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Garmin Software Version 0858.09 Cockpit Reference Guide

1. Hazard Displays with Loss of GPS Position Unusual Attitudes snnnnnnnnnnnnn MEC O iem te e ere ee eter ANNUNCIATIONS amp 57 WARNING Annunciation sse 57 CAUTION Annunciation sssssssennennnnnnnnnnnnne 57 ADVISORY Annunciation sse 58 Alert Message eee teen ie Ee iba deett 58 APCS ALERTS non eno 0000000000 0 58 esee ote SEHR LE Reb P EA te endis 59 TAWS B System Status Annunciations ssssssenes 61 Voice Alerts MFD amp PFD Message Advisories ssssssssenne 63 Database Message Advisories GMA 1347 Message Advisories GIA 63W Message Advisories GEA 71 Message Advisories sssssssseee ne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories sssssesee nne GDL 69 69A Message Advisories GDC 74A Message Advisories GTS 820 Message Advisories Miscellaneous Message Advisories Flight Plan Import Export Messages APPENDIX GT T M 79 PED Softkey Map rct titt e tutt tete ette 79 MED Softkey nnne nnne 84 Database Updat
2. 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 c Press the ENT Key 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 25 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 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 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 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 c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 11 Press the ENT Key The curs
3. The PFD and or MFD has incorrect software installed The system should be serviced The PFD configuration settings do not match backup configuration memory The system should be serviced MFD1 CONFIG MFD1 config error Config service req d The MFD configuration settings do not match backup configuration memory The system should be serviced SW MISMATCH GDU software version mismatch Xtalk is off The MFD and PFD have different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor MFD1 COOLING MFD1 has poor cooling Reducing power usage 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 free 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 190 00525 04 Rev A 63 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 soJnjeoJ 2 Buruuejg AEN Sd 24V olpny uqax sia s u un sul paezey nubi u102 AEN nubi jeuonippy
4. 2 Buruuejd AeN Sd5 S24V oipny uadx sia siu u nnsul fila Tu102 AEN 346 aoueplony paezey xipuaddy suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Entering a Channel Directly 1 2 3 4 While on the XM Radio Page press the CHNL Softkey Press the DIR CH Softkey The channel number in the Active Channel Box is highlighted Press 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 while listening to an Active Channel that is wanted for a preset press the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Press the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Pressing the MORE Softkey repeatedly cycles through the preset channels 3 Press the SET Softkey 4 Press any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 1 On the XM Radio Page press the RADIO Softkey 2 Press
5. n e 4 aoueplony s mp oold Buruue d AEN Sd5 unuuy jeuuouqy jeuonippy paezey xipueddy x pul nu GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 59 oipny uadx U10 AeEN s24v AeN Sd5 buluueld r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 636 12 A GARMIN AUTOMATIC FLIGHT CONTROL SYSTEM AFCS NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavallable 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 PIT AP Key Roll Hold default ROL Pitch Hold default PIT CWS Switch Roll Hold default ROL Pitch Hold default PIT GA Switch Go Around GA Go Around GA ALT Key Roll Hold default ROL Altitude Hold ALT VS Key Roll Hold d
6. r3 v3 AIRWAY HI Press the ENGINE or BACK softkey on any level to return to the default page level 1 Y LEAN SYSTEM FCYLSLCT assist BACK F3 A F3 V3 V EN MFD Softkeys Level 1 Level 2 Level 3 Description ENGINE Displays the LEAN and SYSTEM softkeys LEAN Displays the engine leaning softkeys CYLSLCT Selects the desired cylinder for monitoring ASSIST Highlights the first cylinder that peaks and displays information for that cylinder BACK Press to return to the top level softkeys SYSTEM Displays fuel system softkeys DEC FUEL Press to decrease fuel quantity in 1 gallon increments INCFUEL Press to increase fuel quantity in 1 gallon increments RST FUEL Press to reset fuel to full 84 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description MAP BACK TRAFFIC PROFILE TOPO TERRAIN AIRWAYS STRMSCP NEXRAD XM LING METAR Press to return to the top level softkeys Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays removes Profile View on Navigation Map Page Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles throug
7. A GARMIN 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 Press the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Press 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 Press 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 Navigation Map displayed press the MAP Softkey Press the TRAFFIC Softkey Traffic is now displayed on the map Traffic Advisory System TAS If Installed Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 7 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 or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the ALT MODE Softkey to change the altitude volume Select the desired altitude volume by pressing the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field Select the STANDBY Softkey to place the system in th
8. BRG1 GPS BRG1 OFF BRG GPS L 1L IL L veers Jane ec J ater F3 V3 V3 F3 n n nn n n n onm umumi o su o io L Lom oem opts or ll l amp c ALERTS 7 V3 V3 7 7 HU UNU n9 nm Ene fared ses CCC ee raz Nu m im PFD Configuration Softkeys 80 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description PFD SYN VIS DFLTS WIND DME BRGI HSI FRMT PATHVVAY SYN TERR HRZN HDG APTSIGNS OPTN1 OPTN 2 OPTN 3 OFF 360 HSI ARC HSI Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Headwind tailwind and crosswind arrows with numeric speed componen
9. 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 SVS offers a three dimensional view of terrain and obstacles Terrain and obstacles that pose a threat to the aircraft in flight are shaded yellow or red In addition to SVS enhancement to the PFD the following feature enhancements 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 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 Press the SYN TERR Softkey 4 Press the BACK Softkey to return to the previous page 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 4 xipuaddy SH V uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax 513 sjuauimasu junuuy Jeuuouqy Jeuonippy paezey ubi wo gt AeN ubiu x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN Displaying Pathvvays 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN
10. 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 waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Flight Planning 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 sec
11. aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 A GARMIN 190 00525 04 Rev A GARMIN Engine Indication System ENGINE INDICATION SYSTEM s3u u nnsu sub ENGINE DISPLAY In all cases green indicates normal operation yellow indicates caution and red indicates warning Pressing the ENGINE Softkey makes available the LEAN and SYSTEM Softkeys which in turn provide access to the Lean Page and the System Page respectively Manifold Pressure Gauge BAEO E 3f BS ED e 524 52 S i lt RPM Gauge RPH 2080 Fuel Fl za 0 uet FLOW 2380 a Fuel Flow FFLOW GPH Readout Indicator Leaning E Pointer 8 Cylinder Head Oil Temperature OIL TEMP Temperature ndicator x Indicator z OIL PRES SE x Oil Pressure ALT LOAD Indicator d Ammeter MS z BUS VOLTS p ze ah Voltmeter 8g Fuel Quantity rd a 92 Indicator LEE LN 88 i 37 2 Default Engine Page Sue v unuuy In a maximum power climb or cruise climb engine leaning may be done using the Leaning Pointer
12. 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 IMPORT A FLIGHT PLAN FROM AN SD CARD 28 1 2 3 4 5 6 7 8 NOTE See the Annunciations amp Alerts section for flight plan import message descriptions Insert the SD card containing the flight plan in the top card slot on the MFD Press the FPL Key on the MFD to display the Active Flight Plan Page Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn either FMS Knob to highlight an empty or existing flight plan Press the IMPORT Softkey If an empty flight plan is selected a list of the available flight plans on the SD card will be displayed Or If an existing flight plan is selected an Overwrite existing flight plan OK or CANCEL prompt is displayed Press the ENT Key to choose to overwrite the selected flight plan and see a list of the available flight plans on the SD card If overwriting the exis
13. ut the express written permission of Garmin Garmin hereby grants permission to 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 nted copy of this manual or revision must contain the complete text of this copyright hat any unauthorized commercial distribution of this manual or any ct Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and used without the express permis NavData is a registered trademark o f afeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be ion of Garmin Un f Jeppesen Inc Stormscope and SkyWatch are registered trademarks of L 3 Communications and SiriusXM is a registered trademark of SiriusXM Satellite Radio Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fi f tness for a particular purpose The information is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances including negligence
14. x pul Flight Instruments Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun EIS GPS Nav AFCS Appendix Alerts Operation Features Avoidance Procedures 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 distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or 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 Press 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
15. CARD 2 ERR Card 2 is invalid MFD conta he SD card in the bottom card slot of the PFD or ins invalid data 76 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 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 A flight plan file stored on the SD card was successfully imported as a stored flight plan Description 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 waypoints have been saved to the system user waypoints No flight plans stored in the system have been user waypoints These modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight p imported from the SD card an data was not successfully Flight plan partially imported Some fl imported from the SD card however others had e stored flight plan now exists in the system 4 ight plan waypoints were successfully rors and were not imported A partial File contained user waypoints only Th ab Su e fi flight p more of these waypoints did n
16. COM1 TEMP COM over temp The system has detected an over temperature Reducing transmitter power condition in COM1 and or COM2 The transmitter COM2 TEMP 2 over temp is operating at reduced power If the problem Reducing transmitter power persists the system should be serviced COM1 SERVICE COM1 needs 7 service Return unit for repair The system has detected a failure in COMI and or COM2 1 and or COM2 may still be usable com2 SERVICE m COM2 needs The system should be serviced when possible service Return unit for repair 68 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN GIA 63W MESSAGE ADVISORIES CONT Annunciations amp Alerts Message is stuck COMI PTT COM1 push to talk key COM2 PTT COM2 push to talk key is stuck Comments The 1 and o switch is stuck in position Press th operation If the problem pe serviced COM2 external push to talk the enable or pressed e PTT switch again to cycle its sists the system should be COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or 2 transfer switch is stuck in the enabled o transfer switch again to cycle its operation If the problem persists pressed position Press the the system should be serviced COM1 CONFIG COM1 config error Config s
