 2 Approaches 00 0 0 ccs 9 2 Load and or Activate an Approach Procedure 9 3 Activate An Approach in the Active Flight Plan 9 3 Section 10 Hazard Avoidance 10 1 10 1 Customizing the Hazard Displays on the Navigation Map 0 0 cccccceseeesteeeesen 10 1 10 2 STORMSCOPE Optional 0 c 10 1 Displaying Stormscope Lightning Data on the Navi
150. ld be serviced The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The G1000 system should be serviced The 1 AHRS is not receiving backup GPS information The G1000 system should be serviced The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced The 1 AHRS and 2 AHRS magnetic model database versions do not match The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid The 1 AHRS has incorrect software installed The G1000 system should be serviced 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GMU 44 Message Advisories HDG FAULT AHRS1 magnetometer A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS fault has occurred uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software The GMU 44 has incorrect sottware installed The G1000 system should be mismatch communication halted serviced GDL 69A Message Advisories Message GDL69 CONFIG GDL 69 contig GDL 69 contiguration settings do not match those of backup configuration error Contig service req d memory The G1000 system should be
151. limb Rate Caution NCR 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 15 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 Available will be heard when sufficient GPS signal is re established Alert Annunciations mC BA 1002 H TERRAIN 1 D0F1 0001 Figure 10 24 Alert Annunciation on the PFD Alert Annunciation Figure 10 23 Alert Annunciation on the TAWS Page 10 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 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
152. ll 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 Altitude Reference Reference Box Bug ae j Trena i C t Vector 12 00 ree Barometric Altitude Minimums Bug Barometric Figure 2 7 Altimeter Selected Altitude Bug The Selected Altitude Bug is displayed at the Selected Altitude or the edge of the tape whichever is closer to the current altitude to provide increased altitude awareness and to set the desired hold altitude for the autopilot Set the Selected Altitude Bug Turn the ALT Knobs to set the Selected Altitude Bug The small ALT Knob sets the hundreds and the large ALT Knob sets the thousands This altitude also appears in the Selected Altitude Box above the Altimeter Garmin G1000 Cockpit Reference Guide for the DA40 40F Altitude Trend Vector The end of the trend vector displays approximately what the altitude will be in six seconds if the current rate of vertical speed is mai
153. loss of sensor AHRS ADC IAU or navigation data VOR LOC GPS VNAV WAAS required to compute commands When such a loss occurs the system automatically begins to roll the wings level or maintain the pitch angle depending on the affected axis The flashing annunciation stops when the affected mode key is pressed or another mode for the axis is selected If after ten seconds no action is taken the flashing annunciation stops and the flight director enters the default mode for the affected axis Figure 6 4 Loss of VOR Signal 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL If the information required to compute a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis The flight director is automatically disabled if the attitude information required to compute the default flight director modes becomes invalid or unavailable Pitch Modes Pitch Hold default mode Holds the current aircraft pitch attitude may be used to climb descend to the Selected Altitude Selected Altitude Capture Captures the Selected Altitude Altitude Hold Holds the current Altitude Reference Vertical Speed Maintains the current aircraft vertical speed may be used to climb descend to the Selected Altitude e Flight Level Change Maintains the current aircraft airspeed while the aircraft is climbing descending to the Selected Altitude e Ver
154. ltitude 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 descends 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 generated Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 SECTION 2 FLIGHT INSTRUMENTS 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 Within 100 ft 00 Caso a J Barometric 3 19080 Minimum Bug Barometric __ Minimum Box aii BARO MIN 30 041N Figure 2 17 Barometric Minimum Descent Altitude Alerting Visual Annunciations 2 8 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 HSI FRMT Softkey followed by the 360 HSI or the ARC HSI Softkey O Turn Rate Indicator 2 Current Track G Navigation Source Aircraft Symbol G Cross Track Error 6 Rotating Compass Rose T TO FROM Indicator Heading Bug E OBS Mode Course Deviation Indicator 1 Flight Phase Course Pointer 13 Turn Rate and Heading Trend Vector Heading 15 Lubber Line Figure 2 18 Horizontal
155. mb Rate After Takeoff Alert NCR 10 13 Five Hundred Aural Alert 10 14 Displaying Terrain and Obstacles on the Navigation NUS E atten heen Coe nie onan TEI TE AT 10 14 POD UD AlE cai caitesetinietatosernrkcnenaemneliteds 10 14 TAWS Alerts SUMMALY scssseseecsssssecsessesseeeseeseeeses 10 15 Aler Annuncia ONS nananana 10 16 Section 11 Abnormal Operation 11 1 11 1 Reversionary Mode 0 cccccce cesses 11 1 11 2 Abnormal COM Operation 0 0 0 0 00 11 2 11 3 Unusual Attitudes sees 11 2 11 4 Stormscope operation with loss of Heading QUE societal eer ee aaah eee 11 2 11 5 Hazard Displays with Loss of GPS Position 11 2 11 6 Dead Reckoning cscs teeters 11 3 Section 12 Annunciations amp Alerts 12 1 12 1 Alert Level Definitions 0 0 0 0 ccc 12 2 12 2 Aircraft Alerts ccc cesses ese 12 3 WARNING ANGUS minsanan ecco sete N 12 3 CAUTION AGUS aamuun 12 3 Message Advisory Alerts c sssssecsesssesssessesseesneeen 12 3 TABLE OF CONTENTS 12 4 RECS BIGIAS she hte eet ee 12 4 System Status ANNUNCIATION ccissssssssssairvesessesvvanesien 12 4 12 5 TAWS ALERTS yt s cictspetcis iets tcocdeanshehsictcaclentiee 12 5 TAWS System Status Annunciations s es 12 6 12 6 G1000 System Annunciations 00 12 6 12 7 Other G1000 Aural Alerts 0 0 ccc ee 12 8 12 8 G1000 System Message Advisories
156. ment The Aircraft Flight Manual takes precedence over any conflicting guidance found in this section MFD amp PFD Message Advisories 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 crosstalk error has occurred should 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 MFD1 SERVICE MFD1 needs be serviced service Return unit for repair MANIFEST PFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The G1000 system should MANIFEST MFD1 software be serviced mismatch communication halted PFD1 CONFIG PFD1 config error Contig service req d The PFD and or MFD configuration settings do not match backup configuration MFD1 CONFIG MFD1 config error memory The G1000 system should be serviced Contig service req d SW MISMATCH GDU software The MFD and PFD have different software versions installed The G1000 system version mismatch Xtalk is off should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by MFD1 COOLING MFD1 has poor dimming the display If problem persists the G1000 system should be serviced cooling Reducing
157. n TRAFFIC Press to display traffic on the map TOPO Press to display topographical data Q e coastlines terrain rivers lakes etc and elevation scale on the Inset Map TERRAIN Press to display terrain information on the Inset Map STRMSCP optional Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft NEXRAD optional Press to display NEXRAD weather and coverage information on the Inset Map XM LTNG optional Press to display XM lightning information on the Inset Map BACK Press to return to the previous level softkey configuration Garmin G1000 Cockpit Reference Guide for the DA40 40F SECTION 1 SYSTEM OVERVIEW POR nnonnnnnn n nA A on A eo BRG1 NAV1 BRG2 NAV2 Press the STD BARO or BACK Softkey to return to the top level softkeys Figure 1 4 PFD Configuration Softkeys PFD Press to display the additional softkeys for additional configuration of the PFD DFLTS Press to reset default settings on the PFD WIND Displays softkeys to select wind data parameters OPTN I Longitudinal and lateral components OPTN 2 Total direction and speed OPTN 3 Total direction with headwind and crosswind speed components OFF Information not displayed DME optional Press to display the DME Information Window BRG bearing Press to cycle through the following Nav sources making
