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Garmin Software Version 0534.21 Cockpit Reference Guide

1. Rate Caution EDR PFD MFD MFD Alert Type TAWS B Page Aural Message Pop Up Alert Annunciation Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up himni 7 Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain 5 i Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN 1 AHED 0 Terrain Ahead Terrain Impact Caution ITI or Ahead TION TERRAIN i Caution Terrain Caution Terrain Reduced Required TERRAIN cCAUTION OBSTACLE Caution Obstacle Cau Obstacle Clearance or tion Obstacle Caution ROC BB AHEAD or Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN 1 OBSTACLE AHEAD 1 Obstacle Ahead Obstacle Impact Caution 101 or Ahead OBSTACLE Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN TOOLOW TERRAIN Too Low Terrain Alert Caution PDA Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate 76 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567
2. 41 Activate An Approach in the Active Flight 7 42 Activate a Vector to Final Approach Fix 5 42 Activate A Missed Approach in the Active Flight 77 7 556 42 HAZARD AVOIDANCE n 43 Customizing the Hazard Displays on the Navigation 43 STORMSCOPE Optional 0 ccccccsssssssssssssccsssssssssscsssssssssesesssssssssscesssssssssscesassssssnsess SiriusXM Weather Optional Traffic Systems ie debet P e e ede Terrain And Obstacle Proximity sssssssseeee 49 Teirain SVS os emet prem e pede t ted de 50 Terrain Awareness amp Warning System TAWS Display Optional 52 ADDITIONAL FEATURES sn nenne 55 Synthetic Vision Optional 55 Terminal Procedure Charts seen 56 Airport Directory SiriusXM Radio Entertainment sn 59 Auxiliary Video 61 Electronic Checklists ennnn 63 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN table of Co
3. paezey GARMIN AFCS Sjueuinijsu fila 593 oipny uadx U105 AEN 52 AeN 5492 4 qos Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00567 05 Rev A Garmin 61000 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 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 2 Tum the large FMS Knob to place the curso
4. music copilot copilot 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 15 s u wnysu 59 S24V oipny uddx JUI05 AEN sual uone1edo s m aoueplony s mp oold Buruue d AEN Sd5 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui Wfi l4 A Nav Com XPDR Audio Panel GARMIN Fight Instruments EIS Nav Com 05 x 22 o x 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 05 Rev A A GARMIN SSCS GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis 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 Lateral Vertical FD Key Roll Hold default ROL Pitch Hold default
5. A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page 1 2 Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob until the Stormscope Page is selected Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page Press the MODE Softkey The CELL and STRIKE Softkeys are displayed Press the CELL Softkey to display CELL data or press the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the View
6. 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 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 system should be serviced COM1 RMT XFR 1 remote transfer key is stuck COM2 RMT XFR 2 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 system should be serviced COM1 CONFIG COM config error Config service req d COM2 CONFIG COM config error Config service req d The COM1 and or COM2 configuration settings do not match backup configuration memory The system should be serviced 88 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 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 sate
7. One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 98 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A dh GARMIN Appendix APPENDIX sjuauimasu sub PFD SOFTKEY MAP 59 optional mer L 1 999 C55 foe xe ST pweme Wer wmm 77 um m 7 uu uu m olpny uqax uo2 AEN CD NAV2 x d Top Level PFD Softkeys 9 optional S D v3 HU s n n n n n Duruue d wold optional optional optional optional optional F V3 V vv nv mnm SeJnpa20Jd Press the BACK Softkey to return to the top level softkeys aoueplony paezey Inset Map Softkeys soJnjeoJ jeuonippy Levell Level2 Level 3 Description uoneiedo Jeuuouqy INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map DCLIR 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 t
8. 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 the large FMS Knob to highlight the LEG field 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 25 oipny uddx 59 sjuauimasu U105 AEN 3463 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo s n e 4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation
9. 400 123456 DEC FUEL INC FUEL RST FUEL Engine Leaning Assist Mode Corvalis 10 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Engine indication System When the first peak is detected the cylinder numbers disappear Ist 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 8 e 3 Temperature Deviation from Peak First Cylinder TEMPERATURE TE V KEEPER 3 140413961396 PEAK 346 346 346 141413961418 11 sog 328 328 328 Licht AREE Blue Bar 2582 wk z Represents uin nt a Peak 0 300 Indicates 200 9 a 2 Cylinder 100 r a io Peak ist 1 3455 Assist Mode First Peaked Cylinder Corvalis H The system continues to detect peak EGTs for each cylinder as the fuel flow is 2 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 gt and the EGT readout is outlined in light blue Temperature Deviation fm Peah Last Cylinder 2 TEMPERATURE TF CHT F 1410 1386 1402 4 PEAK 346 346 346 opo 138414281424 18 328 328328 3 woo i iii 1450 Li ir iot i 1300 a Cylinder to S 8 Peah Ls Assist Mode Last Peaked Cylinder Corvalis z 190 00567 05 Rev A Garmin G1000 Co
10. 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 desired 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 CREATE A USER WAYPOINT USING THE MAP POINTER 1 Press the Joystick to activate the panning function and pan to the map location of the desired user waypoint 2 Press the ENT Key The User Waypoint Information Page is displayed with the captured position
11. The PFD and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch DB MISMATCH Obstacle database mismatch The PFD and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on The PFD and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Airport Terrain database mismatch The PFD and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on TERRAIN DSP PFD1 MFD1 Terrain awareness d
12. 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 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 wit
13. 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 GPS Navigation 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 KARLA 21 Insertion MENT 224 LEVYN 220 11 7NM 9 QNM 8 0NH Approach KDFH RNAV 17LGPs RIVET iaf 262 176 INWOD 176 MENOL faf 176 RW17L map 176 99 FT POLKE 18 8NM 3 3NM 3 2NH ASIN 5 3NM 8NM 13000FT 12400FT 9900 q l rr 2000FT Large White Text Large Light Blue Text Small Light Blue Text Small Li Blue Sub ed Text Sma 1 White Text with Altitude SIUE Cross AT or ABOVE 5 000 fi Facing Cross AT 2 300 fi Cinn 11 Cross AT or BELOW 3 000 ft Restriction Bar 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT sia sjuaumasu Yid olpny uqax uo2 AEN Suelv uoneiedo sainjea4 SoJnpa204d Duruue d unuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning
14. GARMIN Additional Features 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 Airport information is displayed on the right half of the display SIRIUSXM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 Tum 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 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 Bo
15. Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER f 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 PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card Selected course for LOC2 differs from published localizer course by more than 10 degrees 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 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 TRN AUD FAIL Trn Awareness audio source unavailable The audio source for terrain awareness is offline Check GIA 1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req d Terrain audio alerts are not configured properly The system should be serviced 96 Garmin G1000 Cockpit R
16. 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 is now displayed 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 sjuaumasu sub oipny uddx 93 UI0JNeN 52 AEN 540 Duruue d wold s mp old eouepioAy paezey 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure 10 Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 11 Turn the large FMS Knob to select either LOAD or ACTIVATE Selecting LOAD enters the selected approach procedure into the active flight plan but is not currently active Selecting ACTIVATE enters the selected approach procedure into the active flight plan and activates the first leg of the approach 12 Press the ENT Key 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 41 so1njeoJ jeuonippy suelv uoneiedo junuuy Jeuuouqy xipuaddy x pul Nav Com XPDR Audio E Abnorm
17. 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 s mp ooud AEN 540 nubi CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 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 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 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for t
18. 105 Fuel remaining calculated GAL REM 8 Fuel used calculated GAL USED 8 H Horizon heading 55 Inhibit TAWS 53 Inhibit Terrain 51 Insertion Point Indicator 23 33 34 38 Inset Map 99 100 IOI 74 76 J Jeppesen 57 L Lightning 43 44 106 M Magnetic Field Variation Database 111 Map panning 45 Message advisories 78 96 MET 73 METAR 45 Minimums 78 Mistrim 73 MKR MUTE 15 Mode 104 Mode selection softkeys 13 Multi Function Display MFD Softkeys 105 ndex 2 Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT A GARMIN N NAV 14 NAV1 2 14 NAV2 2 14 Navigation database 23 24 NEXRAD 45 100 106 0 OBS 2 Obstacles 82 87 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 P Pathways 55 56 Power up page 63 Profile View 106 R Reversionary mode 65 ROC 74 76 S Safelaxi amp 56 Secure Digital SD card 63 Split COM operation 14 Standby Navigation Database 110 Store Flight Plan 35 Stormscope lightning data 43 44 106 Strike 43 Strike mode 44 SVS 55 96 190 00567 05 Rev A A GARMIN SVS Terrain 55 W Synchronization 108 SYNC Status 110 Synthetic Vision System 55 Waypoint Selection Submenu 32 Weather data link page 45 Wind data 102 X TA 78 Tachometer RPM 5 6 XM lightning 100 106 TAF 45 XM Radio
19. 1900 150 1750 Vcn a 400 p E 1600 8 1450 1300 3 1300 200 AILERON TRIM 1150 non Y 1000 PIT sn WO zaas ziz 7 se EE 1 DCLTR ASSIST DEC FUEL INC FUEL RST FUEL c Engine Page Corvalis TT 8 2 S m 8 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 Sue v uoneiado SoJnjeaJ eouepioAy unuuy jeuuouqy jeuonippy paezey xipuaddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 7 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 The fuel remaining can be adjusted using the following softkeys DEC FUEL Decreases totalizer based fuel remaining in
