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Garmin Software Version 0858.07 Cockpit Reference Guide

1. 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 Repeating 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 03 Rev A 24 amps Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sainjea4 SoJnpa204d buluueld AEN Sd5 S24JV olpny uqax SI3 sjuauimnasu 2 Wil uio AeN 1i jeuonippyv uoneiedo Jeuuouqy d E x pul Hazard Flight Nav Com Flight Feat
2. Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT m e 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 SO40 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 2010 Garmin Ltd or its subsidiaries 190 00525 03 Rev A
3. synvis T pFtrs wind pme amp Re l Baro BACK ALERTS n n Ex m Press the BACK Softkey to return to the top level softkeys BRG2 OFF 1 I L METERS EF LA BACK yum m um L r r Jd Jess Js 10 310 310 Tree Taza vumumummmu muss presses TS ET aE PFD SYN VIS 80 PFD Configuration Softkeys Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN DFLTS WIND DME BRGI HSI FRMT BRG2 190 00525 03 Rev A PATHWAY SYN TERR HRZN HDG APTSIGNS OPIN 1 OPTN 2 OPTN 3 OFF 360 HSI ARC HSI Appendix 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 co
4. 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sainjea4 2 buluueld AEN Sd5 S24JV olpny uqax sia s uawin jsu 2 nubi JUI05 AEN jeuonippy uoneiedo Jeuuouqy 5 EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix sd Annunciations amp Alerts GTS 820 MESSAGE ADVISORIES A GARMIN 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 if it no longer exists in any database O
5. SVS SVS DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVS SVS DISABLED Terrain DB resolution too low Synthetic Vision is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed SCHEDULER message Message criteria entered by the user CHECK CRS Database course for LOC1 LOC ID is CRS Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 or MFD1 CARD 1 REM Card 1 was removed Reinsert card The SD card was removed from the top card slot of the PFD or MFD The SD card needs to be einserted PFD1 or MFD1 CARD 2 REM Card 2 was removed Reinsert card he SD card was removed from the bottom card slot of the PFD or MFD The SD card needs to be einserted PFD1 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the PFD or MFD contains invalid data PFD1 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the PFD or MFD contains invalid data 190 00525 03 Rev A Garmin G1000 Cockpit Referenc
6. Turbulence PIREPs NEXRAD XM Lightning Echo Top Cloud Top and Echo Top Mutually Exclusive Cyclone Warnings AIREPs City Forecast H Cell Movement 4 Freezing Levels l METARs Surface Analysis County Warnings Cloud Top SIGMETS AIRMET5 Winds Aloft TRAFFIC SYSTEMS If Traffic information Service TIS is configured STANDBY OPERATE and TNA MUTE softkeys are displayed Ifa Traffic Advisory System TAS is configured STANDBY NORMAL TEST and ALT MODE softkeys are displayed Traffic Symbol Description e Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA Not available with TIS system intruder is within 5 nm and less than 1200 vertical separation O Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Q Traffic Advisory Off Scale Traffic Symbol Description Traffic Information Service TIS 42 NOTE If the G1000 is configured to use a Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A 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
7. 11 12 13 A GARMIN Selecting FPL 00 displays the active flight plan If an active flight plan is selected REM is an available option to display planning data for the remainder of the flight plan NOTE The page mode must be set to MANUAL to perform the following steps Turn the large FMS Knob to highlight the departure time DEP TIME field NOTE The departure time on the Trip Planning Page is used for preflight planning Refer to the Utility Page for the actual flight departure time Enter the departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings The flashing 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
8. 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s m p q aoueplony SoJnpa204d Duruue d AEN 540 S24V olpny uqax 913 sjueumasu puezey ubi UI05 AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ec Annunciations amp Alerts A GARMIN GIA 63W MESSAGE ADVISORIES CONT Message MANIFEST GFC software mismatch communication halted Comments Incorrect servo software is installed or gain settings are incorrect COM1 TEMP COM1 over temp Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM1 needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair The system has detected a failure in COM1 and or COM2 COM1 and or COM2 may still be usable The system should be serviced when possible COM1 PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck The COM1 and or COM2 external push to talk switch is stuck in the enable or pressed position Press the PTT switch again to cyc
9. 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 xipuaddy Suelv uoneiedo sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 52 oipny uddx sia sjuauimasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN iui x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal Annun EIS AFCS GPS Nav Procedures Appendix Alerts Operation Index A aditional Ecate 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 tha
10. 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 e displayed in the Selected Altitude ALTS Armed window Altitude Hold Holds fe curent Altitude Key nnnnn et Reference Maintains the current aircraft 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 WAAS 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 A36 G36 ly when PIT VS
11. 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAVVS Press the ENT Key Enable TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1 2 3 Or While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS WAAS approach a LOWALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 AEN 540 52 orpnyyuqax sia 34 buluueld Wila aoueploay s mp oold paezey suelv uoneiedo s m junuuy jeuuouqy jeuonippy xipueddy x pul A GARMIN Hazard Avoidance Sjueuinijsu nubi 59 U105 AEN s24v AeN Sd5 Duruue d Blank Page 6 2 4 eouepioAy paezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 636 46 GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVS
12. 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 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 Re
13. 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 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Hazard Avoidance AEN 540 52 olpny yqax sia Sjueumajsul Tuo2 AEN fid buluueld ni aoueploay s mp oold paezey suelv uoneiedo sainjea4 Junuuy 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 Hazard Avoidance A GARMIN System Self Test 1 2 3 4 With the Traffic Map Page displayed set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey 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 2 3 Ensure TAS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic is now displayed on the map TERRAIN AWARENESS amp WARNING SYSTEM TAWS DISPLAY 44 NOTE Terrain data is not displayed when the aircraft latitude is greater than 75 degrees north o
14. 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 G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations 8 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 disconnect 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 SFE
15. 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjuauimasu nubi 59 oipny uddx UI0JNeN ACN 540 52 suelv uoneiedo sainjea4 aoueplony 2 Duruue d unuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS Procedures Appendix Alerts Operation Features Index GPS Navigation 7 8 9 10 11 12 13 14 15 A GARMIN Turn the small FMS Knob to enter the desired altitude Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET 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 way
16. Stop Navigating a Flight 5 9 Vertical Navigation VNAV sssssseeet nnne 9 FLIGHT PLANNINI a o io 21 Trip Planning ron erre tren ania rd e ERREUR 21 Create a New User Waypoint Defined by Latitude amp Longitude 23 Create a New User Waypoint Defined by Radials from Other Waypoints 23 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Table of Contents GARMI N Create a New User Waypoint Defined by a Radial amp Distance from Another Vlaypolnt U esasda anadan eee ash Delete a User 1 4 Create a New Flight Plan mport 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 PROLEDURE LU Redoute Load and Activate a
17. 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 the Standby Mode STANDBY is displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter
18. 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 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 oipny uddx s q sjuauimasu U105 AEN 1614 52 2 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments EIS AFCS Flight Procedures Planni