158. n 12 1 12 2 CDI 2 9 2 11 7 3 7 6 7 12 7 16 7 20 9 2 12 20 Cell 10 2 Cell mode 10 2 Cell movement 10 5 CLR 1 3 Coast mode 10 7 Code selection 4 5 4 6 Command Bars flight director 6 2 COM Frequency Window 4 1 COM knob 4 3 Controls 1 2 4 1 Control Wheel Steering 6 1 Control Wheel Steering CWS 6 21 Create a new user waypoint 8 1 INDEX CWS 6 1 CWS Button 6 5 6 10 6 13 6 18 6 20 6 21 Cyclones 10 5 D Databases 1 12 Dead Reckoning 2 12 11 3 Departures 9 1 Direct to 7 1 7 5 7 11 7 12 8 9 DME 4 4 DR 2 12 DR mode 11 3 Dual CDU failure 11 2 E Edit a flight plan 8 7 EDR 10 13 Endurance 3 2 3 3 Engine system 3 3 Excessive Descent Rate 10 13 F FD 1 4 12 4 Five Hundred Aural Alert 10 14 FLC 1 4 Flight director 6 1 6 1 6 2 Pitch modes 6 3 6 9 Roll modes 6 16 6 19 Flight ID 4 6 Flight level change 1 4 Flight Level Change Mode 6 27 6 29 Flight Level Change Mode FLC 6 8 Flight Plan Catalog 9 1 9 2 FLTA 10 12 Forward Looking Terrain Avoidance 10 12 FPL Key 1 3 Freezing level 10 5 Frequency toggle key 1 3 4 3 Fuel remaining 3 2 3 3 Fuel used 3 2 3 3 Garmin G1000 Cockpit Reference Guide for the DA40 40F Index 1 INDEX Index 2 G GA 6 1 Glidepath 2 6 7 19 Glidepath Mode 6 14 6 20 Glidepath Mode GP 6 31 Glideslope 2 6 7 19 Glideslope Mode 6 15 6 20 6 30 Glidesope Indicator 2 2 GMA 1347 1 1 Go Around 6 1 Go Around Mod
159. n G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 91 3 397 828 Garmin AT Inc oe 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton S040 ORB 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 07 Rev A 2004 2007 Garmin Ltd or its subsidiaries
160. n SAJNA FT 128 132m rT Figure 8 19 Airway Added to Flight Plan 8 9 LOAD A DEPARTURE See the Procedures section for a discussion on loading Figure 8 17 Select Desired Airway and activating departure procedures 8 Turn either FMS Knob to highlight the desired 949 LOAD AN ARRIVAL airway 9 Press the ENT Key A list of available exits is now See the Procedures section for a discussion on loading displayed and activating arrival procedures 10 Turn either FMS Knob to highlight the desired exit 8 11 LOAD AN APPROACH Ea point See the Procedures section for a discussion on loading and activating approach procedures 8 12 REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 1 With the Active or Stored Flight Plan Page displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints Figure 8 18 Select Desired Exit Point 3 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove 11 With the desired exit point highlighted press the the selected procedure or airway ENT Key 8 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A 8 13 STORE A FLIGHT PLAN After creating a flight plan on either the PFD or MED it may be saved by pressing the MENU Key Turn the la
161. ne 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 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 Annunc
162. ng the arrival procedure the aircraft is cleared for descent in preparation for the approach to KCOS Three methods are presented for the descent from 12 000 ft e Flight Level Change descent Flight Level Change Mode can be used to descend to the Selected Altitude at a constant airspeed This descent method does not account for flight plan waypoint altitude constraints e Vertical Path Tracking descent Vertical Path Tracking Mode is used to follow the vertical descent path detined in the GPS flight plan Altitude constraints correspond to waypoints in the flight plan Before VNV flight control can provide vertical profile guidance a VNV flight plan must be entered and enabled e Non path descent in a VNV scenario While the flight director is following VNV guidance for descent Pitch Hold Vertical Speed or Flight Level Change Mode can be used to descend to the VNV Target Altitude prior to reaching the planned TOD Flight Level Change Mode is used in the example Flight Level Change descent 1 Select Flight Level Change Mode a Using the ALT Knob set the Selected Altitude to 10 000 feet SECTION 6 AUTOMATIC FLIGHT CONTROL b Press the FLC Key to activate Flight Level Change Mode The annunciation FLC appears next to the Airspeed Reference which defaults to the current aircraft airspeed Selected Altitude Capture Mode is armed automatically J GPS TAP ALTS 2 3 _ GPS AP ALT Use the NOSE UP NO
163. nnunciation The Selected Altitude is shown as the Altitude Reference beside the ALTS annunciation At 50 ft from the Selected Altitude the flight director automatically transitions from Selected Altitude Capture to Altitude Hold Mode and holds the Selected Altitude shown as the Altitude Reference As Altitude Hold Mode becomes active the white ALT annunciation moves to the active pitch mode field and flashes green for ten seconds to indicate the automatic transition Altitude Reference In This Case Equal to Selected Altitude Flash Up to 10 sec Indicating Automatic Transition Figure 6 6 Automatic Mode Transitions During Altitude Capture Garmin G1000 Cockpit Reference Guide for the DA40 40F Changing the Selected Altitude NOTE Pressing the CWS Button while in Selected Altitude Capture Mode does not cancel the mode Use of the ALT Knob to change the Selected Altitude while Selected Altitude Capture Mode is active causes the flight director to revert to Pitch Hold Mode with Selected Altitude Capture Mode armed for the new Selected Altitude Altitude Hold Mode ALT Altitude Hold Mode can be activated by pressing the ALT Key the flight director maintains the current aircraft altitude to the nearest ten feet as the Altitude Reference The flight directors Altitude Reference is shown in the AFCS Status Box and is independent of the Selected Altitude displayed above the Altimeter Altitude Hold Mode active is in
164. ntained Barometric Setting Box Select barometric pressure Turn the BARO Knob to select the desired setting Quickly enter standard pressure 1 Press the PFD Softkey 2 Press the STD BARO Softkey Altitude Alerting Within 1000 ft Within 200 ft K 4000 Deviation of 200 ft E 4000 Figure 2 8 Altitude Alerting Visual Annunciations Visual annunciations appear in the Altitude Reference Box Whenever the setting is changed the Altitude Alerter is reset The Altitude Alerter is independent of the Automatic Flight Control System 190 00324 07 Rev A Metric Display Display altitude in meters and barometric pressure in hectopascals 1 2 3 4 5 190 00324 07 Rev A Press the PFD Softkey to display the second level softkeys Press the ALT UNIT Softkey Press the METERS Softkey to display altitude in meters Press the HPA Softkey to display the barometric setting in hectopascals Press the IN Softkey to display the barometric setting in inches of mercury Press the BACK Softkey to return to the previous level softkeys Figure 2 9 Altimeter Metric SECTION 2 FLIGHT INSTRUMENTS Low Altitude Annunciation WAAS Only A NOTE The LOWALT annunciation is not available when the G1000 is configured with TAWS Terrain Awareness amp Warning System unless TAWS is inhibited When the Final Approach Fix FAF is the active waypoint in a GPS WAAS approach using vertical guidance
165. o activate the cursor b Turn the small FMS Knob to highlight the desired altitude c Press the CLR Key d Press the FMS Knob to deactivate the cursor After making the altitude non designated it is displayed as white text Garmin G1000 Cockpit Reference Guide for the DA40 40F Altitude constraint values associated with the Final Approach Fix FAF and waypoints beyond the FAF cannot be designated for vertical guidance These altitude values will always be displayed as white text as in Figure 7 34 Vertical guidance to the FAF and on to the Missed Approach Point MAP is given using the WAAS GPS altitude source therefore the displayed altitude values are for reference only r ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS ALT FSHER 352 9 8M 1000 FT PYNON 352 11 93m 10000FT Approach KCOS RNAV 35RGPS LPV HABUK iof 021 5 9M J000FT FALUR 261 5 0NH 8600 CEGIX faf 351 GON 7800F1 RW3S5R aap 351 5 1NH 6368FT 348 O 4NH 6370r1 MOGAL mahp 1000061 6 0NH CURRENT VNV PROFILE ACTIVE VNV WPT 10 000FT at OPSHN 3NH VS TGT 7S6FPM FPA VS REQ Figure 7 34 Vertical Guidance is Active to the FAF 14 As the aircraft approaches OPSHN it may be desirable to adjust how fast or steep the upcoming descent will be The default Flight Path Angle FPA is 2 5 degrees and a required vertical speed will be computed to maintain the 2 5 FPA To change the vertical flight path perform the following steps 190 003