20. Features Index Flight Planning 26 5 6 7 8 9 10 11 12 13 A GARMIN 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 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 cursor 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
21. MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB Verify the correct active navigation database cycle information is shown for each display 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 109 s tin sul BUT saunqea4 2 Buruuejd AEN 5649 2 oipny uadx Jeuonippy paezey ni uo2 AEN uoneiedo Jeuuouqy Sue v unuuy 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 Loading the Standby Navigation Database The purpose of the Standby Navigation Database is to allow the loading of the next cycle of the Navigation Database to the bottom SD card prior to its effective date The Navigation Database is available seven days prior to its effective date 1 2 3 4 5 6 1 8 9 NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD Verify that an SD card is inserted in the bottom slot of each PFD and the MFD Turn the system ON A prompt is displayed Press the YE
22. MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 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 Tum the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field SPLIT COM During Split COM operation both the pilot and the copilot can transmit simultaneously over separate radios The pilot can still monitor NAVI NAV2 ADE DME and MKR Audio as selected but the copilot is only able to monitor COM2 When Split COM operation is selected COMI is used by the pilot and COM2 is used by the copilot The COMI MIC Annunciator flashes when the pilots microphone PTT is pressed The COM2 MIC Annunciator flashes when the copilots microphone PTT is pressed Pressing the COM 1 2 Key selects Split COM operation The COM 1 2 Annunciator is
23. Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN VOICE ALERTS Voice Alert Description Minimums minimums The aircraft has descended below the preset barometric minimum descent altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued Traffic Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued TAS system Traffic Advisory System Played when the TAS system passes a pilot initiated self test Test Passed Traffic Advisory System Played when the TAS system fails a pilot initiated self test Test Failed MFD amp PFD MESSAGE ADVISORIES Message Comments DATA LOST Pilot stored data was lost Recheck settings XTALK ERROR A flight display crosstalk error has occurred The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair MFD1 SERVICE MFD1 needs service Return unit for re
24. 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 SAS Go Around n air GA Go Around in air 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 must have a valid VOR or LOC signal or active GPS course before NAV or APR Key press activates flight director The selected navigation receiver must have a valid LOC signal before BC Key press activates flight director 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 17 sjuauimasu UATE 59 oipny uadx 0105 AEN ARN Sd5 So4V Suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d unuuy jeuuouqy Jeuonippy paezey nuru xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS GPS Nav AFCS
25. Reference Gui de for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN GIA 63W MESSAGE ADVISORIES CONT Annunciations amp Alerts Message GIA1 CONFIG G A1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d Comments The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced GIA1 SERVICE GIA1 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 system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable MANIFEST GIA1 software mismatch communication halted MANIFEST GIA2 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software installed The system shoul
26. 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 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 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 49 AEN Sd5 S24V oipny duadx 99 Sjuouinsu u102 AEN ibid Duruue d nf s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN 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 dis
27. 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 Turn the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 Turn 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 Tum the small FMS Knob to choose between Day Auto and Night Options 6 Auto Mode turn the large FMS Knob to select the percentage field and change percentage with the small FMS Knob The percentage of change is the day night crossover point based on backlighting intensity 7 Press the FMS Knob when finished to remove the Chart Setup Menu AIRPORT DIRECTORY The Aircraft Owners and Pilots Association AOPA or AC U KWIK Airport Directory database offers detailed information regarding services hours of operation lodging options and more for various airports This information is viewed on the WPT Airport Information Page The Airport Directory databases are revised every 56 days The Airport Directory is always available for use after the expiration date Check fly garmin com for the current database 58 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A
28. 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 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Flight Planning CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Tum 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 The cursor is now in the WAYPOINT TYPE field If desired the waypoint
29. charts for appropriate minimum clearance altitudes 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 WARNING Do not rely on information from the lightning detection system display as the sole basis for hazardous weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to documentation from the lightning detection system manufacturer for detailed information about the system WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT A Wamingst
30. desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint Select the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 2 3 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 Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS 1 2 3 Select the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 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 Tu
31. each display Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN 0 Appendix Loading the Active Navigation Database The Navigation Database that is loaded to internal memory as the active database will be used by the system 1 2 3 4 5 6 7 8 9 10 11 xw NOTE Loading the Navigation Database as the active 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 NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 or MFD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database After the update completes the display starts in normal mode Turn the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other displays PFD1 or MFD 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
32. illuminated indicating Split COM operation COMI and COM2 frequencies are 14 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Nav Com XPDR Audio Panel displayed in green indicating that both transceivers are active Split COM operation is cancelled by pressing the COM 1 2 Key again at which time the annunciator is extinguished 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 INTERCOM SYSTEM ICS ISOLATION Press the PILOT and or COPLT Key to select those isolated from hearing the Nav Com radios and music a ANNUNCIATOR ANNUNCIATOR Hears Hears Selected Selected Selected radios pilot radios pilot radios pilot OFF OFF copilot copilot copilot passengers passengers passengers music music music Copilot Copilot radios pilot i music music Selected Selected COPILOT OFF ON radios pilot Copitot s n Mu passengers passengers music music Selected Selected CREW ON ON radios pilot radios pilot
33. is available 18 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT en Selected Altitude 190 00567 05 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 tal fr ic Capture Track GDU 1044 only g backcourse approaches Captures and tracks 7 Backcourse GDU 10448 only a localizer signal for 10448 BC backcourse 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 19 913 Sjueumasu oipny uadx 0105 AEN ARN Sd5 52 Suelv uoneiedo s n e 4 e uepioAy SoJnpa20Jd Duruue d Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul 1i
34. 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 m E NH Calculation Fuel Calculations Group 8 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Engine Indication system Engine Temperature Group The temperature group displays the Cylinder Head Temperature CHT and Exhaust Gas Temperature EGT in degrees Fahrenheit for each eylinder 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 sjueuinasu UATE 3f BS ED e 524 DCLTR Removes displays the EGT and CHT readouts from the display ASSIST Accesses the Engine Leaning Assist Mode 52 Cylinder Head emperature AEN Sd5 Exhaust Gas TEMPERATURE EGT F F Temperature 174616141726 372 366 354 499g 68816581702 909 358 374 CHT Duruue d Wil 1750 SeJnpa20Jd 400 1600 1458 300 1308 200 1150 1000 123405 6 1007773456 Engine Temperature Group Corvalis eouepioAy paezey saunyea4 Jeuonippy Turbine Inlet Cyl
35. waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 1 2 3 4 5 6 1 38 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Contol Unit 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 the large FMS Knob to highlight the flight plan to be exported Press the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Tum the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure is active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key on the MFD to display the active flight plan 2 Press the FMS Knob to
36. 05 Rev A A GARMIN Annunciations amp Alerts PFD MFD MFD Alert Type 1 TAWS B Page Aural Message Fue Pop Up Alert Annunciation Negative Climb TERRAIN CDONTS K Don t Sink Rate Caution NCR or or DOn 100 Low Terrain TAWS B System Status Annunciations PFD MFD Alert TAWS B Page Aural Alert Type RES Annunciation Annunciation Message TAHS TEST None Progress TANS System System Test Pass None None Test OK TAWS B System Test TANS System Fail TAMS FAIL Failure Terrain or Obstacle database unavailable or invalid TAWS System invalid software TAMS FAIL Failure configuration system audio fault MFD Terrain o Obstacle database unavailable or invalid None None System operating with PFD Terrain or Obstacle databases T TAWS Not No GPS position TAWS N A Available Excessively degraded GPS signal or out of TAWS Not database coverage TAWS N A Nate Available area Sufficient GPS signal None None TAWS Available database coverage area entered 90 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 1 soinjeo4 9e2uepioAy SoJnpa20Jd Duruue d ACN Sd5 S24V olpny uqax s q Sjueuinijsu 2 nf JU105 AEN yb jeuonippv uoneiedo jeuuouqv iue ER x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS
37. 165 GMU 44 Message Advisories GDL 69A Message 150 15 GDC 74A Message Advisories ssssssseenne GCU 476 Message Advisories ssssssssseee nne Miscellaneous Message Advisories Flight Plan Import Export Messages PFD Softkey MED Softkey Map sse 105 Loading Updated 107 INDEX qe MH Index 1 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT il Table of Contents GARMIN Blank Page iv Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 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
