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Garmin Software Version 0534.15 Cockpit Reference Guide

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1. 42 HAZARD AVOIDANCE e 43 Customizing the Hazard Displays on the Navigation 43 XM Weather Optional seen Traffic Systems Terrain And Obstacle Proximity Terrain SVS Terrain Awareness amp Warning System TAWS Display Optional 49 ADDITIONAL FEATURES Synthetic Vision Optional Terminal Procedure Charts AOPA Airport Directory ssssssseeeeenennennnnnnnnnns Radio Entertainment Optional Auxiliary Video 5 Electronic Checklists 2 atti hr trt Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN table of contents ABNORMAL OPERATION 61 Reversionary 61 Abnormal COM Operation L sse 61 Audio Panel Fail safe Operation 1 Hazard Displays with Loss of GPS Position 61 Unusual Attitudes seen 62 Dead Reckonlhg ccecce ee tee me erm e etn td 62 ANNUNCIATIONS amp 65 WARNING Alerts ene tte tene desee ee tibt 65 CAUTION Alerts eere Re eire YD d He ee a 65 Annunciation Advisory
2. WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A amp Namings udun amp Notes WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING The Garmin G1000 as installed in the Cessna Corvalis Corvalis TT 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 lt 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 an
3. beraten ded NR 6 Engine Leaning Assist Mode ssssssssee nnn 0 NAV COM TRANSPONDER AUDIO PANEL 3 ADF Tuning Optional sssssssseetenn enne 3 DME Tuning Optional cc ccccccccssssssssssssssccssssssssssesssssssssssesssssssssscesssssssssssessssssssnsess 3 Enter a Transponder Code 3 Selecting a COM Radio sss 4 Selecting a NAV Radio 4 NAV COM Tuning 56r iet erem tht trem tht one seen rm ep ee 4 Digital Clearance Recorder and Player 4 Intercom System ICS Isolation sss 5 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM 7 Flight Director Activation sse 7 Vertical Modes ra une tania teh ete id he 8 Lateral Modes 9 GPS NAVIGATION o tt ataca aa a a z old 21 Direct to Navigation sssssssssseeeen nnne 21 Activate a Stored Flight Plan 22 Activate a Flight Plan Leg 22 Stop Navigating a Flight Plan 23 Vertical Navigation VNAV s s nnne 23 FLIGHT PLANNING ssec 25 Trip Planning cem e rene re ibd bei aer 25 Create a New User Waypoint Defined by Latitude amp Longitude 2 Create a New User Waypoint Defined by Radials from Other Waypoints 2 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Table of Con
4. PFD MFD MFD Alert Type 1 TAWS B Page Aural Message Pop Up Alert Annunciation mminent Obstacle Obstacle Ahead Pull Up Impact Waming or Obstacle Ahead Pull Up 0 or Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain Caution RTC TERRAIN AHEAD or Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN AHEAD Terrain Ahead Terrain Impact Caution ITI or Ahead CATION TERRAIN Caution Terrain Caution Terrain Reduced Required TERRAIN AUTTON OBSTACLE Caution Obstacle Cau Obstade Clearance or tion Obstade Caution ROC o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN 1 OBSTACLE AHEAD 1 Obstacle Ahead Obstacle Impact Caution 101 or Ahead CATION OBSTACLE Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN TOOLOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Climb TERRAIN bDNTSIK Don t Sink Rate Caution NCR or or Low Tern 70 Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN TAWS B System
5. NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Selecting the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Selecting the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Selecting 52 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Selecting the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuverin
6. LOI GPS integrity lost Crosscheck with other NAVS Loss of GPS integrity monitoring GPS NAV LOST Loss of GPS naviga tion Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to position error Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation TRUE APR True north approach Change hdg reference to TRUE Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in the GPS1 and or GPS2 receiver The receiver is unavailable The G1000 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still
7. Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message FPL TRUNC Flight plan has been truncated Comments This occurs when a newly installed aviation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded appr
8. Appendix Alerts Operation Features Index GPS Navigation 1 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or tum the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 22 1 2 3 From the Active Flight Plan Page press the FMS Knob to activate t
9. 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Tum the small FMS Knob to select MSL or AGE 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 8 2 Tum the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 21 sjuauimasu wp 59 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures
10. Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Bazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page XM WEATHER OPTIONAL N V ARNING Use of XM vveather for hazardous vveather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and T
11. Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation Doox The position of the selected waypoint xxxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint TRAFFIC FAIL Traffic device has failed The G1000 is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 87 s m p q eo ueproAy SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix pos Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAG
12. Index Flight Planning 5 6 7 A GARMIN with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list IMPORT A FLIGHT PLAN FROM AN SD CARD 1 2 3 4 5 6 7 8 Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the MFD to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight plan Press the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select anothe
13. MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced 74 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations 8 Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Chartview database error exists Comments The MFD and or PFDs detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the G1000 system should be serviced DB MISMATCH Aviation database version mismatch Xtalk is off The PFDs and MFD have different aviation database versions installed Crossfill is off Install correct aviation database version in all displays DB MISMATCH Aviation database type mismatch Xtalk is off The PFDs and MFD have different aviation database types installed Americas European etc Crossfill is off Insta
14. The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key Select an Available Channel within the Selected Category 1 While on the XM Radio Page select the CHNL Softkey 2 Select the CH Softkey to go down through the list in the Channel Box or move up the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 55 xipuaddy Suelv uoneiedo sainyea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx 913 sjuaumasu unuuy Jeuuouqy jeuonippy paezey fil U10 AEN iui x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A GARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Sele
15. displayed 6 With OK highlighted press the ENT Key to copy the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key DELETE A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 5 Select the DELETE Softkey A Delete flight plan 82 confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key 36 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key to display the Active Flight Plan Page on the MFD Flight Planning 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 3 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point 4 Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default
16. 04 Rev A flight director Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT ust have a valid VOR or LOC signal or active GPS course before have a valid LOC signal before BC Key press activates flight director 17 sia sjueunasu oipny uadx u102 AEN ARN Sd5 52 suey uoneiedo sainjea4 aoueplony 2 Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul nb n paezey Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch Pitch Hold attitude may be used to dimb default PIT descend to the Selected Altitude 7v77 77 Captures the Selected Altitude ALTS Armed Altitude Hold Holds the current Altitude Key AUT Reference Holds aircraft vertical speed may Vertical Speed be used to climb descend to the VS Key VS nnnnreM Selected Altitude Holds aircraft airspeed while aircraft Flight Level Change 1 is dimbing descending to the FLCKey FLC nnnkr Selected Altitude Vertical Path Tracking capturas 15 d VNV Key VPTH an active vertical profile VNAV Target Altitude 1 Captures the Vertical Navigation T ATV Capture VNV Target Altitude Glidepat
17. CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the PFD or MFD contains invalid data 88 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A amp GARMIN Appendix APPENDIX sjuauimasu sub PFD SOFTKEY MAP 59 optional mer E 997 C590 foe xe ST pweme Wer wmm 77 um m 7 uu uu m olpny uqax uo2 AEN CD NAV2 Top Level PFD Softkeys E optional mnnunnn buluueld nubi optional optional ess E parce oS n E 8 LA FHN EE S Press the BACK Softkey to return to the top level softkeys gt Chr 5 aa m 2E Inset Map Softkeys ge go os dasi INSET Displays Inset Map in PFD lower left corner 92 OFF Removes Inset Map eki DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan Sue v unuuy gt 5 o 3 a x x pul 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 89 Annun Abnormal Additional Hazard Flight Nav Com Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav AF
18. Card Reader SanDisk SDDR 93 SanDisk SDDR 99 Verbatim 96504 or equivalent Updated database obtained from the Garmin website 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 97 uone1edo aoueplony SoJnpa204d buluueld AEN Sd5 S24JV oipny uddx 513 sjueumasu Jeuuouqy Jeuonippy puezey ubi U10 AEN 1461 Sue v unuuy A k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Existing Supplemental Database SD Card 010 00330 41 42 or 43 from the MFD The supplemental data card from the MFD should be used because all databases except the active navigation database are required to reside on this card Jeppesen Databases NOTE The Jeppesen aviation navigation database is now referred to as the navigation database Previously this database had been referred to as the aviation database The ChartView database should be copied to the Supplemental Data Card which will reside in the bottom card slot on the MFD The navigation database is be loaded from the Jeppesen or user supplied SD data card Contact Jeppesen www jeppesen com for subscription and update information The navigation database is loaded from an SD card inserted into the top card slot of each displayed The database is copied from the SD card
19. ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure Procedures 4 Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 39 oipny uddx 59 sjuauimasu U105 AEN 346 3 52 AEN 540 Duruue d wold s mp old uoneiado saunyea4 unuuy jeuuouqy