17. Equipment required to perform the update is as follows 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 87 uone1edo s m aoueplony SoJnpa204d Duruue d AEN Sd5 S24JV oipny uadx 513 sjueumasu Jeuuouqy Jeuonippy puezey ubi U105 AEN ubiu Sue v unuuy i k Additional Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix GARMIN Windows compatible PC computer running Windows XP Vista or Windows 7 SD Card Reader SanDisk SDDR 93 SanDisk SDDR 99 Verbatim 96504 or equivalent Updated database obtained from the Garmin website Existing Supplemental Database SD Card 010 00330 41 42 or 43 from the MFD The supplemental data card from the MFD should be used because all databases except the active navigation database are required to reside on this card Jeppesen Databases NOTE The Jeppesen aviation navigation database is now referred to as the navigation database Previously this database had been referred to as the navigation database The ChartView database should be copied to the Supplemental Data Card which will reside in the bottom card slot on the MFD The navigation database is be loaded from the Jeppesen or user supplied SD data card Contact Jeppesen www jeppesen com for subscription and update information The n
18. Selection Softkey switches between PFD1 and MFD1 Database status information in the Database Window will reflect the database of the PFD or MFD esos oie Unselected MFDI DB Selected PFD DB Selected Display Database Selection Softkey Garmin Databases The following databases are stored on Supplemental Data Cards provided by Garmin Expanded basemap Obstacle Airport Directory Terrain SafeTaxi AOPA Airport terrain FliteCharts After subscribing to the desired database product updates these updated databases are copied to each Supplemental Data Card for each display the card that contains the FliteCharts or ChartView database resides in the MFD Since these databases are not stored internally in the displays these Supplemental Data Cards must remain in the bottom card slot of each display NOTE The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data Obtaining Garmin Database Updates The Garmin database updates can be obtained by following the instructions detailed in the Aviation Databases section of the Garmin website fly garmin com Once the updated files have been downloaded from the website a PC equipped with an appropriate SD card reader is used to unpack and copy the new databases onto the appropriate Supplemental Data Cards
19. 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 83 AEN 549 S24V oipny uadx si syueumasu jeuonippy 2 Wil Tuo2 NeN qb uoneiedo Jeuuouqy Sue v unuuy ee m Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix 6 GARMIN MFD SOFTKEY MAP n pF EY EF ES EN ES ES EY FX DCLTR 1 Press the BACK softkey on this level to return to the top softkey level 7 ENGINE LEAN SYSTEM BACK mes 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 TRAFFIC PROFILE ToPo TERRAIN AIRWAYS 1 STRMSCP NEXRAD XMLING METAR LEGEND BACK F3 F V3 VF F3 V3 V V D AIRWY ON ENGINE system becruet iwcrue esrruec 1 fawo F3 V3 V3
20. CODE IDENT ADS B TX BACK ALERTS D nm Press the BACK Softkey to return to the top level softkeys ETT IE AES AE Tom Tser TES Yaram Press the BACK Softkey to return to the previous level softkeys Transponder Softkeys Level 1 Level2 Level 3 Description XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does not reply to any interrogations 82 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description IDENT TMR REF NRST ALERTS ON ALT GND VFR CODE IDENT ADS B TX 190 00525 04 Rev A 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 softkeys 0 7 Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Activates deactivates transmission of the aircrafts three dimensional position and aircraft heading for reception by ADS B systems
21. Cockpit Reference Guide for the Beechcraft G36 oipny uddx s q sjuauimasu U105 AEN 16114 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo s m unuuy Jeuuouqy Jeuonippy xipueddy x pul Nav Com Flight EIS Instruments XPDR Audio AFCS Flight Procedures Planning GPS Nav Hazard Features Avoidance Additional Abnormal Operation Appendix Index Flight Planning GARMI N 4 5 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 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Press the INVERT Softkey Invert and activate stored flight plan is displayed 6 With OK highlighted press the ENT Key The selected flight plan is now inverted and activated The original flight plan remains intact in its flight plan catalog storage location COPY A FLIGHT PLAN 1 Press the FPL Key on the MFD 2 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the
22. 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 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 fi
23. 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 s mp old ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Tum the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key 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 final approach course becomes the active leg 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 37 siu uin su iui sua uonejedo sainjea4 Buluueld AEN 549 52 oipny uadx junuuy jeuuouqy jeuonippy paezey 16114 uo2 AEN xipuaddy x pul Nav Com XPDR Audio EE Additional Hazard Avoidance Abnormal Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index A Procedures GARMIN ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 38 1 2 3 4 Press the PROC Key
24. Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix CCUG ARMIN Loading the Jeppesen navigation database NOTE Loading the Jeppesen navigation database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow 1 Copy the new navigation database to an SD card obtained from Garmin or the aircraft manufacturer 2 With the G1000 system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD label of SD card facing left 3 Turn the system ON A prompt similar to the following illustration is displayed DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE SELECTING YES WILL QUERWRITE THE ACTIVE NAVIGATION DATABASE FROM TO REGION WORLDWIDE WORLDWIDE YELE 1812 1613 Li EFFECTIVE 19 NOU 20180 17 DEC 28010 EXPIRES 17 DEC 2818 14 2011 INO WILL ASSUMED IN 28 SECONDS UPDATING NAVIGATION DATABASE PLEASE WAIT Navigation Database Load Prompt 4 Select the YES Softkey to update the navigation database in the MFD 5 After the update completes the display starts in normal mode 6 Turn the system OFF and remove the SD card from the top card slot 7 Repeat steps 2 through 6 for the PFD 8 Apply power to the system and press the E
25. Safe Taxi database error exists The MFD and or PFD detected a failure in the Safe Taxi database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Chartview database error exists The MFD detected a failure in the ChartView database optional feature Ensure the data card is properly inserted Replace data card If problem persists system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists MFD1 DB ERR MFD1 Airport Directory database error exists The MFD detected a failure in the FliteCharts database optional feature Ensure the data card is properly inserted Replace data card If problem persists system should be serviced The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 multiple database errors exists database errors exists PFD1 DB ERR PFD1 multiple The MFD and or PFD detected a failure in more than one database If problem persists the system should be serviced 190 00525 04 Rev A 65 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 so1njeaJ 2 Buruuejd AEN 5640 24V olpny uqax sia siu un su paezey nubi nubi jeuonippy uoneiedo Jeuu
26. Selects desired amount of map detail Sue v unuuy 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 gt 5 o x x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 19 Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index A Appendix GARMIN Level 1 Level 2 Level 3 Description TRAFFIC Displays traffic information on Inset Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map TERRAIN Displays terrain information on Inset Map STRMSCP Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft NEXRAD Displays NEXRAD weather and coverage information on Inset Map optional feature XM LING Displays XM lightning information on Inset Map optional feature METAR Displays METAR flags on airport symbols shown on the Inset Map optional optional meer EE Coe 3998 WENT eT eS mn p nannnnununn e n ses qno Joe ee sez Jr lino sso eS n n r Km rs SYNVIS Press the BACK Softkey to return to the top level softkeys
27. System Test OK is heard Display Terrain on the TAWS B Page 1 Tum the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 If desired press the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is pressed a radar like 120 view is displayed Press the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 4 AEN Sd5 S24V oipny uddx sia siu umnisul Tuo2 AEN iui Duruue d Wil s mp oold paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipueddy 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 A Hazard Avoidance GARMIN Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstade between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Enable Disable Aviation Data 1 While the 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 Inhibit TAWS Wh
28. Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH Press the ENT Key A confirmation window is displayed With ACTIVATE highlighted press the ENT Key Or Press the Go around Button Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN 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 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 KJ Strike is between 6 and 60 seconds old A Strike is between 1 and 2 minutes old Strike is
29. 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 Beechcraft G36 flight path guidance 190 00525 04 Rev A GARMI N Flight Planning FLIGHT PLANNING TRIP PLANNING 1 Tur the large FMS Knob to select the AUX page group 2 If necessary turn the small FMS Knob to select the Trip Planning Page 3 The current page mode is displayed at the top of the page AUTOMATIC or MANUAL To change the PAGE MODE press the AUTO or MANUAL Softkey 4 For Direct to planning a Press 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 bot
30. between 2 and 3 minutes old e 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 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 39 sjueuimasu sub APN 549 S24Y oipny uddx U105 AeN buluueld nubi 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 40 5 6 7 8 9 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
31. by SiriusXM Radio Service is approved only for weather avoidance not penetration Displaying XM WX Weather on the Navigation Map Page 1 Press the MAP Softkey 2 Press the NEXRAD or XM LTNG Softkey to display the desired weather Press the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Tum the large FMS Knob to select the WPT Page Group 2 Tum the small FMS Knob to select the Airport Information Page 3 Press the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Tum the large FMS Knob to select the Map Page Group 2 Tum the small FMS Knob to select the Weather Data Link Page 3 Press the available softkeys to select the desired XM weather product 4 Press the LEGEND Softkey to view the legends for the selected products If necessary turn 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 th
32. computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced 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 The 1 AHRS is not receiving any or any useful GPS information Check AFMS limitations The system should be serviced AHRS1 GPS AHRS1 not receiving backup GPS information The 1 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exdusively in no GPS mode AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS is operating exclusively in no GPS mode The system should be serviced The 1 AHRS and 2 AHRS magnetic model database versions do not match 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sainqea4 aoueplony s mp oold Buruue d AEN Sd5 yi oipny uddx 913 siu umnnsu paezey nubi jeuonippy uoneiedo Jeuuouqy i EST x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN GRS 77 MESSAGE ADVISORIES CONT Message AHRS1 SRVC AHRS1 Magnetic field model needs update Comments The 1 AHRS earth magn
33. 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 Viewing 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 Beechcraft G36 190 00525 04 Rev A A GARMIN Vazari Avaldance XM WX SATELLITE WEATHER SUBSCRIPTION OPTIONAL WARNING Use of XM WX Satellite Weather for hazardous weather penetration is not recommended Weather information provided
34. flight plan import export Updated procedure for entering User Waypoints Updated XM weather products Updated TAWS annunciations Added CDI operation in Dead Reckoning mode Added AOPA Airport Directory Added temporary user waypoints Added database synchronization Added GTS 820 TAS Removed support for non WAAS systems Various clerical corrections Added Profile View Added new weather product symbols and legend Added MV DB update proceedure Added other GDU 11 12 parameters Revision Date of Revision Affected Pages September 2011 Production release 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Record of Revisions GARMI Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Tale of Contents FLIGHT INSTRUMENTS 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg 1 Change Altimeter Barometric Pressure Setting Units 1 Change Navigation Sources sssssssseeeenennn nnns 1 Enable Disable OBS Mode While Navigating with 6 5 5 2 Generic TIGE rmn ho qas ica in ice n a 2 Configure Vspeed Bugs Individually sss 2 Set Barometric Minimum Descent
35. highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 2 3 4 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 Press the ACT LEG Softkey on the MFD 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 Beechcraft G36 190 00525 04 Rev A A GARMIN GPS Navigation 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 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This does not delete the stored flight plan only the active flight plan VERTICAL NAVIGATION VNAV The navigation database only contains altitudes for procedures that call for Cross at altitudes If the procedure states Expect to cross at the altitude is not in the database In this case the altitude may be entered manually ACTIVE FLIGHT PLAN LEMYN RIVET iaf DRAAK INWOD MENOL faf RW17L map 930FT ZAR Yi MICI IE S aroe White 22177 9 NM 12400FT m 220 8 0NM 9900FT4E Large Lig 2 Blue Tex
36. 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 Press the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and press the SHW CHRT Softkey 2 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 Press the GO BACK Softkey to return to the previous page 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 49 2 Puluueld AeN Sd5 S24V olpny uqax sia siu u nnsul Wfl Tu102 AEN UTE aoueplony paezey s m e q jeuonippy xipuaddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A Additional Features GARMIN View Charts from the Active Flight Plan Page 1 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor 2 Tum the large FMS Knob to select the departure airport destination airport departure arrival or approach 3 Press the SHW CHRT Softkey The appropriate chart is displayed if available for the item selected 4 Press the GO BACK Softkey to return to the pr
37. on the PFD to select VOR1 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 illuminated indicating Split COM operation COMI and COM2 frequencies are displayed in green indicating that both transceivers are active Split COM operation 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN N
38. to Bus 1 None ALERT MESSAGE Alerts Window Message Audio Alert PFD FAN FAIL The cooling fan for the PFD is inoperative None MFD FAN FAIL The cooling fan for the MFD is inoperative None AVIONICS FAN The cooling fan for remote avionics is inoperative None AFCS ALERTS Condition Annunciation Description Pitch Failure Pitch axis control failure AP is inoperative Roll Failure ROLL Roll axis control failure AP is inoperative MET Switch Stuck or Pitch Trim Axis Control Failure D m zs If annunciated when AP is engaged take control of the aircraft and disengage the autopilot If annunciated when AP is not engaged move each half of the MET switch separately to check if a stuck switch is causing the annunciation Yaw Damper Failure YD control failure AP also inoperative System Failure AP and MET are unavailable FD may still be available Elevator Mistrim Up PEE A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose up control wheel force upon autopilot disconnect 58 Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts Condition Annunciation Description Elevator Mistrim Down A condition has developed causing the pitch servo to provide a sustained force Be prepared to apply nose down control wheel force upon autopilot d
39. uoneiedo Jeuuouqy PEST 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 MFD amp PFD MESSAGE ADVISORIES CONT Message PFD1 VOLTAGE PFD1 has low voltage Reducing power usage Comments 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 Comments MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation 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 MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists The MFD and or PFD detected a failure in the basemap database The MFD and or PFD detected a failure in the terrain database Ensure that the 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
40. when the GTS 820 TAS system fails a pilot initiated self test Failed One o clock through Twelve o clock or No Bearing Intruder bearing GTS 820 only High Low Same Altitude if within 200 feet of own altitude or Altitude not available Less than one mile One Mile through Ten Miles or More than ten miles Intruder relative altitude GTS 820 only Intruder distance GTS 820 only 62 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts MFD amp PFD MESSAGE ADVISORIES Message DATA LOST Pilot stored data was lost Recheck settings Comments 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 XTALK ERROR flight display crosstalk error has occurred The MFD and PFD 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 repair 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 PFD1 CONFIG PFD1 config error Config service req d
41. 2 standby frequency 3 Press the CDI Softkey a third time to return to GPS suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Nav Com XPDR Audio Abnormal Additional Hazard Flight Planning Annun AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index A Flight Instruments GARMIN ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 Press the OBS Softkey to select OBS Mode 2 Tum a CRS Knob to select the desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint 3 Press the OBS Softkey again to disable OBS Mode GENERIC TIMER 1 Press the TMR REF Softkey then turn the large FMS Knob to select the time field hh mm ss Turn the FMS Knobs to set the desired time then press the ENT Key The UP DOWN field is now highlighted 2 Tum 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 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it starts counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window CONFIGURE VSPEED BUGS INDIVIDUALLY 1 2 3 4 5 6 Press the TMR REF Softkey Turn the large FMS Knob to highlight the desired Vs
42. 540 S24V oipny uadx 913 sjueumasu puezey ubi UI05 AeN ubi jeuonippy uoneiedo Jeuuouqy EST x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 Alerts A GARMIN PFD MFD MFD Alert Type TAWS B Page Aural Message 7 Pop Up Alert Annunciation Imminent Terrain PULL UP Terrain Ahead Pull Up Impact Warning ITI or Terrain Ahead Pull Up UA Terrain Terrain Pull Up Pull Up Reduced Required PULL UP Obstacle Obstacle Pull Obstacle Clearance or Up Pull Up Wanna ROG Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle PULL UP Obstacle Ahead Pull Up Impact Warning or Obstacle Ahead Pull Up 0 OBSTACLE PULL UP or Obstacle Obstacle Pull Up Pull Up Reduced Required TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain Caston Re TERRAIN EAD y Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRMNAMAD Terrain Ahead Terrain Impact Caution ITI or Ahead 25 a Caution Terrain Caution Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Obstacle Clearance or Caution Obstacle Caution ROC BHB a Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacl
43. Altitude sss 3 Displaying Wind Data 3 Changing HSI Format nennen 3 ENGINE INDICATION SYSTEM 5 Engine Display serene etn ete en ae a 5 Lean Engine Display sssssseenenen nennen 6 Engine System Display sssssssseeeeenennnnnnnnnnnnnes 8 NAV COM TRANSPONDER AUDIO PANEL 9 ADF Tuning 7 9 DME Tuning Optional ccc ccccccscssssssssssessssssssssssssssssssssssssscsssssvsssscessssssssscesassnsesseess 9 Enter a Transponder Code sss 9 Activate ADS B Tra smit aiunt in ci E 9 Selecting a COM Radio seen 0 Selecting a NAV Radio 0 NAV COM Tuning sssseeeeen ennt ennt 0 5222222000 0000 0 0 0 Digital Clearance Recorder and 1 Intercom System ICS Isolation 1 AUTOMATIC FLIGHT CONTROL SYSTEM 5 3 Flight Director Activation sssssssssen nnn 3 Vertical Modes are rrt co cb e anun 4 Lateral Modes 5 GPS NAVIGATION ioris ote 7 Direct to Navigation ssssssseseenee nennen 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8 Stop Navigating a Flight Plan 9 Vertical Na
44. Cockpit Reference Guide for the Beechcraft G36 3 eouepioAy Senpa204d Buruue d AEN Sd5 S23V olpny qqax 53 s3u u n sul puezey 1461 U105 AEN ubiu saunqea4 jeuonippy Sue v unuuy xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index A Abnormal Operation GARMIN UNUSUAL ATTITUDES The PFD declutters when the aircraft enters an 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 e AFCS Annunciations 9 PFD Setup Menu path and Vertical Flight director Com Windows displayed in Deviation Indicators mand Bars the lower right comer Altimeter Barometric Inset Map of the PFD Setting Temperatures Timer References Selected Altitude DME Information Nearest Airports VNV Target Altitude Window Flight Plan Wind Data Messages Selected Heading Box Procedures Selected Course Box 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
45. G 1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft G36 A GARMIN Copyright 2005 2011 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0858 08 or later for the Beechcraft G36 manu Garm Tel 9 Garmi Some differences in operation may be observed when comparing the information in this al to earlier or later software versions in International Inc 1200 East 151st Street Olathe Kansas 66062 U S A 13 397 8200 Fax 913 397 8282 n AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmi South n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park ampton 5040 9RB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garm in Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 STI or af Web Site Address www garmin com Except ter hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 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 witho down other or pri notice and provided furthe revision hereto is strictly prohibited
46. NT Key to acknowledge the startup screen 9 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 Select the Display Database Selection Softkey to show navigation database information for each display MFD1 DB PFD1 DB 90 Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN 000 Appendix MFD1 DATABASE NAVIGATION INTERNAL REGION WORLDWIDE CYCLE 1013 EFFECTIVE 17 DEC 10 EXPIRES 14 JAN 11 Copyright 2011 Jeppesen Sanderson Inc BASEMAP BOTTOM CARD REGION VERSION GARMIN LTD AND ITS SUBSIDIARIES 2011 SAFETAXI BOTTOM CARD REGION VERSION Check Database Cycle Number MFD shown Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by the AHRS GRS 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 GRS MV DB Update Available Update from 2005 to 2010 0l 4 GRS Magnetic Field Variation Database Update Prompt 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 uonesdo saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 2 olpny uqax sia Sjueunasu jeuonippy paezey jeuuouqy Sue v unuuy gt k o x 3 x x pul iui UI0JNeN nuru Annun Abnormal Addi