166. oach is loaded into the under GPS Approach Mode flight plan see LOC Approach Mode Glideslope Moves LOC HDG AP ALT 100001 GS Gaus Jas ia ie ee wee Figure 6 18 Glideslope Mode Armed NOTE Pressing the CWS Button while Glideslope Mode is active does not cancel the mode The Once the localizer has been set as the navigation autopilot guides the aircraft back to the glides source the localizer and glideslope can be captured Upon lope upon release of the CWS Button reaching the glideslope the flight director transitions to Glideslope Mode and begins to intercept and track the glideslope Approach Mode Active Glideslope Mode Active PATYI ors 1 7m 118 200 136 975 con Active ILS oh 136 975 118 000 conz Frequency Tuned rae hen 4 ee a fd Command Bars eae Indicate Descent on Localizer Glideslope Path HSI Set to LOC2 LT RLL S 4Q 27PH Figure 6 17 Glideslope Mode 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 15 SECTION 6 AUTOMATIC FLIGHT CONTROL Go Around GA Mode Pushing the GA Switch engages the flight director in a wings level 7 pitch up attitude allowing the execution of a missed approach or a go around This mode is a both a pitch and roll mode and is annunciated as GA in both the pitch and roll active mode fields Go Around Mode disengages the autopilot and arms Altitude Hold Mode automatically Subsequent autopilot engagement is allowed Attempts to
167. of available airways for TOP as seen in Figure 7 16 ENTRY TOF mae AN LOAD Figure 7 16 List of Available Airways for TOP g Turn either FMS Knob to highlight V4 in the list as seen in Figure 7 16 h Press the ENT Key The list of V4 airway exit points is now displayed as in Figure 7 17 Figure 7 17 List of Available Exits for V4 Garmin G1000 Cockpit Reference Guide for the DA40 40F i If necessary turn either FMS Knob to select the desired exit In this case Salina VOR SLN is selected as seen in Figure 7 17 j Press the ENT Key The selected airway and exit are displayed the prompt LOAD highlighted as in Figure 7 18 260 97 71M Figure 7 18 Ready to Load V4 k Press the ENT Key V4 is now loaded into the flight plan as shown in Figure 7 19 190 00324 07 Rev A SECTION 7 NAVIGATION FPL ACTIVE FLIGHT PLAN 136 975 NORTH UP mi U ACTIVE FLIGHT PLAN KMKC KCOS ACTIVE FLIGHT PLAN KMKC KCOS DTK DIS Departure KMKC ALL TIFTO2 TIFTO MCI TIFTO 286 Enroute TOP 146 Airway V4 SLN SLN 250 Airway Y244 LAA HYS 262 LAA Airway 263 TBE MCI piai Enroute pe TOP Airvoy V4 SLN AT hng SLN Airway V244 LAA HYS LAA Airway V263 TBE TBE CURRENT UNU PROFILE ACTIVE VNV WPT SAG pee oe VS TGT FPH FPA CURRENT VNV PROFILE ACTIVE VNU WPT 5 gp 0 Terrain ia PH TIMET v DEV ae 1009r1 1000r1 M TIME TO TOO Ig 4000 CNEL VNV
168. oftkey to display METAR and TAF again to remove weather data from the Navigation text METAR and TAF information is updated every Map Page 12 minutes at mAIRFORT a KMSP PUBLIC MINNEAPOLIS ST PAUL INTL MINNEAPOLIS MN 136 975 roe HNEAPOLTS NORTH UF TACDFFT TSQRHFT BRO EN IT 250 i Ar n JR EN en DEW POINT 14 c ke ETER 29 721N a M M i oMMM aa ee TOPO TERRAIN Figure 10 7 Navigation Map Page Displaying NEXRAD Weather Figure 10 8 METAR and TAF Text Displayed on the Airport Weather Information Page 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 3 SECTION 10 HAZARD AVOIDANCE Displaying Weather on the Weather Data Link 10 4 Page Select the Weather Data Link Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the fourth rectangular page icon Press the available softkeys to select the desired XM weather product 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 i o ICELL MOV SIG AIR METAR LEGEND MORE HX Figure 10 9 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 gray
169. oll steering commands from the Selected Course and deviation Navigation Mode can also be used to fly non precision GPS and LOC approaches where glideslope capture is not required SECTION 6 AUTOMATIC FLIGHT CONTROL Backcourse Navigation Mode is armed when the localizer front course is greater than 105 from the aircratt heading The annunciation BC in the AFCS Status Box indicates Backcourse Navigation Mode When the HSI is coupled to VOR or LOC the flight director creates roll steering commands from the Selected Course and deviation If the Course Deviation Indicator CDI shows greater than one dot when the NAV Key is pressed the selected mode is armed The armed annunciation appears in white to the left of the active roll mode For cases where the projected course is offset a large distance from the present course for turn anticipation GPS Navigation Mode can be activated with crosstrack error up to 10 nm when the NAV Key is pressed GPS ROL ALT Figure 6 23 GPS Navigation Mode Armed GPS Navigation Choe Med P Altitude Hold Mode Active Ae Mode Armed NAVI 113 08 WPT nav2 148 88 117 95 Command Bars Indicate Left Turn to Track GPS Course and Climb to Intercept Selected Altitude GPS is Active Navigation Receiver on HSI S Pa i d A A GY ON N Cy TRK 133 558 128 058 con ALT 121 988 CON 14400 14300 vu 14iga K 14190 13988 M _23 551N Figure 6 22 Navigation Mode 190
170. on EDR Negative Climb Rate Caution NCR Don t Sink or Too Low Terrain 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 5 SECTION 12 ANNUNCIATIONS amp ALERTS TAWS System Status Annunciations PFD MFD TAWS Alert Type Page Annunciation MFD Pop Up Alert Aural Message TAWS System Failure No GPS position or excessively degraded TAWS Not Available GPS signal TAWS Available will be heard when sufficient GPS signal is re established None TAWS System Test OK 12 6 G1000 SYSTEM ANNUNCIATIONS A NOTE Upon power up of the G1000 system When an LRU or an LRU function fails a large red 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 Attitude and Heading Reterence System is aligning Display system is not receiving attitude information trom the AHRS Indicates a contiguration module failure 12 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A
171. on the Active Flight Plan Page MFD All remaining vertical waypoints deleted from the flight plan Displays entering Reversionary Mode Non Path Descents Pitch Hold Vertical Speed and Flight Level Change modes can also be used to fly non path descents while 6 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A VNAV flight control is selected If the VS or FLC Key is pressed while Vertical Path Tracking Mode is selected Vertical Path Tracking Mode reverts to armed along with the appropriate altitude capture mode to allow profile re capture GPS 20k ALTS VPTH Figure 6 13 Flight Level Change VNAV Non Path Descent To prevent immediate profile re capture the following must be satished e Atleast ten seconds have passed since the non path transition was initiated e Vertical deviation from the profile has exceeded 250 ft but is now less than 200 ft Pressing the VNV Key twice re arms Vertical Path Tracking for immediate profile re capture VNAV Target Altitude Capture Mode ALTV NOTE Armed VNAV Target Altitude and Selected Altitude capture modes are mutually exclusive However Selected Altitude Capture Mode is armed implicitly not annunciated whenever VNAV Target Altitude Capture Mode is armed This ensures the Selected Altitude is not violated during a change from VNAV Target Altitude Capture to Selected Altitude Capture Mode close to Selected Altitude interception VNAV Target Altitude
172. operly inserted Replace data card If problem persists the G1000 system should be serviced The MFD and or PFD detected a failure in the SafeTaxi database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced DB MISMATCH Aviation database The PFD and MFD have different aviation database versions installed Crossfill is version mismatch Xtalk is off off Install correct aviation database version in both displays DB MISMATCH Aviation database The PFD and MFD have different aviation database types installed Americas type mismatch Xtalk is off European etc Crossfill is off Install correct aviation database type in both displays DB MISMATCH Terrain database The PFD and MFD have different terrain database versions installed Install version mismatch correct terrain database version in both displays DB MISMATCH Terrain database The PFD and MFD have ditterent terrain database types installed Install correct type mismatch terrain database type in both displays DB MISMATCH Obstacle database The PFD and MFD have different obstacle database versions installed Install version mismatch correct obstacle database version in both displays DB MISMATCH Airport Terrain The PFD and MFD have different airport terrain databases installed Install database mismatch correct airport terrain database in both displays 190 00324 07 Rev A Garmin G100