19. sjuaumnasu sub soinjeo4 e2uepioAy s mp old buluueld ACN 540 S24V oipny uadx Jeuonippy puezey yfi A102 AEN uoneiedo Jeuuouqy Sue v unuuy k A GARMIN Appendix MFD SOFTKEY MAP E ENGINE MAP DCLTR 1 k ird Es F3 F3 V3 V3 V3 N a ES DCLTR 1 mi Press the BACK softkey on this level to return to the top softkey level 7 me ENGINE LEAN SYSTEM BACK gt Es n n semen Baie orum op 95 optional optional optional se TRAFFIC TOPO_ TERRAIN AIRWAYS STRMSCP NEXRAD XMLTNG Back nea F3 nanan F3 AIRWY ON o Y ARW LO ENGINE LEAN system 1 oecruet incruet srruet 1 _Back AIRWAY HI 7 A vx ES 2 Press the E x 5255 on any level to o return to the default page level 8 1 NE LEAN SYSTEM CYLSLCT ASSIST BACK pi EN v3 9s ES n zs MFD Softkeys ENGINE Displays the LEAN and SYSTEM 2 softkeys 7 LEAN Displays the engine leaning softkeys 85 CYL SLCT Selects the desired cylinder for monitoring ir ASSIST Highlights the first cylinder that peaks 52 and displays information for that eylinder Es BACK Press to return to the top level softkeys SYSTEM Displays fuel system softkeys 5 DEC FUEL Press to decrease fuel quantity in 1 24 gallon increments INC FUEL Press to increase fuel quantity in 1 gallon increments RST FUEL Press to reset fuel to full BACK Press to
20. EEE E Preflight system test has failed TAWS B ALERTS PFD MFD MED Alert Type TAWS B Page Aural Message eee 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 9 s m p q aoueplony SoJnpa204d Duiuue d AEN 540 S24V oipny uadx 913 sjueumasu puezey 346 wio gt AeN ubiu jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts A GARMIN PFD MFD MFD Alert Type TAWS B Page Aural Message ex Pop Up Alert Annunciation Imminent Terrain PULL UP Terrain Ahead Pull Up Ter Impact Warning ITI or rain Ahead Pull Up O 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 101 OBSTACLE PULL UP or Obstacle Obstacle Pull Up Pull Up Reduced Require
21. ENT Key and the flashing cursor moves to the ending waypoint field d Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint Or For point to point planning a Enter the identifier of the starting waypoint b Once the waypoint s identifier is entered press the ENT Key to accept the waypoint The flashing cursor moves to the ending waypoint Again enter the identifier of the ending waypoint d Press the ENT Key to accept the waypoint Or For flight plan leg planning a Press the FPL Softkey at the bottom of the display b Turn the small FMS Knob to select the desired flight plan already stored in memory by number Turn the large FMS Knob to highlight the LEG field d Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 21 oipny uddx s q sjuauimasu UI05 AEN 1614 52 2 4 AEN 540 nubi uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 22 6 7 8 9 10
22. FLC or GA active and under VPTH when Selected Altitude 190 00525 03 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 navigation 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 13 sia sjueunasu oipny uadx 0105 AEN ARN Sd5 52 suelv uoneiedo sainjea4 a2ueplony 2 Duruue d Tunuuy Jeuuouqy Jeuonippy xipueddy x pul ii TL paezey GARMIN AFCS Sjueuinijsu fila 59 Tu102 AEN 52 AeN 5492 4 qos Blan
23. 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 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 AHRS1 SRVC AHRS1 Magnetic field model needs update The 1 AHRS earth magnetic field model is out of date Update magnetic field model when practical 70 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations 8 Alerts GRS 77 MESSAGE ADVISORIES CONT Message GEO LIMITS AHRS1 too far North South no m
24. Transponder Softkeys XPDR Displays transponder mode selection softkeys STBY Selects Standby Mode transponder does no t reply to any interrogations ON Selects Mode A transponder replies to interrogations ALT Selects Mode C Altitude Reporting Mode transponder replies to identification and altitude interrogations 82 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN o Appendix GND 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 VFR Automatically enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen ADS B TX Activates deactivates transmission of the aircrafts three dimensional position and aircraft heading for reception by ADS B systems 0 7 Use numbers to enter code BKSP Removes numbers entered one at a time IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen TMR REF Displays Timer References Window NRST Displays Nearest Airports Window ALERTS Displays Alerts Window 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36
25. Vspeed Bugs Individually sss 2 Set Barometric Minimum Descent Altitude sss 3 Displaying Wind Data 3 Changing HSI Format nennen 3 ENGINE INDICATION SYSTEM 5 Engine Display eene etn teer 5 Lean Engine Display ssssssseeeenn nennen 6 Engine System Display sssssssseeeeenenennnnnnnnnnnnes 8 NAV COM TRANSPONDER AUDIO PANEL 9 ADF Tuning Optional 0 0 0 ccccccccssssssssssssssssssccsssssssssscessssssssscessssssesssssssssesnecssassneees 9 DME Tuning Optional cc cccccscsssssssssssssesssssssssssssssssssssvssssssessssssssscesssssvsssesesassnsesseess 9 Enter a Transponder Code sss 9 Activate ADS B Transit aiunt ian Pe dn 9 Selecting a COM Radio seen 0 Selecting a NAV Radio 0 NAV COM Tuning nnne 0 Digital Clearance Recorder and Player 1 Intercom System ICS Isolation sss 1 AUTOMATIC FLIGHT CONTROL 5 3 Flight Director Activation sss 3 Vertical Modes nnne 4 Lateral Modes insana icr tb oe E n eet 5 GPS NAVIGATION atio Gat e aii tt b M al bp dad 7 Direct to Navigation ssssssssseenee nennen 7 Activate a Stored Flight Plan 8 Activate a Flight Plan Leg 8
26. d GIA1 CONFIG GIA1 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio GIA2 CONFIG GIA2 audio config configuration The system should be serviced error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 COOLING GIA1 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to 2 COOLING GIA2 temperature operating temperature 00 low GIA1 COOLING GIA1 over temperature The G A1 and or GIA2 temperature is too high If GIA2 COOLING GIA2 over problem persists the system should be serviced temperature GIA1 SERVICE GIA1 needs ervice Return the unit for repai GIA2 SERVICE GIA2 needs ervice Return the unit for repai HW MISMATCH GIA hardware mismatch GIA1 communication halted A GIA mismatch has been detected where only HW MISMATCH GIA hardware one is WAAS capable mismatch GIA2 communication halted MANIFEST GIA1 software mismatch communication halted The GIA1 and or GIA 2 has incorrect software MANIFEST GIA2 software installed The system should be serviced mismatch communication halted The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced n n 3 PE
27. 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjueumasu S24V orpnyygqax si JUI05 AEN Sue v uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld ARN Sd5 yunuuy jeuuouqy jeuonippy paezey xipueddy x pul iui nu Flight Instruments Nav Com AFCS XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav Procedures Appendix Alerts Operation Features 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 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
28. 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 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 4 xipueddy suelv uoneiedo sainjea4
29. leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint Crosstrack error VNV Unavailable Excessive The current crosstrack exceeds the limit causing vertical deviation to go invalid selected VNV Unavailable Parallel course A parallel course has been selected causing the vertical deviation to go invalid NO WGS84 WPT Non WGS 84 waypoint for navigation xxxx The position of the selected waypoint xxxx is not calculated based on the WGS84 map reference datum and may be positioned in error as displayed Do not use GPS to navigate to the selected non WGS84 waypoint failed TRAFFIC FAIL Traffic device has f The system is no longer receiving data from the traffic system The traffic device should be serviced FAILED PATH A data path has failed A data path connected to the GDU GSD 41 or the GIA 63 W has failed 74 Garmin 61000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations 8 Alerts MISCELLANEOUS MESSAGE ADVISORIES CONT Message MAG VAR WARN Large magnetic variance Verify all course angles Comments The GDU internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2
30. nav angle is set to AUTO GPS1 SERVICE GPS1 needs af service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs Service Return unit for repair NAV2 SERVICE NAV2 needs if Service Return unit for repair 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 If the problem persists the system should be serviced 6 51 FAIL G S1 is inoperative 6 52 FAIL G S2 is inoperative A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced Return unit for repair Return unit for repair G S1 SERVICE G S1 needs service G S2 SERVICE G S2 needs service A failure has been detected in glideslope receiver 1 and or receiver 2 The receiver may still be available The system should be serviced when possible GEA 71 MESSAGE ADVISORIES
