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Garmin G1000 Cockpit Reference Guide for the DA42

190-00406-06 Rev. A

Warnings, Cautions & Notes

 

WARNING: 

NEXRAD weather data is to be used for long-range planning 

purposes only.  Due to inherent delays in data transmission and the relative 
age of the data, NEXRAD weather data should not be used for short-range 
weather avoidance.

 

WARNING: 

Use of the Stormscope is not intended for hazardous weather 

penetration  (thunderstorm  penetration).    Stormscope  information,  as 
displayed on the G1000 MFD, is to be used only for weather avoidance, not 
penetration.

 

WARNING: 

The Garmin G1000, as installed in the Diamond DA42 aircraft, has 

a very high degree of functional integrity.  However, the pilot must recognize 
that providing monitoring and/or self-test capability for all conceivable system 
failures is not practical.  Although unlikely, it may be possible for erroneous 
operation to occur without a fault indication shown by the G1000.  It is 
thus the responsibility of the pilot to detect such an occurrence by means of 
cross-checking with all redundant or correlated information available in the 
cockpit.

 

WARNING: 

For safety reasons, G1000 operational procedures must be learned 

on the ground.

 

WARNING: 

The United States government operates the Global Positioning 

System and is solely responsible for its accuracy and maintenance.  The GPS 
system is subject to changes which could affect the accuracy and performance 
of  all  GPS  equipment.    Portions  of  the  Garmin  G1000  utilize  GPS  as  a 
precision electronic NAVigation AID (NAVAID).  Therefore, as with all NAVAIDs, 
information presented by the G1000 can be misused or misinterpreted and, 
therefore, become unsafe.

 

WARNING: 

To  reduce  the  risk  of  unsafe  operation,  carefully  review  and 

understand all aspects of the G1000 Pilot’s Guide documentation and the 
Diamond DA42 Pilot’s Operating Handbook (POH).  Thoroughly practice basic 
operation prior to actual use.  During flight operations, carefully compare 
indications  from  the  G1000  to  all  available  navigation  sources,  including 
the information from other NAVAIDs, visual sightings, charts, etc.  For safety 
purposes, always resolve any discrepancies before continuing navigation.

Summary of Contents for DA42 G1000

Page 1: ...G1000 Integrated Flight Deck Cockpit Reference Guide for the DA42...

Page 2: ......

Page 3: ...GINE INDICATION SYSTEM NAV COM TRANSPONDER AUDIO PANEL AUTOMATIC FLIGHT CONTROL SYSTEM GPS NAVIGATION FLIGHT PLANNING PROCEDURES HAZARD AVOIDANCE ADDITIONAL FEATURES ABNORMAL OPERATION ANNUNCIATIONS A...

Page 4: ......

Page 5: ...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 si...

Page 6: ...geometric height above Mean Sea Level and could vary signi cantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in aircraft GPS altitude...

Page 7: ...ct 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 gr...

Page 8: ...and 165 East CAUTION The PFD and MFD displays use a lens coated with a special anti re ective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL...

Page 9: ...to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please r...

Page 10: ...Garmin G1000 Cockpit Reference Guide for the DA42 190 00406 06 Rev A Warnings Cautions Notes Blank Page...

Page 11: ...g capability Updated Annunciations and Alerts 190 00406 03 Rev A Rev B Added XM Weather capability Added TAWS B Updated Message Advisories Added Lycoming engine parameters Changed System SW applicabil...

Page 12: ...A RR 2 Record of Revisions Part Number Change Summary 190 00406 06 Added Airways WAAS VNAV Charts Updated G1000 System Messages Added other GDU 8 20 parameters Reformatted manual Revision Date of Revi...

Page 13: ...Engine Display 5 System Display 6 Fuel Display 6 NAV COM TRANSPONDER AUDIO PANEL 9 Enter or Change Flight ID 9 Enter a Transponder Code 9 ADF Tuning Optional 9 DME Tuning Optional 10 Selecting a COM R...

Page 14: ...Activate A Departure Leg 31 Load An Arrival Procedure 31 Activate An Arrival Leg 32 Load and or Activate an Approach Procedure 32 Activate An Approach in the Active Flight Plan 33 Activate a Vector t...

Page 15: ...S Alerts 50 Voice Alerts 51 MFD PFD Message Advisories 52 Database Message Advisories 53 GMA 1347 Message Advisories 55 GIA 63 Message Advisories 56 GIA 63W Message Advisories 58 GEA 71 Message Adviso...

Page 16: ...Garmin G1000 Cockpit Reference Guide for the DA42 190 00406 06 Rev A iv Table of Contents Blank Page...

Page 17: ...SURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in H...

Page 18: ...o set the desired time then press the ENT Key The UP DOWN eld is now highlighted 2 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 S...

Page 19: ...mall FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey DISPLAYIN...

Page 20: ...ide for the DA42 190 00406 06 Rev A 4 Flight Instruments Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun...

Page 21: ...Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun Alerts Appendix Index ENGINE INDICATION SYSTEM ENGINE DISPLAY ENGINE Display Engine Load Indicator Tachometer...