47. PFD1 DB ERR PFD1 terrain database missing MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists The terrain database is present on another LRU but is missing on the specified LRU 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 64 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists Comments 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 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 Safe Taxi database error exists PFD1 DB ERR PFD1
48. System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Beechcraft G36 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 Beechcraft G36 190 00525 04 Rev A A GARMIN Warnings Cautions 5 Notes V ARNING 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 mu
49. TERR Softkey 4 Press the PATHVVAY Softkey 5 Press the BACK Softkey to return to the previous page Displaying Heading on the Horizon 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press 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 Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN 0 Additional Features ID the VOR symbo
50. YSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE soltkeys 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 o Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS A NOTE If the G1000 is configured to use a Traffic Advisory System TAS TIS is not available for use A NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sub oipny uadx 59 010 AEN 52 AEN 540 Duruue d nubi aoueploay s mp oold paezey suelv 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
51. age of the displayed data for each is shown at the right F us 8m CN Em 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 shown at the right AIREP The age of the displayed data is shown at the right qe Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Hazard Avoidance Wx Product Status Icons Description Ch Sm PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow iss TURBULENCE The age of the displayed data is shown at the right The Al n a mm altitude selection is shown at the bottom gil ICING POTENTIAL The age of the displayed data is shown at the right 6000FT The altitude selection is shown at the bottom TRAFFIC S
52. al Leg Load and or Activate an Approach Procedure 36 Activate An Approach in the Active Flight Plan 37 Activate a Vector to Final Approach Fix sss 37 Activate A Missed Approach in the Active Flight Plan 38 HAZARD AVOIDANCE 39 Customizing the Hazard Displays on the Navigation 39 STORMSCOPE Optional cccccscccsssssssssccssssssssescsssssssssssesssssssssscesssssssssecesassnsssnsess 39 XM WX Satellite Weather Subscription Optional 41 Traffic Systems tite ed etae d be ed edle 43 Terrain Awareness amp Warning System TAWS Display 45 ADDITIONAL FEATURES enne Synthetic Vision sss Terminal Procedure Charts AOPA Airport Directory sssssseeeeeennnnnnnnnnnnns SiriusXM Radio Entertainment Subscription 51 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN of Contents ABNORMAL OPERATION Reversionary Mode Abnormal COM Operation
53. as a reference when adjusting fuel mixture xipuaddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Flight Instruments NX Annun Abnormal Additional Hazard Flight Nav Com Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Appendix Index Engine Indication System GARMIN LEAN ENGINE DISPLAY HAN IN HG 35 Fuel Flow 21 R t 7 a FFLOW GPH 14 0 7 temperature rates Difference between DEMENS peak and current Exhaust Gas temperature of Temperature selected cylinder Bar Graph EGT Readout For Selected Cylinder Cylinder Head Temperature CHT Readout For Selected Cylinder LEAN Engine Page 1 Press the ENGINE Softkey then the LEAN Softkey to display the LEAN Engine Page 2 Press the CYL SLCT Softkey to select the desired cylinder for monitoring 3 Press the ASSIST Softkey to hightlight the first cylinder that peaks Information for that cylinder is displayed NOTE The pilot should follow the engine manufacturer s recommended leaning procedures in the Pilot s Operating Handbook POH Pressing the CYL SLCT Softkey cycles through the cylinders the selected cylinder is displayed in light blue The CYL SLCT Softkey is disabled during warning or caution conditions or when the ASSIST Softkey is pressed Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Engine Indication System When th
54. ating Tone Oil pressure is less than 10 psi Repeating Tone Lor R fuel qty is at zero Repeating Tone CAUTION ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Air conditioner on and door extended Single Chime Starter relay has power applied Single Chime Bus 1 voltage greater than 30 VDC Single Chime Bus 2 voltage greater than 30 VDC Single Chime Aft door not latched Single Chime Oil pressure is between 30 and 10 psi Single Chime Lor R fuel qty is less than or equal to Single Chime 13 gal Alternator 1 load exceeds 100 amps Single Chime Alternator 2 load is between 20 and Single Chime 190 00525 04 Rev A 24 amps Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 s n e 4 2 Duruue d AEN Sd5 241V oipny uaddx 93 5349 0115 2 nf uio AeN jeuonippyv uoneiedo jJeuuouqv 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations 8 Alerts A GARMIN Annunciation Text Alerts Window Message Audio Alert Alternator 2 load exceeds 24 amps Single Chime Bus 1 voltage less than 24VDC Single Chime Bus 2 voltage less than 24VDC Single Chime ADVISORY ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Bus 2 is tied
55. av AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair Comments A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced uf Return unit for repair n NAV1 SERVICE NAV1 needs service n Return unit for repair NAV2 SERVICE NAV2 needs service A failure has been detected in the NAV1 and or NAV2 receiver The receiver may still be available The system should be serviced NAV1 RMT XFR NAV1 remote transfer key is stuck NAV2 RMT XFR NAV2 remote transfer key is stuck The remote NAV1 and or NAV2 transfer switch is stuck in the enabled or pressed state Press the transfer switch again to cycle its operation f the problem persists the system should be serviced G S2 FAIL G S2 is inoperative G S1 FAIL G S1 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair GEA 71 MESSAGE ADVISORIES A fail
56. av Com XPDR Audio Panel 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 PLAY once plays the latest recorded memory block then returns to normal operation Pressing MKR MUTE while playing a memory block stops play Pressing the PLAY Key during play begins playing the previously recorded memory block Each subsequent press of the PLAY Key begins playing the next SjueuinJjsu Yid 59 S24V oipny uddx JUI05 AEN 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 PILOT KEY COPLT KEY Pilot Hears Copilot Passenger ANNUNCIATOR ANNUNCIATOR Hears Hears Selected radios pilot OFF OFF copilot passengers music radios pilot Selected COPILOT OFF ON radios plot passengers music Selected CREW ON ON radios pilot copilot 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Selected radios pilot copilot passengers music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music sual uonesado s
57. avigation database is loaded from an SD card inserted into the top card slot of each displayed The database is copied from the SD card in the top card slot to the displays internal memory Loading Updated Databases In some cases it may be necessary to obtain an unlock code from Garmin in order to make the database product functional It may also be necessary to have the system configured by a Garmin authorized service facility in order to use some database features Loading the Garmin database updates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 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 88 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN V Checklist File N A 80 Basemap Land 4 00 SafeTaxi Expires 10 MAR 2011 A Terrain 2 04 Airport Terrain 2 04 bstacle Expires 10 MAR 2011 A Navigation Expires 10 MAR 2011 S Apt Directory Expires 10 MAR 2011 L7 FliteCharts Expires 10 MAR 2011 All map and terrain data provided is only to be used ds a general reference to your su
58. d 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 One or more imported user waypoints were renamed when imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported Flight plan export failed The stored flight plan was successfully exported to the SD card 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 78 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A amp GARMIN Appendix APPENDIX sjuauimasu Yid PFD SOFTKEY MAP optional r mu m r 7 mu uu m r 59 CDI NAV1 CD NAV2 olpny uqax uo2 AEN CDI GPS 3 Top Level PFD Softkeys optional me E a 085 5866 CONT REY ST NERIS n 77 O v HU v nnn on optional optional optional optional OFF DCLTR TRAFFIC ToPo TERRAN BTRMSCP NEXRAD xm LTNG METAR a D Ou A BL HELL buluueld qwbl4 s snp oold Press the BACK Softkey to return to the top level softkeys Ez Inset Map Softkeys e Level 1 Level 2 Level 3 Description p INSET Displays Inset Map in PFD lower left corner f HE OFF Removes Inset Map zi DCLTR 3
59. e ASSIST Softkey is selected the system initially highlights and selects the cylinder number with the hottest EGT and displays its temperature below the EGT bar graph A readout showing the difference between peak APEAK and the current temperature for the selected cylinder is displayed above the EGT bar graph As the mixture is leaned a light blue line will appear above each cylinder to indicate EGT peak When the system detects the first cylinder to peak the cylinder numbers below the EGT graph disappear and 1st is annunciated below the first peaked cylinder to indicate the other cylinders are rich of peak As the mixture is further leaned Last is annunciated below the last peaked cylinder indicating all cylinders are lean of peak Refer to the POH and AFM for the recommended mixture adjustment procedures Monitoring of the cylinder continues until the ASSIST Softkey is pressed again which disables lean assist and removes the peak lines from the bar graph and the temperature deviation from peak APEAK The system then returns to seeking the hottest cylinder 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Sjueunasu NS suelv uoneiedo sainjeay aoueplony SoJnpa204d Duruue d AEN Sd5 S24V oipny uadx junuuy Jeuuouqy Jeuonippy puezey Tu102 AEN xipuaddy x pul iui nuru Flight Instruments m Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance A
60. e Ahead Obstacle Impact Caution 101 or Ahead OBSTACLE d i Caution Obstacle Caution Obstacle Premature Descent TERRAIN TOO LOW TERRAIN Too Low Terrain Alert Caution PDA 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts PFD MFD MFD Alert Type 1 TAWS B Page Aural Message Pop Up Alert Annunciation Altitude Callout None None Fve Hundred 500 Excessive Descent TERRAIN SKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN vars n Don t sink Rate Caution NCR or or reuse 100 Low amin TAWS B SYSTEM STATUS ANNUNCIATIONS PFD MFD j TAWS B Page Aural Alert Type Alert EE Annunciation Message Annunciation System Test in Progress TAHS TEST None TAWS System System Test Pass None None Test OK TAWS Alerting is disabled TAWS INH None None MFD Terrain or Obstacle database unavailable or invalid iiis Nene TAWS operating with PFD Terrain or Obstacle databases TAWS B System Test Fail ITAWS FAIL 77 Terrain or Obstacle database unavailable or invalid invalid TANS System software configuration system TAMS FAIL Failure audio fault T TAWS Not D No GPS position TAHS N A Available Excessively degraded GPS TAWS Not signal Out of database TAMS N A None Available coverage area Suff