31. return to the top level softkeys 84 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN MAP DCLTR 190 00525 03 Rev A TRAFFIC TOPO TERRAIN AIRWAYS STRMSCP NEXRAD XM LING BACK Appendix Enables second level Navigation Map softkeys Displays traffic information on Navigation Map Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map Displays terrain information on Navigation Map Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed Displays 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 Returns to top level softkeys Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s n e 4 auepiony 2 buluueld AEN Sd5 52 olpny uqax sia sjuaumnasu jeuonipp
32. ssseeennnnnnnnnnn MEC O eue ie eee te er ete eie eerie 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 ssssssssee e 63 Database Message Advisories GMA 1347 Message Advisories GIA 63W Message Advisories ssssssse nne GEA 71 Message Advisories sssssssseeee enne GTX 33 Message Advisories GRS 77 Message Advisories GMU 44 Message Advisories sssssssee ne GDL 69 69A Message Advisories GDC 74A Message Advisories GTS 820 Message Advisories Miscellaneous Message Advisories Flight Plan Import Export Messages o m dite b 79 PED Softkey Map 5 erc et tere eee eae 79 MED Softkey Map nnne 84 Database Updates sssssssseeeneenn nnne 86 ndex 1 ii 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Table of Contents GARMI N Blank P
33. 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 2 4 AEN 540 nubi CREATE A NEW 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 the NEW Softkey A waypoint is created at the current aircraft position 4 Enter the desired waypoint name 5 Press the ENT Key 6 cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sia sjuounasu U105 AEN 3461 olpny uqax 52 eouepioAy paezey spay uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Haza
34. 000 Cockpit Reference Guide for the Beechcraft A36 G36 n soJnjeoJ 2 AEN Sd 24V oipny uadx si siu umn sul paezey nubi jeuonippy uoneiedo Jeuuouqy x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 12 Annunciations amp Alerts A GARMIN MISCELLANEOUS MESSAGE ADVISORIES CONT vertical waypoint Message Comments SLCT NAV Select NAV on CDI for The system notifies the pilot to set the CDI to the approach correct NAV receiver Set the CDI to the correct NAV receiver PTK FAIL Parallel track unavailable lal aa bad geometry p 9 Y 10 UL IAF waypoint for parallel offset has been passed past IAF 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 within the maximum flight path angle and vertical speed constraints The system automatically transitions to the next vertical waypoint angle error VNV Unavailable Excessive track The current track angle error exceeds the limit causing the vertical deviation to go invalid type in flight plan VNV Unavailable Unsupported leg The lateral flight plan contains a procedure turn vector or other unsupported
35. 00525 03 Rev A A GARMIN 00000 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 If the Display Database Selection Softkey is pressed repeatedly the softkey will switch between PFD1 and MFDI Database status information in the Database Window will reflect the database of the PED or MFD Protos PROT a 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 validat
36. 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 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 indi
37. AEN paezey saunyea4 Jeuolppy Sue v unuuy xipueddy x pul iui TL Nav Com XPDR Audio Hazard Avoidance Additional Annun Flight Instruments Flight Planning EIS AFCS Alerts Features Procedures GPS Nav Appendix Index Abnormal Operation GARMI N CDI DR Indication on PFD Symbolic Aircraft Map pages and Inset Map Dead Reckoning Indications As a result of operating in DR Mode all GPS derived data is computed based upon an estimated position and is displayed as yellow text on the display to denote degraded navigation source information This data includes the following Navigation Status Box fields except Active Leg TAS and DTK GPS Bearing Pointer Wind data and pointers in the Wind Data Box on the PFD Current Track Indicator All Bearing Pointer Distances Active Flight Plan distances bearings and ETE values Also while the G1000 is in DR Mode the autopilot will couple to GPS for up to 20 minutes 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 A36 G36 190 00525 03 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS
38. 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 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 A36 G36 190 00525 03 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 desi
39. 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 previous page Change Day Night View 1 While viewing a chart press the MENU Key to display the Page Menu OPTIONS 2 Tum the large FMS Knob to highlight the Chart Setup Menu Option and press the ENT Key 3 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 f
40. DI 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 WAAS source data resumes automatically once a valid GPS solution is restored It is important to note that estimated navigation data supplied by the G1000 in DR Mode may become increasingly unreliable and must not be used as a sole means of navigation If while in DR Mode airspeed and or heading data is also lost or not available the DR function may not be capable of estimating your position and consequently the system may display a path that is different than the actual movement of the aircraft Estimated position information displayed by the G1000 through DR while there is no heading and or airspeed data available should not be used for navigation DR Mode is inherently less accurate than the standard GPS WAAS 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 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sepeooid uluueld AEN 540 S24Y oipny uadx si uo2
41. Departure Procedure Activate A Departure Leg Load An Arrival Procedure Activate An Arrival 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 30 Customizing the Hazard Displays on the Navigation 39 STORMSCOPE Optional XM Weather Subscription Optional Traffic Systems s b z SUZ oce rS Allah e edes Terrain Awareness amp Warning System TAWS Display 44 ADDITIONAL FEATURES Synthetic Vision sss Terminal Procedure Charts AOPA Airport Directory ssssssseeeeennennennennnnnnns Radio Entertainment Subscription Optional 51 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN Tale of Contents ABNORMAL OPERATION Reversionary Mode ssssssssssseeeenenne nennen Abnormal COM Operation ssssssssseeeennennnnnn Hazard Displays with Loss of GPS Position Unusual Attitudes
42. EL 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 point 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 2 Press the FPL Key to display the Active Flight Plan Page on the MFD 3 Turn the smal card into the top card slot on the MFD 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 03 Rev A Garmin G1000 Cockpit Reference Guide
43. G1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft A36 G36 A GARMIN Copyright 2005 2010 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0858 07 or later for the Beechcraft A36 G36 Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton 5040 ORB U K Tel 44 0870 8501241 Fax 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shiir Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 STI or after 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 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby grants permission to download a single copy of this manual and of an
44. HE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings CAUTION The Garmin G1000 does not contain any user serviceable parts Repairs should only be made by an authorized Garmin service center Unauthorized repairs or modifications could void both the warranty and the pilot s authority to operate this device under FAA FCC regulations Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Sing Cautions amp Notes 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 co
45. MS 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 cursor is displayed in the RAD radial field Enter the desired radial from the reference waypoint 12 Press the ENT Key 13 The cursor is now displayed in the DIS distance field Enter the desired distance from the reference waypoint 14 Press the ENT Key 15 Press the FMS Knob to remove the flashing cursor 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 A36 G36 190 00525 03 Rev A GARMIN 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
46. Message Comments GEA1 CONFIG GEAT config error Config service req d The GEA1 configuration settings do not match those of backup configuration memory The G1000 system should be serviced MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The G1000 system should be serviced 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s m 2 4 4 AEN 5640 yi oipny uddx sia sjueumansu paezey nubi wi0 gt AeN Wil jeuonippy uoneiedo Jeuuouqy R x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix Ea Annunciations amp Alerts GTX 33 MESSAGE ADVISORIES A GARMIN 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 1 is inoperative There is no communication with the 1 transponder GRS 77