20. GIA2 audio config error Config service req d GIA1 COOLING G A1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 have an error in the audio configuration The G1000 system should be serviced The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING G A1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the G1000 system should be serviced GIA1 SERVICE G A1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 79 saunqee4 uepjoay sanpa20Jd Buruuejg AEN 5649 S24V oipny uadx sia siu umn sul paezey nubi Juo ney Wil jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 2 Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 c
21. GPS1 and or GPS2 receiver The receiver may still be available The G1000 system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operation If the problem persists the G1000 system should be serviced 6 51 FAIL 6 51 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 81 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy INN Ea x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service
22. Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The G1000 system should be serviced when possible GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced GTX 33 MESSAGE ADVISORIES Message Comments XPDR1 CONFIG XPDR1 config error Config service req d The transponder configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The G1000 system should be serviced XPDR1 SRVC XPDR1 needs service Return unit for repair The 1 transponder should be serviced when possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder 82 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations 8 Alerts
23. Sd5 S24JV oipny uadx 913 unuuy Jeuuouqy Jeuonippy paezey Wfil4 U10 AEN x pul GARMIN Flight Instruments Eu E oipny uadx U105 AEN S2dV AeN Sd5 Duruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 04 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT A GARMIN FUEL QTY GAL 6 16 20 30 40 F FFLOW OIL PSI 46 OIL F CHE O Engine Manifo 2 Tachometer 0 Fuel Quantity Fuel Flow Indi EGT F Vv ENGINE INDICATION SYSTEM FUEL QTY GAL v I X y ani 10 20 30 40 F GPH 17 0 FFLOW GPH 16 0 he 7 MH HM ET 45 OIL PSI 46 A 4 Eee OIL F ELEV 178 TRIM 4M 1543 7 1549 1350 X 350 x AILERON TRIM AILERON TRIM v v Corvalis Corvalis TT EIS Display ld Pressure Gauge O Exhaust Gas Temperature Indicator Corvalis only Turbine Inlet Temperature Indicator Indicator Corvalis TT only cator 9 Cylinder Head Temperature Indicator G Oil Pressure Indicator Trim Group Oil Temperatu 190 00567 04 Rev A re Indicator Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Engine Indication System 5 Sjueuinagjsu MU xipuaddy uoneiedo sounjeo4 e2uepioAy SoJnpa20Jd buluueld AEN Sd5 S24V oipny duadx Jeuuouqy jeuonippy x pul UATE UI0JN
24. Softkey changes to UNCHECK when the checklist item is already checked SYSTEM CHECK EXIT EMERGCY nnn O MFD Softkeys Access the EIS functions Returns to the top level EIS display Turns the oxygen system on or off optional Cycles the EGT and CHT cylinder temperatures on and off Accesses the Engine Leaning Assist Mode Resets the CO Guardian and acknowledges an alert Decreases the gallons of fuel remaining GAL REM in 1 gallon increments Increases the gallons of fuel remaining GAL REM in 1 gallon increments Resets the fuel remaining to 98 or 102 gallons 94 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN MAP DCLTR 3 SHVV CHRT CHKLIST 190 00567 04 Rev A TRAFFIC TOPO TERRAIN AIRWAYS NEXRAD XM LING BACK CHECK EXIT EMERGCY Appendix Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays NEXRAD weather and coverage information on Navigation Map optional Displays XM lightning information
25. Status Annunciations Annunciations amp Alerts database coverage area entered PFD MFD Alert TAWS B Page Aural Alert Type Annunciation Annunciation Message 777 TAHS TEST None Progress TANS System System Test Pass None None Test OK TAWS B System Test TAWS System Fail Failure Terrain or Obstade database unavailable or invalid TAWS System invalid software Failure configuration system audio fault MFD Terrain or Obstacle database unavailable or invalid None None System operating with PFD Terrain or Obstacle databases gt TANS Not No GPS position Available Excessively degraded GPS signal or out of None TAWS Not database coverage Available area Sufficient GPS signal 1606017 None None TANS Available 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 71 sainjea4 2 buluueld AEN Sd5 S24JV olpny uqax sia sjuauimasu 2 nubi JU10 AEN ui jeuonippy uoneiedo Jeuuouqy ME x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix pres Annunciations amp Alerts A GARMIN VOICE ALERTS Voice Alert Description Minimums minimums The aircraft has descended below
26. and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 34 1 2 3 4 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 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 Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure or airway Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN STORE A FLIGHT PL
27. automatically reverts to the default mode for that axis NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed z Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Switch Roll Hold default ROL Pitch Hold default PIT Takeoff on ground TO Takeoff on ground d GA Go 5 x 25 ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold default ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH FLC Key Roll Hold default ROL Flight Level Change GPS NAV Key Navigation VOR Pitch Hold default PIT LOC BC Key GDU 1044B Backcourse BC Pitch Hold default PIT GPS Pitch Hold default PIT APR Key Approach VAPP Glidepath GP LOC Glideslope GS HDG Key Heading Select HDG Pitch Hold default PIT Valid VNV flight plan must be entered before VNV Key press activates flight director The selected navigation receiver NAV or APR Key press activates The selected navigation receiver mus 190 00567
28. error exists Comments The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 terrain database missing PFD1 DB ERR PFD1 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists The G1000 system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU
29. jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures GARMIN 4 5 6 1 8 3 10 11 12 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired waypoint within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highligh
30. of the PFD or MFD n e Unselected MFDI DB Selected PFD DB Selected Display Database Selection Softkey Garmin Databases The following databases are stored on Supplemental Data Cards provided by Garmin Expanded basemap Obstacle Airport Directory Terrain SafeTaxi AOPA Airport terrain FliteCharts After subscribing to the desired database product updates these updated databases are copied to each Supplemental Data Card for each display the card that contains the FliteCharts or ChartView database resides in the MFD Since these databases are not stored internally in the displays these Supplemental Data Cards must remain in the bottom card slot of each display 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 Obtaining Garmin Database Updates The Garmin database updates can be obtained by following the instructions detailed in the Aviation Databases section of the Garmin website ly garmin com Once the updated files have been downloaded from the website a PC equipped with an appropriate SD card reader is used to unpack and copy the new databases onto the appropriate Supplemental Data Cards Equipment required to perform the update is as follows Windows compatible PC computer Windows 2000 or XP recommended SD
31. sse 66 Message Advisory Alerts 66 CO Guardian Messages nennen 66 ECS Alerts El Terrain SVS Alerts TAWS B Alerts aeo tenen en o deni uci Voice Alerts tee tute td e o dba RO RR BR MFD amp PFD Message Advisories Database Message Advisories GMA 1347 Message Advisories sssssssssseeeeene GIA 63 Message Advisories GIA 63W Message Advisories sss GEA 71 Message Advisories ssssssssee nne GTX 33 Message Advisories GRS 77 Message 501165 GMU 44 Message Advisories GDL 69A Message 15015 GDC 74A Message Advisories GCU 476 Message Advisories Miscellaneous Message Advisories sssssss 85 APPENDIX oto too osi dla du d l d PFD Softkey Map MED Softkey Map 94 Database O T ET nie ette ttt ente iem tit Get 96 INDEX d Index 1 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT il Table of Contents GARMIN Blank Page V Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTIN
32. system should be serviced when possible COM1 PTT COM push to talk key is stuck COM2 PTT COM push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM 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 RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM from the FAF to the MAP waypoints 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 71 soJnjeoJ 2 Buruuejd AEN Sd 2 olpny yqax sia sjuauwinsu paezey ETSI Wil jeuonippy uoneiedo Jeuuouqy IBN EE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments
33. to 20 minutes Terrain Proximity TERRAIN SVS and TAWS are also disabled Additionally the accuracy of all nearest information airports airspaces and waypoints is questionable Finally airspace alerts continue to function but with degraded accuracy 64 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ALERTS Annunciation Window Alerts Window Message Audio Alert Voice Text Message Repeating Door not secured Chime Door Open Fuel tank is not correctly selected Chime Fuel Valve or in OFF position No power on the left bus Chime No power on the right bus Chime Carbon Monoxide level is too high Chime Carbon Monoxide Low oil pressure Chime Oil Pressure Low CAUTION ALERTS Annunciation Window Alerts Window Message Audio Alert Voice Text Message Corvalis only 4 High pressure oxygen outlet only tLow pressure oxygen outlet only 190 00567 04 Rev A Left Alternator offline Single Chime Left Alternator Out Right Alternator offline Single Chime Right Alternator Out Fuel pump is operating Single Chime Fuel Pump Low fuel in the left tank Single Chime None Low fuel in the right tank Pressure above 12 000 ft and oxygen off Single Chime None Single Chime None Oxygen outlet pressure below
34. 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 Echo Top Cloud Top and Echo Top Mutually Exclusive Cyclone Warnings AIREPs City Forecast Icing Potential E Cell Movement Freezing Levels l Turbulence P IREP ae XM Lightning METARs Surface Analysis County Warnings Cloud Top SIGMETS AIRMET5 Winds Aloft TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed 44 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Hazard Avoidance Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation S Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS NOTE If the G1000 is configured to
35. 0 Softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Displaying Terrain and Obstacles on the Navigation Map 1 With the Navigation Map displayed select the MAP Softkey 2 Select the TERRAIN Softkey Terrain and obstacle proximity will now be displayed on the map TERRAIN SVS NOTE Terrain SVS is only available when the Synthetic Vision System SVS option is installed and the TAWS option has not been installed NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south Display Terrain on the TERRAIN SVS Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain SVS Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwi
36. 1000 system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The G1000 system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The G1000 system should be serviced DATABASE MESSAGE ADVISORIES Message MFD1 DB ERR MFD1 aviation database error exists PFD1 DB ERR PFD1 aviation database error exists Comments The MFD and or PFD detected a failure in the aviation database Attempt to reload the aviation database If problem persists the G1000 system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists The MFD and or PFD detected a failure in the basemap database 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 13 saunqea4 2 AEN Sd S24V oipny uadx sia siu umn sul paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy IBN PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR 1 terrain database
37. 2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency 3 Select the CDI Softkey a third time to return to GPS Nav Com XPDR Audio AFCS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Select the OBS Softkey to select OBS Mode 2 Turn a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Select the OBS Softkey again to disable OBS Mode GPS Nav Flight Planning GENERIC TIMER Procedures 1 Select the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Turn the small FMS Knob to display the UP DOVVN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window Hazard Features Avoidance Additional Abnormal Operation CONFIGURE VSPEED BUGS Annun Alerts 1 Select the TMR REF Softkey 2 Turn the large FMS Knob to highlight the desired Vspeed 3 Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to th
38. 22 Active Channel 55 ADF 13 14 62 91 92 Advisory alerts 66 AHRS 83 84 Airport Signs 51 52 Airways 95 AOPA s Airport Directory 54 AP 67 Assist engine leaning 10 12 Audio panel controls NAV1 NAV2 14 Audio panel fail safe operation 61 Autopilot 67 Auxiliary video 57 Barometric Altitude Minimums 3 Barometric pressure 92 C Carbon monoxide detection 7 CDI 2 14 86 Channel Presets 56 ChartView 52 53 Checklists 59 60 Clearance player 14 Clearance Recorder 14 Code selection softkeys 13 COM 14 61 Cylinder Head Temperature CHT F 5 8 D Databases 96 Database updates 96 97 98 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Index DCLTR Softkey 52 Dead Reckoning 62 Declutter 62 89 95 Declutter EIS 8 Direct to 21 DME 13 14 DR mode 62 63 64 E Edit a flight plan 35 Electronic checklists 59 60 Emergency checklist 60 Enable Terrain 48 Endurance calculated ENDUR 8 Engine leaning assist 10 12 Engine Manifold Pressure MAN IN HG 5 6 Exhaust Gas Temperature EGT F 5 8 10 11 F Fail safe operation 61 FD 67 Flight Director 17 Flight path marker 51 FliteCharts 52 53 Frequency Transfer 14 Fuel calculations 8 Fuel Flow FFLOW GPH 5 6 10 Fuel flow totalizer 8 Fuel quantity FUEL QTY GAL 5 6 Fuel remaining 94 Fuel remaining calculated GAL REM 8 Fuel used calculated GAL USED 8 H Horizon hea
39. 4 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 57 2 Buluueld AeN Sd5 S24V oipny uadx sia siu u nnsul fila Tu102 AEN UTE eouepioAy paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Nav Com XPDR Audio Hazard Additional Features Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Procedures Avoidance Appendix Alerts Operation Index Additional Features GARMIN Display Selection Pressing the HIDE MAP Softkey removes the map and displays video on the full screen The softkey label changes to grey with black characters Pressing the HIDE MAP Softkey again restores the map view and the small video image The softkey label returns to white characters on a black background Input Selection While on the AUX VIDEO Page press the INPUT Softkey to select the EVS or AUX video source Zoom Range Pressing the VID ZM or VID ZM Softkeys increases or decreases video display magnification between 1x and 10x The RANGE Knob can be used to increase or decrease the range setting on the map display or zoom in and out on the video display While in the Split Screen mode pressing the MAP ACTV or VID ACTV Softkey determines which display the RANGE Knob adjusts Pressing the softkey to display MAP ACTV allows the RANGE Knob to control the range setting of the map display Pressing the softkey to di
40. 5 Once all changes have been made press the FMS Knob to remove the cursor 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 35 sjuauimasu nubi 59 olpny uqax 0105 AEN 52 2 AEN 540 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning A GARMIN INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Tur the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan 4 confirmation window is
41. 60 psi Single Chime None Oxygen outlet pressure below 16 5 psi Single Chime None Oxygen quantity below 250 psi Rudder limter is engaged Starter relay has power applied Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 65 s m 2 buluueld AEN Sd5 52 olpny uqax sia sjuauimasu 2 nubi uio AeN 1i euonippv uoneiedo jJeuuouqv dd EE x pul Annunciations 8 Alerts A GARMIN 2 ANNUNCIATION ADVISORY t Annunciation Window Alerts Window Message Audio Alert Text 8 AP TRIM OFF AP TRIM master switch is in the OFF position None OXYGEN ON Reminder Tum off oxygen None E RUDR HOLD Rudder hold is engaged None 2g SPEED BRAKES Speed brakes are active None Corvalis TT only MESSAGE ADVISORY ALERTS 8 Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative one 2 MED FAN FAIL The cooling fan for the MFD is inoperative one AVIONICS FAN The cooling fan for remote avionics is inoperative one TIMER ZERO Timer has counted down to zero Timer Expired Procedures FUEL IMBAL Fuel imbalance is greater than 10 gallons one LOW MAN PRES Manifold pressure is below 15 in one VAPOR SUPPR Turn on Vapor Suppression one Hazard Avoidan
42. A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 11 Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS GPS Nav Procedures Appendix Alerts Operation Features Index Engine Indication System Corvalis TT A GARMIN Once the ASSIST Softkey is selected the peak of each TIT is indicated by a light blue bar which moves and remains at the peak Turbine Inlet Temperature Peak TIT TEHPERATURE 1608 1450 1300 1158 1990 Lean or Rich T T Deviation From Peak Peak Engine Leaning Assist Mode Corvalis TT Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL 1 Select the ADF DME Softkey 2 Turn the small FMS Knob to enter the first digit of the desired ADF frequency 3 Turn the large FMS Knob to select the next desired field 4 Turn the small FMS Knob to enter the desired number 5 Repeat steps 3 and 4 until the desired ADF frequency is entered 6 Press the ENT Key to accept the new frequency 7 Press the ENT Key again to transfer the frequency to the active field 8 Turn the large FMS Knob to select the MODE field 9 Turn the small FMS Knob to select ANT ADF ADF BFO or ANT BFO 10 Press the ENT Key to complete the selection DME TUNING OPTIONAL 1 Select the ADF DME or DME So
43. A condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained right force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test Performing preflight system test Upon completion the aural alert will be heard Preflight system test has fai 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 67 Sjueuingjsu iui saunyea4 aoueplony saunpa20Jd Fuluueld AEN SdD 2 olpny uqax si paezey 346 3 u102 AEN jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix nd Annunciations amp Alerts TERRAIN SVS ALERTS A GARMIN PFD MFD Alert Type TERRAIN SVS MFD Aural yp Page Pop Up Alert Message Annunciation Reduced Required Terrain TERRAIN WARNING TERRAIN Warning Terrain Clearance Warning RTC Terrain Imminent Terrain Impact TERRAIN Waring Terrain Warning ITI Terrain Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Wa
44. AF 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 Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select the available softkeys to select the desired XM weather product 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 43 AEN 540 S24V orpnyyuqax sia Sjueumajsul Tuo2 AEN fid Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 4 Select the LEGEND Softkey to view the legends for the selected products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARs SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport
45. AN 1 After creating a flight plan on either the PFD or MED it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD and turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Select the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location 6 Enterthe changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD and turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window Flight Planning 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
46. CS XPDR Audio EIS Instruments Appendix Index A Appendix GARMIN TRAFFIC Cycles through traffic display options TRFC 1 Traffic displayed on inset map TRFC 2 Traffic Map Page is displayed in the inset map window TOPO Displays topographical data e g coast lines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature D n nN S OODD HU 75 75 058 n synvis pets wmo DME BRet ctunrr sto BARo BACK ALERTS n n T LA m Select the BACK Softkey to return to the top level softkeys r mon r en zen BL HE ML r ooo r PFD Configuration Softkeys 90 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN PFD SYN VIS PATHWAY SYN TERR HRZN HDG APTSIGNS DFLTS WIND OPTN I OPTN 2 OPTN3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI Appendix Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays
47. DR 92 BRG2 Cycles the Bearing 2 Information Win dow through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency ALT UNIT Displays softkeys for setting the altimeter and BARO settings to metric units METERS When enabled displays altimeter in meters IN Select to display the BARO setting as inches of mercury HPA Select to display the BARO setting as hectopacals STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa 1 C rz CPR er pent rvanerl vest atenrs r n F rnm v n mn n mu n E Press the BACK Softkey to return to the top level softkeys ETT IE TT De Ese Sex er Ev 75 5 73 75 77 75 77 74 74 7 7 Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to interrogations Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN ALT GND VFR CODE 0 7 BKSP IDENT TMR REF NRST ALERTS Appendix Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatica
48. E ADVISORIES CONT Message MAG VAR WARN Large magnetic variance Verify all course angles Comments The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOCI LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be reinserted PFD1 or MFD1
49. G 1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Corvalis Corvalis TT M CESSNA CORVALIS CESSNA CORVALIS TT A GARMIN Copyr This m Corva inform ight 2006 2010 Garmin Ltd or its subsidiaries All rights reserved anual reflects the operation of System Software version 0534 15 or later for the Cessna is Corvalis TL Some differences in operation may be observed when comparing the ation in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 91 3 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmi T and in Web S Except n Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 or after hours emergency aircraft on ground AOG technical support for Garmin panel mount tegrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 ite Address www garmin com 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 per