61. e 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 FLT ID Softkey to enable or disable Flight ID displayed with the intruder information GTS 820 only Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Hazard avoidance System Self Test 1 With the Traffic Map Page displayed set the range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test takes approximately eight seconds to complete When completed successfully traffic symbols are displayed and a voice alert is heard see Alerts and Annunciations section If the self test fails the system reverts to Standby Mode and a voice alert is heard 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 AWARENESS amp WARNING SYSTEM TAWS DISPLAY NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS
62. e sole source of obstacle and terrain avoidance information Always refer to current aeronautical charts for appropriate minimum clearance altitudes WARNING The altitude calculated by G1000 GPS receivers is geometric height above Mean Sea Level and could vary significantly from the altitude displayed by pressure altimeters such as the GDC 74A Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING Traffic information shown on the G1000 Multi Function Display is provided as an aid in visually acquiring traffic Pilots must maneuver the aircraft based only upon ATC guidance or positive visual acquisition of conflicting traffic WARNING Do not use datalink weather products e g XM WX Satellite Weather GFDS World Wide Weather or FIS B for hazardous weather penetration Weather inf
63. e 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 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 AEN 640 S24V oipny uadx sia siu umnnsul Tuo2 AEN iui Duruue d nubi 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 EIS GPS Nav Hazard Avoidance Procedures Appendix Alerts Operation Features Index Hazard Avoidance A GARMIN XM 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
64. edures 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 activate the cursor 3 Turn the large FMS Knob to highlight the desired waypoint within the departure 4 Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the PROC Key 2 Tum the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00525 04 Rev A Garmin G1000 Cockpit Ref
65. efault ROL Vertical Speed VS VNV Key Roll Hold default ROL Vertical Path Tracking VPTH GPS NAV Key Navigation VOR Pitch Hold default PIT LOC 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 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sjuaumasu nubi 53 olpny uqax uo2 AEN ARN Sd5 52 suelv uoneiedo sainjea4 aoueplony saunpadoid Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch Pitch Hold attitude may be used to climb default PIT descend to the Selected Altitude AFCS armed to capture the altitude 7777 displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds fe curent Altitude Key nn et Reference Maintains the current aircraft
66. eliminates an obsolete approach or rrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach e ab LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint xxxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the 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 n 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 frequenc
67. erence Guide for the Beechcraft G36 35 oipny uddx s q sjuauimasu U10 AEN fija 52 AEN 540 Duruue d nubi s mp old aoueplony paezey suelv uoneiedo sainjea4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000 GARMIN 5 6 7 8 9 10 11 12 Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways may be displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key With LOAD highlighted press the ENT Key The arrival becomes part of the active flight plan If an altitude associated with a waypoint in an arrival procedure is to be used to calculate vertical guidance perform the following steps a Press the FMS Knob to activate the cursor b Turn the large FMS Knob to highlight the desired waypoint altitude c Press the ENT Key to designate the altitude for use in giving vertical guidance ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key on the MFD 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 a
68. ers land and SUA data DCLTR 3 Removes everything except the active flight plan When available displays optional airport and terminal procedure charts When available displays optional checklists Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in maintenance being required to reboot the system The system uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as well as Jeppesen navigation and Jeppesen ChartView database updates Not all SD cards are compatible with the G1000 system Use only SD cards supplied by Garmin or the aircraft manufacturer NOTE DO NOT use the database SD cards for any purpose other than database storage Information regarding the various databases may be viewed on the AUX System Status Page 86 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Appendix The Display Database Selection Softkey is used to place the cursor in the Database Window Upon first press of the Display Database Selection Softkey the softkey will change to a selected state black text on gray background and the cursor will appear in the Database Window At this point the user can scroll through all databases in the Database Window to view status information Pressing the Display Database
69. ervice req d COM2 CONFIG COM2 config error Config service req d The COM1 and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced LOI GPS integrity lost Crosscheck with other NAVS GPS integrity is of flight insufficient for the current phase GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance unavailable use LNAV only minimums generated by SBAS is 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 00525 04 Rev A 69 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 so1njeoJ 2 Buruuejd AEN 5649 24V olpny uqax sia siu un su paezey nubi u102 AEN nubi jeuonippy uoneiedo Jeuuouqy uc PSY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS N
70. es sssssssssseeeneenn nennen 86 INDEX iem T T Index 1 ii 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Table of Contents GARMI N Blank Page Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING mal ca g 2 o a 59 Tum the BARO to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG olpny uqax Wi0 gt AeN 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure 52 CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys SoJnpa20Jd Duruue d AEN Sd5 Wil aoueplony paezey CHANGE NAVIGATION SOURCES 1 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This places the light blue tuning box over the NAV1 standby frequency in the upper left corner of the PFD 2 Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This places the light blue tuning box over the NAV
71. etic 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 G1000 system should be serviced The GMU 44 has incorrect software installed The G1000 system should be serviced GDL 69 69A MESSAGE ADVISORIES Message Comments GDL69 CONFIG GDL 69 config error Config service req d GDL 69 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The G1000 system should be serviced MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The G1000 system should be serviced GDC 74A MESSAGE ADVISORIES Message Comments MANIFEST GDC1 software mismatch c
72. evious page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 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 Turn the small FMS Knob to choose between Day Auto and Night Options 6 In 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 AOPA AIRPORT DIRECTORY AOPA Airport Directory adds enhanced airport information when viewing airports on the WPT Airport Information Page This database is updated four times per year Check flygarmin com for the current database View Airport Directory Information While viewing the WPT Airport Information Page if necessary press the INFO 1 Softkey to change the softkey label to display INFO 2 AOPA airport information is displayed on the right half of the display 90 Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Md itinal Features SIRIUSXM RADIO ENTERTAINMENT SUBSCRIPTION OPTIONAL The XM Radio Page provides informat
73. flight plan to be copied 5 Press the COPY Softkey A Copy to flight plan 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 Tum the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be deleted 32 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Flight Planning 5 Press the DELETE Softkey A Delete flight plan confirmation window is displayed 6 With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 Press the FPL Key on the MFD to display the Active Flight Plan Page 2 Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan 3 The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion p
74. h the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays Stormscope weather and coverage information on Navigation Map optional feature Displays NEXRAD weather and coverage information on Navigation Map optional feature Displays XM lightning information on Navigation Map optional feature Displays METAR flags on airport symbols shown on the Inset Map optional 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 85 s n e 4 2 Duruue d AEN Sd5 S24JV olpny uqax 513 sul jeuonippy 2 Wil Tuo2 NeN 1i uoneiedo Jeuuouqy Sue v unuuy z a Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Appendix 5 Appendix A GARMIN Level 1 Level 2 Level 3 Description LEGEND BACK DCLTR SHW CHRT CHKLIST DATABASE UPDATES Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutt
75. he transponder code selection softkeys for digit entry 3 Press 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 ACTIVATE ADS B TRANSMIT 1 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the ADS B TX Softkey to enable transmission of three dimensional aircraft position and aircraft ground track 3 Press the ADS B TX Softkey again to disable transmission 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Sjueumasu S24V oipny 4ddX sia JUI05 AEN Suelv uoneiado SoJnjeaJ eouepioAy SoJnpa20Jd Fuluueld ARN Sd5 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul iui Wfi l4 Flight Instruments 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 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
76. icient GPS signal received TANS None None D after loss Available 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 el sainjea4 2 Duruue d AEN Sd5 241V oipny uaddx 593 siu umn sul p ezeH nubi M102 AEN 1i jeuonippy uoneiedo jJeuuouqv es EY x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Amundatons amp Alerts GARMIN VOICE ALERTS Voice Alert Minimums minimums Description he aircraft has descended below the preset barometric minimum Vertical track f he aircraft is one minute from Top of Descent Issued only when 1 descent altitude 1 vertical navigation is enabled Traffic Played when a Traffic Advisory TA is issued TIS and GTS 820 TIS Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Played when a Traffic Advisory TA is issued Skywatch TAS system Traffic Advisory System Played when the Skywatch TAS system passes a pilot initiated self Test Passed test Traffic Advisory System Played when the Skywatch TAS system fails a pilot initiated self test Test Failed TAS System Test Played when the GTS 820 TAS system passes a pilot initiated self Passed test TAS System Test Played
77. ile the TAWS B Page is displayed press the 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 press 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 TAVVS 3 Press the ENT Key 46 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN 0 Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS is intended as an aid to situational awareness only and may not provide the accuracy and or fidelity upon which to solely base decisions and or plan maneuvers to avoid terrain obstacles or traffic A WARNING Do not use SVS runway depiction as the sole means for determining the proximity of the aircraft to the runway or for maintaining the proper approach path angle during landing Synthetic Vision System SVS functionality is offered as an enhancement to the G1000 Integrated Flight Deck System