47. NE 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 1 500 Fuel Calculation Information ELECTRICAL 1 ALT LOAD _2 40 50 Electrical 1 BUS VOLTS_2 Information 28 0 274 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 A36 G36 190 00525 03 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 the 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
48. NOTE The Jeppesen aviation navigation database is now referred to as the navigation database Previously this database had been referred to as the aviation database The ChartView database should be copied to the Supplemental Data Card which will reside in the bottom card slot on the MFD The navigation database is be loaded from the Jeppesen or user supplied SD data card Contact Jeppesen www jeppesen com for subscription and update information The navigation database is loaded from an SD card inserted into the top card slot of each displayed The database is copied from the SD card in the top card slot to the displays internal memory Loading Updated Databases n 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 88 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Appendix 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 G 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 armin databases on the MFD card Fli
49. 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 guidance Altitude has been retrieved from the navigation database and is provided as a reference Altitude has been retrieved from the navigation database or has been entered by the pilot and matches a published altitude in the navigation database flight path guidance 190 00525 03 Rev A GARMI N 8 Hil htPlanning 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
50. V 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 Message GMA 1347 MESSAGE ADVISORIES Comments GMAT FAIL GMAT is inoperative GMA1 CONFIG GMAT config error Config service req d be serviced should be se The audio panel self test has detected a failure The audio panel is unavailable The system should The audio panel configuration settings do not match backup configuration memory The system rviced MANIFEST GMA1 software mismatch communication halted GMA1 SERVICE GMAT needs Service Return unit for repair The audio panel has incorrect software installed The System shou The audio panel self test has detected a problem in rtain audio functions may still be avail able and the audio panel may still be usable The the unit Ce system shou d be serviced d be serviced when possible 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Ainnir S Ales GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG G A1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req
51. WS 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 TANS FAIL Failure audio fault T TAWS Not D No GPS position TAMS N A Available Excessively degraded GPS TAWS Not signal Out of database TAMS N A None Available coverage area Sufficient GPS signal received TANS None None D after loss Available 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s m 2 buluueld AEN Sd5 S241V olpny uqax sia sjuaumasu 2 Wil uio AeN Yid jeuonippyv uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix ec Annunciations 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
52. Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key CREATE A NEW FLIGHT PLAN NOTE When creating a new flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 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 selection 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 Tum 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 4 Turn the small FMS Knob to display the Waypoint Inf
53. a2ueplony sainpadold buluueld AEN Sd5 S241V olpny uqax 913 sjuaumasu unuuy Jeuuouqy jeuonippy paezey nu U10 AEN 3 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 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 taxiw
54. adout 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Sjueunasu EJ sH ly uoneiado SoJnjeaJ eouepioAy saunpa20Jd Fuluueld AEN Sd5 2 olpny uqax unuuy jeuuouqy jeuonippy paezey U105 AEN xipueddy x pul iui n Flight Instruments E Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Engine Indication System GARMIN ENGINE SYSTEM DISPLAY 1 Press the ENGI
55. age Garmin 61000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN Flight instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Turn the BARO Knob to select the desired setting SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure 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 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 NAV2 standby frequency 3 Press the CDI Softkey a third time to return to GPS 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 xipueddy Suelv uoneiedo s m aoueplony s mp ooud Duruue d AEN Sd5 S24JV olpny uqax sia Tunuuy Jeuuouqy Jeuonippy paezey Wfi l4 U10 AEN x pul Nav Com XPDR Audio Abnormal A
56. agnetic compass Comments 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 11 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 communication halted The GDC 74A has incorrect software installed The G1000 system should be serviced
57. ation 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 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjuauimasu sub AEN Sd5 52 oipny uddx 010 AEN Duruue d s mp oold paezey Sue v uoneiedo SaJnjeoJ Junuuy 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 Hazard Avoidance 40
58. ays 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 ID the VOR symbol and intersection names if within the airport plan view Pressing 48 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure 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 diagra
59. by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system The flashing cursor moves to the barometric setting PRESSURE field Enter the desired baro setting Press the ENT Key when finished Note that in AUTOMATIC page mode the baro setting is provided by the setting entered on the PFD The flashing cursor moves to the air temperature TOTAL AIR TEMP field Enter the desired air temperature Press the ENT Key when finished Note that in AUTOMATIC page mode air temperature is provided by the system outside air temperature Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN ri htranning CREATE A NEW USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the MFD to select the WPT page group 2 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
60. cate 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 A36 G36 190 00525 03 Rev A A GARMIN HatardAvaldance XM WEATHER SUBSCRIPTION OPTIONAL WARNING Use of XM weather for hazardous weather penetration is not recommended Weather information provided by XM Radio Service is approved only for weather avoidance not penetration Displaying XM Weather on the Navigation Map Page 1 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
61. d TERRAIN CAUTION TERRAIN Caution Terrain Caution Terrain Clearance or Terrain UE 5 5 y Terrain Ahead Terrain Ahead Imminent Terrain TERRAIN TERRAIN Terrain Ahead Terrain Impact Caution ITI or Ahead TERRAIN 9 Caution Terrain Caution Terrain Reduced Required TERRAIN CAUTION OBSTACLE Caution Obstacle Cau Obstade Clearance or tion Obstade Caution ROC BHB o Obstacle Ahead Obstacle Ahead Imminent Obstacle TERRAIN OBSTACLE AHEAD Obstacle Ahead Obstacle Impact Caution 101 or Ahead OBSTACLE T Caution Obstacle Cau tion Obstacle Premature Descent TERRAIN T00LOW TERRAIN Too Low Terrain Alert Caution PDA 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations amp Alerts PFD MFD MED Alert Type TAWS B Page Aural Message Pop Up Alert Annunciation Altitude Callout None None Five Hundred 500 Excessive Descent TERRAIN SIKRE Sink Rate Rate Caution EDR Negative Cimb TERRAIN MEn Don t sink Rate Caution NCR or or TO0 LOW TERRAIN Too Low Terrain TAWS B SYSTEM STATUS ANNUNCIATIONS PFD MFD TAWS B Page Aural Alert Type Alert 27 un Annunciation Message Annunciation System Test in Progress TAHS TEST None TA
62. d 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 arrival 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 WAAS 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 A36 G36 190 00525 03 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 select
63. d from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as the sole source of obstacle and terrain avoidance information Always refer to current aeronautical 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 gui