50. G STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Select the PFD Softkey 2 Select the STD BARO Softkey to set standard barometric pressure CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Select the HPA Softkey to display the barometric pressure setting in hectopascals 4 Select the BACK Softkey to return to the top level softkeys CHANGE ALTIMETER AND SELECTED ALTITUDE DISPLAY UNITS 1 Select the PFD Softkey to display the second level softkeys 2 Select the ALT UNIT Softkey 3 Select the METERS Softkey to add or remove the metric units display for the altimeter and selected altitude 4 Select the BACK Softkey to return to the top level softkeys 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 1 sual uonesado So1nje2J aoueplony SoJnpa20Jd Buruue d AEN Sd5 2 oipny uddx sia junuuy jeuuouqy paezey nubi u102 NEN xipueddy x pul A Flight Instruments GARMIN CHANGE NAVIGATION SOURCES iz T Instruments 1 Select the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Select the CDI Softkey again to change from VOR1 or LOC1 to VOR
51. IN DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL THE ACTIVE NAVIGATION DATABASE REGION CYCLE FROM TO WORLDWIDE WORLDWIDE 8912 6913 EFFECTIVE 19 NOU 2009 is ee EXPIRES NO WILL 17 DEC 2889 14 BE ASSUMED IN 28 SECONDS UPDATING NAUTBATIDN DATABASE PLEASE WAIT 4 5 6 7 8 9 10 11 Navigation Database Load Prompt Press the YES Softkey to update the navigation database in the MFD After the update completes the display starts in normal mode Turn the G1000 system OFF and remove the SD card from the top card slot Repeat steps 2 through 6 for the PFD Apply power to the system and press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show navigation database information for each display MFD1 DB and PFD1 DB MFD1 DATABASE NAVIGATION INTERNAL REGION WORLDWIDE CYCLE 0313 EFFECTIVE 17 DEC 09 EXPIRES 14 JAN 10 Copyright 2009 Jeppesen Sanderson Inc BASEMAP BOTTOM CARD REGION WORLDWIDE VERSION 3 00 GARMIN LTD AND ITS SUBSIDIARIES 2008 SAFETAXI BOTTOM CARD REGION VERSION Check Database Cycle Number MFD shown Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN A Activate a flight plan
52. IN A FLIGHT PLAN 1 Press the FPL Key 2 Press the FMS Knob to activate the cursor not required on the PFD 3 Turn the large FMS Knob to highlight the waypoint after the desired airway entry point If this waypoint is not a valid airway entry point a valid entry point should be entered at this time 4 Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 33 oipny uddx 59 sjuaumnasu U10 AEN 16114 52 SoJnpa204d Buruuejd AEN Sd5 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 5 6 7 A GARMIN Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list
53. Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The G1000 system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The G1000 system should be serviced when possible AHRS1 GPS AHRS1 not receiving any GPS information AHRS1 GPS AHRS1 not receiving backup GPS information 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 AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The G1000 system should be serviced AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The G1000 system should be serviced GMU 44 MESSAGE ADVISORIES Messag
54. N sirin optem ot Available Excessively degraded arta Sete GPS signal or out of TER N A None 7 ot Available database coverage area Suffident GPS signal received after loss or Terrain System None None ET database coverage area Available entered TAWS B ALERTS PFD MFD MFD Alert Type 1 TAWS B Page Aural Message E Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up TERRAIN PULL UP TRO Terrain Terrain Pull Up Pull Up Reduced Required PULL UP OBSTACLE PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up Warning ROC OBSTACLE AHEAD PULL UP or Obstacle Ahead Pull Up Obstacle Ahead Pull Up 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 69 sainjea4 2 Duruue d AEN Sd5 S241V olpny uqax sia sjuauimasu 2 nubi u102 AEN Yid jeuonippy uoneiedo Jeuuouqy s PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Appendix Index Annunciations amp Alerts A GARMIN
55. Press the FMS Knob to remove the flashing cursor Flight Planning CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Tum the small FMS Knob to select RAD DIS radial distance 9 Press the ENT Key 10 The cursor moves to the REFERENCE WAYPOINTS field With the first vvaypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select th
56. T Key Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable TAWS 3 Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION OPTIONAL WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational aware ness only and may not provide either the accuracy or reliability upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision System SVS functionality is offered as an optional enhancement to the G1000 system SVS is primarily comprised of a computer generated forward looking attitude aligned view of the topography immediately in front of the aircraft from the pilots perspective SVS information is shown on the primary flight display PFD In addition to SVS enhancement to the PFD the following features have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting Three dimensio
57. URATION ID 4 OE 27000008 202d CRG PART NUMBER 190 00567 04 SYSTEH ID 00000000A 47801548 105 j CHECKLIST NOT AVAILABLE EDLE3 47801373 1 05 1 47750372 30200 MEDI DATABASE VERSION 1 21 Fi Fi 6141 45701311 2 07 CYCLE 0903 6142 45701913 207 15 JUL 09 GHA FFFFFFFFF 1 02 EXPIRES 14 OCT 09 GHU1 68500319 1 02 Copyright 2009 Aircraft Owners and Pilots Assn CHART BOTTOM CARD CHART FliteCharts GPS1 48400000 3 01 GPS2 48900001 3 01 REBTON US 6851 2024 CYCLE 0925 651 47500583 2 01 EFFECTIVE 07 MAY 09 552 47500607 2 01 EXPIRES 04 UN 09 DISABLES 1 DEC 29 Copyright 2009 Garmin Ltd or its subsidiaries GSA PTCH CTL 680062149 23 AFTM Display Database Selection Softkey AUX System Status Page The Display Database Selection Softkey is used to place the cursor in the Database Window Upon first press of the Display Database Selection Softkey the softkey will change to a selected state black text on gray background and the cursor will appear in the Database Window At this point the user can scroll through all databases in the Database Window to view status information If the Display Database Selection 96 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN 0 Hppendix Softkey is pressed repeatedly the softkey will switch between PFD1 and MFDI Database status information in the Database Window will reflect the database
58. ___ Baal indication System L FUEL QTY GAL R FUEL QTY GAL 1900 1750 1600 z 1450 m 300 1300 1 1150 3 n Arie 100 1000 SYSTEM OXYGEN DEC FUEL INC FUEL RST FUEL Engine Page Corvalis TT Carbon Monoxide Detection If carbon monoxide CO in the cabin becomes too high exceeds 50 ppm a flashing red annunciation and the current level of CO in parts per million ppm are displayed in the lower right corner of the Engine Page When a warning is generated the CO RST Softkey becomes available to reset the CO Guardian and acknowledge the alert 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 7 sjueuinasu x Suelv uoneiedo saunjea4 SoJnpa20Jd buluueld AEN 540 S24V junuuy jeuuouqy feuonippv xipuaddy x pul sufi t a 3 bid paezey Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine Indication System GARMIN Fuel Calculations Group NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset Fuel used GAL USED endurance ENDUR and range RANGE NM are all calculated based on the displayed fuel remaining GAL REM and the fuel flow totalizer T
59. be available The G1000 system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer Switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation If the problem persists the G1000 system should be serviced 6 51 FAIL G S1 is inoperative 6 52 FAIL 6152 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The G1000 system should be serviced 78 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations amp Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may G S2 SERVICE G S2 needs service Return unit for repair still be available The G1000 system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The G A1 and or GIA2 configuration settings do not match backup configuration memory The G1000 system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG
60. bine Inlet Cylinder Head Temperature Temperature buluueld nubi HE Temperate E T DUM 1626 1428 1428 378 348 374 1 zi 1900 1642 1740 1674 508 364 360 366 H 1750 1500 1450 a d 1300 1150 ge Engine Temperature Group Corvalis TT xipuaddy suelv uoneiedo junuuy jeuuouqy x pul 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 9 GARMIN ENGINE LEANING ASSIST MODE NOTE Consult the Cessna Corvalis Corvalis TT Aircraft Flight Manual AFM for leaning procedures From the Engine Page the Engine Leaning Assist Mode may be accessed by selecting the ASSIST Softkey Selecting the ASSIST Softkey again returns the MFD to the Engine Page Use the SYSTEM Softkey to exit the Engine Page While in Assist Mode the EIS Display is shown along with the Fuel Flow Gauge and an expanded Engine Temperature Group Corvalis When the ASSIST Softkey is selected the system initially highlights the number and EGT readout of the cylinder with the hottest EGT Fuel Flow Gauge nav1188 88 113 00 TRK357 134 888 118 800 con navz 108 00 118 68 S ENGINE 193 800 118 000 conz FFLOM GPH EGT Deviation 1 2 from Peak TEMPERATURE EGT CHT F F 1562 1382 1202 356 338 320 16521472 92 500 292 320 374 1900 1750 1600 bi 400 1450 300 ME 200 1150 1000 100 7572 3456 DELTR DEC FUEL INC FUEL RST FUEL Engine Leaning Assist Mode Co
61. ble to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on system displays is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic
62. ce Corvalis TT only Additional Features CO GUARDIAN MESSAGES zs Alerts Window Message Comments f CO DET SRVC The carbon There is a problem within monoxide detector needs the CO Guardian that service requires services CO DET FAIL The carbon Loss of communication monoxide detector is inopera between the 61000 and tive the CO Guardian Index Appendix Ea 66 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN amp Aleris AFCS ALERTS Condition Annunciation Description Pitch Failure PT CH Pitch axis control failure AP is inoperative Roll Failure Roll axis control failure AP is inoperative MET Switch Stuck or f annunciated when AP is engaged take control Pitch Trim Axis Control of the aircraft and disengage the autopilot If Failure annunciated when AP is not engaged move each half of the MET switch separately to check if a stuck switch is causing the annunciation System Failure AP and MET are unavailable FD may still be able Elevator Mistrim Up A condition has developed causing the pitch rvo to provide a sustained force Be prepared apply nose up control wheel force upon topilot disconnect Elevator Mistrim Down condition has developed causing the pitch rvo to provide a sustained force Be prepared apply nose down control wheel force upon autopilot disconnect Aileron Mistrim Left
63. ct the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select the SET Softkey 4 Select any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 With the XM Radio Page displayed select the VOL Softkey 2 Select the VOL Softkey to reduce volume or select the VOL Softkey to increase volume Once the VOL Softkey is selected the volume can also be adjusted using the small FMS Knob 3 Select the MUTE Softkey to mute the audio Select the MUTE Softkey 56 again to unmute the audio Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN AUXILIARY VIDEO OPTIONAL Additional Features There are four modes of operation of the optional auxiliary video display Full Screen Full Screen with Digital Zoom Split Screen with Map and Split Screen with Map and Digital Zoom Displaying auxi