78. ing GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair Comments 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 AGIA mismatch has been detected where only one is SBAS capable mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The G A1 and or GIA 2 has incorrect software MANIFEST GIA2 software installed The system should be serviced mismatch communication halted MANIFEST GFC software Incorrect servo software is installed or gain mismatch communication halted settings are incorrect MANIFEST COM1 software mismatch communication halted 1 and or 2 software mismatch The MANIFEST COM2 software G1000 system should be serviced mismatch communication halted MANIFEST NAV1 software mismatch communication halted NAV1 and or NAV2 software mismatch The MANIFEST NAV2 software G1000 system should be serviced mismatch communication halted
79. ing provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Record of Revisions Part Number Change Summary 190 00525 00 190 00525 01 RevA 190 00525 02 RevA 190 00525 03 190 00525 04 Added GDU software version 6 13 parameters Added TAWS Changed system software number to 0464 08 Changed to smaller format Added Airways WAAS VNAV amp Charts Updated G1000 System Messages Added other GDU 8 10 parameters Removed FD Formatting featur Added GDU 11 01 parameters Added Synthetic Vision System Added
80. ion 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 Tum the small FMS Knob to select the displayed AUX XM Information Page 3 Press 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 Press the CATGRY Softkey on the XM Radio Page 2 Press 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 press the CHNL Softkey 2 Press the CH Softkey to go up through the list in the Channel Box or move down the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels 3 With the desired channel highlighted press the ENT Key 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36
81. ired 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 cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sjuauimasu nubi 53 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d unuuy Jeuuouqy Jeuonippy paezey n xipuaddy
82. irspeed 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 JUMPE CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 55 sjueuingjsu sub xipu ddy suay saunyea4 seinpeooid Buluusld AEN Sd5 52 oipny uddx si unuuy jeuonippy paezey T TR 0105 AEN 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
83. 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 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 56 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Annunciation Text Alerts Window Message Audio Alert Gear up with power below 12 in Hg or Continuous Tone flaps down received through the G1000 audio from another source Alternator 1 offline Repeating Tone Alternator 2 offline Repeating Tone Alternators 1 and 2 offline Repeating Tone Fuel flow is greater than 27 4 gph Repeating Tone CHT is greater than 238 deg C Repeating Tone Oil temp is greater than 116 deg C Repeating Tone Oil pressure is greater than 100 psi Repe
84. isconnect Aileron Mistrim Left Aileron Mistrim Right A condition has developed causing the roll servo to provide a sustained left force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits A condition has developed causing the roll servo to provide a sustained right force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Rudder Mistrim Left A condition has developed causing the yaw servo to provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Rudder Mistrim Right A condition has developed causing the yaw servo to provide a sustained force Ensure the slip skid indicator is centered and observe any maximum fuel imbalance limits Preflight Test TI Performing preflight system test Upon completion of the test the aural alert will be heard us EEE EE Preflight system test has failed TAWS B ALERTS PFD MFD MED Alert Type TAWS B Page Aural Message Bg Pop Up Alert Annunciation Excessive Descent PULL UP Pull Up Rate Warning EDR Reduced Required PULL UP Terrain Terrain Pull Up Terrain Clearance or Pull Up Warning RTC l Terrain Ahead Pull Up Terrain Ahead Pull Up 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 9 s m p q aoueplony SoJnpa204d Duruue d AEN
85. l and intersection names if within the airport plan view Pressing the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing 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 Optional FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database
86. ll 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 INVERT AN ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan Press the MENU Key to display the Page Menu Turn the large FMS Knob to highlight Invert Flight Plan Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPROACH OR AIRWAY FROM A FLIGHT 30 1 2 PLAN Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Flight Planning 3 Press the CLR Key to display a confi
87. match 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 NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstacle databases required for TAWS in the specified PFD or MFD is missing or invalid 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations 8 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 The audio panel has incorrect software installed The mismatch communication halted System should be serviced GMA1 SERVICE GMAT needs The audio panel self test has detected a problem in Service Return unit for
88. n submenu allowing selection of active flight plan nearest recent user or airway waypoints 4 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 5 Repeat step numbers 3 and 4 to enter each additional flight plan waypoint 6 When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 Press the FPL Key 2 Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page 3 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 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 21 sjuauimnasu nubi olpny uqax si UI0JNeN 52 2 4 AEN 540 nubi eouepioAy paezey suelv uoneiedo s n e 4 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 4 5 6 7 A GARMIN Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window
89. nished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN FlightPlamning 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 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 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 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 saunpadold Buruuejd AEN Sd5 nubi CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 1 Tum the large FMS Knob on the MFD to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press
90. nnun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Engine Indication System GARMIN ENGINE SYSTEM DISPLAY 1 Press the ENGINE Softkey then the SYSTEM Softkey to display the SYSTEM Engine Page 2 If desired use the DEC FUEL INC FUEL and RST FUEL Softkeys to adjust the amount of fuel remaining for totalizer calculations NOTE Fuel calculations do not use the aircraft fuel quantity indicators and are calculated from the last time the fuel was reset Vi 35 45 HAN IN HG System Information 01 PsI 500 Fuel Calculation Information ELECTRICAL 1 ALT LOAD Z 2 40 50 Electrical 1 BUS VOLTS_2 Information 28 0 214 SYSTEM Engine Page Any exceedance of default Engine Page parameters while viewing the System Engine Page causes the display to automatically switch back to the default Engine Page Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Nav Com XPDR Audio Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING OPTIONAL 1 Press the 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 Press the XPDR Softkey to display the transponder mode selection softkeys 2 Press the CODE Softkey to display t
91. ns cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 A Wamings Cautions Notes 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 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 be
92. oint 4 Press 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 5 To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD NOTE See the Annunciations amp Alerts section for flight plan export message descriptions 1 Insert the SD card into the top card slot on the MFD 2 Press the FPL Key to display the Active Flight Plan Page on the MFD 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to highlight the flight plan to be exported 6 Press the EXPORT Softkey 7 Press the ENT Key to confirm the export 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 33 oipny uddx 59 sjuaumasu U10 AEN 346 3 52 2 AEN 540 nubi aoueplony paezey suelv uoneiedo s n e 4 Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 oipny uadx U105 AEN s24v AeN Sd5 buluueld 346 Blank Page 5 2 4 puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 636 34 GARMIN 7 Proc
93. ommunication halted The GDC 74A has incorrect software installed The G1000 system should be serviced 72 Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN GTS 820 MESSAGE ADVISORIES Annunciations amp Alerts Message Comments GTS CONFIG GTS config error Config service req d The GTS and GDU have incompatible configurations This alert is also set when the GTS has an invalid mode S address configured or the mode address does not match both XPDR mode addresses MANIFEST GTS software mismatch communication halted The GTS has incorrect software installed The G1000 system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked Upon power up the system detects that a stored flight plan waypoint is locked This occurs when an navigation 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 longer exists in any database Or update the waypoint name identifier to refle the new information if it no t 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 ne
94. ond vvaypoint Enter the desired radial from the reference vvaypoint 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 sjuauimasu sub oipny uddx 93 UI0JNeN 52 1 Tum the large FMS Knob on the to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the NEW Softkey A waypoint is created at the current aircraft position 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 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 2 4 AEN 540 nubi
95. or 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 DELETE A USER WAYPOINT 1 Tum the large FMS Knob to select the WPT page group 2 Tum the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 26 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN FlightPlamning 4 Turn the large FMS Knob to the place the cursor in the USER WAYPOINT LIST field 5 Turn the small FMS Knob to highlight the desired waypoint 6 Press the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A FLIGHT PLAN 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 Press the FPL Key 2 Press the FMS Knob to activate the cursor only on MFD 3 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 selectio
96. ormation provided by these products is aged by up to several minutes and may not depict actual weather conditions as they currently appear 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 A Wamings Cautions amp Notei ___ GARMIN WARNING NEXRAD weather data is to be used for long range planning purposes only Due to inherent delays in data transmission and the relative age of the data NEXRAD weather data should not be used for short range weather avoidance WARNING Use of the Stormscope is not intended for hazardous weather penetration thunderstorm penetration Stormscope information as displayed on the G1000 MFD is to be used only for weather avoidance not penetration WARNING The Garmin G1000 as installed in the Beechcraft G36 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