38. 17 95 navz 108 00 117 95 MAN IN HG 25 L FUEL QTY BAL TEMPERATURE EGT F 1 1724 1634 1552 1900 16521580 1506 1750 OCLTR ASSIST CHT F 320 338 356 356 356 374 _ 136 975 118 888 com 136 975 118 800 corz RPM 2300 FUEL CALC GAL REH ENDUR 98 9 5 48 GAL USED RANGE NH 21 930 ELEV TRIH ELECTRICAL T u ALT AMPS BATT AHPS BUS VOLTS 55 55 55 55 278278 iar 1 1450 SJ gt 1300 5 1150 1000 12345585 100 173245585 AILERON TRIM 2 Carbon CO LVL HIGH PPM 55 0 Monoxide COLONNA A Warning Engine Page Corvalis O Oil Temperature Pressure Gauge Engine Manifold Pressure Gauge 0 Tachometer Fuel Calculations Group Oxygen Quantity Gauge Corvalis FR T9 Gauss Oxygen Outlet Pressure Gauge Low Pr ssure Gauge shown High Pressure Gauge optional Corvalis IT only 6 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT O Electrical Group Trim Group 2 Engine Temperature Group Fuel Quantity Gauges Fuel Flow Gauge 190 00567 05 Rev A GARMIN ___Engine Indication System 2 iz Q a neve 108 00 RPH SE 2300 82 BS 2 FUEL CALC s 3 GAL REM ENOUR 101 4 5 37 4 GAL USED RANGE NM L FUEL QTY GAL R FUEL QTY GAL 05 921 A TEHPERATURE ELECTRICAL v GT F TIT F ELEV A etd 3 A DP TA TRIM 172416341562 1472 154 ALT aes AMPS BUS VOLTS 165215801508 s 218 218 i
39. 30 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN 00 Flight Planning NOTE If the pointer has highlighted a map database feature one of three things happens upon pressing the ENT Key 1 information about the selected feature is displayed instead of initiating a new waypoint 2 a menu pops up allowing a choice between Review Airspaces or Create User Waypoint or 3 a new waypoint is initiated with the default name being the selected map item s tin sul nubi 3 oipny uddx JUI0JNeN 3 Enter a user waypoint name up to six characters 4 Press the ENT Key to accept the selected name 5 If desired define the type and location i e LAT LON RAD RAD or RAD DIS of the waypoint 52 6 Press the ENT Key to accept the new waypoint 7 If desired change the storage method of the waypoint to TEMPORARY or NORMAL by moving the cursor to TEMPORARY and selecting the ENT Key to check or uncheck the box 8 Press the FMS Knob to remove the flashing cursor 9 Press the GO BACK Softkey to return to the map page 2 Buruuejd AEN Sd5 Juil 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 4 Turnthe large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn th
40. 4JV oipny uadx sia sjueumasu Jeuuouqy Jeuonippy puezey ubi U105 AEN ubiu Sue v unuuy k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts A Appendix MUG ARMIN Uploading GRS1 Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS1 2 When the upload is complete the prompt for the next GRS upload is displayed as seen in the following figure GRS2 MV DB Update Available Update from 2005 to 2010 OK CANCEL GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use Uploading GRS2 Has Var Database STARTING UPLOAD 2 Uploading Database to GRS2 112 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN A Activate a flight plan 22 Active Channel 59 Active database 109 Active Navigation Database 109 AC U KWIK 58 ADF 13 14 66 102 Advisory alerts 72 AHRS 69 91 92 Airport Directory 58 Airport Signs 55 56 Airways 106 AOPA 58 AOPA s Airport Directory 58 AP 73 Assist engine leaning 10 12 Audio panel controls NAV1 NAV2 14 Audio panel fail safe operation 65 Autopilot 73 Auxiliary video 61 Barometric Altitude Minimums 3 Ba
41. 5 Trip Planrilng rete in etr ne 00000 25 Create a User Waypoint Defined by Latitude amp Longitude 2 Create a User Waypoint Defined by Radials from Other Waypoints 2 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Table of Contents GARMIN Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 29 Create a User Waypoint using the Map Pointer 30 Delete a User Waypoint Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan sssse 33 Enter an Airway in a Flight Plan 34 Invert An Active Flight Plan 35 Remove a Departure Arrival Approach or Airway from a Flight Plan 35 Store a Flight Plan co eoo t iei tn s 35 Edit a Stored Flight Plan 36 Delete a Waypoint from the Flight Plan sss 36 Invert and Activate a Stored Flight Plan 36 Copy a Flight Plan Delete a Flight Plan etc Graphical Flight Plan Creation Export a Flight Plan to an SD Card UR Rada Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg Load and or Activate an Approach Procedure
42. 59 TAS 48 78 91 XM weather 45 TAWS 52 53 75 Terrain 49 50 52 82 100 106 Terrain SVS 50 51 Zoom Window 62 Timer 93 Topographical data 100 106 Traffic 43 48 105 Traffic advisory 48 78 Traffic map page 48 49 50 Transponder 13 104 Trim 5 6 Turbine Inlet Temperature TIT F 5 12 V Vertical speed guidance 24 Vertical track 78 Video 61 VNV 21 66 95 Vspeed 2 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Index Index 3 sainjea4 aoueplony 2 buluueld AEN Sd5 S24JV olpny uqax 413 sjuauimasu jeuonippy 2 wold Tuo2 NeN wb uoneiedo Jeuuouqy Sue v unuuy ow GARMIN Index Sjueuinijsu fila 593 U105 AEN S24V AeN Sd5 Duruue d Blank Page 6 2 4 aoueplony puezey soinjeod Jeuonippy uoneiedo jeuuouqy suay unuuy e E 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Index 4 A GARMIN Garmin International Inc 1200 East 151st Street M a zo theKS66082 U A 9 3978282 7 in Europe pe Liberty c Copse Road Park utha No 68 Gach m su m Teo T 2006 2010 2012 Garmin Ltd or its subsidiaries 190 00567 05 Rev A
43. A condition has developed causing the roll servo to eft force Ensure the slip skid indicator is centered and observe any maximum uel imbalance limits A condition has developed causing the pitch ustained force Be prepared down control wheel force upon Aileron Mistrim Right to provide a s maximum fue A condition has ustained right force Ensure the slip skid indicator is centered and observe any imbalance limits developed causing the roll servo Preflight Test anf F Performing preflight system test Upon completion the aural alert will be heard Preflight system test has failed 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 73 s m aoueplony SoJnpa204d Duruue d AEN 540 52 oipny uadx 513 sjueumasu piezeH ubi U10 AEN ubiu jeuonippy uoneiedo Jeuuouqy EY x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 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 Te
44. AC U KWIK information included mited to the implied warranties of ormation is provided as is and esentations regarding its accuracy ue AC U KWIK Organizations and ess AC U KWIK Organizations tual or alleged inaccurac ormation in the datasets Some ju exclusion of implied warranties or liability for incident e above limitati uential dam its related organizations hereinafter collectively mation included in this f merchantability ot Wise cidental special he ated ages S to the ies in the isdictions al or ons or exclusions may not apply to licensee 190 00567 05 Rev A Printed in the U S A amp GARMIN _ sing Cautions amp Notes e e e 6 6 V ARNING 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 able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical
45. Abnormal Additional Hazard Avoidance Annun EIS AFCS 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 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 cann
46. 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 27701 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 nnnn rem 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 Captures the Vertical Navigation T ATV Capture VNV Target Altitude Glidepath 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
47. CK Softkey to return a to the top level softkeys a m lt 3E E eee ee 5 73 a a Press the BACK Softkey to return to the previous level softkeys Duruue d ni Transponder Softkeys so1njeoJ 2 jeuonippy paezey uoneiedo Jeuuouqy Sue v unuuy gt 5 3 x x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 103 Additional Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description XPDR IDENT STBY ON ALT GND CODE TMR REF NRST ALERTS 104 0 7 BKSP Displays transponder mode selection softkeys Selects Standby Mode transponder does not reply to any interrogations Selects Mode A transponder replies to interrogations Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations Manually selects Ground Mode the transponder does not allow Mode A and Mode C replies but it does permit acquisition squitter and replies to discretely addressed Mode S interrogations Automatically enters the VFR code 1200 in the U S A only Displays transponder code selection soft keys 0 7 Use numbers to enter code Removes numbers entered one at
48. 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 Softkey 2 Tum the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 13 sjueumasu S24V oipny 4ddX sia JUI05 AEN uoneiedo sainjea4 aoueplony SoJnpa204d buluueld AEN Sd5 Jeuuouqy Jeuonippy paezey xipuaddy x pul iui nu unuuy ight H 2 m u E Nav Com AFCS XPDR Audio EIS Annun Abnormal Additional Hazard Flight Alerts Operation Features Avoidance Procedures Planning GPS Nav Appendix Index A Nav Com XPDR Audio Panel GARMIN SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3
49. G1000 Integrated Flight Deck Cockpit Reference Guide for the Cessna Corvalis Corvalis TT LB CESSNA CORVALIS CESSNA CORVALIS TT A GARMIN Copyr This m Corva inform ight O 2006 2010 2012 Garmin Ltd or its subsidiaries All rights reserved anual reflects the operation of System Software version 0534 18 or later for the Cessna is Corvalis TT 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
50. 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 system should be serviced if the problem persists 92 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES Message FPL WPT LOCK Flight plan waypoint is locked Comments Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an aviation database update eliminates an obsolete waypoint The flight plan cannot find the specified waypoint and flags this message This can also occur with user waypoints in a flight plan that is deleted Remove the waypoint from the flight plan if it no longer exists in any database Or update the waypoint name identifier to reflect the new information FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new aviation database update Verify that stored flight plans contain correct waypoint locations The system notifies the pilot that the timer has expired DB CHANGE Database changed Verify user modified procedures This occurs when a stored flight plan contains procedures that have been manually edited This alert is issued only after an aviation database upda
51. 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 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 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 85 so1njeoJ 2 AEN 5649 S24V oipny uadx sia syu unysu paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy EST x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix od Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments 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 system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair A failure has been detected in the GPS1 and GPS2 SERVICE GPS2 needs service Return unit for repair or GPS2 receiver The receiver may still be av