173. or approach to arm Approach and Glideslope modes LOC and GS appear in white as armed mode annuncia tions LOC HDG AP ALT 90001 GS c The navigation source automatically switches to LOC After this switch occurs the localizer signal can be captured and the flight director determines when to begin the turn to intercept the final approach course The flight director now provides guidance to the Missed Approach Point Figure 6 36 ILS Approach to KCOS 3 There are two options available at this point as the autopilot flies the ILS approach e Push the AP DISC Switch at the decision height and land the aircraft e Use the GA Switch to execute a missed approach 6 30 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A Flying a WAAS precision approach 1 Arm flight director modes for a precision approach a Make sure the navigation source is set to GPS use CDI Softkey to change navigation source b Select the Runway 35R LPV approach for KCOS Load and activate the approach into the flight plan 2 Press the APR Key once clearance for approach has been acquired GPS Approach Mode is activated and Glidepath Mode is armed _ GPS APL VPTE ALTS GP 3 Once the glidepath is captured Glidepath Mode becomes active The flight director now provides guidance to the Missed Approach Point 4 There are two options available at this point as the autopilot flies the approach e Push the AP
174. or to OPSHN h Press the ENT Key twice to activate the direct to Note in Figure 7 29 the magenta arrow in the Active Flight Plan Window indicating the direct to OPSHN after the offset waypoint for OPSHN The preceding offset waypoint indicates the offset distance and altitude that was previously entered The remaining waypoints in the loaded arrival procedure have no database specified altitudes therefore dashes are displayed Keep the CDI centered and maintain a track along the magenta line to OPSHN NOTE If the loaded arrival procedure has waypoints with altitude constraints retrieved from the database those altitudes will be displayed as white numerals This indicates the altitudes will not be used by the system for vertical guidance until manually accepted by the pilot To accept the displayed altitude place the cursor over the altitude and press the ENT Key The altitude entry will then change to light blue numerals indicating the altitude will now be used by the system for providing vertical guidance pe ACTIVE FLIGHT PLAN KMKC KCOS TFR NO DATA TRE Arriv FSHER PY NUON CURRENT VNV PROFILE ACTIVE VNV WPT 1000F t OPSHN F VS TGT Q taaan gt E TV DEV VIEH VNV PROF CNCL VNV VNV Figure 7 29 Direct to Active 12 While proceeding to OPSHN the LPV approach to runway 35R is preferred and will be used a Press the PROC Key to display the Procedures Window If the GPS system is not
175. orture KMKC ALL TIFTO2 TIFTO MCI TIFTC 287 Enroute SLN ee abe Airwoy V263 TBE TBE 218 Arrivol KCOS TBE DBRY 1 ALL CURRENT VNV PROFILE ACTIVE UNV WPT aa VS TOGT _ _FPH FPA VS REQ FPN TIME TO TOD TERRAIN j V DEV GA 100r1 1000r1 Mi yee 30nn CNCL VNV 9 A eh hA Figure 7 11 Assigned Heading of 240 7 6 Garmin G1000 Cockpit Reference Guide for the DA40 40F ATC now assigns routing to join V4 A heading of 290 is assigned to intercept V4 The aircraft turns to heading 290 as seen in Figure 7 12 Note the current CDI flight phase is now ENR Enroute When the aircraft reached 30 nautical miles from the departure point the flight phase changed from TERM to ENR on the HSI and CDI scaling changed to 2 0 nm 136 975 ACTIVE FLIGHT FLAN KMKC KOOS FPL ACTIVE FLIGHT PLAN HORTH UF m TFR HI DATA OTK DIS Deporture KMKC ALL TIFTOY TIFTO MCI TIFTO Enroute SLN Aire E LAA Airway Y263 TBE TBE Arrival ECOS TEE DSRY7 ALL W441 Ad CURRENT WW PROFILE ACTIVE VM WPT ___FT o VS TGT TERAATH DDFT ipl Figure 7 12 Assigned Heading of 290 190 00324 07 Rev A SECTION 7 NAVIGATION 4 V4 will now be entered into the flight plan ee a Press the FMS Knob to activate the cursor ers b Turn the large FMS Knob to highlight the desired eevee es 2 entry point as shown in Figure 7 13 The V4 entry ree NORTH UF will be placed immediately ab
176. otifies 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 truncated approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate This occurs when the pilot attempts to activate a stored flight plan that contains locked flight plan locked waypoint Remove locked waypoint trom flight plan Update flight plan with current waypoint TA E 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 ih i Special use airspace is near and ahead of the aircraft position AE EAR E es Special use airspace is within 2 nm of the aircraft position than 2 nm LEG UNSMOOTH Flight plan leg will The approaching fligh
177. ove the highlighted waypoint ACTIVE FLIGHT PLAN KMKC KEUS OTK DIS Departure KMKC ALL TIFTO2 1TIFTO MCI TIFTO 266 5SQ 2NH FT Enroute SLM Ck FT Airwoy W244 LAA HYS 262 TLI ___FT LAA fol TGSI Airvay V 263 1BE TBE 217 LAM LOCATION ERG B20 N 39 08 23 DIS 22 9NH ppo 90 Press ENT to accept Figure 7 14 Entering V4 Entry Point d Press the ENT Key TOP is now inserted into the CURRENT VNU PROFILE flight plan as in Figure 7 15 VS TOT VS REG KEOS J22 TBNH ACTIVE FLIGHT PLAN KMEC KOOS Figure 7 13 Begin Adding V4 to the Flight Plan a Ss pee Enroute g TOP 146 32 3NH c Turn the small FMS Knob to display the Waypoint EEM 260 97 7 Information Window Enter the desired beginning jaia ii E E point for V4 leg in this example Topeka VOR LAA 165 TOP will be used as shown in Figure 7 14 aa Gla i n A KCOS dez TIBBNH _ FT CURRENT WNW PROFILE ACTIVE WNW WPT By Oe ee WS TGT FP FPA VS REU O FPA TIME TO TOD Figure 7 15 TOP Inserted into the Flight Plan e With SLN still highlighted as in Figure 7 15 turn the small FMS Knob to the right The Waypoint Information Page is displayed and the LD AIRWY Softkey is now available 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 7 7 SECTION 7 NAVIGATION 1 8 f Press the LD AIRWY Softkey to display the list
178. parture Climbing to the Selected Altitude and flying an assigned heading 1 2 Before takeoff set the Selected Altitude to 12 000 feet using the ALT Knob In this example Vertical Soeed Mode is used to capture the Selected Altitude Pitch Hold Vertical Speed or Flight Level Change Mode may be used a Adjust the vertical speed to the desired value In this example 500 fom is used b Press the VS Key to activate Vertical Speed and Roll Hold modes and arm Selected Altitude Capture Mode The Vertical Speed Reference may be adjusted after Vertical Speed Mode is selected using the NOSE UP DN Key or pushing the CWS Button and hand tlying the aircraft adjusting pitch angle to establish a new Vertical Speed Reference then releasing the CWS Button HD G Moy d TO Mode KMKC a yoo a2 xO c Press the AP Key to engage the autopilot in a climb using Vertical Speed Mode o ROL AP ALTS 3 Use the HDG Knob to set the Selected Heading complying with ATC vectors to intercept Airway V4 Press the HDG Key to activate Heading Select Mode while the autopilot is engaged in the climb The autopilot follows the Selected Heading Bug on the HSI and turns the aircraft to the desired heading a HDG AP TEE 4 As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds At 50 f
179. pdated 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 190 00324 07 Rev A 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 MORE WX Press the MORE WX Softkey to display the following group of softkeys for additional weather control 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 SECTION 10 HAZARD AVOIDANCE CYCLONE Pressing the CYCLONE Softkey shows the current location of cyclones hurricanes and tropical storms