97. ot import ccessfully e stored on the SD card did not contain an only user waypoints One o Too many points Flight plan truncated Th Th e flight plan on the SD card contains more waypoints than the system can support e flight waypoints as possible plan was imported with as many Some waypoints not loaded Waypoints locked m e flight plan on the SD card contains one ore waypoints that the system cannot in the navigation database The flight has been imported but must be edited ru in the system before it can be activated se 190 00525 04 Rev A 7 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 so1njeoJ 2 Buruuejd AEN 5649 24V oipny uadx sia syu unysu paezey nubi nubi 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 Ea Annunciations amp Alerts A GARMIN 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 locke
98. ouqy i ES x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix res Annunciations amp Alerts A GARMIN DATABASE MESSAGE ADVISORIES CONT Message DB MISMATCH Navigation database mismatch Xtalk is off Comments 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 DB MISMATCH Terrain 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 DB MISMATCH Obstacle database mismatch 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 mis
99. peed 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 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Vi it instruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE mal ca g 2 o a 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to BARO 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey 59 olpny uqax Wi0 gt AeN 52 DISPLAYING WIND DATA AEN Sd5 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data to the left of the HSI 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey Duruue d Wil s mp 01d CHANGING HSI FORMAT 1 Press the PFD Softkey 2 Press the HSI FRMT Softkey 3 Press the 360 HSI Softkey to display the full size HSI Or Press the ARC HSI Softkey to display the arc style HSI
100. rallel course A parallel course has been selected causing the selected vertical deviation to go invalid NON WGS84 WPT Do navigation to boo not use GPS The position of the select ed waypoint Doox is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use selected non WGS84 waypoint GPS to navigate to the TRAFFIC FAIL Traffic device has failed The system is no longer receiving data traffic system The traffic d 4 rom the evice should be serviced 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 75 s m s mp oold Buruue d AEN Sd5 yi oipny uddx 913 sjueumasu paezey nubi Wil jeuonippy uoneiedo Jeuuouqy PET x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix d Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message STRMSCP FAIL Stormscope has failed Comments Stormscope has failed The G1000 system should be serviced FAILED PATH A data path has failed A data path connected to the GDU GSD 41 or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s exact magnetic variance for geographic location
101. raphical data 80 85 Traffic 39 44 80 85 Traffic Advisory 62 Traffic advisory 43 Traffic map page 44 45 Transponder 9 82 83 V Vertical speed guidance 20 Vertical track 62 VNV 17 54 75 Vspeed 2 W Waypoint Selection Submenu 27 28 Weather data link page 41 Wind data 81 X XM lightning 80 85 XM weather 41 XPDR Softkey 9 190 00525 04 Rev A A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 21 Garmin Europe Ltd Liberty House Bulls Copse Roa Hounsdown Business Park Southampton 5040 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2005 2011 Garmin Ltd or its subsidiaries 190 00525 04 Rev A
102. repair the unit Certain audio functions may still be avail able and the audio panel may still be usable The System should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG G A1 audio config error Config service req d error Config service req d GIA2 CONFIG GIA2 audio config The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced GIA1 COOLING GIA1 temperatu too low e The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to GIA2 COOLING GIA2 temperature operating temperature too low GIA1 COOLING GIA1 over temperature The G A1 and or GIA2 temperature is too high If GIA2 COOLING GIA2 over temperature problem persists the system should be serviced 190 00525 04 Rev A 67 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Sonje24 aoueplony s mp oold Buruue d AEN Sd5 2 oipny uddx 913 sjueumasu paezey ETSI JU05JAEN nubi jeuonippy uoneiedo Jeuuouqy 1 x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Plann
103. rmation 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 MED it may be saved by pressing the MENU Key 2 Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key 3 With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 Press the FPL Key on the MFD then turn the small FMS Knob to display the Flight Plan Catalog Page 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan 4 Press the EDIT Softkey 5 Turn the large FMS Knob to place the cursor in the desired location 6 Enter the changes then press the ENT Key 7 Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or for a stored flight plan a Press the FPL Key on the MFD b Turn the small FMS Knob to select the Flight Plan Catalog Page c Press the FMS Knob to activate the cursor d Turn the large FMS Knob to highlight the desired flight plan e Press the EDIT Softkey 2 Tum the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window 190 00525 04 Rev A Garmin G1000
104. rrival Press the ACT LEG Softkey A confirmation window showing the selected leg is displayed With ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 36 1 2 3 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN Procedures 4 Turn either FMS Knob to highlight the desired approach 5 Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA
105. rrounding and as an aid to situational awareness Database Information on the Power up Screen Appendix 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Tum the smal FMS Knob to select the System Status Page 8 Make sure the SYNC DBS Softkey is in the enabled state 9 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Complete being displayed 10 Remove and reapply power to the system 11 Turn the large FMS Knob to select the AUX Page group on the MFD 12 Turn the smal 13 FMS Knob to select the System Status Page Select the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB Verify the correct database cycle information is shown for each database for each display Canceling an automatic database synchronization 1 While synchronization is in progress select the SYNC DBS Softkey to disable automatic database synchronization 2 Acknowledge the cancelation by pressing the ENT Key 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 89 saunqee4 2 Buruuejg AEN Sd5 S24V oipny uadx sia sjuawin4su Jeuonippy paezey ni UI05JNeN nubi uoneiedo Jeuuouqy Sue v unuuy k Additional Hazard Flight
106. s near the magnetic poles Displayed magnetic internal model cannot determine the course angles may differ from the actual magnetic heading by more than 2 SVS SVS DISABLED Out of available Synthetic Vision is disabled because the aircraft is terrain region not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB Synthetic Vision is disabled because a terrain resolution too low database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOC1 LOC ID is CRS Selected cou localizer co se for LOC1 differs from published urse by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected cou localizer co se for LOC2 differs from published urse by more than 10 degrees PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card of the PFD reinserted The SD card was removed from the top card slot or MFD The SD card needs to be PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card reinserted The SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be PFD1 or MFD1 CARD 1 ERR Card 1 is invalid MFD conta he SD card in the top card slot of the PFD or ins invalid data PFD1 or MFD1
107. select the desired waypoint Press the ENT Key Press the ENT Key again to accept the waypoint ENTER AN AIRWAY IN A FLIGHT PLAN 1 2 3 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 If this waypoint is not a valid airway entry point a valid entry point should be entered at this time 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 29 oipny uddx s q sjuauimasu U105 AEN 3463 52 2 4 AEN 540 nubi aoueplony paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Avoidance Index Flight Planning 4 5 6 7 A GARMIN Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway The Select Airway Page is displayed The LD AIRWY Softkey or the Load Airway menu item is available only when an acceptable airway entry waypoint has been chosen the waypoint ahead of the cursor position 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 a
108. shall AOPA be liable for any incidental special or consequential damages that result from the use or inability to use the software or related documentation even if AOPA or an AOPA authorized representative has been advised of the possibility of such damages User agrees not to sue AOPA and to the maximum extent allowed by law to release and hold harmless AOPA from any causes of action claims or losses related to any actual or alleged inaccuracies in the information Some jurisdictions do not allow the limitation or exclusion of implied warranties or liability for incidental or consequential damages so the above limitations or exclusions may not apply to you September 2011 190 00525 04 A Printed in the U S A da GARMIN Warnings Cautions k Notes e e WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not 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 th
109. ssing 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 is not used to give vertical flight path guidance Other displayed altitudes may change due to re calculations or rendered invalid as a result of manually changing an altitude to a non designated altitude GPS Navigation White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by the Altitude has been entered The system cannot system estimating the by the pilot Altitude is use this altitude in altitude of the aircraft as it designated for use in determining vertical passes over the navigation giving vertical flight path flight path guidance point This altitude is guidance Altitude does provided as a reference not match the published and is not designated to altitude in navigation be used in determining database or no published vertical flight path altitude exists guidance Small Text Altitude is not designated Altitude is designated The system cannot to be used in determining for use in giving vertical use this altitude in vertical flight path flight path guidance determining vertical 20 guidance Altitude has been retrieved from the navigation database and is provided as
110. st be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp WARNING Because of variation in the earth s magnetic field operating the system within the following areas could result in loss of reliable attitude and heading indications North of 72 North latitude at all longitudes South of 70 South latitude at all longitudes North of 65 North latitude between longitude 75 W and 120 W Northern Canada North of 70 North latitude between longitude 70 W and 128 W Northern Canada North of 70 North latitude between longitude 85 E and 114 E Northern Russia South of 55 South latitude between longitude 120 E and 165 E Region south of Australia and New Zealand WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass le