52. KLIST 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 63 s mp oo4d Buruuejd AeN Sd5 S24V oipny uadx sia sjuoumnasul Tu102 AEN UTE aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy 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 64 From any page on the MFD press the CHKLIST Softkey Press the EMERGCY Softkey Turn the FMS Knob to select the desired emergency 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 b
53. S Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD After the navigation database files are copied to the bottom SD card press any key to verify as instructed After database verification is complete press any key to continue as instructed on the display Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting Press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD 10 Turn the small FMS Knob to select the System Status Page 11 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN 0 Hppendix 12 Turn system povver OFF 13 Remove the SD card from the top card slot of the MFD 14 Turn system power ON 15 Press the ENT Key to
54. S WIND DME BRG1 HSI FMT BRG2 ALTUNIT STD BARO BACK ALERTS Es LA TERES nmnmnmnmnmnmnnnnnnnn L JL E E E BesE rr r Eu uu vu mumu umu mmm m nn 53 Select the BACK Softkey to return to the top level softkeys oipny uadx 010 AEN 52 AEN 540 Duruue d Wil s mp 01d PFD Configuration Softkeys P Level 1 Level2 Level 3 Description EE PFD Displays second level softkeys for additional PFD configurations ze SYN VIS Displays the softkeys for enabling or 2 Hd disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction uoneiedo Jeuuouqy Sue v unuuy HRZN HDG Displays compass heading along the Zero Pitch line gt 5 x x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 101 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix Appendix A GARMIN Level 1 Level 2 Level 3 Description APTSIGNS Displays position markers for airports DFLTS WIND OPIN 1 OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT 360 HSI ARC HSI BRG2 ALT UNIT METERS IN within a
55. STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Press the MAP Softkey 2 Press the STRMSCP Softkey Press the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old Strike is between 6 and 60 seconds old Da Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 43 AEN 540 S24V oipny duadx 99 syuauuni su u105 AEN fila buluueld ni e uepioAy s mp oold paezey Sue v uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 44 5 6 7 8 9
56. 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 57 s mp o4d Buruuejd AeN Sd5 S24V oipny uadx sia siu u nnsul nubi Tu102 AEN UTE eouepioAy paezey s n ze 4 jeuonippy xipueddy 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 Addend Features 1 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 Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Select the SHW CHRT Softkey The
57. VE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT PLAN 52 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor AEN Sd5 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 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 pu i8 EES 2 2 eouepioAy soJnjeoJ jeuonippy 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or MFD 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 xipuaddy Suelv uoneiedo junuuy Jeuuouqy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 35 Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Op
58. 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN 0 Appendix MFD SOFTKEY MAP mn am 5 SYSTEM MAP SHVV CHRT CHKLIST 3 z LA a optional optional m a Press the BACK Softkey on this Default softkey level to return to the top softkey level is dependant on the selection made in the map setup options optional optional optional optional optional TRAFFIC PROFILE TOPO AIRWAYS me STRMSCP NEXRAD XMLTNG T METAR LEGEND BACK olpny uqax 0105 AEN gt Press the SYSTEM Softkey to 2 return to the default page level optional EY EY V3 V3 V3 V3 V3 7 3 The CHECK Softkey changes to UNCHECK when v the checklist item is already checked 9 m nnn A s MFD Softkeys 3 Level 1 Level 2 Description i SYSTEM Access the EIS functions iz SYSTEM Returns to the top level EIS display 8 OXYGEN Turns the oxygen system on or off optional pE DCLTR Cycles the EGT and CHT cylinder temperatures 23 on and off or ASSIST Accesses the Engine Leaning Assist Mode 7 5 CORST Resets the CO Guardian and acknowledges an m alert zb DEC FUEL Decreases the gallons of fuel
59. acknowledge the startup screen 16 Turn the large FMS Knob to select the AUX Page group on the MFD 17 Turn the small FMS Knob to select the System Status Page 18 Press the Display Database Selection Softkey to shovv standby navigation database information for each display MFD1 DB PFD1 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRS1 and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 111 uone1edo s m aoueplony SoJnpa204d Duruue d AEN Sd5 S2
60. 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 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 39 oipny uddx s q sjuauimasu U10 AEN fija 52 AEN 540 Duruue d nubi s mp old eouepioAy paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy 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 A Procedures GARMIN LOAD AN ARRIVAL PROCEDURE 1 2 3 4 5 6 1 8 9 10 11 12 Press the PROC Key Turn the large FMS Knob to highlight SELECT ARRIVAL Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 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 arriv
61. ailable The system should be serviced Return unit for repair NAV1 SERVICE NAV1 needs service A failure has been detected in the NAV1 and Return unit for repair NAV2 SERVICE NAV2 needs service or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck The remote NAV1 and or NAV2 transfer Switch is stuck in the enabled or pressed NAV2 RMT XFR NAV2 remote transfer key is stuck state Press the transfer switch again to cycle its operation If the problem persists the system should be serviced G S1 FAIL G S1 is inoperative A failure has been detected in glideslope G S2 FAIL G S2 is inoperative receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver G S2 SERVICE G S2 needs service Return unit for repair may still be available The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced 86 Garmin G1000 Cockpit
62. al Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index A Procedures GARMIN ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window is displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the Go around Switch 42 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page
63. al 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 c Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 40 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 highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN LOAD AND OR ACTIVATE AN APPROACH PROCEDURE Procedures 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 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT APPROACH 3 Press the ENT Key A list of available approaches for the destination airport 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 6
64. atabase unavailable or aridis Sistan invalid invalid software TER FAIL 7 Failure configuration system audio fault MFD Terrain or Obstacle database unavailable or invalid System operating with PFD Nong Mille Terrain or Obstacle databases Excessively degraded Tearrain System GPS signal or out of TER N A None Not Available database coverage area Sufficient GPS signal received after loss or Terrain System None None HE database coverage area Available entered TAWS B ALERTS PFD MFD MFD Alert Type TAWS B Page Aural Message aa Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Reduced Required Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up TERRAIN PULL UP Terrain Terrain Pull Up Pull Up 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 15 sainjea4 2 buluueld AEN Sd5 241V oipny uddx 53 siu umn sul p ezeH ni uio AeN Yid jeuonippyv uoneiedo jJeuuouqv FW x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN
65. aypoint 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 05 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 Press the FMS Knob to remove the flashing cursor CREATE A 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 automat
66. c Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI Format nennen 3 ENGINE INDICATION SYSTEM 5 beraten ded NR 6 Engine Leaning Assist Mode sss 0 NAV COM TRANSPONDER AUDIO PANEL 3 ADF Tuning 3 DME Tuning 5 7 2 3 Enter a Transponder Code 3 Selecting a COM Radio 4 Selecting a NAV Radio 4 NAV COM Tuninj itcr rete erem trt rem tht bt m ep es 4 4 Digital Clearance Recorder and Player 5 Intercom System ICS Isolation 5 GFC 700 AUTOMATIC FLIGHT CONTROL SYSTEM 7 Flight Director Activation 55 7 Vertical Modes nnne 8 Lateral Modes asas b oe Rn ee a 9 GPS NAVIGAMONM atii atcp actin tt M at bp adad 21 Direct to Navigation 21 Activate a Stored Flight Plan sse 22 Activate a Flight Plan Leg 22 Stop Navigating a Flight Plan 23 Vertical Navigation VNAV sssssseeeetnnnn nen 23 FLIGHT PLANNING LL Ra Bad 2
67. 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 again to unmute the audio Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN AUXILIARY VIDEO OPTIONAL 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 auxiliary 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
68. ckpit Reference Guide for the Cessna Corvalis Corvalis TT 11 iui UI0JNeN n jeuuouqy jeuonippy paezey unuuy Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Appendix 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 TEMPERATURE EL TIT F CHT F 1398 1400 1440 346 346 346 1900 1900 1416 H E PR ER 328 328 1600 amp 1450 1300 1150 10600 H A 6 A 12 345 6 RICH Lean or Rich TIT Deviation From Peak from Peak Engine Leaning Assist Mode Corvalis TT Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 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
69. d MANIFEST GIA1 software mismatch MANIFEST GIA2 software mismatch The GIA1 and or GIA 2 has incorrect software installed The system should be serviced communication halted MANIFEST GFC software mismatch Incorrect servo software is installed or gain Settings are incorrect mismatch communication MANIFEST COM1 software halted mismatch communication MANIFEST COM2 software halted COM1 and or COM2 software mismatch The system should be serviced mismatch communication MANIFEST NAV1 software halted mismatch communication MANIFEST NAV2 software halted NAV1 and or NAV2 software mismatch The system should be serviced COM1 TEMP COM ove Reducing transmitter power rtemp 0 2 TEMP 2 ove Reducing transmitter power r temp 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 system should be serviced COM1 SERVICE COM1 vice Return unit for repair needs ser COM2 SERVICE COM2 vice Return unit for repair needs ser The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible 84 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annuncia