180. pproved for weather avoidance only not DISPLAYS ON THE NAVIGATION MAP weather penetration Refer to the WX 500 Pilot s o Guide for detailed operation 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup Displaying Stormscope Lightning Data on the option Navigation Map Page 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select D ea E MASOK the Weather group to customize the display of 2 Press the STRMSCP Softkey Press the STRMSCP weather features Select Traffic to customize the Softkey again to remove Stormscope Lightning Data display of traffic from the Navigation Map Page 3 Press the small FMS Knob to return to the Pa aes Sy Navigation Map Page PAGE HENU OF TIONS mamn Hop Setup OOOO O Measure Bearing Distance Press the FMS CRSR knob to return to bose poge Figure 10 1 Page Menu HAP SETUP STRHSCP LTNG 4Gn STRHSCP HODE Ce STRHSCP SHEL AANA NEMRAD DATA OFF 20 ANH were OFF 2000NH Figure 10 4 In Flight Navigation Map Page Displaying CELL HOVEHENT 40n Stormscope Lightning Data TOPO TERRAIN AIRWAYS NEXRAD XM LING Figure 10 2 Map Setup Menu HAP SETUP GROUP Mop eathe On All Traffic Troffic Ay atio Lond E 150NH ewer ata stetats SANM Strike is between 2 and 3 minutes old Figure 10 3 Map Setup Group List 19
181. prior to the active vertical waypoint This will prevent vertical guidance to the active vertical waypoint MEY SE E Nee The current crosstrack exceeds the limit causing vertical deviation to go invalid crosstrack error VNV Unavailable Excessive track The current track angle error exceeds the limit causing the vertical deviation to angle error go invalid palcnehsollise A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 The selected waypoint xxxx does not use the WGS 84 datum Cross check waypoint for navigation xxxx position with alternate navigation sources TRAFFIC FAIL Traffic device has The G1000 is no longer receiving data trom the traffic system The trattic device failed should be serviced ay ind SS Stormscope has failed The G1000 system should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic The GDU s internal model cannot determine the exact magnetic variance for variance Verity all course angles geographic locations near the magnetic poles Displayed magnetic course angles may differ trom the actual magnetic heading by more than 2 SCHEDULER lt message gt Message criteria entered by the user 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 21 SECTION 12 ANNUNCIATIONS amp ALERTS Blank Pa
182. re has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S needs service may still be available The G1000 system should be serviced when possible Return unit for repair 12 14 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories GIA1 CONFIG GIA1 configuration error Contig 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 Contig service req d GIA1 CONFIG GIA1 audio contig error Contig service req d The GIA1 and or GIA2 have an error in the audio configuration The G1000 GIA2 CONFIG GIA2 audio config system should be serviced error Contig 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 temperature 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 Ret
183. rence to the Flight Director while operating in Heading Select Mode Joystick Changes the map range distance top to bottom of map display when rotated Activates the map pointer when pressed 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 O Dual COM Knob Tunes the MHz large knob and kHz small knob standby frequencies for the COM transceiver Pressing this knob switches the 190 00324 07 Rev A SECTION 1 SYSTEM OVERVIEW tuning box light blue box between the COM1 and COM2 fields COM Frequency Transfer Key Transfers 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 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 percentage 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 active route or taken from the map pointer position FPL Key
184. rendered invalid as a result of manually changing an altitude to a non designated altitude To help interpret the meanings of how the altitudes are presented keep the following points in mind e When the altitude is displayed in light blue the system is using that altitude designated to determine vertical speed and deviation guidance e When the altitude is displayed in white it is not being used by the system non designated to determine the vertical speed and deviation guidance e An altitude displayed as small text is an altitude that is published in the navigation database e Altitudes displayed as a light blue subdued text cannot be used in the current vertical navigation calculations 190 00324 07 Rev A SECTION 1 SYSTEM OVERVIEW WhiteText Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the system Altitude has been entered by the The system cannot use this altitude estimating the altitude of the pilot Altitude is designated for in determining vertical speed and aircraft as it passes over the use in giving vertical speed and deviation guidance navigation point This altitude deviation guidance Altitude does is provided as a reference and not match the published altitude is not designated to be used in in navigation database or no determining vertical speed and published altitude exists deviation guidance Small Text Altitude is not designated to Altitude is designated for use in The
185. rge 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 20 Store Flight Plan Confirmation 8 14 EDIT A STORED FLIGHT PLAN 190 00324 07 Rev A Press the FPL Key and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan and press the EDIT Softkey 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 SECTION 8 FLIGHT PLANNING 8 15 DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 With either the Active or Stored Flight Plan displayed press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to select the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wot Name confirmation window Remove KCRQ OK or CANCEL Figure 8 21 Remove Waypoint Confirmation 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key 5 Once all changes have been made press the FMS Knob to remove the cursor 8 16 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 From the Flight Plan Catalog Page press the FMS
186. roach field Turn the small FMS Knob to display a list of available approaches Figure 9 6 Selecting an Approach Procedure 6 Turn either FMS Knob to highlight the desired 190 00324 07 Rev A approach Press the ENT Key 1 8 SECTION 9 PROCEDURES 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 FMS 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 1 2 3 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 Garmin G1000 Cockpit Reference Guide for the DA40 40F J3 SECTION 9 PROCEDURES Blank Page 9 4 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 10 HAZARD AVOIDANCE SECTION 10 HAZARD AVOIDANCE 10 2 STORMSCOPE OPTIONAL 10 1 CUSTOMIZING THE HAZARD WARNING Weather information on the G1000 MFD is a
187. s 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 When the last digit is entered the transponder code becomes active 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 Enter Code Using the FMS Knob 1 Press the XPDR Softkey to display the transponder Mode Selection softkeys 2 Press the CODE Softkey to display the transponder Flight ID Reporting If so configured the Flight ID may be entered in the Timer Reterence Window a REFERENCES aa softkeys which includes the digit TER GOOOG0 UP START l GLIDE F3KT ON 3 Turn the small FMS Knob to enter the first two i E9KT ON digits Ux 64kT ON 4 Turn the large FMS Knob to place the cursor in Uy G6KT ON position to change the second two digits ABQOET AIR2Z65 BARO MINIMUMS 5 Turn the small FMS Knob to enter the second two FLIGHT ID Flight ID 6 digits Press the ENT Key to activate the code immediately or wait 10 seconds and the code will become active Figure 4 16 Timer References Window Press the TMR REF Softkey to display the Timer References Window 2 Turn the large FMS Knob to place the cursor in the
188. s active FPL ACTIVE FLIGHT PLAN 136 975 OLORDO SPRINGS ORTE UF ACTIVE FLIGHT PLAN p TFR KMKC KCOS O DATA 6368FT NO OA I srr ESNS om FSHER PYNON so Approach KCOS RNAV 35Roes LPV HABUK iof De tigen FORT CARSON FALUR L CEGIX fof RHSSR map 6368FT MOGAL aahp CURRENT UNV PROFILE ACTIVE VNV WPT LU VS TGT temai gt Ree i mp V DEV GSA j 100r7 l 1000r7 ale ed B 30Nn _ CNCL VNV d E T j d Pz Oaar 6880 2 E eo B nE 8700 T o Pee oO gt Figure 7 46 Descending to the FAF 190 00324 07 Rev A SECTION 7 NAVIGATION The descent continues through the FAF CEGIX using the Glidepath Indicator as one would use a glideslope indicator to obtain an altitude AT 7 800 feet at the FAF Note the altitude restriction lines over and under At the altitude in the ALT field in Figure 7 46 24 After crossing CEGIX the aircraft continues following the glidepath to maintain the descent to AT or ABOVE 6 370 feet at the Missed Approach Point MAP RW35R as seen in Figure 7 47 FPL ACTIVE FLIGHT PLAN 136 975 ORTH uP i ACTIVE FLIGHT PLAN TFR KMKC KOOS HO DATA DTK DIS FSHER eee paced PYNOM oes ce n Approoch KOOS RMAY 35Riees LPV HABUK tof ee retinal A a _SECURITY WIDEPIELD FALUR Se yen ee CEGL fof ee ee F RHR mnp 351 4 3HH BS68FT 348 D4NH cat MOGAL mahp fat