64. d to smaller format Added Airways WAAS VNAV amp Charts Updated G1000 System Messages Added other GDU 8 10 parameters Removed FD Formatting featur 190 00525 03 Added GDU 11 01 parameters Added Synthetic Vision System Added 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 Fe Date of Revision Affected Pages July 2010 Production release 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Record of Revisions Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 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
65. dance or positive visual acquisition of conflicting traffic WARNING XM Weather should not be used for hazardous weather penetration Weather information provided by the GDL 69A is approved only for weather avoidance not penetration Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A amp GARMIN 5 ing Cautions amp Notes V ARNING NEXRAD vveather 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 vveather 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 A36 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
66. dditional 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 Vspeed Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field Turn the small FMS Knob cloc
67. 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 existing flight plan is not desired select CANCEL using the FMS Knob press the ENT Key select another existing or empty flight plan and again press the IMPORT Softkey 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 A36 G36 190 00525 03 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
68. e 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 Flight Instruments EIS Canceling an automatic database synchronization 1 While synchronization is in progress press the SYNC DBS Softkey to ES 7 92 disable automatic database synchronization sO x 2 Acknowledge the cancelation by pressing the ENT Key Loading the navigation database NOTE Loading the Jeppesen navigation database prior to its effective date E 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 zs 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 as 3 Turn the G1000 system ON A prompt similar to the following illustration is T displayed 58 DO YOU WANT TO UPDATE THE ACTIVE NAVIGATION DATABASE s g SELECTING YES WILL OVERWRITE THE ACTIVE NAVIGATION DATABASE FROM TO WORLDWIDE WORLDWIDE 0912 6913 19 NOL 009 17 DEC 2009 EL 17 DEC 2089 14 2010 2 8 INO WILL ASSUMED IN 28 SECONDS UPDATING NAVIGATION DATABASE PLEASE WAIT se Navigation Database Load Prompt 24 4 Pre
69. e Guide for the Beechcraft A36 G36 soJnjeoJ 2 AEN Sd S24V oipny uadx si syu unysu paezey nubi u102 AEN nubi jeuonippy uoneiedo Jeuuouqy EE x pul Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix eee A Annunciations amp Alerts GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Description Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User The file stored on the SD card did not contain waypoints imported successfully No a flight plan only user waypoints These stored flight plan data was modified waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import The SD card contains no flight plan data Flight plan import failed Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contai
70. e 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 A36 G36 190 00525 03 Rev A GARMIN FlightPlamning 3 Press the CLR Key to display a confirmation window 4 With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 After creating a flight plan on either the PFD or 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 Pa
71. eN Sd5 buluueld qos Blank Page 6 2 4 aoueplony puezey saunjyea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 636 92 A GARMIN A Activate a flight plan 18 Active Channel 51 ADF 9 10 54 ADS B 83 AHRS 70 71 Airport Signs 47 48 Airways 85 ALT 43 Altitude mode 43 Altitude volume 43 AOPAs 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 74 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 90 Index Database updates 86 88 89 Database Updates 86 DCLTR Softkey 48 Dead Reckoning 55 Declutter 54 79 85 Direct to 17 DME 9 10 DR mode 55 56 E Edit a flight plan 31 F FD 58 Flight Director 13 Flight path marker 47 Flight plan import export messages 76 77 FliteCharts 48 49 Frequency Transfer 10 H HF 10 Horizon heading 47 Inhibit 45 Inhibit TAVVS 45 nset Map 79 80 IOI 60 leppesen 49 L Lightning 39 40 80 ndex 1 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 24JV olpny uqax sia sjua
72. ed 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 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 Pr
73. erviced 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 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 A36 G36 190 00525 03 Rev A A GARMIN Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT Message MFD1 DB ERR MFD1 airport terrain database error exists
74. es the data but cannot guarantee the accuracy and completeness of the data 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjueuinasu sub uone1edo sounqea4 saunpa20Jd Fuluueld AEN 540 S24V oipny uadx jeuuouqy jeuonippy paezey Wija u102 AEN Sue v unuuy k Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Index Appendix A Appendix 60 GARMIN 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 Equipment required to perform the update is as follows Windows compatible PC computer Windows 2000 or XP recommended e 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
75. ess the ENT Key 4 final approach course becomes the active leg 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Sjueuinajsu iui Sue v uone1edo s n e 4 e uepioAv AEN 540 24V olpny uqax junuuy Jeuuouqy Jeuonippy puezey ubi Tu102 AEN xipueddy x pul Nav Com XPDR Audio Procedures 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 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 A36 G36 190 00525 03 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navig
76. evere or giving an intense radar echo WARNING Lamp s inside this product may contain mercury HG and must be recycled or disposed of according to local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal 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 T
77. following table when the flight director is not active activates the pilot side flight director in the listed modes Modes Selected Control Pressed E 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 default 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjuauimasu 1i 59 oipny uadx u102 AEN ARN Sd5 52 spay uoneiedo s m e uepioAy 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey TL xipuaddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard Avoidance Annun EIS GPS Nav AFCS
78. for the Beechcraft A36 G36 oipny uddx 59 sjuauimnasu U10 AEN 346 3 52 2 AEN 540 nubi uonesado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipueddy x pul GARMIN Flight Planning Ssjueuinijsu fila 59 U105 AEN s24v AeN Sd5 4 34 Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 636 34 A GARMIN Procedures 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 displa
79. ge 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 oipny uddx s q sjuaumasu U10 AEN 16114 52 2 4 AEN 540 nubi uonesado saunyea4 e uepioAy Junuuy jeuuouqy jeuonippy paezey xipuaddy 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 P
80. hen imported due to naming conflicts with waypoints already existing in the system Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have sufficient available memory or the card may have been removed prematurely 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 saunyea4 aoueplony 2 fuluueld ARN SdD 2 oipny uddx sia Sjueunasu u102 AEN jeuonippy uoneiedo Jeuuouqy x pul iui Wfi l4 paezey Ins Flight Instruments Nav Com XPDR Audio Flight Planning Additional Hazard Avoidance Abnormal EIS AFCS Procedures GPS Nav Features Operation Appendix Index Annunciations amp Alerts Blank Page 78 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 636 A GARMIN 190 00525 03 Rev A A GARMIN SSP Peernix APPENDIX PFD SOFTKEY MAP optional r mu m r 7 m mu m r CDI NAV1 CD NAV2 CDI GPS Top Level PFD Softkeys optional me E El 999 Ez r1 owe 1 5866 fer REY ST ERTS n 77 O D v nnn on optional optional optional OFF DCLTR TRAFFIC TOPO_ TERRAIN STRMSCA NEXRAD XM LING a D Ou vu mu m Press the BACK Softkey to return t
81. ing AFCS GPS Nav Appendix Alerts Operation Features Avoidance Procedures Index Engine Indication System LEAN ENGINE DISPLAY EGT peak temperature Exhaust Gas Temperature Bar Graph Cylinder Head Temperature Bar Graph HAN IN HG 35 23 FFLOW GPH 14 0 APEAK 11 C A GARMIN Fuel Flow Numeric Readout Difference be tween peak and current tempera ture e selected cylinder LEAN Engine Page EGT Readout For Selected Oylinder CHT Readout For Selected Oylinder 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 A36 G36 190 00525 03 Rev A GARMIN Engine Indication System When the 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 re