70. d be serviced MANIFEST GFC software mismatch communication halted 190 00567 05 Rev A Incorrect servo software is installed or gain settings are incorrect Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 87 SoJnjeo aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu euonippv uoneiedo Jeuuouqy ui EY x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message MANIFEST COM1 software mismatch communication halted MANIFEST CON2 software mismatch communication halted Comments COM1 and or 2 software mismatch The system should be serviced MANIFEST NAV1 software mismatch communication halted MANIFEST NAV2 software mismatch communication halted NAV1 and or NAV2 software mismatch The 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 temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE
71. d 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 It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of 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 measurements needed to determine a position Changes in wind speed and or wind direction compounds the relative inaccuracy of DR Mode Because of this degraded accuracy the crew must maintain position awareness using other navigation equipment until GPS derived position data is restored CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 67 sjueuingjsu UATE s mp oud Bu
72. do Jeuuouqy PY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea 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 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The system should be serviced GDC 74A MESSAGE ADVISORIES Message Comments MANIFEST GDC1 software mismatch communication halted The GDC 744 has incorrect software installed The 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 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
73. e mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced GTX 33 MESSAGE ADVISORIES Message XPDR1 CONFIG XPDR1 config error Config service req d Comments The transponder configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GTX1 software mismatch communication halted The transponder has incorrect software installed The 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 90 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN GRS 77 MESSAGE ADVISORIES Annunciations amp Alerts Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The 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 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
74. e highlighted waypoint as indicated by the insertion point indicator If this waypoint is not a valid airway entry point a valid entry point should be entered at this time Turn the small FMS Knob one click clockwise and 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 Turn the FMS Knob to select the desired airway from the list and press the ENT Key Low altitude airways are shown first in the list followed by all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Flight Planning INVERT AN ACTIVE FLIGHT PLAN sjuauimasu BUT 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan 59 oipny uadx 0105 AEN REMO
75. e small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 Themessage Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 31 Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 32 NOTE When creating a 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 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 The active flight plan is modified as each waypoint is entered R
76. eference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified The file stored on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import Flight plan import failed The SD card contains no flight plan data Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan truncated The flight plan on the SD card contains more waypoints than t
77. eferences 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 66 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN 0 Abnormal operation A NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displaye
78. entane amp Notet GARMIN ee WARNING Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age 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 It is thus the responsibility of the pilot to detect such an occurrence by means of cross checking with all redundant or correlated information available in the cockpit WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs informatio
79. epeat 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 5 6 1 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 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN IMPORT A FLIGHT PLAN FROM AN SD CARD 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the MFD to display the Ac
80. eration Features Avoidance Index A Flight Planning GARMIN EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 1 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 EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 2 3 4 5 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 waypoint to be deleted Press the CLR Key to display a REMOVE Wpt Name confirmation window With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key Once all changes have been made press the FMS Knob to remove the cursor INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 2 3 36 Press the FPL Key on the MFD Turn the s
81. ertical speed input from the air data computer A red X through any other display field such as engine instrumentation display indicates that the field is not receiving valid data 70 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN 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 Left Alternator offline Single Chime Left Alternator Out Corvalis only 4 High pressure oxygen outlet only tLow pressure oxygen out 190 00567 05 Rev A 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 Single Chime None Pressure above 12 000 ft and oxygen off Single Chime None Oxygen outlet pressure below 60 psi Single Chime None Oxygen outlet pressure below 16 5 psi Single Chime None Oxygen
82. ervice req d The GIA1 and or GIA2 have an error in the GIA2 CONFIG GIA2 audio config error Config service req d audio configuration The system should be serviced GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too low GIA2 COOLING GIA2 temperature too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIAT ove temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 83 soJnjeoJ 2 Buruuejd AEN 5649 24V olpny uqax sia siu un su paezey nubi jeuonippy uoneiedo Jeuuouqy Hw x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN GIA 63 MESSAGE ADVISORIES CONT Message Comments Return the unit for repair GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced communication halted communication halte
83. ex Appendix 5 Annunciations 8 Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR 1 terrain database error exists PFD1 DB ERR 1 terrain database error exists Comments The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace terrain card If problem persists the 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 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 system should be serviced MFD1 DB ERR MFD1 air
84. he active flight plan Sue v unuuy gt 5 3 x x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 99 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A GARMIN Appendix Level 1 Level 2 Level 3 Description VVX LGND Displays icon and age on the Inset Map for the selected weather products optional 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 STRMSCP Displays Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft optional NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optional 100 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Appendix wser 1 85 cor wrowe ror weNr mR vest atenrs p n NS Eu au n siu un sul sub n gt SYN VIS DFLT
85. he Cessna Corvalis Corvalis TT 2 sia sjueuinsu wio gt AeN iui olpny uqax 52 eouepioAy paezey Suelv uoneiedo sainjea4 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 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 w
86. he INHIBIT Softkey Or 1 Press the MENU Key 2 Turn the small FMS Knob to select Inhibit TAWS 3 Press the ENT 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 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 53 AeN Sd5 S24V oipny uadx si syueuimnajsu u102 AEN 1014 buluueld nubi e uepioAy s mp oold paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Hazard Avoidance Sjueuinijsu fila 59 oipny uadx U105 AEN S2dV AeN Sd5 Duruue d Blank Page 6 2 4 eouepioAy DX s m d Jeuonippy uoneiedo jeuuouqy suay junuuy xipuaddy x pul 190 00567 05 Rev A Garmin 61000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 54 GARMIN 0 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 de
87. he Terrain SVS Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Enable Terrain 3 Press the ENT Key A NOTE If Terrain SVS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 51 AEN 640 S24V oipny uadx sia Sjueumajsul J05 AeN iui Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index A Hazard Avoidance GARMIN TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY OPTIONAL NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS operation is only available when the G1000 is configured for a TAWS B installation Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in wor
88. he system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 97 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 Sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy ic PET x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES CONT Flight Plan Import Export Results User waypoint database full Not all loaded Description The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed Flight plan successfully exported
89. hin the airport plan view Selecting 56 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN 0 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 maneuvering 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
90. ht Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint 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 the 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 05 Rev A A GARMIN STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window
91. ically 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 Flight Planning 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 waypoint 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 the desired waypoint Press the ENT Key 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 29 sjuauimasu sub oipny uddx 993 UI0JNeN 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy 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
92. ication system ENGINE INDICATION SYSTEM Sjueuinijsu UATE SE H e HE o 52 AEN 549 a EAL 8 10 z 30 40 F FFLOWGPH 17 0 FUEL QTY GAL v i 6 16 26 38 46 F FFLOW GPH 16 2 LOL n j j ja Duruue d Wil 6 45 OIL PSI 46 Ld A 4 Cd OIL F 30 OIL PSI 46 s ELEV OIL F 178 TRIM 11 SeJnpa20Jd TIT F 1549 1549 Al 4 aoueplony paezey EGT F 1350 hq 350 Vv sounjeo4 Jeuonippy CHE 9 AILERON TRIM w AILERON TRIM b d eoo Corvalis Corvalis TT 2 EIS Display 27 O Engine Manifold Pressure Gauge Exhaust Gas Temperature Indicator 5 Corvalis only Tachometer Turbine Inlet Temperature Indicator Q Fuel Quantity Indicator Corvalis TT only Fuel Flow Indicator 9 Cylinder Head Temperature Indicator G Oil Pressure Indicator Trim Group Oil Temperature Indicator xipueddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 5 ENGINE PAGE GARMIN 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 navi 108 00 1