189. s 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 10 5 SECTION 10 HAZARD AVOIDANCE e Freezing Levels e Winds Aloft e County Warnings e Cyclone Warnings as Echo Top Cloud Top and Echo Top Mutually Exclusive Figure 10 10 Weather Product Symbols 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 Weather Product Expires After that it is available minutes ___ ________ _ ___ SIGMETs AIRMETs o o A NOTE The DONE Softkey on the AUX XM INFORMATION Page is used to save the GDL City Forecasts oOo w 69 A activation data when the XM services County Warnings o are initially set up It is not used during normal Cyclone Warnings o w operation of the GDL 69 A and it should have no adverse effects if inadvertently selected during oe flight Refer to the GDL 69 69A XM Satellite Freezing Levels o Radio Activation Instructions 190 00355 04 Rev METARs wooo E or later for further information TE Fonetica O NEXRAD Weather Product Age Radar Coverage The age for each of the enabled products is displayed Cell Movement on the right side of the display Times are based on Zulu Surface Analysis time when the d
190. s of GPS navigation Abort approach TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav Change hdg reference to TRUE angle is set to AUTO SPIE ere eave A failure has been detected in the GPS1 and or GPS2 receiver The receiver 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 NAV 1 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transter switch again to cycle its operation If the problem persists NAV RMT XFR NAV2 remote the G1000 system should be serviced transfer key is stuck Sr tne esol Ope IStIN 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 failu
191. s should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F WARNINGS CAUTIONS amp NOTES NOTE When using Stormscope there are several atmospheric phenomena in addition to nearby thunderstorms that can cause isolated discharge points in the strike display mode However clusters of two or more discharge points in the strike display mode do indicate thunderstorm activity if these points reappear after the screen has been cleared 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 b
192. small FMS Knob to the left to display a list of flight plan waypoints as shown in Figure 7 3 IDENT FACILITY CITY KELN H CEN USA so NORTH UP Figure 7 3 Flight Plan Waypoint List MFD 3 Turn the large FMS Knob to select the desired waypoint 4 Press the ENT Key The cursor is now displayed on ACTIVATE 5 Press ENT again to activate a Direct to Garmin G1000 Cockpit Reference Guide for the DA40 40F Select a Direct to Destination to a Nearest Airport 1 Press the Direct to 8 Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 3 The list is populated only when navigating a flight plan IDENT FACILITY CITY KSLH W N CEN USA mie NORTH UP Figure 7 4 Nearest Airport List MFD 3 Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position as shown in Figure 7 4 4 Turn the large FMS Knob to select the desired airport 5 Press the ENT Key The cursor is now displayed on ACTIVATE 6 Press ENT again to activate a Direct to Select a Direct to Destination to a Recently Entered Identifier 1 Press the Direct to f Key 2 Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed as in Figure 7 3 The list is populated only when navigating a flight plan 190 00324 07 Rev A 3 4 5 6 DIRECT TO m IDENT FACILITY CITY KSLH
193. sor on the desired airport identifier 2 Press the ENT Key to display airport information 3 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 shown in the window 2 Press the ENT Key and the selected frequency will be placed in the COM standby frequency field 3 Press the Frequency Transfer Key to make the frequency the active frequency 7 26 Garmin G1000 Cockpit Reference Guide for the DA40 40F NEAREST INTERSECTIONS Figure 7 62 Nearest Intersections Page Select the Nearest Intersections Page 1 Turn the large FMS Knob on the MFD 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 190 00324 07 Rev A NEAREST NDB Figure 7 63 Nearest NDB Page Select the Nearest NDB 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 Kno
194. speed Trend VeCtOr v sssssessessecsesseesseesecsesseeaseesees 2 3 Vspeed Referentes corinae 2 3 2 2 Attitude Indicator 0 0 0 2 3 23 AIIM CD eetesiicscscncirccanecmienonnnenunnewn 2 4 Selected Altitude BUG c scssssssessessecsessessnesseesean 2 4 Altitude Trend Vector mususi ba iaSineneses 2 4 Barometric Setting BOK ssscacase tant duneeter tered ecedluustirec 2 4 Altitude Aleni aaien aE 2 4 Metric DisplaV isrtri a 2 5 Low Altitude Annunciation WAAS Only 2 5 2 4 Vertical Deviation Glidepath Glideslope Indicator nanana a 2 6 2 5 Marker Beacon Annunciations 2 7 2 6 Vertical Speed Indicator 0 ccceees 2 7 2 7 Barometric Altitude Minimume 2 7 2 8 Horizontal Situation Indicator HSI 2 8 Course FONE earns E 2 9 Course Deviation Indicator CDI 2 9 Bearing Pointers and Information Windows 2 11 DME OPTION esnan S 2 11 Navigation SOUPCES eninin sass 2 11 2 9 Wind Data ccc ccsesseeseeseestesseeseanes 2 12 2 10 Generic Timer 00 cece ees tessees testes eeaees 2 13 Section 3 Engine Indication System EIS 3 1 3 1 DA40 Engine Display 0 0 0 cece 3 2 3 2 DA4OF Engine Display 0 cc ccc 3 3 3 3 Engine Leaming 0 0 c ccc cesses 3 4 TABLE OF CONTENTS Section 4 NAV COM and Transponder 4 1 4 1 Radio Status Indications 0 cccccseen 4 3 42 Volume nsina 4 3 4 3
195. t ITI and Imminent Obstacle Impact IOI 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 Phase of Flight Level Flight Descending am 300 ft 100 ft 100 ft 350 Approach 150 ft co 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 runway or is below 125 feet AGL while within 1 nm of the runway 190 00324 07 Rev A Premature Descent Alert PDA 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 aircratt is either 0 5 nm from the runway threshold OR is at an altitude 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 parameters Height Above Terrain Feet unwa 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 h i i i Distance From Destination
196. t OPSHN 7 16 Garmin G1000 Cockpit Reference Guide for the DA40 40F 18 The aircraft is approaching OPSHN The upcoming turn and next heading will be annunciated at the top lett of the PFD as seen in Figure 7 40 Initiate the turn and maneuver the aircraft on a track through the turn radius to intercept the magenta line tor the OPSHN to FSHER leg and center the CDI 117 95 259 136 975 LL EEE FPL ACTIVE FLIGHT PLAN ronm ue f ACTIVE FLIGHT PLAN KMKC KOOS y W26S TBE E SEE i G Arrival KOOS TBE DBRY1 ALL OPSHH JMH fo SELENA TOCOOFT 25g JONH TOCHUFT ETY GSH TOCOUFT ak Jz 11 51 ORT Approach KCOS RNAY 35RioGrs LPY HABUK inf rea SSN S000 FALUR 261 SONH 8600 CURRENT WHY PROFILE ACTIVE Ve WPT V5 TGT aN 9 Y DEI 10 FT 136 975 136 975 d y k a i T 7 _ A y N i t Nt A a R Vee N f 7 Bons p g f e we aS ze p d ri 4 Pm 1 FA ON a aN Z Figure 7 40 Turn to intercept OPSHN to FSHER Leg 190 00324 07 Rev A SECTION 7 NAVIGATION 19 After passing OPSHN the next leg of the arrival will turn magenta as shown in Figure 7 41 The GOSEE magenta arrow in the flight plan list now indicates Co Sy r o l the OPSHN to FSHER leg of the arrival procedure is TEA m J o Airwoy W263 TBE TEE Arrival EICOS TBE DBRY 1 ALL delala KPUB rus OPSHN SnH