82. installed navigat tored flight plan The obsolete flight plan with cu rrent arrival or approach o n r o Update LOCKED FPL Cannot navigate locked flight plan This occurs when stored flight plan Remove Update flight plan that with current waypoint the pilot attempts to activate a contains locked waypoint ocked waypoint from flight plan WPT ARRIVAL Arriving at waypoint xxxx Arriving at waypoint xxxx where xxxx waypoint name is the STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less Special use airspace is ahead of aircraft The than 10 minutes aircraft will penetrate the airspace within 10 minutes ARSPC NEAR Airspace near and Special use airspace is near and ahead of the ahead aircraft position ARSPC NEAR Airspace near less Special use airspace is within 2 nm of the aircraft than 2 nm 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 The system notifies the pilot to load the approach frequency for approach frequency for the appropriate NAV receiver Select the correct frequency for the approach 190 00525 03 Rev A Garmin G1
83. k Page 6 2 4 aoueplony puezey s m d Jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 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 desired press the ENT Key to activate To enter an altitude constraint proceed to step 5 5 Turn the large FMS Knob to place the cursor over the VNV altitude field 6 Enter the desired altitude 7 Press the ENT Key If the waypoint entered is an airport the option to select MSL or AGL is now displayed If the waypoint is not an airport proceed to step 9 8 Turn the smal 9 Press the ENT Key The cursor is now flashing in the VNV offset distance field FMS Knob to select MSL or AGL 10 Enter the desired offset distance before the waypoint 11 Press the ENT Key The Activate field is highlighted 12 Press the ENT Key to activate Direct to Navigation from the PFD 1 Press the Direct to Key 8 2 Tum the large FMS Knob to place the cursor in the desired selection field 3 Turn the small FMS Knob to begin selecting the desired identifier location etc 4
84. kwise 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 A36 G36 190 00525 03 Rev A A GARMIN Vi git instruments SET BAROMETRIC MINIMUM DESCENT ALTITUDE mal ED g 2 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 593 olpny uqax ui0 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 SeJnpa20Jd 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 sual uoneiado saunyea4 unuuy jeuuouqy jeuonippy paezey xipueddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Nav Com XPDR Audio Flight Planning Abnormal Additional Hazard A
85. le its operation If the problem persists the system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck COM2 RMT XFR COM2 remote transfer key is stuck The COM1 and or COM2 transfer switch is stuck n the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the system should be serviced ENS LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase with other NAVS of flight GPS NAV LOST Loss of GPS Loss of GPS navigation due to insufficient navigation Insufficient satellites satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Approach downgraded Vertical guidance generated by WAAS is unavailable use LNAV only minimums 68 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations 8 Alerts GIA 63W MESSAGE ADVISORIES CONT Message TRUE APR True north approach Change HDG reference to TRUE Comments Displayed after passing the first waypoint of a true north approach when the
86. lected COPILOT OFF ON radios pilot passengers music Selected CREW ON ON radios pilot copilot Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A Selected radios pilot copilot passengers music Copilot passengers music Copilot Selected radios pilot copilot Selected radios pilot copilot passengers music Copilot passengers music Selected radios pilot passengers music Passengers music uonesado s n e 4 eouepioAy s mp oold Buruue d AEN Sd5 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul n GARMIN Nav Com XPDR Audio Panel Sjueuinijsu fila 59 oipny uadx U10 AeEN S2dV AeN Sd5 Duruue d qos Blank Page 6 2 4 aoueplony puezey saunjea4 jeuonippy uoneiedo jeuuouqy suay Junuuy x pu ddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 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
87. mponents 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 waypoint identifier 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 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s m aoueplony SoJnpa204d Duruue d AEN Sd5 52 olpny uqax sia sjuauimasu jeuonippy 2 nubi JUI0 NEN Yid uoneiedo Jeuuouqy Sue v unuuy ER Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix ALT UNIT METERS HPA STD BARO A GARMIN 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 EM onno m nn AA Press the BACK Softkey to return to the top level softkeys ET TT Press the BACK Softkey to return to the previous level softkeys
88. ms 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 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Seunpa20Jd Buruuejd AeN Sd5 S24V olpnyyuqax sia siu uinnsul fila Tu102 AEN 346 aoueplony paezey s m e q jeuonippy xipueddy suelv uoneiedo junuuy Jeuuouqy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional Features Abnormal
89. ned user waypoints only The file stored on the SD card did not contain a flight plan only user waypoints One o more of these waypoints did not import successfully 1 Too many points Flight plan truncated 1 The flight plan on the SD card contains more waypoints than the system can support The flight plan was imported with as many waypoints as possible Some waypoints not loaded Waypoints 1 The flight plan on the SD card contains one locked or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use 4 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations amp Alerts FLIGHT PLAN IMPORT EXPORT MESSAGES CONT Flight Plan Import Export Results User waypoint database full Not all loaded Description The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system capacity therefore not all the user waypoints on the SD card have been imported Any flight plan user waypoints that were not imported are locked in the flight plan The flight plan must be edited within the system before it can be activated for use One or more user waypoints renamed One or more imported user waypoints were renamed w
90. ng 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 all altitude airways and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted 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 th
91. ntain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional information please refer to our web site at www garmin com prop65 NOTE Interference from GPS repeaters operating inside nearby hangars can cause an intermittent loss of attitude and heading displays while the aircraft is on the ground Moving the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE The purpose of this Cockpit Reference Guide is to provide the pilot a resource with which to find operating instructions on the major features of the G1000 system more easily It is not intended to be a comprehensive operating guide Complete operating procedures for the system are found in the G1000 Pilot s Guide for this aircraft 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A Warnings Eu uode SMotes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN Record of Revisions Part Number Change Summary 190 00525 00 190 00525 01 RevA Added GDU software version 6 13 parameters Added TAWS Changed system software number to 0464 08 190 00525 02 RevA Change
92. nto 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 3 eoueproAy Senpa204d Buruue d AEN Sd5 52 44 53 5149 11 15 puezey ubi U10 AEN ubiu saunqee4 jeuonippy Sue v unuuy xipueddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional Annun EIS AFCS GPS Nav Avoidance Procedures Features Appendix Alerts Index Abnormal Operation UNUSUAL ATTITUDES A GARMIN 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 54 Traffic Annunciations AFCS Annunciations Flight director Com mand Bars Inset Map Temperatures DME Information Window Wind Data Selected Heading Box Selected Course Box Transponder Sta
93. o the top level softkeys Inset Map Softkeys INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map DCLTR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan TRAFFIC Displays traffic information on Inset Map 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 s m aoueplony SoJnpa204d buluueld AEN 540 S24JV olpny uqax 513 sjueumasu puezey U105 AEN jeuonippy uoneiedo Jeuuouqy Sue unuuy gt 5 x x pul ii TL Flight Instruments Annun Abnormal Additional Hazard Flight Nav Com Appendix Alerts Operation Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Index Appendix TOPO TERRAIN STRMSCP NEXRAD XM LING A GARMIN Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Inset Map Displays terrain information on Inset Map Press to display the Stormscope lightning data on the Inset Map within a 200 nm radius of the aircraft Displays NEXRAD weather and coverage information on Inset Map optional feature Displays XM lightning information on Inset Map optional feature optional me C7 ES eS C837 Love Ge ee per sr eS pnpnnunanunnniuoMnT9