93. ilable bad geometry Comments Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected A parallel course has been selected causing the vertical deviation to go invalid NON WGS84 WPT Do not use GPS navigation to Xxxx 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 no
94. inder Head Temperature emperature uoneiedo Jeuuouqy TEHPERATURE IE Gas EST F TIT F CHT F emperature 163415801624 1463 1436 382 328 374 1908 499g 88216521652 Pu saa 20 355 356 1758 1600 5 unuuy xipueddy 400 1620 1450 1450 E 380 1300 1150 200 1150 1800 7584556 180 123456 Engine Temperature Group Corvalis TT x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 9 ENGINE LEANING ASSIST MODE GARMIN 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 nav1 188 88 113 08 B TRK navz 108 00 118 68 EIS ENGINE FFLOW GPH TEMPERATURE EGT F PER 156213821202 A PEAK aqa 165214721282 500 1750 1600 V 1450 1300 1150 lt 1000 Tz L4 OCLTR 134 888 118 888 com 123 888 118 888 conz EGT Deviation from Peak CHT F 356 338 320 sog 792 320 374
95. ing Mode Between 360 and 120 1 2 Select the Stormscope Page Press the VIEW Softkey The 360 and ARC Softkeys are displayed Press the 360 Softkey to display a 360 viewing area or press the ARC Softkey to display a 120 viewing area Press the CLEAR Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Hesr Avoidance SIRIUSXM WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions Displaying SiriusXM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD XM LTNG and METAR 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 Tum 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 TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 3 Select
96. ion If the problem persists the system should be serviced G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 89 s m p q e ueproAy SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 Sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy EST x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 224 Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair Comments A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEAT configuration settings do not match those of backup configuration memory The system should be serviced MANIFEST GEA1 softwar
97. is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The 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 system should be serviced GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred MANIFEST GMU1 software mismatch communication halted A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced The GMU 44 has incorrect software installed The system should be serviced 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 91 sainjeay aoueplony SoJnpa204d buluueld AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneie
98. isplay unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid 82 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts 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 system should be serviced GMA1 CONFIG GMAT config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced MANIFEST GMAT software mismatch communication halted The audio panel has incorrect software installed The system should be serviced GMA1 SERVICE GMAT needs service Return unit for repair The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63 MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d The GIA1 and or GIA2 configuration settings GIA2 CONFIG GIA2 config error Config service req d EL o not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 audio config error Config s
99. ith 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 approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 94 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message PTK FAIL Parallel track unava
100. ity to operate this device under FAA FCC regulations 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT A Warnings Cintana S H l GARMIN NOTE All visual depictions contained within this document including screen images of the G1000 panel and displays are subject to change and may not reflect the most current G1000 system and aviation databases Depictions of equipment may differ slightly from the actual equipment NOTE This device complies with part 15 of the FCC Rules 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 Do not rely solely upon data link services to provide Temporary Flight Restriction TFR information Always confirm TFR information through official sources such as Flight Service Stations or Air Traffic Control 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 q
101. 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 100 3 Press the CNTRST or CNTRST to adjust display contrast in five percent increments from 0 to 100 4 Press the SAT or SAT to adjust display saturation in five percent increments from 0 to 100 Additional Features 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 61 s mp o4d Buruuejd AeN Sd5 S24V olpny uqax sia s u u nnsul Wfl Tu102 AEN sub aoueplony paezey xipuaddy Sue v uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy 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 Selecti
102. king order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 2 3 4 52 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page 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 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Hazard avoidance 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 A 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 t
103. lity or city b Press the ENT Key 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 33 sjuauimasu UATE olpny uqax si UI0JNeN 52 SoJnpa204d 4 AEN 540 nubi eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy 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 A GARMIN 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 c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key e Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 34 1 2 3 4 5 6 7 Press the FPL Key Press the FMS Knob to activate the cursor not required on the PFD Turn the large FMS Knob to highlight the waypoint after the desired airway entry point The airway is inserted before th
104. llites 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 GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cyde its operat
105. mall FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN ri ht tanning 4 Turn 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 Turn 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 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 Turn 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
106. n WGS84 waypoint TRAFFIC FAIL Traffic device has failed The system 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 95 sainjeay aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy EET x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments SRMSCP FAIL Stormscope has failed Stormscope has failed The system should be serviced MAG VAR WARN Large magnetic variance Verify all course angles 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
107. n 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A amp GARMIN Warnings Camions amp Notes WARNING The illustrations in this guide are only examples Never use the G1000 to attempt to penetrate a thunderstorm Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding by at least 20 miles any thunderstorm identified as severe or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal isp WARNING Because of variation in the earth s magnetic field operating the system within the following area
108. nal LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected BACK Returns to top level softkeys 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Appendix Level 1 Level 2 Description SHW CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists CHECK Pressing this softkey checks off a checklist item If an item is already checked an UNCHECK Softkey is displayed EXIT Press to exit the checklist EMERGCY Press to display the emergency checklist LOADING UPDATED DATABASES Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in main tenance being required to reboot the system NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to ob
109. ntents ABNORMAL OPERATION Reversionary Mode sssssssssseseeene nennen Abnormal COM Operation sse Audio Panel Fail safe Operation Hazard Displays with Loss of GPS Position 65 Unusual Attitudes uode ete nn ee Lau be od bea incedit 66 Dead Reckoning orem te e med rm e e ten 66 ANNUNCIATIONS amp ALERTS LL 69 61000 System Annunciations sse 69 WARNING Alerts ete n CAUTION Alerts eee ete eni ee el a n Annunciation Advisory ssssssssseeenenennennnennnnnnns 72 Message Advisory Alerts 72 CO Guardian Messages 72 AFCS Alerts Terrain SVS Alerts oot Guten anes ot deer atrae 74 Terrain SVS System Status 5 74 TAWS B Alerts Voice Alerts saddle rena be dn urba Ra dn boi la Ha M s MFD amp PFD Message Advisories ssssssssseenne 78 Database Message Advisories GMA 1347 Message Advisories ssssssssseene GIA 63 Message Advisories sssssssssee nnne GIA 63W Message Advisories GEA 71 Message Advisories GTX 33 Message Advisories GRS 77 Message 501
110. on 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 display 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 62 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Md itimal Features ELECTRONIC CHECKLISTS The system acces
111. or exc im ndi 2 m othe tent seo information arisin the August 2012 f pa da allowed by g out of Ga imitation o action dai sclaim all warranties wi ied including but not limited to the implied warran ticular purpose The information is provided as is and AOPA does n ke any representations regardi iabili stances including negligence shall AOPA be mages that result from the use or inability to even if AOPA or an AOPA authorized representati uch damages User agrees not e and hold harmless AOPA from any causes o alleged inaccuracies in the inform usion of implied warranties o tations or exclusions may not ts related organizations hereafte all warranties with respect ess or implied including but ty and fitness for a particular pu WIK Organizations do not warrant o Wise Licensee agrees not aw to release ms or losses re rmin s use of th and hold harm th respect to the AOPA ng its accuracy re iab h to sue AOPA and to t f acti ation Some ju e for use t ve has been advised of t e maximum extent allowed or losses re risdictions do not allow the infor ties 0 ty or othe any in he sof on daims liabi app lity for incidenta y to you to not li pose The in make any rep tos f ated e inf to any ac tware or related or conseq collectively AC U KWIK Organization the
112. orvalis TT Traffic Symbol Description 4 Sue v uoneiedo SoJnjeaJ EI SaJnpa20Jd Duruue d AEN Sd5 S24V oipny uadx 93 siu uinnsu junuuy Jeuuouqy Jeuonippy p EzeH Tu102 AEN xipuaddy x pul iui nuru Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance 48 A GARMIN Traffic Information Service TIS NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Naviga
113. ot 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 in the navigation database Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT flight path guidance 190 00567 05 Rev A GARMI N LLL Hlght Planning FLIGHT PLANNING TRIP PLANNING 1 Tum the large FMS Knob to select the AUX page group 2 Turn the small FMS Knob to select the Trip Planning 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