197. t engaged the pitch trim ser vo may be used to provide manual electric trim MET This allows the aircraft to be trimmed using a control wheel switch rather than the trim wheel Manual trim commands are generated only when both halves of the AP TRIM Switch are operated simultaneously Trim speeds are scheduled with airspeed to provide more consistent response Servo motor control limits the maximum servo speed and torque The servo mounts are equipped with slip clutches allowing the servos to be overridden in case of an emergency 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL Engaging the Autopilot A NOTE Autopilot engagement disengagement is not equivalent to servo engagement disengage ment Use the CWS Button to disengage the pitch and roll servos while the autopilot remains active When the AP Key is pressed the autopilot and flight director ifnot already engaged are activated Engagement is indicated by a green AP annunciation in the center of the AFCS Status Box The flight director engages in Pitch and Roll Hold modes when initially activated Autopilot Engaged ROL APP ALTS Figure 6 25 Autopilot Engaged Control Wheel Steering During autopilot operation the aircraft may be hand flown without disengaging the autopilot Pressing and holding the CWS Button disengages the pitch and roll servos from the flight control surfaces and allows the aircraft to be hand flown At the same time the fli
198. t plan waypoints are too close to allow for smooth turns not be smooth Prepare for steep turns ahead and expect noticeable course deviations APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate The system notifies the pilot to load the approach frequency for the appropriate frequency for approach NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for The system notities the pilot to set the CDI to the correct NAV receiver Set the approach CDI to the correct NAV receiver PTK FAIL Parallel track unavailable Bad parallel track geometry bad geometry PTK FAIL Parallel track unavailable mae Invalid leg type for parallel offset invalid leg type 12 20 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS Miscellaneous Message Advisories Cont sa im Tela taaa AF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current The current vertical waypoint can not be reached within the maximum flight path vertical waypoint angle and vertical speed constraints The system will automatically transition to the next vertical waypoint VNV Unavailable Unsupported leg The lateral flight plan contains a procedure turn vector or other unsupported leg type in flight plan type
199. the left to display a list 2 Turn the small FMS Knob to the left Initially a flight of flight plan airports as shown in Figure 7 54 plan waypoint list is displayed as in Figure 7 54 a The list is populated only when navigating a flight KMCI p an 3 Turn the small FMS Knob to the right to display the RECENT airports as shown in Figure 7 56 Figure 7 54 Flight Plan Airport List 3 Turn the large FMS Knob to select the desired airport 4 Press the ENT Key Figure 7 56 Recently Entered Airports List Select a Nearest Airport 4 Turn the large FMS Knob to select the desired 1 With the Airport Information Page displayed press ener the FMS Knob to activate the cursor 5 Press the ENT Key 2 Turn the small FMS Knob to the left Initially a Select an Airport by Facility Name or City flight plan airport list is displayed as in Figure 7 54 Location The list is populated only when navigating a flight l l l l plan 1 With the Airport Information Page displayed press the FMS Knob to activate the cursor 3 Turn the small FMS Knob to the right to display the 7 NRST airports to the aircraft s current position as 2 Turn the large FMS Knob to select the facility name shown in Figure 7 55 or location city field oe 3 Enter the desired facility name or city ocr 4 Press the ENT Key 5 To remove the flashing cursor press the FMS Knob Figure 7 55 Nearest Airport List 4 Turn the large FMS Knob to select the desired airport 5 Press the
200. tical Path Tracking Follows an active vertical profile for enroute and terminal phases of flight e VNAV Target Altitude Capture Captures the VNAV Target Altitude e Glidepath Intercepts and tracks the WAAS glidepath on approach only available in installations with GIA 63W Integrated Avionics Units and when WAAS is available e Glideslope Intercepts and tracks the ILS glideslope on approach e Go Around Automatically disengages the autopilot and commands a constant pitch angle and wings level while in the air Garmin G1000 Cockpit Reference Guide for the DA40 40F 6 3 SECTION 6 AUTOMATIC FLIGHT CONTROL Table 6 1 lists the pitch modes with their corresponding controls and annunciations The mode reference shown with default measurement units is displayed next to the active mode annunciation for Altitude Hold Vertical Speed and Flight Level Change modes The NOSE UP NOSE DN Keys can be used to change the pitch mode reference while operating under Pitch Hold Vertical Speed or Flight Level Change Mode Reference Pitch Mode Control Annunciation Reference Range Change Increment Selected Altitude Capture j ALTS Altitude Hold ALT Key Vertical Speed VS Key 3000 to 1500 fpm 100 tom FLC Flight Level Change IAS FLC Key aia 70 to 165 kt 1 kt Hold l Pitch Hold default T 1 P Vertical Path Tracking VNV Key VPTH VNAV Target Altitude m NITV Capture cepa APR Key Glideslope
201. ting NAV1 2 GPS or ADF for display using the corresponding pointer fee Information Bearing 1 Window Pointer Bearing 2 Pointer T Bearing 1 Bearing 2 Information Information Window Window Figure 2 25 HSI with Bearing Information Distance to Bearing Source Waypoint p Identifier EA Bearing Pointer Source Icon Figure 2 26 BRG1 Information Window SECTION 2 FLIGHT INSTRUMENTS Distance to Bearing Source 6 o gt _NAV2 Identifier Pointer Bearing Icon Source Figure 2 27 BRG2 Information Window DME optional To display the DME Information Window press the PFD Softkey followed by the DME Softkey Figure 2 28 DME Information Window Navigation Source Change CDI navigation sources 1 Press the CDI Softkey to change trom GPS to VOR1 LOC1 2 Press the CDI Softkey again to change from VOR1 LOC1 to VOR2 LOC2 3 Press the CDI Softkey a third time to return to GPS When using GPS as the navigation source the following may appear e LOI GPS position integrity is inadequate for the current procedure being flown If GPS is being used as primary navigation and LOI is annunciated other means of primary navigation will be required such as VHE LOI is also displayed during GPS position initialization e WARN GPS detects a position error e OBS Displayed when operating in OBS Mode 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 2 1
202. tor will command descent to the Selected Altitude rather than the VNV Target Altitude once Vertical Path Tracking Mode becomes active ALTS will be armed rather than ALTV c If Vertical Path Tracking Mode is armed more than 5 minutes prior to descent path capture acknowledgment is required for the flight director to transition from Altitude Hold to Vertical Path Tracking Mode To proceed with descent path capture if the white VPTH annunciation begins flashing do one of the following ALT Mode Cruise Altitude of 12 000 MSL e Press the VNV Key e Turn the ALT Knob to adjust the Selected Altitude If the descent is not confirmed by the time of interception Vertical Path Tracking Mode remains armed and the descent is not captured 2 When the top of descent TOD is reached the flight director transitions to Vertical Path Tracking Mode and begins the descent to the VNV Target Altitude Intention to capture the VNV Target Altitude is indicated by the white ALTV annunciation _ GPS AP ALTV 3 As the aircraft nears the VNV Target Altitude the flight director transitions to VNV Target Altitude Capture Mode indicated by the green ALTV annunciation flashing for up to 10 seconds SS GPS AP ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the VNV Target Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft at the verti
203. trieved from the navigation database Since altitudes loaded with an arrival procedure are published only for turbojet aircraft the altitudes are displayed as white text indicating that the altitudes are displayed for reference only An arrival waypoint altitude may be used or designated as is or changed to a different altitude An altitude is designated by pressing the FMS Knob and turning the large FMS Knob to place the cursor on the desired altitude and pressing the ENT Key or entering a different value and pressing the ENT Key The altitude will now be displayed as light blue text indicating that the altitude is now designated to give vertical speed and deviation guidance Garmin G1000 Cockpit Reference Guide for the DA40 40F Approach waypoint altitude constraints are designated in the same way as previously described for arrivals These altitudes will also be displayed as light blue text after being designated for use Waypoint altitude constraints may be designated up to but not including the FAE The FAF will always be a reference only altitude and cannot be designated unless the selected approach does not provide vertical guidance In this case the FAF altitude can be designated Altitudes that have been designated for use in vertical guidance may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key Other displayed altitudes may change due to re calculations or