64. d 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 Cessna Corvalis Corvalis TT 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 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 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Wamings cantons amp Notes GARMIN WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our webs
65. ding 51 ndex 1 uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy Ju105 AEN jeuuouqy Sue v unuuy iui nuru paezey Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts es Appendix Index Inhibit TAWS 50 Inhibit Terrain 48 Inset Map 89 90 IOI 68 70 J Jeppesen 53 M Map panning 44 Message advisories 72 88 MET 67 METAR 43 Minimums 72 Mistrim 67 MKR MUTE 14 Mode 5 93 Mode selection softkeys 13 Multi Function Display MFD Softkeys 94 N NAV 14 NAV1 2 14 NAV2 2 14 Navigation database 23 24 NEXRAD 43 44 90 95 0 OBS 2 Obstacles 75 80 Oil Pressure OIL PSI 5 6 Oil Temperature OIL F 5 6 Overspeed Protection 18 Oxygen Outlet Pressure OXY OUTLET PSI 6 Oxygen Quantity OXY QTY PSI 6 Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT A GARMIN P Pathways 51 52 Power up page 59 R Reversionary mode 61 ROC 68 69 70 S SafeTaxi 52 Secure Digital SD card 59 Secure Digital SD cards 96 Store Flight Plan 35 Supplemental Data Card 97 98 SVS 51 88 SVS Terrain 51 Synthetic Vision System 51 T TA 72 Tachometer RPM 5 6 TAF 43 TAS 46 72 83 TAWS 49 50 69 Terrain 46 47 49 75 90 95 Terrain SVS 47 48 Timer 85 Top
66. e Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The G1000 system should be serviced MANIFEST GMU1 software mismatch communication halted The GMU 44 has incorrect software installed The G1000 system should be serviced 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 83 soJnjeaJ 2 Buruuejd AEN 5649 24V oipny uadx sia 2 u102 NEN nubi jeuonippy uoneiedo Jeuuouqy 3 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix en Annunciations amp Alerts GDL 69A MESSAGE ADVISORIES A GARMIN Message GDL69 CONFIG GDL 69 config error Config service req d Comments GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced GDC 74A MESSAGE ADVISORIES Message C
67. e approaches only Approach GPS GPS Approach VOR Capture Track aplures and tracks Ue Apr VAPP selected navigation source Approach LOC Glideslope GPS VOR LOC Key 25 M LOC Mode automatically armed Disengages the autopilot GA Go Around and commands a constant Switch GA 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 19 sia Sjueumansu oipny uadx 0105 AEN ARN Sd5 52 suelv uoneiedo s m aoueplony 2 Duruue d Junuuy jeuuouqy jeuonippy xipueddy x pul iui Wfi l4 paezey A GARMIN AFCS Sjueuinijsu fila 59 Tu102 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 20 A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to E Key 2 Enter the waypoint identifier 3 Press the ENT Key to confirm the identifier The Activate field is highlighted 4 If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude
68. e desired waypoint Press the ENT Key 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 29 sjuauimasu nubi oipny udax si U105 AeN 52 s mp ooud buluueld AEN Sd5 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning GARMI N Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The cursor is displayed in the RAD radial field Enter the des
69. e of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the ovm aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored t is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS SBAS Mode due to the lack of satellite measureme
70. e speed Appendix Index 2 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN 4 5 6 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob clockwise to ON or counterclockwise to OFF To remove the window press the CLR Key or the TMR REF Softkey SET BAROMETRIC MINIMUM DESCENT ALTITUDE 1 Select the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or select the TMR REF Softkey DISPLAYING WIND DATA 1 Select the PFD Softkey 2 Select the WIND Softkey to display wind data to the left of the HSI 3 Select one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window select the OFF Softkey CHANGING HSI FORMAT 1 Select the PFD Softkey 2 Select the HSI FRMT Softkey 3 Select the 360 HSI Softkey to display the full size HSI Or Select the ARC HSI Softkey to display the arc style HSI 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Flight Instruments 3 mal ED g 2 a xipueddy Suelv uoneiedo sainjea4 aoueplony 2 Duruue d AEN
71. eN nubi paezey unuuy GARMIN ENGINE PAGE Selecting the SYSTEM Softkey on the MFD accesses the Engine Page which displays all Engine Indication System instruments selecting the softkey again exits the Engine Page Oxygen quantity and outlet pressure are also shown on the Engine Page The OXYGEN Softkey can be used to turn the optional oxygen system on off If an oxygen system is not installed blank gauges are displayed D d 135 975 118 088 cor 136 975 118 009 con I 15 N 10 20 S TE MAN IN HG RPM 25 1 2300 FUEL CALC GAL REH ENDUR 98 3 5 48 GAL USED RANGE NH 930 19 y A 17 0 L FUEL QTY GAL A 21 30 10 TEHPERATURE 4 ELECTRICAL ya EBT F 1724 1834 1552 CHT F 338 356 amp TATS GATT SUS voLTs agg 165215801508 NEED 702 1750 1600 1450 1300 1150 l AILERON Y EI S Carbon CO LVL HIGH PPH 550 Monoxide DCLTR ASSIST ca Warning Engine Page Corvalis O Oil Temperature Pressure Gauge O Electrical Group Engine Manifold Pressure Gauge Trim Group 0 Tachometer Engine Temperature Group Fuel Calculations Group Fuel Quantity Gauges QR Quantity Gauge Corvalis Fuel Flow Gauge TT only Oxygen Outlet Pressure Gauge Low Pressure Gauge shown High Pressure Gauge optional Corvalis 1T only 6 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A amp GARMIN _
72. ed Stormscope 190 00567 04 Added Tach Timer Added Flight Plan Import Export Added AOPA Airport Directory Added Auxiliary Video Added temporary user waypoints Added CDI availability during Dead Reckoning mode Added new MFD page navigation Added other GDU 10 01 parameters z sl Date of Revision Affected Pages 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT RR 1 Record of Revisions GARMI Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 5 1 Change Altimeter Barometric Pressure Setting Units 1 Change Altimeter and Selected Altitude Display Units V 1 Change Navigation Sources ssssssssseeeeennnnnnnnns 2 Enable Disable OBS Mode While Navigating with 6 5 5 2 Generic Time cL or e p RO a re s mi dd duda 2 Configure Vspeed Bugs 2 Set Barometric Minimum Descent 2 3 Displaying Wind Data 3 Changing HSI Format nennen 3 ENGINE INDICATION SYSTEM 5
73. errain SVS alerts are inhibited vvhen the Final is the 48 active waypoint in a GPS SBAS approach a LOVVALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Hazard Avoidance TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north or 60 degrees south NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwi
74. erviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The G1000 system should be serviced MANIFEST GMAT software mismatch communication halted he audio panel has incorrect software installed service Return unit for repair GMA1 SERVICE GMA1 needs 1 The G1000 system should be serviced 1 he audio panel self test has detected a problem n the unit Certain audio functions may still be available and the audio panel may still be usable he G1000 system should be serviced when pos sible a GIA 63 MESSAGE ADVISORIES Message Comments GIA1 CONFIG GIA1 config er Config service req d ror he G A1 and or GIA2 configuration settings GIA2 CONFIG GIA2 config er Config service req d ror e o not match backup configuration memory he G1000 system should be serviced G error Config service req d A1 CONFIG GIA1 audio config he GIA1 and or GIA2 have an error in the G error Config service req d A2 CONFIG GIA2 audio config ab udio configuration The 61000 system should be serviced GIA1 COOLING temperat too low GIA2 COOLING GIA2 temperature The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature t
75. ftkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 Select the XPDR Softkey to display the transponder mode selection softkeys Nav Com XPDR Audio Panel 2 Select the CODE Softkey to display the transponder code selection softkeys for digit entry 3 Select the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 13 sjueumasu S24V orpnyygqax si JUI05 AEN uoneiedo sainjea4 aoueplony 2 Duruue d AEN Sd5 Jeuuouqy Jeuonippy paezey xipuaddy x pul iui Wfl unuuy Flight Instruments Nav Com AFCS XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio pane
76. g the aircraft on the ground This database is updated on a 56 day cycle ChartView Optional ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 00567 04 Rev A Garmin G1000 Cockp
77. h Cap ures and tracks the SBAS GP glidepath on approach m Captures and tracks the ILS Glideslope GS glideslope on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude GA Switch and wings level in the air ALTS armed automatica ly when PIT VS FLC or GA active and under VPTH w is to be captured instead of VNAV Target Altitude ALTV armed automatically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude GP is available in installations with GIA 63W IAUs when SBAS is available 18 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT en Selected Altitude 190 00567 04 Rev A A GARMIN pitch angle and wings level AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds the current aircraft roll Roll Hold attitude or rolls the wings default ROL level depending on the commanded bank angle Captures and tracks the HDG Selected Heading Key 0 Navigation GPS GPS Navigation VOR Enroute Captures and tracks the 7 VOR Capture Track selected navigation source Navigation LOC Capture Track GPS VOR LOC NAV T No Glideslope Key Navigation Bakcouse gal fr ic Capture Track GDU 1044 only g backcourse approaches Captures and tracks 7 Backcourse GDU 10448 only a localizer signal for 10448 BC backcours
78. he cursor and turn the large FMS Knob to highlight the desired waypoint On the MFD select the ACT LEG Softkey Or Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN STOP NAVIGATING A FLIGHT PLAN GPS Navigation 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN 190 00567 04 Rev A 221 221 11 7NH 13000FT 9 2 12400FT 8 0NH Approach KDFH RNAV 17LePs LPV RIVET iof DRAAK TNWOD RW17L map 930FT POLKE RISE Cross AT or ABOVE 5 000 ft VA L D R Cross AT 2 300 ft iin Cross AT or BELOW 3 000 ft 259 176 176 176 176 174 9900 Large W
79. he fuel remaining can be adjusted using the following softkeys DEC FUEL Decreases totalizer based fuel remaining in one gallon incre ments INC FUEL Increases totalizer based fuel remaining in one gallon increments RST FUEL Resets totalizer based fuel remaining to the aircrafts fuel capacity 98 gal or 102 gal usable and sets the GAL USED display to zero Fuel Endurance Remaining ENDUR Calculation 79 6 4 40 Fuel Used R calan 7 NH Calculation Fuel Calculations Group Engine Temperature Group The temperature group displays the Cylinder Head Temperature CHT and Exhaust Gas Temperature EGT in degrees Fahrenheit for each cylinder using bar graphs and digital readouts For the Corvalis TT Turbine Inlet Temperature TIT is shown on a sliding bar scale The following softkeys can be used to modify the display of engine temperature information DCLTR Removes displays the EGT and CHT readouts from the display ASSIST Accesses the Engine Leaning Assist Mode 8 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Engine Indication System Cylinder Head lemperature Sjueuingjsu nubi Exhaust Gas TEMPERATURE EGT F CHT F Temperature 174616141726 370 366 354 16801658 1702 1988 1750 1500 1450 1300 1150 1000 E Engine Temperature Group Corvalis 3g BES BO 84 52 AEN 540 Tur