114. ottom 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 05 Rev A GARMIN X U AlomalOperatin ABNORMAL OPERATION REVERSIONARY MODE sjueuinasu nubi 59 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 oipny uddx UI0JNeN Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel S24V NOTE The Cessna Corvalis Corvalis TT Airplane Flight Manual AFM always takes precedence over the information found in this section AEN Sd5 ABNORMAL COM OPERATION Duruue d nubi 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 s snp old AUDIO PANEL FAIL SAFE OPERATION aoue
115. ow 15 in one VAPOR SUPPR Turn on Vapor Suppression one Corvalis TT only CO GUARDIAN MESSAGES Alerts Window Message Comments monoxide detector needs Services Service tive CO DET FAIL The carbon Loss of communication between the G1000 and the CO monoxide detector is inopera Guardian 72 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts 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 2 c MET Switch Stuck or Pitch Trim Axis Control Failure D 20 lt If annunciated when oft half of the MET switch separately to check if a stuc switch is causing the annunciation AP is engaged take control e aircraft and disengage the autopilot If annunciated when AP is not engaged move each System Failure T gt TI SE Cc AP and MET are unavailable FD may still be available Elevator Mistrim Up A condition has developed causing the pitch to apply nose Servo to provide a s autopilot disconnect up control wheel force upon ustained force Be prepared Elevator Mistrim Down Aileron Mistrim Left to apply nose provide a sustained f Servo to provide a s autopilot disconnect
116. pair The PFD and or MFD self test has detected a problem The system should be serviced MANIFEST PFD1 software mismatch communication halted MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CONFIG PFD1 config error Config service req d The PFD configuration settings do not match backup configuration memory The system should be serviced 78 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp 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 system should be serviced The MFD and PFDs have different software versions installed The 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 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 f
117. permission 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 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 of L 3 f Jeppesen Inc Stormscope is a registered trademark Communications SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AOPA Membership Publications Inc and AOPA expressly di data express or imp f and fitness warrant or m Under no ci or conseque documentat possibility of by law to re to any actua limitation or so the above AC U KWIK a y disc in this data exp express merchantabil AC U K eliability or maximum ex from any cau do not allow consequential damages so th C n io S 0 d d um tla n eas
118. played when the aircraft is outside the installed terrain database coverage area Display Terrain on the TERRAIN SVS Page 1 Turn 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 clockwise to display a smaller area Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude Black 50 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Hazard avoidance 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 t
119. plony paezey If there is a failure of the Audio Panel a fail safe circuit connects the pilot s headset and microphone directly to the COMI transceiver Audio is not available on the speaker during Fail safe operation saunyea4 Jeuonippy 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 Sue v unuuy BACK Loss of Hazard Functions with Loss of GPS Position xipuaddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 65 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 unusual attitude Only the primary functions are displayed in these situations The following information is removed from the PFD and corresponding softkeys are disabled when the aircraft experiences unusual attitudes Traffic Annunciations System Time Glideslope Glide 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 R
120. port terrain database missing PFD1 DB ERR PFD1 airport terrain database missing MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1 Safe Taxi database error exists The airport terrain database is present on another LRU but is missing on the specified LRU 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 system should be serviced 80 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 Chartview database error exists Comments The MFD detected a failure in the ChartView database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists PFD1 DB ERR PFD1 Airport Directory database error exists The MFD and or PFD detected a failure in the Airport Directory database Ensure that the data card is properly inse
121. pproximately 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 Cycles the Bearing 2 Information Win dow through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Select to display the BARO setting as inches of mercury 102 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A dh GARMIN Appendix Level 1 Level2 Level 3 Description 2 HPA Select to display the BARO setting as 5 hectopacals STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa E olpny uqax uo2 AEN n n n nnnu gt nm nu n LA n Press the BA
122. quantity below 250 psi Single Chime None Rudder limter is engaged Starter relay has power applied g Single Chime None g Single Chime None et only Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 71 soinjeo4 9e2uepioAy SoJnpa20Jd Duruue d ACN 540 S24V olpny uqax s q Sjueuinijsu 2 Wil uio AeN iui jeuonippy uoneiedo jJeuuouqv iie EN x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Med Annunciations amp Alerts A GARMIN ANNUNCIATION ADVISORY Annunciation Window Alerts Window Message Audio Alert Text AP TRIM OFF AP TRIM master switch is in the OFF position None OXYGEN ON Reminder Turn off oxygen None RUDR HOLD Rudder hold is engaged None SPEED BRAKES Speed brakes are active None Corvalis TT only MESSAGE ADVISORY ALERTS Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative one MFD 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 FUEL IMBAL Fuel imbalance is greater than 10 gallons one LOW MAN PRES Manifold pressure is bel
123. r errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Loading Garmin Database Updates 1 2 3 4 5 6 7 8 9 10 11 12 108 With system power OFF remove the MFD database card from the bottom card slot of the MFD Update the Garmin databases on the MFD card Insert the MFD database card into the bottom card slot of the MFD Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 Acknowledge the Power up Page agreement by pressing the ENT Key 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 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed Remove and reapply power to the system 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 PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for
124. r 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 21 sjuauimasu UATE 53 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d unuuy Jeuuouqy Jeuonippy paezey n xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlig
125. rary user waypoints Added CDI availability during Dead Reckoning mode Added new MFD page navigation Added other GDU 10 01 parameters 190 00567 05 Updated to GDU 12 03 parameters Added METAR STRMSCP and weather LEGEND softkey functions Added Profile View Added AC U KWIK Airport Directory Added MV DB update procedure Added Stormscope Added flight plan enhancements Updated weather legend Updated database procedures Updated message advisories nm Date of Revision Affected Pages August 2012 Production Release 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT RR 1 Record of Revisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 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 Tlmel cito e RO a re as mid duda 2 Configure Vspeed Bugs 2 Set Barometri
126. ree the stuck key by pressing it several times The system should be serviced if the problem persists CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced MFD1 VOLTAGE MFD1 has low voltage Reducing power usage The MFD voltage is low The system should be serviced DATABASE MESSAGE ADVISORIES Message MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists Comments The MFD and or PFD detected a failure in the navigation database Attempt to reload the aviation database If problem persists the 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 79 saunqea4 2 AEN 5649 24V olpny uqax sia s u un su paezey nubi u102 AEN Wil jeuonippy uoneiedo Jeuuouqy EST x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Ind
127. remaining GAL 28 REM in 1 gallon increments INCFUEL Increases the gallons of fuel remaining GAL 8 REM in 1 gallon increments RST FUEL Resets the fuel remaining to 98 or 102 gallons MAP Enables second level Navigation Map softkeys H TRAFFIC Displays traffic information on Navigation Map 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 105 Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix A Appendix GARMIN Level 1 Level 2 Description PROFILE Displays removes Profile View on Navigation Map Page TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map TERRAIN Displays terrain information on Navigation Map AIRWAYS 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 STRMSCP Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft NEXRAD Displays NEXRAD weather and coverage information on Navigation Map optional XM LTNG Displays XM lightning information on Navigation Map optional METAR Displays METAR flags on airport symbols shown on the Inset Map optio
128. rn 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 Toremove 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 Toremove 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Flight Instruments 3 ze ca m a g 2 o a sualy uonesado so1njeoJ 2 Buruuejg AEN 5649 S24V oipny uadx sia junuuy jeuuouqy feuonippv paezey ETSI wio gt AeN xipuaddy x pul GARMIN Flight Instruments I x oipny uadx U105 AEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT GARMIN Engine Ind
129. rometric pressure 103 C Carbon monoxide detection 7 CDI 2 14 94 Cell 43 44 Cell mode 44 Channel Presets 60 ChartView 56 57 Checklists 63 64 Clearance player 15 Clearance Recorder 15 190 00567 05 Rev A Index Code selection softkeys 13 COM 14 15 65 Cylinder Head Temperature CHT F 5 9 D DB Mismatch 107 110 DCLTR Softkey 56 Dead Reckoning 66 Declutter 66 99 106 Declutter EIS 9 Direct to 21 DME 13 14 DR mode 66 67 68 E Edit a flight plan 36 Electronic checklists 63 64 Emergency checklist 64 Enable Terrain 51 Endurance calculated ENDUR 8 Engine leaning assist 10 12 Engine Manifold Pressure MAN IN HG 5 6 Exhaust Gas Temperature EGT F 5 9 10 11 F Fail safe operation 65 FD 73 Flight Director 17 Flight path marker 55 Flight plan import export messages 97 98 FliteCharts 56 57 Frequency Transfer 14 Fuel calculations 8 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT ndex 1 sainjea4 aoueplony SoJnpa204d buluueld AEN Sd5 S24JV olpny uqax sia s tin sul jeuonippy 2 wold Tuo2 NeN qb uoneiedo Jeuuouqy sue v unuuy 1221 Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Lee Appendix Index Fuel Flow FFLOW GPH 5 6 10 Fuel flow totalizer 8 Fuel quantity FUEL QTY GAL 5 6 Fuel remaining