Page 22: ...ex SYSTEM DISPLAY Pressing the ENGINE Softkey displays the SYSTEM and FUEL softkeys Press the SYSTEM Softkey to show the System Display SYSTEM Display Engine Load Indicator Tachometer Gearbox Temperat...

Page 23: ...red fuel quantity has no effect on fuel calculations Fuel calculations are based on sensed fuel ow and the last manual adjustment of the fuel remaining DEC FUEL Allows the pilot to decrease the gallon...

Page 24: ...for the DA42 190 00406 06 Rev A 8 Engine Indication System Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation An...

Page 25: ...oftkeys 2 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Press the digit softkeys to enter the code in the code eld When entering the code the next key in...

Page 26: ...if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 Press the CDI Softkey to select NAV1 VOR1 LOC1 or NAV...

Page 27: ...lay begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next previously recorded block INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COP...

Page 28: ...for the DA42 190 00406 06 Rev A 12 Nav Com XPDR Audio Panel Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation An...

Page 29: ...llowing table when the ight director is not active activates the pilot side ight director in the listed modes Control Pressed Modes Selected Lateral Vertical FD Key Roll Hold default ROL Pitch Hold de...

Page 30: ...lected Altitude VS Key VS nnnn FPM Flight Level Change Maintains the current aircraft airspeed in IAS while the aircraft is climbing descending to the Selected Altitude FLC Key FLC nnn KT VNAV GDU 104...

Page 31: ...aptures and tracks the Selected Heading HDG Key HDG Navigation GPS Captures and tracks the selected navigation source GPS VOR LOC NAV Key GPS Navigation VOR Enroute Mode VOR Navigation LOC Glideslope...

Page 32: ...nce Guide for the DA42 190 00406 06 Rev A 16 AFCS Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun Alerts...

Page 33: ...s the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the small FMS Knob to select MSL or AGL...

Page 34: ...ter the desired course to the waypoint 14 Press the ENT Key to highlight ACTIVATE 15 Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD and turn...

Page 35: ...Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the ight plan This does not delete the stored ight plan only the active ight plan VERTICAL NAVIGATION VNAV...

Page 36: ...Key The altitude is now displayed only as a reference It will not be used to give vertical ight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a resul...

Page 37: ...Key and select Set WPT to Present Position to display P POS c Press the ENT Key and the ashing cursor moves to the ending waypoint eld d Enter the identi er of the ending waypoint and press the ENT Ke...

Page 38: ...system settings 7 Enter the fuel ow Press the ENT Key when nished Note that in AUTOMATIC page mode fuel ow is provided by the system 8 The ashing cursor moves to the fuel onboard eld Modify the fuel...

Page 39: ...select the desired waypoint d Press the ENT Key 7 After pressing the ENT Key the cursor is displayed in the RAD radial eld Enter the desired radial from the reference waypoint 8 Press the ENT Key 9 Th...

Page 40: ...the departure waypoint 6 Press the ENT Key 7 Repeat step number 4 5 and 6 to enter the identi er for each additional ight plan waypoint 8 When all waypoints have been entered press the FMS Knob to ret...

Page 41: ...erted before the highlighted waypoint 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new ight plan waypoint by one of the following a Enter the user waypoint id...

Page 42: ...ceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position 5 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are s...

Page 43: ...mation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a ight plan on either the PFD or MFD it may be saved by pressing t...

Page 44: ...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 INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Ke...

Page 45: ...hted press the ENT Key to delete the ight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flig...

Page 46: ...uide for the DA42 190 00406 06 Rev A 30 Flight Planning Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun...

Page 47: ...ct the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION eld with a list of available transitions 7 Turn the large FMS Knob to highlight the desired transition 8 Press the E...

Page 48: ...int in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired wayp...

Page 49: ...es vectors will be received to the nal course segment of the approach and will provide navigation guidance relative to the nal approach course 7 Press the ENT Key LOAD or ACTIVATE is now displayed wit...

Page 50: ...edures Hazard Avoidance Additional Features Abnormal Operation Annun Alerts Appendix Index ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highli...

Page 51: ...ll FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MF...

Page 52: ...ell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 Turn the large FMS Knob until the Map Page group is selected 2 Turn the small FMS Knob until the Stormsc...

Page 53: ...e 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Ma...

Page 54: ...rface Analysis Freezing Levels Winds Aloft County Warnings Cyclone Warnings TRAFFIC SYSTEMS If Traf c information Service TIS is con gured STANDBY OPERATE and TNA MUTE softkeys are displayed If a Traf...

Page 55: ...ayed in the Traf c Mode eld 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Displaying Traf c on the Navigation Map 1 Ensure TIS is opera...

Page 56: ...e 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 i...

Page 57: ...d airport identi cation labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time rem...

Page 58: ...ess the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 Press the DP STAR APR WX and NOTAM softkeys to access charts for...

Page 59: ...es information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS K...

Page 60: ...Box is highlighted 3 Press the numbered softkeys located on the bottom of the display to directly select the desired channel number 4 Press the ENT Key to activate the selected channel Assigning Chan...

Page 61: ...display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Diamond DA42 Pilot s Operating Handbook POH always takes precedence over t...