80. he large FMS Knob to highlight the LEG field d Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 25 oipny uddx 59 sjuauimnasu U105 AEN 16114 52 2 AEN 540 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 26 6 7 8 9 10 11 12 13 A GARMIN Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing curs
81. hite Text Large Light Blue Text _ Small Lig Blue Text Small Light Blue Subd Text Small Wh t ed with Altitude Restrictio Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Bar ite Text 23 siu uinnsu sub 59 oipny uadx 0105 AEN suelv uoneiedo sainjea4 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Nav Com XPDR Audio GPS Nav AFCS Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS Procedures Appendix Alerts Operation Features Index A GARMIN Altitudes associated with approach procedures are auto designated This means the system automatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may also be
82. ield and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check flygarmin com for the current database View Airport Directory Information While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display 54 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Additional Features XM RADIO ENTERTAINMENT OPTIONAL The XM Radio Page provides 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 Knob to select XM Radio 3 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category
83. in the top card slot to the displays internal memory Loading Updated Databases In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features Loading the Garmin database updates 1 With G1000 system power OFF remove the SD card from the bottom card slot of each display 2 Using a personal computer update the Garmin databases on each SD card FliteCharts or ChartView databases are copied to the MFD SD card 3 After all database cards are updated insert each database SD card into the bottom card slot of the appropriate display 4 Apply power to the G1000 system check that the databases are initialized and displayed on the power up screen 98 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN 0 Appendix 5 6 1 8 DATABASE V Checklist File N A Busemup Land 2 00 SafeTaxi N A Terrain Data N A de Airport Terrain Data N A gt lt Obstacle Data N A 7 Apt Directory N A BY Chart Dato N A All map and terrain data provided is only to be used as d general reference to your surrounding und as an aid to situational awareness Database Information on the Power up Screen Acknowledge the Power up Page agreement by pressing the ENT Key
84. information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Recent of Restsinns Change Summary 190 00567 00 Rev A Production release Rev B Added C350 parameters TAWS changes and Stormscope 190 00567 01 Rev A Added GDU 8 10 parameters WAAS VNAV Airways and Charts Rev B Changed company references to Cessna 190 00567 02 Reformatted manual Added GDU 9 03 parameters 190 00567 03 Added GDU 9 05 with Synthethic Vision System SVS Remov
85. ios and music PILOT KEY COPLT KEY Pilot Hears Copilot Passenger ANNUNCIATOR ANNUNCIATOR Hears Hears PILOT Selected radios pilot copilot passengers music radios pilot Selected radios pilot OFF ON passengers music Selected CREW ON ON radios pilot copilot 190 00567 04 Rev A Selected radios pilot copilot passengers music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Nav Com XPDR Audio Panel 15 Sjueuinajsu nubi 59 S24V oipny uddx JUI05 AEN sual uonesado s n e 4 eouepioAy s mp oold Buruue d AEN Sd5 junuuy jeuuouqy Jeuonippy paezey nubi xipueddy x pul A Nav Com XPDR Audio Panel GARMIN Flight Instruments EIS Nav Com KA m x a o E GPS Nav AFCS Flight Planning Blank Page Annun Abnormal Additional Hazard Alerts Operation Features Avoidance Procedures Appendix Index 16 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM AFCS NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director
86. ired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor DELETE A USER WAYPOINT 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 30 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN ri ht tanning 4 5 6 1 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field Turn the small FMS Knob to highlight the desired waypoint Press the DELETE Softkey The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu al
87. it Reference Guide for the Cessna Corvalis Corvalis TT 53 s mp o4d Buluueld AeN Sd5 S24V olpnyyuqax sia siu u nnsul Wfil4 Tu102 AEN 346 2 s m e q jeuonippy xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Select the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Select the GO BACK Softkey to return to the previous page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Tum the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options 4 Turn the small FMS Knob to choose between the On and Off Full Screen Options 5 Turn the small FMS Knob to choose between Day Auto and Night Options 6 In Auto Mode tum the large FMS Knob to select the percentage f
88. ite at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners 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 ser
89. l SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field DIGITAL CLEARANCE RECORDER AND PLAYER NOTE Only the audio for the selected COM MIC Key is recorded Audio is not recorded for COM3 MIC Pressing the PLAY Key once plays the latest recorded memory block then returns to normal operation 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 begins playing the next previously recorded block Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Com rad
90. liary video 1 Turn the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select VIDEO and display the AUX VIDEO Page The video display softkeys shown below appear on the AUX VIDEO Page Control of the AUX VIDEO Page can also be accessed through the Page Menu Selecting video menu options 1 While viewing the AUX VIDEO Page press the MENU Key to display the Page Menu OPTIONS 2 Turn the large FMS Knob to highlight the desired video adjustment option and press the ENT Key Once the ENT key is pressed on any option the page menu closes and returns to the AUX VIDEO Page Video Setup Video brightness contrast and saturation may be adjusted be selecting the setup function While viewing the setup function softkeys after 45 seconds of softkey inactivity the system reverts to the AUX VIDEO Page softkeys Adjusting the video settings 1 With the AUX VIDEO Page displayed press the SETUP Softkey 2 Press the BRIGHT or BRIGHT to adjust display brightness in five percent increments from 0 to 10096 3 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 10096 4 Press the SAT or SAT to adjust display saturationin five percent increments from 0 to 10096 5 If desired return the display to the default settings by pressing the RESET Softkey 6 Press the BACK Softkey to return to the previous softkey level 190 00567 0
91. ll correct aviation database type in all displays DB MISMATCH Terrain database version mismatch The PFDs and MFD have different terrain database versions installed Install correct terrain database version in all displays DB MISMATCH Terrain database type mismatch The PFDs and MFD have different terrain database types installed Install correct terrain database type in all displays DB MISMATCH Obstacle database version mismatch The PFDs and MFD have different obstacle database versions installed Install correct obstacle database version in all displays DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrrain databases installed Install correct airport terrain database in all displays 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 15 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubiu UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy 3 PE x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 2 Annunciations 8 Alerts A GARMIN GMA 1347 MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The G1000 system should be s
92. lly enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 Use numbers to enter code Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 93 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu Jeuonippy nubi Tuo2 NeN ui uoneiedo Jeuuouqy Sue v unuuy End Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix MFD SOFTKEY MAP Press the SYSTEM Softkey to Fk FN A 7 F wo return to the default page level optional A GARMIN SHW CHRT A optional optional Default softkey is dependant on Press the BACK Softkey on this the selection made level to return to the top softkey level options optional optional TRAFFIC TOPO TERRAIN AIRWAYS lt NEXRAD XM LTNG BACK SYSTEM OXYGEN DCLTR ASSIST CORST DEC FUEL INC FUEL RST FUEL mre on SYSTEM SYSTEM OXYGEN DCLTR ASSIST CO RST DEC FUEL INC FUEL RST FUEL The CHECK
93. lowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 31 oipny uddx s q sjuauimnasu U10 AEN 346 3 52 2 4 AEN 540 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance
94. made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude GPS Navigation White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance Small Text Altitude is not designated Altitude is designated The system cannot to be used in determining for use in giving vertical use this altitude in vertical flight path flight path guidance determining vertical 24 guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude i
95. mission of Garmin Garmin hereby grants permission to down other oad a single copy of this manual and of any revision to this manual onto a hard drive or electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must conta notice revision hereto is strictly prohibited Garmi n the complete text of this copyright hat any unauthorized commercial distribution of this manual or any ot and provided furthe n and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark o Satelli f Jeppesen Inc XM is a registered trademark of XM te Radio Inc August 2010 190 00567 04 Rev A Printed in the U S A Warnings Cantans amp Notes GARMIN WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not a
96. n the navigation database Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT flight path guidance 190 00567 04 Rev A GARMI N LLL RHlght Planning FLIGHT PLANNING 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 select the AUTO or MANUAL Softkey 4 For Direct to planning a Select the WPTS Softkey and verify that the starting waypoint field indicates P POS present position b If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Press the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn t
97. nal Traffic Airport Signs e Runway Display Displaying SVS Terrain 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 Select the SYN TERR Softkey 4 Select the BACK Softkey to return to the previous page 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 51 xipueddy suelv uoneiedo sainyea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN iui x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A GARMIN Displaying Pathways 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the PATHWAY Softkey 5 Select the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the HRZN HDG Softkey 5 Select the BACK Softkey to return to the previous page Displaying Airport Signs 1 Select the PFD Softkey 2 Select the SYN VIS Softkey 3 If not already enabled select the SYN TERR Softkey 4 Select the APTSIGNS Softkey 5 Select the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS
98. nts needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 63 sjuauinajsu Wfl Buluueld AEN 540 S24V oipny udax TL aoueplony paezey saunyea4 jeuonippy xipueddy Suelv unuuy x pul Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning EIS AFCS GPS Nav Avoidance Procedures Features Annun Appendix Alerts Index Abnormal Operation GARMIN As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD e Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up
99. nusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glide e AFCS Annunciations PFD Setup Menu path and Vertical Flight director Com Windows displayed in Deviation Indicators mand Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box ADF DME Tuning Transponder Status Barometric Minimum Box Descent Altitude Box Extreme Pitch Indication DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position 62 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Abnormal Operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phas
100. o d When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN 12 Press the ENT Key 13 Repeat step 10 to enter the next waypoint name 14 Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16
101. oach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CD for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 86 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISOR ES CONT Message PTK FAIL Parallel track unavailable bad geometry Comments Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV
102. ographical data 90 95 Traffic 43 45 95 Traffic advisory 45 72 Traffic map page 45 46 47 Transponder 13 92 93 Trim 5 6 Turbine Inlet Temperature TIT F 5 12 V Vertical speed guidance 24 Vertical track 72 190 00567 04 Rev A A GARMIN Video 57 VNV 21 62 87 Vspeed 2 W Waypoint Selection Submenu 31 32 Weather data link page 43 Wind data 91 X XM lightning 90 95 XM weather 43 Z Zoom Window 58 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Index Index 3 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sia sjuauimasu Jeuonippy nf JUI0 NEN nubi uoneiedo Jeuuouqy Sue v unuuy GARMIN index Sjueuinijsu sub 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy mu 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Index 4 A GARMIN Garmin International Inc 1200 East 1 51 st Street Le 66062 U A ud AU a 5040 9RB n No 68 Jangshu 2nd Shiir Taipei County 2006 2010 Garmin Ltd or its subsidiaries 190 00567 04 Rev A
103. omments MANIFEST GDC1 software mismatch communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced GCU 476 MESSAGE ADVISORIES Message Comments GCU CNFG GCU Config error Config service req d GCU FAIL GCU is inoperative GCU 476 configuration settings do not match those of backup configuration memory The G1000 system should be serviced A failure has been detected in the GCU 476 The GCU 476 is unavailable MANIFEST GCU software mismatch communication halted The GCU 476 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 476 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 84 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the G1000 system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoin
104. ommunication halted Comments A GIA mismatch has been detected where only one is SBAS capable MANIFEST G A1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The G1000 system should be serviced MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The G1000 system should be serviced when possible COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the G1000 system should be serviced COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR 2 remote transfer ke
105. on Navigation Map optional Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists Pressing this softkey checks off a checklist item If an item is already checked an UNCHECK Softkey is displayed Press to exit the checklist Press to display the emergency checklist Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 95 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV olpny uqax 513 sjuauimnasu jeuonippy 2 nubi JUI0 NEN iui uoneiedo Jeuuouqy Sue v unuuy m GARMIN DATABASE UPDATES The system uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as vvell as Jeppesen navigation and Jeppesen ChartView database updates Not all SD cards are compatible with the G1000 Use only SD cards supplied by Garmin or the aircraft manufacturer Information regarding the various databases may be viewed on the AUX System Status Page 17 95 136 975 118 200 cone STATUS SERIAL NUMBER VERSION AIRFRAME Cessna 350 CO GUARDIAN 7 00 SYS SOFTWARE VERSION 0534 14 con 7 00 CONFIG
106. oo low GIA1 COOLING GIAT over l eh The GIA1 and or GIA2 temperature is too high perature If problem persists the G1000 system should GIA2 COOLING GIA2 ove e cericed temperature 76 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN GIA 63 MESSAGE ADVISORIES CONT Annunciations amp Alerts Message Comments GIA1 SERVICE G A1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The G1000 system should be serviced MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect soft ware installed The G1000 system should be serviced COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over tempera ture condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the G1000 system should be serviced COM1 SERVICE COM1 needs ser vice Return unit for repair COM2 SERVICE COM2 needs ser vice Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM may still be usable The G1000
107. or the right most softkey Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB and PFD1 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen navigation database 1 2 3 NOTE Loading the Jeppesen navigation database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow Copy the new navigation database to an SD card obtained from Garmin or the aircraft manufacturer With the G1000 system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD label of SD card facing left Turn the G1000 system ON A prompt similar to the following illustration is displayed 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 99 sainjea4 aoueplony 2 Duruue d AEN Sd5 S241V olpny uqax sia sjuaumasu jeuonippy 2 Juil JUI0 NEN nubi uoneiedo Jeuuouqy Sue v yunuuy in uu Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix 0808080 GARM
108. or moves to the ground speed GS field Enter the ground speed Press the ENT Key when finished Note that in automatic page mode ground speed is provided by the system The flashing cursor moves to the fuel flow field Enter the fuel flow Press the ENT Key when finished Note that in AUTOMATIC page mode fuel flow is provided by the system The flashing cursor moves to the fuel onboard field Enter the fuel onboard Press the ENT Key when finished Note that in AUTOMATIC page mode fuel onboard is provided by the fuel totalizer The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature Garmin G1000 Cockpi
109. ox The next line item is automatically selected for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text Press the ENT Key GO TO NEXT CHECKLIST will be highlighted by the cursor Press the ENT Key to advance to the next checklist Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 59 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx sia siu u nnsul Tu102 AEN UTE eouepioAy paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Nav Com XPDR Audio Hazard Avoidance Additional Features Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index Additional Features A GARMIN Immediately Accessing Emergency Procedures 1 2 3 4 5 6 7 8 9 60 From any page on the MFD press the CHKLIST Softkey Press the EMERGCY Softkey Turn the FMS Knob to select the desired emergenc
110. r existing or empty flight plan and again press the IMPORT Softkey Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 32 1 2 3 Press the FPL Key to display the active flight plan If necessary press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN 4 Turn the small FMS Knob The Waypoint Information Window is now displayed 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or Flight Planning a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY
111. rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings includ ing changing units to standard Displays softkeys to select wind data parameters Wind direction arrows with headwind and crosswind components Wind direction arrow and speed Wind direction arrow with headwind tailwind and crosswind components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 91 s n e 4 auepiony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uddx sia sjuauimasu jeuonippy 2 nubi Tuo2 NeN sub uoneiedo Jeuuouqy Sue v unuuy Est Hight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix GARMIN XP
112. rning ROC Obstacle Imminent Obstacle Impact TERRAIN Warning Obstacle Warning 101 Obstacle Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Clearance Caution RTC Terrain Imminent Terrain Impact TERRAIN CAUTION TERRAIN Caution Terrain Caution ITI Terrain Reduced Required Obstacle TERRAIN CAUTION OBSTACLE Caution Obstacle Clearance Caution ROC Obstacle Imminent Obstacle Impact TERRAIN CAUTION OBSTACLE Caution Obstacle Caution 101 Obstacle Terrain SVS System Status Annunciations PFD MFD Alert TERRAIN SVS Page Aural Alert Type ib Annunciation Annunciation Message System Test in Progress TER TEST one System Test Pass None Terrain System Test Fail Terrain or Obstacle database unavailable or invalid invalid software configuration system audio fault None 68 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Terrain System Test OK Terrain System Failure Terrain System Failure 190 00567 04 Rev A A GARMIN Annunciations amp Alerts PFD MFD Alert TERRAIN SVS Page Aural Alert Type ae Cone Annunciation Annunciation Message MFD Terrain or Obstacle database unavailable or invalid System operating with PFD TE Nate Terrain or Obstacle databases No GPS position TER
113. rvalis 10 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Engine indieation System When the first peak is detected the cylinder numbers disappear st isannunciated in light blue below that cylinders EGT bar the temperature is marked in light blue on the graph and the EGT readout is outlined m E qom r 39 gt oe 3 B a Temperature Deviation from Peak First Cylinder TEMPERATURE x EST CHF SE 1442 1452 1382 A peak 394 378 380 25 1900 1414 1416 1374 6 son 374382 1358 RB Light EN RUE Bluc Bar ix Dum uk a gt Represents Peak Indicates 22 2 First Cylinder 188 ep ae E to Peak Assist Mode First Peaked Cylinder Corvalis zs The system continues to detect peak EGTs for each cylinder as the fuel flow is decreased and the peak of each cylinders EGT is indicated by a light blue marker The last cylinder to peak is denoted by the Last annunciation below its bar on the graph and the EGT readout is outlined in light blue paezey Temperature Deviation fm Peah Last Cylinder p ES TEHPERATURE Tir a CHT FF 1426 1438 1366 392 378 378 e 00 1402 137 7 80 as 4500 1400 1402 1374 Son 372 380 352 3 3 l H 11 1 er Indicates gt Last 3 y as 2 ME 4 5 6 Cylinder to m un 2 Peah Assist Mode Last Peaked Cylinder Corvalis x pul 190 00567 04 Rev