94. o 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 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 eouepioAy paezey suelv uoneiedo sainjea4 unuuy Jeuuouqy Jeuonippy xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 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 F
95. ormation Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjuauimasu sub oipny uadx si U105 AeN 52 2 4 AEN 540 nubi uoneiado saunyea4 aoueplony unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Additional Hazard Avoidance Abnormal Annun Flight Instruments EIS AFCS Flight Procedures Planning GPS Nav Appendix Alerts Operation Features Index Flight Planning 5 6 7 A GARMIN with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list IMPORT A FLIGHT PLAN FROM AN SD CARD 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
96. our 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 G1000 Cockpit Reference Guide for the Beechcraft A36 636 190 00525 03 Rev A A GARMIN Additional Features XM RADIO ENTERTAINMENT SUBSCRIPTION OPTIONAL The XM Radio Page provides information and control of the audio entertainment features of the XM Satellite Radio Selecting the XM Radio Page 1 Turn the large FMS Knob to select the Auxiliary Page Group 2 Turn the small FMS Knob to select 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
97. place data card If problem persists the system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFD and MFD have different navigation database versions or types Americas European etc installed Crossfill is off Install correct navigation database version or type in all displays DB MISMATCH Terrain database The PFD and MFD have different terrain database mismatch versions or types installed Install correct terrain database version or type in all displays 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 65 saunqee4 2 AEN Sd 24V oipny uadx sia syu unysu paezey u102 NEN nubi jeuonippy uoneiedo Jeuuouqy p x pul Hazard Flight Nav Com Hight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix fee Annunciations amp Alerts DATABASE MESSAGE ADVISORIES CONT A GARMIN Message DB MISMATCH Obstacle database mismatch Comments The PFD and installed Install cor displays MFD have different obstacle database rect obstacle database in all DB MISMATCH Airport Terrain database mismatch The PFD and databases installed Install correct airport terrain database in all displays MFD have different airport terrrain NA
98. point 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 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 A36 G36 190 00525 03 Rev 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 deacti
99. procedures must be learned on the ground WARNING The United States government operates the Global Positioning System and is solely responsible for its accuracy and maintenance The GPS system is subject to changes which could affect the accuracy and performance of all GPS equipment Portions of the Garmin G1000 utilize GPS as a precision electronic NAVigation AID NAVAID Therefore as with all NAVAIDs information presented by the G1000 can be misused or misinterpreted and therefore become unsafe WARNING To reduce the risk of unsafe operation carefully review and understand all aspects of the G1000 Pilot s Guide documentation and the Beechcraft A36 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 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A Warnings Kanan 2 Notes GARMIN 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 s
100. r update the waypoint name identifier to refle the new information t an FPL WPT MOVE Flight plan waypoint moved TIMER EXPIRD Timer has expired The system has detected that a waypoint coordinate has changed due to a new navigation databas update Verify that stored flight plans contain correct waypoint locations D 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 72 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Annunciations 8 MISCELLANEOUS MESSAGE ADVISORIES CONT Alerts Message DB CHANGE Database changed Verify stored airways Comments an use of airways in stored flight plans and irways as needed ab This occurs when a stored flight plan contains airway that is no longer consistent wit navigation database This alert is issued only after an navigation database update Ver h the ify eload FPL TRUNC Flight plan has been truncated database eliminates an obsolete approach rrival used by a s procedure is removed from the flight plan ab This occurs when a newly
101. r 60 degrees south Manual System Test 1 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Test TAWS Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain on the TAWS B Page 1 2 3 4 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the TAWS B Page 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 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A GARMIN Hazara avoidance 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 2 3 While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Show or Hide Aviation Data Press the ENT Key TAWS Inhibit Inhibit TAWS While the TAWS B Page is displayed press the INHIBIT Softkey 1
102. rd 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 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 Initiall
103. red 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 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 Ke
104. ress 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 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 A36 G36 190 00525 03 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 CANC
105. 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 the text of the report Panning over an airport with METAR information does not display more information but allows the user to press the ENT Key and select that Airport s Information Page to display the text of the report Pressing the ENT Key when panning over a TFR displays TFR specific information 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 ARN Sd5 S24V olpny uqax 59 UI0 AeN buluueld ni aoueploay s mp oold paezey Suelv uoneiedo sainjea4 junuuy jeuuouqy jeuonippy xipuaddy x pul Nav Com XPDR Audio Hazard Avoidance Procedures Abnormal Additional Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Index Hazard Avoidance GARMIN Weather Products and Symbols Icing Potential
106. ss the YES Softkey to update the navigation database in the 5 After the update completes the display starts in normal mode 6 Tum the G1000 system OFF and remove the SD card from the top card slot 7 Repeat steps 2 through 6 for the PFD Index Appendix 90 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Appendix 8 Apply power to the system and press the ENT 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 Press the Display Database Selection Softkey to show navigation database information for each display MFD1 DB PFD1 DB MFD1 DATABASE NAVIGATION INTERNAL REGION WORLDWIDE CYCLE 0913 EFFECTIVE 17 0 09 EXPIRES 14 JAN 10 Copyright 2009 Jeppesen Sanderson Inc BASEMAP BOTTOM CARD REGION WORLDWIDE VERSION 3 00 GARMIN LTD AND ITS SUBSIDIARIES 2008 SAFETAXI BOTTOM CARD REGION VERSION Check Database Cycle Number MFD shown 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 oipny uddx s q sjuaumasu U105 AEN 52 uoneiado saunyea4 aoueplony saunpa20Jd Fuluueld AEN Sd5 jeuonippy 2 jeuuouqy Sue v unuuy Db 5 o 3 x x pul 346 GARMIN Appendix Sjueuinijsu fila 59 u102 AEN s24v A
107. t 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 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 A36 G36 190 00525 03 Rev A GARMIN X U Abnormal Operation ABNORMAL OPERATION REVERSIONARY MODE Should a system detected failure occur in either display the G1000 automatically enters reversionary mode In reversionary mode critical flight instrumentation is combined with engine instrumentation on the remaining display Reversionary display mode can be manually activated by pressing the DISPLAY BACKUP Button on the audio panel NOTE The Beechcraft A36 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 i
108. teCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or DATABASE 7A Checklist File N A Busemup Land 2 00 SafeTaxi N A Afa Terrain Data N A de Airport Terrain Data N A gt lt Obstacle Data N A 24 35 Apt Directory N BY Chart Dato N A All map and terrain data provided is only to be used as a general reference to your surrounding and as an aid to situational awareness Database Information on the Power up Screen the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn 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 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sainjea4 aoueplony SoJnpa204d Duruue d AEN Sd5 24JV oipny uddx sia sjuauimnasu jeuonippy Wil JUI0 NEN ui uoneiedo Jeuuouqy Sue v unuuy DR A Appendix CCUG ARMIN 12 Turn the small FMS Knob to select the System Status Page 13 Press th
109. 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190 00525 03 Rev A A GARMIN Nav Com XPDR Audio Panel 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 Sjueuingjsu iui 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 Se