204. tude fix would be labeled 5500rFr Again if the aircraft altitude is lower than this prescribed altitude a direct to will be established to this fix when the missed approach procedure is activated 25 Upon reaching the MAP it is decided to execute a missed approach Automatic waypoint sequencing is suspended past the MAP Press the SUSP Softkey on the PFD to resume automatic waypoint sequencing through the missed approach procedure A direct to is initiated to MOGAL which is the Missed Approach Hold Point MAHP as seen in Figure 7 48 The aircraft is climbing to 10 000 feet The CDI flight phase now changes from LPV to MAPR as seen on the HSI ACTIVE FLIGHT PLAN NORTH UP NORTH UF ACTIVE FLIGHT PLAN TFR KMKC KOOS HO DATA FSHER PY NON Approach KCOS RMAV HABUK lof CURRENT VW PROFILE ACTIVE VW WPT __FT at 6900 6840 Figure 7 48 Missed Approach Active 7 20 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 7 NAVIGATION 26 The aircraft continues climbing to AT or ABOVE 7 4 AIRPORT INFORMATION 10 000 feet at MOGAL A holding pattern will be established at the MAHP MOGAL as shown in SSma ann oe feels Figure 7 49 hil o G FPL ACTIVE FLIGHT PLAN 136 975 NORTH UP ACTIVE FLIGHT PLAN TFR KMKC KCOS NO DATA FSHER PYNON DTK DIS EA acer ANAI ae eae Approach KCOS RNAV 35Rees LPV HABUK jaf FALUR CEGIX fo
205. ual 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 Key when finished 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 190 00324 07 Rev A 9 1 SECTION 9 PROCEDURES ARRIVALS AND DEPARTURES Load and Activate a Departure Procedure 1 2 3 4 5 6 1 8 190 00324 07 Rev A Press the PROC Key Turn the large FMS Knob to highlight SELECT DEPARTURE Press the ENT Key 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 identitier of the desired airport Press the ENT Key Turn the large FMS
206. urn the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system MANIFEST GIA2 software should be serviced mismatch communication halted 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 15 A GIA mismatch has been detected where only one is WAAS capable SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63W Message Advisories Cont 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 COM2 SERVICE COM2 needs may still be usable The G1000 system should be serviced when possible service Return unit for repair COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck COM1 RMT XFR COM1 remote transter key is stuck COM2 RMT XFR COM2 remote transter key is stuck LOI GPS integrity lost Crosscheck a SE with other NAVS GPS integrity is insufficient for the current phase of flight at oe D o j oe Loss of GPS navigation due to insufficient satellites navigation Insufficient satellites ae Ay eaa B es Loss of GPS nav
207. w 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 temperature 12 12 Garmin G1000 Cockpit Reference Guide for the DA40 40F 190 00324 07 Rev A SECTION 12 ANNUNCIATIONS amp ALERTS GIA 63 Message Advisories Cont Message Comments 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 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 i The system has detected an over temperature condition in COM1 and or COM2 The gt TEMP CON transmitter will operate at reduced power It the problem persists the G1000 system on laa veep should be serviced Reducing transmitter power C OM1 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 COM2 needs still be usable The G1000 system should be servic
208. wledges 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 190 00324 07 Rev A 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 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 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 12 3 SECTION 12 ANNUNCIATIONS amp ALERTS 12 4 AFCS ALERTS System Status Annunciation wv 113 00 110 90 IDD ufr pis ore T 1118 700 cons naV 118 99 1 32 r System Status Annunciation The
209. xiliary Page Group Number of Pages in Current Group Waypoint Page Group Map Page Group MAP Lx 3 E a a Figure 1 7 Page Group Icon Selected Page 190 00324 07 Rev A Garmin G1000 Cockpit Reference Guide for the DA40 40F 1 9 SECTION 1 SYSTEM OVERVIEW 1 10 1 5 VERTICAL NAVIGATION In WAAS capable installations one of two altitude sources is used by the G1000 when giving vertical navigation guidance WAAS GPS altitude is used when giving guidance for a WAAS approach Baro corrected altitude is used when vertical guidance is given in all other situations and in non WAAS systems The G1000 system can use altitude constraints associated with lateral waypoints to give guidance for vertical navigation These altitudes are depending on the specific instance entered by the pilot or retrieved from the published altitudes in the navigation database The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at then the altitude will not be in the database In this case the altitude may be entered manually NOTE All arrival procedure altitudes contained in the navigation database are for turbojet aircraft only Alter or enter altitudes as desired to comply with the ATC clearance When activating or loading an arrival or approach procedure into an active flight plan the VNV ALT fields will be populated with any altitudes that can be re
210. y As the aircraft nears the Selected Altitude the flight director transitions to Selected Altitude Capture Mode indicated by the green ALTS annunciation flashing for up to 10 seconds Garmin G1000 Cockpit Reference Guide for the DA40 40F Pe GPS AP NMS 100007 ALT The green ALT annunciation flashes for up to 10 seconds upon reaching 50 feet from the Selected Altitude the autopilot transitions to Altitude Hold Mode and levels the aircraft NOTE As a result of calculations performed by the system while flying the holding pattern the display may re size automatically and the aircraft may not precisely track the holding pattern 4 The autopilot flies the holding pattern after the missed approach is activated Annunciations are displayed in the Navigation Status Box above the AFCS Status Box DIS BRG PON AVN Sd5 spol VO N Figure 6 38 Go Around Missed Approach GPS 35R KCOS 190 00324 07 Rev A SECTION 6 AUTOMATIC FLIGHT CONTROL 6 6 AFCS ANNUNCIATIONS AND ALERTS AFCS Status Alerts The following annunciations listed in order of increasing priority can appear on the PFD above the Airspeed and Attitude indicators Only one annunciation may occur at a time and messages are prioritized by criticality nav1 113 84 lt 110 90 IIXD nav2 115 9 110 90 IIXD AFCS Status Annunciation Figure 6 39 AFCS Status Annunciation Alert Condition Aileron Mistrim Right Rol
211. y Mode the tran sponder does not reply to interrogations but new codes can be entered STBY Mode White Code Number and XPDR 6543 STBY Se CC ALERTS Figure 4 12 Standby Mode Manual ON Mode Press the ON Softkey ON Mode generates Mode A and Mode S replies but Mode C altitude reporting is in hibited ON Mode No Altitude cue See ALERTS Figure 4 13 ON Mode Altitude Mode Automatic or Manual Altitude Mode is automatically selected when the air craft becomes airborne Altitude Mode may also be se lected manually by pressing the ALT Softkey All transponder replies requesting altitude information are provided with pressure altitude information __ ALT Mode Mode C Altitude Reporting pT pick A Figure 4 14 Altitude Mode Reply Status When the transponder sends replies to interrogations an R indication appears momentarily in the reply status field 190 00324 07 Rev A SECTION 4 NAV COM amp TRANSPONDER Reply Indication Figure 4 15 Reply Indication Code Selection VFR Code Selection 1 Press the XPDR Softkey to display the transponder Mode Selection softkeys 2 Press the VFR Softkey to enter the VFR code Pressing the VFR Softkey again restores the previous identification code NOTE The pre programmed VFR Code is set at the factory to 1200 Enter Code Using Softkeys 1 Press the XPDR Softkey to display the transponder Mode Selection softkey

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