114. se to display a smaller area 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 4 AEN 540 52 orpnyyuqdax sia Sjueumajsul Tuo2 AEN fid buluueld ni e uepioAy s mp oold paezey suelv uoneiedo sainjea4 Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Terrain SVS Inhibit Inhibit Terrain Alerting While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit Terrain 3 Press the ENT Key Enable Terrain Alerting While the Terrain SVS Page is displayed select the INHIBIT Softkey Or 1 While the Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key NOTE If T
115. se to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 49 AeN 540 S24V oipny uddx sia Sjueumajsul Tuo2 AEN iui Duruue d ni e uepioAy s mp oold paezey SH lV uoneiedo s m Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the EN
116. selected approach procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 41 buluueld nf s mp old uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL Press the ENT Key The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 42 1 2 3 4 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH
117. splay VID ACTV allows the RANGE Knob to control the zoom setting of the video display When zooming in on the video display a Zoom Window will appear in the upper right of the display A box within this window indicates the portion of the display currently being viewed The currently displayed portion of the full display may be adjusted by using the Joystick 58 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN M itimal Features ELECTRONIC CHECKLISTS The system accesses the checklists from an SD card inserted into the bezel slot If the SD card contains an invalid checklist file or no checklist the Power up Page messages display Checklist File Invalid or Checklist File N A not available and the CHKLIST Softkey is not available Accessing and Navigating Checklists 1 2 3 4 5 6 1 8 9 10 From any page on the MFD press the CHKLIST Softkey Turn the large FMS Knob to select the GROUP field Turn the small FMS Knob to select the desired procedure and press the ENT Key Turn the large FMS Knob to select the CHECKLIST field Turn the FMS Knob to select the desired checklist and press the ENT Key The selected checklist item is indicated with white text surrounded by a white box Press the ENT Key or CHECK Softkey to check the selected checklist item The line item turns green and a checkmark is placed in the associated b
118. t Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN ri htrtanning CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 4 Enterthe desired waypoint name 5 Press the ENT Key 6 The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types 8 Turn the small FMS Knob to select LAT LON latitude and longitude 9 Press the ENT Key CREATE A NEW USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position SoJnpa204d 4 AEN 540 nubi 4 Enter the desired
119. t from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation database update Verify that the user modified procedures in stored flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the aviation database This alert is issued only after an aviation database update Verify use of airways in stored flight plans and reload airways as needed 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 85 s m p q aoueplony SoJnpa204d buluueld AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments
120. ted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 1 2 40 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN 5 Press the ENT Key A list of available approaches for the destination is displayed 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO UJ sjueumasu olpny uqax 59 uo2 AEN 52 AEN 540 9 Press the ENT Key The cursor moves to the altitude field Tum the small 34 FMS Knob to enter the published DA MDA for the
121. tents GARMIN Create a New User Waypoint Defined by a Radial amp Distance from Another Waypoint 0 0 0 0 0000 0 Delete a User Waypoint Create a New Flight Plan mport a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 32 Enter an Airway in a Flight Plan 33 Invert An Active Flight Plan 34 Remove a Departure Arrival Approach or Airway from a Flight Plan 34 Store a Flight Plan cerae ciet Ea 35 Edit a Stored Flight Plan 35 Delete a Waypoint from the Flight Plan sss 35 Invert and Activate a Stored Flight 7 555 5 36 Copy a Flight Plan nnn Delete a Flight Plan etc Graphical Flight Plan Creation Export a Flight Plan to an SD Card Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg nennen Load and or Activate an Approach Procedure LLL s s ss 40 Activate An Approach in the Active Flight Plan 41 Activate a Vector to Final Approach Fix s s s s s si s s s 4 Activate A Missed Approach in the Active Flight 7
122. the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued TAS system Traffic Advisory System Played when the TAS system passes a pilot initiated self test Test Passed Traffic Advisory System Played when the TAS system fails a pilot initiated self test Test Failed MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings XTALK ERROR A flight display crosstalk error has occurred The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired The MFD and PFDs are not communicating with each other The G1000 system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for repair The PFD and or MFD self test has detected a problem The G1000 system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect soft
123. tkey 2 Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Traffic Map Page OPERATING is displayed in the Traffic Mode field 3 Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 5 select the MUTE Softkey to mute TAS voice alerts Displaying Traffic on the Navigation Map 1 Ensure TAS is operating 2 With the Navigation Map displayed select the MAP Softkey 3 Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AND OBSTACLE PROXIMITY 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 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Terrain Proximity Page Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN Bazard avoidance 3 If desired select the VIEW Softkey to access the ARC and 36
124. use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 45 AEN Sd5 S24V oipny uddx sia J05 AeN ii Duruue d nf aoueploay s mp oold paezey suelv uoneiedo SaJnjeoJ Junuuy jeuuouqy jeuonippy xipueddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Displaying Traffic on the Navigation Map 1 Ensure TIS is operating With the Navigation Map displayed select the MAP Sof
125. user waypoint naming is USR000 USR001 USR002 and so On 5 change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 Insert the SD card into the top card slot on the MFD 2 Press the FPL Key on the Contol Unit to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to highlight the flight plan to be exported 6 Press the EXPORT Softkey 7 Press the ENT Key to confirm the export 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 37 sjuauimasu wp 59 olpny uqax 0105 AEN 52 2 4 AEN 540 nubi sual uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 U105 AEN s24v AeN Sd5 4 34 Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 38 A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the
126. utton on the audio panel NOTE The Cessna Corvalis Corvalis TT Airplane Flight Manual AFM always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected AUDIO PANEL FAIL SAFE OPERATION If there is a failure of the Audio Panel a fail safe circuit connects the pilots headset and microphone directly to the COMI transceiver Audio is not available on the speaker during Fail safe operation HAZARD DISPLAYS WITH LOSS OF GPS POSITION If GPS position is lost or becomes invalid selected hazards being displayed on the Navigation Map Page are removed until GPS position is again established P BACK Loss of Hazard Functions with Loss of GPS Position 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 61 sjueuinasu wp aoueplony s mp oold Buruue d AEN SdD S24JV oipny uadx paezey 3461 u102 AEN saunyea4 Jeuonippy Sue v unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an u
127. viceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A amp F r ing as n N Notes NOTE This device complies vvith part 15 of the FCC Rules Operation is subject to the following two conditions 1 this device may not cause harmful interference and 2 this device must accept any interference received including interference that may cause undesired operation NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data NOTE This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional
128. ware installed The G1000 system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The G1000 system should be serviced 72 Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A A GARMIN Annunciations 8 Alerts MFD amp PFD MESSAGE ADVISORIES CONT Message Comments MFD1 CONFIG MFD1 config error Config service req d SW MISMATCH GDU software version mismatch Xtalk is off The MFD configuration settings do not match backup configuration memory The G1000 system should be serviced The MFD and PFDs have different software versions installed The G1000 system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the G1000 system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The G
129. waypoint name 5 Press the ENT Key 6 cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 190 00567 04 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 27 s q sjuounasu U105 AEN 3461 olpny uqax 52 eouepioAy paezey suelv uoneiedo SaJnjeoJ unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 28 A GARMIN 7 With the cursor in the WAYPOINT TYPE field turn the small FMS Knob to display a list of waypoint types Turn the small FMS Knob to select RAD RAD radial radial Press the ENT Key The cursor moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows 8 9 10 11 a b o Or a b o d Or a b d Or a b
130. y checklist and press the ENT Key Press the ENT Key or CHECK Softkey to check the selected emergency checklist item The line item turns green and a checkmark is placed in the box next to it The next line item is automatically highlighted for checking Either FMS Knob can be used to scroll through the checklist and select the desired checklist item Press the CLR Key or UNCHECK Softkey to remove a check mark from an item When all checklist items have been checked Checklist Finished is displayed in green text at the bottom left of the checklist window If all items in the checklist have not been checked CHECKLIST NOT FINISHED will be displayed in yellow text Press the ENT Key GO TO NEXT CHECKLIST will be highlighted by the cursor Press the ENT Key to advance to the next checklist Press the RETURN Softkey to return to the previous checklist Press the EXIT Softkey to exit the Checklist Page and return to the page last viewed Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 04 Rev A GARMIN X U Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP B
131. y is stuck 80 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT The COM1 and or COM 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 190 00567 04 Rev A A GARMIN Annunciations amp Alerts GIA 63W MESSAGE ADVISORIES CONT Message with other NAVS LOI GPS integrity lost Crosscheck Comments GPS integrity is insufficient for the current phase of flight GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the

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