110. tomatically uses the altitudes loaded with the approach for giving vertical flight path guidance outside the FAF Note these altitudes are displayed as small light blue text Altitudes associated with arrival procedures are manually designated This means the system does not use the altitudes loaded with the arrival for giving vertical flight path guidance until designated to do so by the pilot Note that these altitudes are initially displayed as white text These altitudes may be designated by placing the cursor over the desired altitude and pressing the ENT Key After designation the text changes to light blue Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It 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
111. tus Box System Time PFD Setup Menu Windows displayed in the lower right corner of the PFD Timer References Nearest Airports Flight Plan Messages Procedures DME Tuning Barometric Minimum Descent Altitude Box Glideslope Glide path and Vertical Deviation Indicators Altimeter Barometric Setting Selected Altitude VNV Target Altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 Extreme Pitch Indication 190 00525 03 Rev A GARMIN Abnormal operation DEAD RECKONING While in Enroute or Oceanic phase of flight if the G1000 detects an invalid GPS solution or is unable to calculate a GPS position the system automatically reverts to Dead Reckoning DR Mode In DR Mode the G1000 uses its last known position combined with continuously updated airspeed and heading data when available to calculate and display the aircrafts current estimated position NOTE Dead Reckoning Mode only functions in Enroute ENR or Oceanic OCN phase of flight In all other phases an invalid GPS solution produces a NO GPS POSITION annunciation on the map and the G1000 stops navigating in GPS Mode DR Mode is indicated on the G1000 by the appearance of the letters DR superimposed in yellow over the own aircraft symbol as shown in the following figure In addition DR is prominently displayed also in yellow on the HSI slightly above and to the right of the aircraft symbol on the C
112. umasu Jeuonippy nf Tuo2 NeN ui uoneiedo Jeuuouqy Sue v unuuy mk Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Abnormal Operation Annun Alerts Appendix index M Map panning 41 Message advisories 63 66 68 75 MET 58 METAR 41 Minimums 62 Mistrim 58 59 MKR MUTE 11 Mode 83 Mode selection softkeys 9 Multi Function Display MFD Softkeys 84 N NAV 10 NAV1 1 10 NAV2 1 10 Navigation database 19 20 65 NEXRAD 41 42 80 85 0 085 2 Obstacles 66 67 P Pathvvays 47 48 R Reversionary mode 53 ROC 60 S SafeTaxi 48 Secure Digital SD cards 86 Store Flight Plan 31 Stormscope lightning data 39 40 80 Strike 39 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A GARMIN Strike mode 40 Supplemental Data Card 87 88 SVS 47 75 Synthetic Vision System 47 T TA 62 TAF 41 TAS 43 62 70 TAWS 44 45 59 Terrain 44 65 80 85 Timer 72 Topographical data 80 85 Traffic 39 43 79 85 Traffic Advisory 62 Traffic advisory 42 Traffic map page 43 44 Transponder 9 82 83 V Vertical speed guidance 20 Vertical track 62 VNV 17 54 74 Vspeed 2 W WAAS 67 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 03 Rev A A GARMIN
113. ures Avoidance Procedures Planning GPS Nav AFCS XPDR Audio EIS Instruments Additional Abnormal Operation Index Appendix 1 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 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 20 x If annunciated when 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
114. vate 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 13000 um White ext COVIE 9 0NM 12400FT LEMYN 220 8 0NM 9900 Large Lig Blue Text Approach KDFW RNAV 17Lsps LPY RIVET iaf 259 18 84 4000FT Sma Lig DRAAK 176 33w 2000r7 202 Text INWOD 176 3 2NH Sma m PA Je EP IE Blue Subdued MENOL faf 176 3 9NM Text RW17L 5 3NM Small White Text 99 FT 8NM with Altitude POLKE Restriction Bar SIUE Cross AT or ABOVE 5 000 fi VAC B Cross AT 2 300 ft ICI Cross AT or BELOW 3 000 ft 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 513 siu uinnsu iui oipny uadx 010 AEN suelv uoneiedo sainjea4 2 buluueld Tunuuy Jeuuouqy Jeuonippy paezey Wfil4 x pu ddy 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 au
115. voidance Annun AFCS Procedures GPS Nav Appendix Alerts Operation Features Index Flight Instruments Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 A GARMIN 190 00525 03 Rev A GARMIN Engine Indication System ENGINE INDICATION SYSTEM sjueuinasu iui 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 F Pressure Gauge BAEO 3f BS P e 524 52 S i H 4 RPM Gauge RPM 3000 Fuel Fl un 0 uet FLOW se 238U Numeric a Fuel Flow FFLOW GPH Readout ndicator Leaning E Pointer 8 Cylinder Head Oil Temperature OIL TEMP Temperature ndicator v Indicator z OIL PRES SE J Oil Pressure ALT LOAD Indicator 2 Ammcter MS BUS VOLTS HE un ali Voltmeter 8g Fuel Quantity rea 2E Indicator s 88 6 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 as a reference when adjusting fuel mixture xipuaddy x pul 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 lel Nav Com XPDR Audio Abnormal Additional Hazard Annun Flight Instruments Flight Plann
116. y 2 nf JUI0 NEN Yid uoneiedo Jeuuouqy Sue v unuuy m GARMIN SHVV CHRT When available displays optional airport and terminal procedure charts CHKLIST When available displays optional checklists DATABASE UPDATES The system uses Secure Digital SD cards to load and store various types of data For basic flight operations SD cards are required for database storage as well as Jeppesen navigation and Jeppesen ChartView database updates Not all SD cards are compatible with the G1000 Use only SD cards supplied by Garmin or the aircraft manufacturer Information regarding the various databases may be viewed on the AUX System Status Page 127 158 com 126 408 conz INFO AIRFRAME STATUS SERIAL NUMBER VERSION AIRFRAME Beechcraft A 7 00 SYS SOFTWARE VERSION 7 00 CONFIGURATION ID 27000006 2024 CP PART NUNBER SYSTEH ID CHECKLIST 47801548 1 05 1 05 num MFD DATABASE VERSION 1 01 46701911 2 07 CYCLE 0903 46701313 2 07 EFFECTIVE 15 JUL 09 FFFFFFFFF 1 02 EXPIRES 14 0cT 09 68500319 1 02 Copyright 2009 Aircraft Owners and Pilots Assn CHART BOTTOH CARD CHART FliteCharts REGION CYCLE 47500583 EFFECTIVE 47500607 EXPIRES 04 JUN 89 DISABLES 01 DEC 09 Copyright 2003 Garmin Ltd or its subsidiaries 48900000 484900001 LRU Display Database Selection Softkey AUX System Status Page 86 Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 190
117. y 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 A36 G36 190 00525 03 Rev A A GARMIN Flight Planning 12 Press the ENT Key 13 Repeat step 1 0 to enter the next waypoint name 14 Press the ENT Key The cursor is displayed in the RAD radial field for the second waypoint Enter the desired radial from the reference waypoint 15 Press the ENT Key 16 Press the FMS Knob to remove the flashing cursor CREATE A NEW USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM ANOTHER WAYPOINT sjuauimasu Yid oipny udax si U105 AeN 52 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 t
118. y 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 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 soJnjeoJ 2 AEN SdD S24V oipny uadx sia siu umn sul paezey nubi nubi euonippv uoneiedo Jeuuouqy IPM PE 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 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 s
119. y revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited ct Garmin and G1000 are registered trademarks of Garmin Ltd or its subsidiaries FliteCharts and SafeTaxi are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin f NavData is a registered trademark of Jeppesen Inc Stormscope and SkyWatch are registered trademarks of L 3 Communications and XM is a registered trademark of XM Satellite Radio Inc July 2010 190 00525 03 Rev A Printed in the U S A A Warnings Cantant amp Notes GARMIN e e WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain function The G1000 Terrain Proximity feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The Terrain Proximity feature is only to be used as an aid for terrain avoidance and is not certified for use in applications requiring a certified terrain awareness system Terrain data is obtaine
120. y 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 a rivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00525 03 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft A36 G36 sjuauimasu sub 59 olpny uqax 0105 AEN 52 AEN 540 Duruue d wold s mp old uonesado saunyea4 unuuy jeuuouqy jeuonippy paezey xipuaddy x pul Nav Com XPDR Audio Procedures Abnormal Additional Hazard Annun Flight Instruments Flight Planning EIS AFCS GPS Nav Appendix Alerts Operation Features Avoidance Index Procedures 0000000 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 highlighte

Garmin Software Version 0858.07 Cockpit Reference Guide

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