111. t Approach KDFW RNAY 17LGPS LPY P IAS an lan a Small Lig 176 33mm 2000Fr Blue Text 176 3 2NM Sma m Blue Subdued 176 3 9NM Ted 5 3NM dea Small White Text 8NH with Altitude Restriction Bar POLKE 190 00525 04 Rev A RISE Cross AT or ABOVE 5 000 fi PAGO Cross AT 2 300 ft cinsli Cross AT or BELOW 3 000 ft Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sjuauimasu nubi 59 oipny uadx U105 AeN sue v uoneiedo s n e 4 SoJnpa20Jd Duruue d unuuy Jeuuouqy Jeuonippy paezey nu xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning 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 pre
112. 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 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 23 sia syuawin4su wio gt AeN 3 olpny uqax 52 aoueplony paezey Ssue v 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 24 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
113. the VOL Softkey to access the volume control softkeys 3 Press VOL or VOL softkeys to adjust the volume level 4 Press the MUTE Softkey to mute the radio audio 52 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMI N Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Beechcraft G36 Pilot s Operating Handbook POH always takes precedence over the information found in this section ABNORMAL COM OPERATION When a COM tuning failure is detected by the system the emergency frequency 121 500 MHz is automatically loaded into the active frequency field of the COM radio for which the tuning failure was detected In the event of a failure of both PFDs the emergency frequency 121 500 MHz automatically becomes the active frequency on both COM radios 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 Loss of Hazard Functions with Loss of GPS Position 190 00525 04 Rev A Garmin G1000
114. ting 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 Turn the small FMS Knob to highlight the desired flight plan for importing Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN 1 2 3 4 5 Press the FPL Key to display the active flight plan If required press the FMS Knob to activate the cursor Flight Planning Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint is inserted before the highlighted waypoint Turn the small FMS Knob The Waypoint Information Window is now displayed Enter the new flight plan waypoint by one of the following a b a b c d a b d e Enter the user waypoint identifier facility or city Press the ENT Key Or 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 airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint Press the ENT Key Or Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to
115. tion source Navigation LOC Glideslope GPS VOR LOC NAV LOC will not arm or capture Key Captures and tracks a Navigation Backcourse localizer signal for backcourse BC approaches Approach GPS Glidepath mode automatically armed if GPS vertical guidance is available 7 and tracks the APR selected navigation source Approach VOR GPS VOR LOC Key VAPP Approach LOC Glideslope LOC Mode automatically armed Disengages the autopilot and GA Go Around commands a constant pitch GA Switch angle and wings level 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 13 sia siu umnnsu oipny uadx U105 AEN ARN Sd5 52 suelv uoneiedo SaJnjeoJ eouepioAy SoJnpa204d Duruue d Tunuuy Jeuuouqy Jeuonippy xipuaddy x pul iui Wfi l4 2 GARMIN AFCS Sjueuinijsu fila 593 oipny uadx U105 AEN 52 AeN 5492 4 r Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay unuuy x pu ddy x pul 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 636 16 A GARMIN GPS Navigation 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 des
116. tional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Index A GARMIN 92 Loading the magnetic field variation database update 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 Uploading GRS Mag Var Database STARTING UPLOAD Uploading Database to GRS When the upload is complete the system is ready for use Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN A Activate a flight plan 18 Active Channel 51 ADF 9 10 54 ADS B 83 AHRS 71 72 Airport Signs 47 48 Airways 85 ALT 44 Altitude mode 44 Altitude volume 44 AOPA s Airport Directory 50 AP 58 Audio panel controls NAV1 NAV2 10 Autopilot 58 59 Barometric Altitude Minimums 3 Barometric pressure 82 C CDI 1 10 75 Cell 39 40 Cell mode 40 Channel Presets 52 ChartView 48 49 Clearance player 11 Clearance Recorder 11 Code selection softkeys 9 COM 10 11 53 CYL SLCT 6 D Databases 86 Database synchronization 89 Index Database updates 86 87 88 Database Updates 86 DCLTR Softkey 48 Dead Reckoning 54 Declutter 54 79 86 Direct to 17 DME 9 10 DR mode 54 55 56 E Edit a flight plan 31 F FD 58 Flight Director 13 Flight path marker 47 Flight plan import e
117. 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 54 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A GARMIN X U 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 ovm aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the CDI as shown in the following figure The CDI deviation bar is displayed in yellow but will be removed from the display after 20 minutes Lastly but at the same time a GPS NAV LOST alert message appears on the PFD Normal navigation using GPS SBAS source data resumes automatically once a valid GPS solution is restored t is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode a
118. tom 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 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 oipny uddx s q sjuauimasu U10 AEN 3463 52 2 4 AEN 540 nubi eouepioAy 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 Features Index Flight Planning 22 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
119. ts Wind direction arrow and numeric speed Wind direction arrow with numeric direction and speed Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS vvaypoint identifter and GPS derived distance information Displays the HSI formatting softkeys Displays the HSI in a 360 degree format Displays the HSI in an arc format 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sia sjuaumasu Jeuonippy 2 nf Tuo2 NeN wb uoneiedo Jeuuouqy Sue v unuuy ae ke Annun Abnormal Additional Hazard Flight Nav Com Flight Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Index Appendix A GARMIN Level 1 Level 2 Level 3 Description ser EY BRG2 ALT UNIT METERS HPA STD BARO Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Displays softkeys for setting the altimeter and BARO settings to metric units When enabled displays altimeter in meters Press to display the BARO setting as inches of mercury Press to display the BARO setting as hectopacals Sets barometric pressure to 29 92 in Hg 1013 hPa optional mumumumn STBY ON ALT GND VFR
120. ure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced 70 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN GTX 33 MESSAGE ADVISORIES Annunciations amp Alerts 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 XPDRT is inoperative There is no communication with the 1 transponder GRS 77 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving airspeed AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is not receiving true airspeed from the air data
121. vertical speed may be used to Vertical Speed to the Selected VS Key VS nnnnreM Altitude Maintains the current aircraft airspeed in IAS while the aircraft is Flight Level Change dlimbing descending to the Selected FLC Key FIC nnn Altitude VNAV VNV Key VPTH VNAV Target Altitude AFCS armed to capture the altitude Armed GDU 1045 displayed in the VNAV Target ALTV only Altitude window Glidepath Captures and tracks the SBAS GP glidepath on approach APR Captures and tracks the ILS Glideslope i GS glideslope on approach Disengages the autopilot and GA Go Around commands a constant pitch attitude i GA Switch and wings level ALTS armed automatica 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 ly when PIT VS FLC or GA active and under VPTH when Selected Altitude 190 00525 04 Rev A A GARMIN 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 Herang aele Selected Heading Key ids Navigation GPS GPS Navigation VOR Enroute Captures and tracks the T VOR Mode selected naviga
122. vigation 5 9 FLIGHT PLANNING Trip Planning ee eee e d z b s eR e d e d debetis ge Create a User Waypoint Defined by Latitude amp Longitude 23 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 Table of Contents GARMI N Create a User Waypoint Defined by Radials from Other V aypoints 23 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 25 Delete a User Waypoint Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 29 Enter an Airway in a Flight Plan 29 Invert An Active Flight Plan 30 Remove a Departure Arrival Approach or Airway from a Flight Plan 30 Store a Flight Plan co erai eie i t iei tt its 31 Edit a Stored Flight Plan 31 Delete a Waypoint from the Flight Plan s 31 Invert and Activate a Stored Flight Plan 32 Copy a Flight Plan Delete a Flight Plan reticere Graphical Flight Plan Creation Export a Flight Plan to an SD Card PROCEDURES eire a ER Pu ed eb Reli Load and Activate a Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arriv
123. w navigation databas 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 navigation database update Verify that the user modified procedures in stored flight plans are correct and up to date 190 00525 04 Rev A 73 Garmin 61000 Cockpit Reference Guide for the Beechcraft G36 saunqee4 2 Buruuejg AEN 5649 24V olpny uqax sia syu unysu paezey nubi u102 NEN Wil jeuonippy uoneiedo Jeuuouqy m x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 5 Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT Message DB CHANGE Database changed Verify stored airways Comments This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload irways as needed ab FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database
124. xport messages 77 FliteCharts 48 49 Frequency Transfer 10 H HF 10 Horizon heading 47 Inhibit 46 Inhibit TAWS 46 Inset Map 79 80 IOI 60 J Jeppesen 49 L Lightning 39 40 80 Index 1 190 00525 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 sainjea4 aoueplony 2 Duruue d AEN Sd5 S24JV olpny uqax sia sjuauimasu jeuonippy 2 nf Tuo2 NeN Yid uoneiedo Jeuuouqy Sue v unuuy 1221 ow Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Lee Appendix Index M Map panning 41 Message advisories 63 76 MET 58 METAR 41 Minimums 62 Mistrim 58 59 MKR MUTE 11 ModeS 83 Mode selection softkeys 9 Multi Function Display MFD Softkeys 84 N NAV 10 NAV1 1 10 NAV2 1 10 Navigation database 19 20 NEXRAD 41 80 85 0 085 2 Obstacles 66 68 P Pathways 47 48 Profile View 85 R Reversionary mode 53 ROC 60 S SafeTaxi amp 48 Secure Digital SD cards 86 Split COM operation 10 Store Flight Plan 31 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 A GARMIN Stormscope lightning data 39 40 80 Strike 39 Strike mode 40 Supplemental Data Card 87 88 SVS 47 76 Synthetic Vision System 47 T TA 62 TAF 41 TAS 44 62 71 TAWS 45 46 59 Terrain 45 66 80 85 Timer 73 Topog
125. y for the approach 74 Garmin G1000 Cockpit Reference Guide for the Beechcraft G36 190 00525 04 Rev A A GARMIN Annunciations amp Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message Comments SLCT NAV Select NAV on CDI for 1 The system notifies the pilot to set the CD to the approach correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable TE PE E bad geometry P 9 dala IAF waypoint for parallel offset has been passed past IAF A d ald L IAF waypoint for parallel offset has been passed past IAF UNABLE V WPT Can t reach current The current vertical waypoint can not be reached vertical waypoint within the maximum f speed constraints The sys tical waypoint transitions to the next ver ight path angle and vertical em automatically VNV Unavailable Excessive track The current track angle error exceeds the limit angle error causing the vertical deviation to go invalid VNV Unavailable Unsupported leg The lateral flight plan contains a procedure tum type in flight plan vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive The current qosstrack exceeds the limit causing crosstrack error vertical deviation to go invalid VNV Unavailable Pa

Garmin Software Version 0858.09 Cockpit Reference Guide

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