Page 62: ...om the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traf c Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Info...

Page 63: ...slightly above and to the right of the aircraft symbol on the CDI as shown in the following gure Also the CDI deviation bar is removed from the display Lastly but at the same time a GPS NAV LOST alert...

Page 64: ...nd is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box elds except Active Leg TAS and DTK GPS Bearing Poi...

Page 65: ...mps L R STARTER Left right engine starter is engaged L R FUEL TEMP Left right fuel temp is greater than 75 deg C DOOR OPEN Front rear or baggage door is not closed AP TRIM FAIL Autopilot automatic tri...

Page 66: ...right fuel transfer from aux to main in progress ALERT MESSAGE Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative None MFD FAN FAIL The cooling fan for the MFD...

Page 67: ...e any maximum fuel imbalance limits Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force Ensure the slip skid indicator is centered and observe any...

Page 68: ...alted The PFD and or MFD has incorrect software installed The G1000 system should be serviced MANIFEST MFD1 software mismatch communication halted PFD1 CONFIG PFD1 con g error Con g service req d The...

Page 69: ...tempt to reload the aviation database If problem persists the G1000 system should be serviced PFD1 DB ERR PFD1 aviation database error exists MFD1 DB ERR MFD1 basemap database error exists The MFD and...

Page 70: ...RU but is missing on the speci ed LRU PFD1 DB ERR PFD1 airport terrain database missing MFD1 DB ERR MFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database...

Page 71: ...cle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismat...

Page 72: ...COOLING GIA1 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA2 COOLING GIA2 over temperature GIA1 SERVICE GIA1 needs service R...

Page 73: ...te transfer key is stuck RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints GPS satellite coverage is insuf cient to perform Receiver Autonomous Integrity Monitoring RAIM from the FAF to the...

Page 74: ...n the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FA...

Page 75: ...system should be serviced GIA2 SERVICE GIA2 needs service Return the unit for repair HW MISMATCH GIA hardware mismatch GIA1 communication halted A GIA mismatch has been detected where only one is WAA...

Page 76: ...XFR COM2 remote transfer key is stuck LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is insuf cient for the current phase of ight GPS NAV LOST Loss of GPS navigation Insuf cient satel...

Page 77: ...ain to cycle its operation If the problem persists the G1000 system should be serviced NAV2 RMT XFR NAV2 remote transfer key is stuck G S1 FAIL G S1 is inoperative A failure has been detected in glide...

Page 78: ...S 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the l...

Page 79: ...n the 1 GMU 44 Heading is agged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect...

Page 80: ...the waypoint name identi er to re ect the new information FPL WPT MOVE Flight plan waypoint moved The system has detected that a waypoint coordinate has changed due to a new aviation database update...

Page 81: ...xxxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the air...

Page 82: ...Unavailable Unsupported leg type in ight plan The lateral ight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidanc...

Page 83: ...EOUS MESSAGE ADVISORIES CONT Message Comments 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 variance Verify all course angl...

Page 84: ...e for the DA42 190 00406 06 Rev A 68 Annunciations Alerts Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annu...

Page 85: ...op Level PFD Softkeys ALERTS ADF DME Inset Map Softkeys Press the BACK Softkey to return to the top level softkeys STRMSCP ALERTS ALERTS ADF DME TRFC 1 TRFC 2 INSET Displays Inset Map in PFD lower lef...

Page 86: ...ys topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Press to display the Stormscope lightning data on t...

Page 87: ...mponents OFF Information not displayed DME Displays the DME Information Window BRG1 Cycles the Bearing 1 Information Win dow through NAV1 or GPS waypoint identi er and GPS derived distance information...

Page 88: ...does not reply to any interrogations ON Selects Mode A transponder replies to interrogations ALT Selects Mode C Altitude Reporting Mode transponder replies to identi cation and altitude interrogation...

Page 89: ...o UNDO when the checklist item is already checked ENGINE FUEL ENGINE RST FUEL DEC FUEL INC FUEL optional TRAFFIC TOPO BACK TERRAIN Press the BACK Softkey on this level to return to the top softkey lev...

Page 90: ...e map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displaye...

Page 91: ...nstruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun Alerts Appendix Index SHW CHRT When available displays optional...

Page 92: ...e Guide for the DA42 190 00406 06 Rev A Appendix 76 Flight Instruments EIS Nav Com XPDR Audio AFCS GPS Nav Flight Planning Procedures Hazard Avoidance Additional Features Abnormal Operation Annun Aler...

Page 93: ...metric pressure 71 C CDI 1 10 65 Cell 35 36 Cell mode 36 Channel Presets 44 ChartView 41 Clearance player 11 Clearance Recorder 11 Code selection softkeys 9 COM 10 11 45 D DCLTR Softkey 41 Dead Reckon...

Page 94: ...7 38 70 74 O OBS 2 Obstacles 55 59 Overspeed Protection 14 R Reversionary mode 45 S SafeTaxi 41 Store Flight Plan 27 Stormscope lightning data 35 36 70 Strike 35 Strike mode 36 T TA 51 TAF 37 TAS 39 5...

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Page 96: ...U S A p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangs...

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