130. rrain Impact TERRAIN Warning Terrain Warning ITI Terrain Reduced Required Obstacle TERRAIN Warning Obstacle Clearance Warning 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 Deis ite Annunciation Annunciation Message System Test in Progress TER TEST one Terrain System Terrain System Test Fail No GPS position System Test Pass None None Test OK Terrain Alerting is disabled TER INH None one 74 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT Terrain System Failure Terrain System Not Available 190 00567 05 Rev A A GARMIN Annunciations amp Alerts Rate Warning EDR PFD MFD Alert TERRAIN SVS Page Aural Alert Type Annunciation Annunciation Message Terrain or Obstacle d
131. rted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 multiple database errors exists PFD1 DB ERR PFD1 multiple database errors exists The MFD and or PFD detected a failure in more than one database If problem persists the system should be serviced NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database DB MISMATCH Navigation database mismatch Xtalk is off The PFD and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 00567 05 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 es EE x pul Hazard Flight Nav Com Fight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Standby Navigation database mismatch Comments
132. ruuejd AEN Sd9 S24V oipny uadx si lu Tuo2 AEN eouepioAy paezey saunyea4 jeuonippy xipuaddy 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 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 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 68 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Amnuncitions amp Alerts ANNUNCIATIONS amp ALERTS G1000 SYSTEM ANNUNCIATIONS When an LRU or an LRU function fails a large red X is typically displayed on win do
133. s 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 serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s author
134. ses 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 7 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 box 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 CHEC
135. 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 1 uonesado So1nje2J aoueplony s mp oold Buruue d AEN Sd5 2 oipny uddx sia junuuy jeuuouqy paezey nubi u102 AEN xipuaddy x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Planning AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Flight Instruments A GARMIN CHANGE NAVIGATION SOURCES 1 2 3 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 Select the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV2 standby frequency Select the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 2 3 Select the OBS Softkey to select OBS Mode Turn a CRS Knob to select the
136. tain 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 If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window 1f synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 107 sainjea4 aoueplony SoJnpa20Jd Duruue d AEN Sd5 S24JV oipny uddx 513 sjuauimasu jeuonippy 2 ni yb uoneiedo Jeuuouqy Sue v unuuy bed 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 7 GARMIN Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all othe
137. te 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 93 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy EST 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 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 w
138. termining 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 dimensional 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 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 55 xipuaddy suelv uoneiedo sainjea4 aoueplony saunpadoig Duruue d AEN Sd5 S241V olpny uqax sia sjuauimasu junuuy Jeuuouqy Jeuonippy p EzeH ubi u05 AeN BUTLER 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 0 GARMIN Displaying Pathways 1 Select the PFD Softkey
139. the available softkeys to select the desired XM weather product 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 or SIGMETs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 45 AEN 640 S24V oipny uddx sia Sjueumajsul Tuo2 AEN iui Duruue d nubi aoueploay s mp oold paezey suelv uoneiedo sainjea4 junuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Annun Flight Instruments Flight Planning AFCS EIS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN Siri
140. tion Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS Optional Displaying Traffic on the Traffic Map Page 1 2 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page OPERATING is displayed in the Traffic Mode field Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A GARMIN Hazard avoidance 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 is outside the installed terrain database coverage area Displaying Terrain and Obstacles on the Terrain Proximity Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Terrain Proximity Page 3 If desired select the VIEW
141. tions amp Alerts GIA 63 MESSAGE ADVISORIES CONT Message Comments COM1 PTT COM push to talk key The COM1 and or COM external push to talk is stuck switch is stuck in the enable or pressed COM2 COM2 push to talk key Position Press the PTT switch again to cycle its is stuck operation If the problem persists the system COM1 RMT XFR COM remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck should be serviced 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 system should be serviced COM1 CONFIG COM1 config error Config service req d COM2 CONFIG 2 config error Config service req d The COM1 and or COM2 configuration settings do not match backup configuration memory The 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 LOI GPS integrity lost Crosscheck with other NAVS Loss of GPS integrity monitoring GPS NAV LOST Loss of GPS naviga ff tion Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of
142. tive 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 either FMS Knob to highlight an empty or existing flight plan 6 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 Flight Planning 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 another existing or empty flight plan and again press the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 If necessary press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint as indicated by the insertion point indicator 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 faci
143. turn the large FMS Knob to highlight CANCEL and press the ENT Key sjuauimasu BUT oipny uddx UI0JNeN 52 2 AEN 540 nubi eouepioAy paezey Suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 37 Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index A Flight Planning GARMIN GRAPHICAL FLIGHT PLAN CREATION 1 2 3 4 5 Press the FPL Key to display the Active Flight Plan Page on the MFD 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 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 as indicated by the insertion point indicator Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint is inserted at the selected point The default user waypoint naming is USR000 USR001 USR002 and so on To change the user waypoint name follow the procedure for modifying a user
144. uestions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide th e 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 Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN 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 Removed Stormscope 190 00567 04 Added Tach Timer Added Flight Plan Import Export Added AOPA Airport Directory Added Auxiliary Video Added tempo
145. usXM Weather Products and Symbols Wx Product Status Icons Description US 3m CN Bm NEXRAD Available for the US and Canada The age of the displayed data for each is shown at the right 5m ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed p 12m CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed 3m i XM LIGHTNING The age of the displayed data is shown at the right 2m CELL MOVEMENT The age of the displayed data is shown at the right SIGMET 2m AIRMET 5m SIGMET amp AIRMET The age of the displayed data for each is shown at the right F us 8m CN 8m METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is Shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom COUNTY WARNING The age of the displayed data is shown at the right CYCLONE WARNING The age of the displayed data is sho
146. wn at the right Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 190 00567 05 Rev A A GARMIN Hazard Avoidance Wx Product Status Icons Description 2m AIREP The age of the displayed data is shown at the right m 2 E PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow 68m 21000FT TURBULENCE The age of the displayed data is shown at the right The altitude selection is shown at the bottom 4m BDO OFT ICING POTENTIAL The age of the displayed data is shown at the right The altitude selection is shown at the bottom No Status Icon TFR Depicted as an area outlined in yellow 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 Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation 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 GOSOD Traffic Advisory Off Scale 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis C
147. ws associated with the failed data Refer to the Corvalis Pilots Operating Handbook POH for additional information regarding pilot responses to these annunciations System Annunciation Comment Attitude and Heading Reference System is aligning Display system is not receiving attitude information from the AHRS GPS information is either not present or is invalid for navigation use Note that AHRS utilizes GPS inputs during normal operation AHRS operation may be degraded if GPS signals are not present see POH Display system is not receiving valid heading input from AHRS BEZ Display system is not receiving valid transponder information 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 69 uonesado so1njeoJ 2 Buruuejd AEN Sd5 24V oipny uadx sia sjuaumjsu jeuuouqy jeuonippy paezey nubi U105JNeN nubi xipuaddy x pul Amundatons amp Alerts GARMIN G1000 SYSTEM ANNUNCIATIONS CONT Flight Instruments System Annunciation Comment Flight Nav Com Planning GPS Nav AFCS XPDR Audio EIS Procedures Hazard Avoidance Other Various Red X Indications Additional Features Abnormal Operation Index Appendix Ea Display system is not receiving airspeed input from air data computer Display system is not receiving altitude input from the air data computer Display system is not receiving v
148. x or move up the list with the CH Softkey 190 00567 05 Rev A Garmin G1000 Cockpit Reference Guide for the Cessna Corvalis Corvalis TT 59 SH lV uonesado s n e 4 aoueplony s mp oold Buruue d AEN Sd5 2 444 sia sjueumasu unuuy jeuuouqy jeuonippy paezey il 0105 AEN ubi xipueddy 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 Additional Features 60 3 A GARMIN Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels With the desired channel highlighted press the ENT Key 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 Select 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

Garmin Software Version 0534.21 Cockpit Reference Guide

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