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Garmin SA01535Wi_D Cockpit Reference Guide

1. Terrain Ahead Terrain head or Caution Terrain Caution Terrain Caution Obstacle Caution Obstacle or Obstacle Ahead Obstacle Ahead 100 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts PFD MFD MFD Map Page Alert Type TAWS Page Bee Voice Message os Pop Up Alert Annunciation SE hace ead mminent Obstacle Impact TERRAIN or a la casi CAUTION GESTARE Caution Obstade Caution Obstacle Premature Descent Alert WERRATN XL TERN Too Low Terrain Excessive Descent Rate SINK RATE uc n Caution EDR TERRAIN Sink Rate ee oueRae TERRAIN T88GN Terain Terain n DONT SING Don t Sink egative Climb Rate TERRAIN ar at Caution NCR mOOLON TERRAIN Too Low Terrain Hight Into Terrain High TOO LOW TERRAIN u su Speed Caution FIT TERRAIN Too Low Terrain Flight Into Terrain Gear TOOLON GER u Caution FIT TERRAIN Too Low Gear Flight Into Terrain Flaps TOO LOW FLAPS u Caution FIT TERRAIN Too Low Flaps Flight Into Terrain Takeoff TOOLOW TERRAIN u su Caution FIT TERRAIN Too Low Terrain Glide Slope Deviation uch n Caution Gsb GLIDES OPE ales ope depends on approach type G
2. Winds Aloft 90 12 County Warnings 60 5 Cydone Warnings g 60 12 cng Potential CIP and EH m a iie ud Report n i T Air Report AIREPs m 90 12 Reports Turbulence R 180 12 Radar Coverage no product image 30 5 Temporary Flight Restrietion no product image 60 12 Terminal Aerodrome no product image 60 T 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 45 AEN Sd5 S24V oipny uadx sjueumasuj U405 AEN Wijd Buruue d 1614 ERIT sainpar0ld puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index A Hazard Avoidance GARMIN CONNEXT WEATHER OPTIONAL NOTE The availability of specific Garmin Connext Weather products varies by region For product coverage information refer to fly garmin com fly garmin gfds weather Weather data is provided when the pilot initiates either a manual or automatic Connext data request on the Weather Data Link CNXT Page on the MFD No weather data is displayed until the first Connext Weather Data Request is made Registering with Garmin Flight Data Services A subscriber account must be established prior to receiving Connext Weather products Contact Garmin Flight Data Services at https fly garmin com fly garmin suppor
3. Procedures REVERSIONARY SENSOR ANNUNCIATIONS Reversionary Sensor Condition Window Text Hazard Avoidance e Both PFDs are displaying data from the number one Air Data Computer Features n E E em 3 3 lt x Both PFDs are displaying data from the number two Air Data Computer Both PFDs are displaying data from the n Reference System mber one Attitude amp Heading f rom the n u Both PFDs are displaying data Reference System mber two Attitude amp Heading Both PFDs are displaying data from the number one GPS receiver Z Both PFDs are displaying data from the number two GPS receiver Appendix PFD2 is displaying data from the 1 Air Data Computer PFD1 is displaying data from the 2 Air Data Computer PFD2 is displaying data from the 1 AHRS Index WO 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Amunciations amp Alerts Reversionary Sensor Condition Window Text sjueuinijsu ufi PFD1 is displaying data from the 2 AHRS PFD2 is displaying data from the 1 GPS PFD1 is displaying data from the 2 GPS oipny uddx U105 AEN AFCS ALERTS a Condition Annunciation Description j Pitch Failure Pitch axis control failure d al C e AEN Sd5 Rol
4. 102 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Amunciations amp Alerts TAWS A Alert Type Availability Under Various Conditions SyueuinJjsu ufi TAWS A Alert Type Available TAWS A zm Status s Prset RTC ITI ROC IOI PDA EDR ECR NCR FIT GSD VCO 23 Displayed TAWS TEST No Nof No No No No No No No No No amp TAMS N A No No No No No Yes Yes Yes Yes No Yes TAMSEAI vo MSIE Ho DPE ve GS INH Yes GP INH Yes FLAP OUR Yes GSD alert will be available if a valid ILS is being used for navigation even if no valid GPS signal is being received No No No No Yes Yes Yes Yes Yes Yes ACN Sd5 No No No No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes No No No No No Yes Yes Yes Yes Yes Yes Yes Yes Yes No Yes Buruue d 164 Yes Yes Yes Yes Yes Yes Yes Yes No Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes Yes SoJnpa o0Jd VCO alerts are not issued if both TAWS and GPWS systems have failed or are not available X Only the portions of FIT Alerting based on flap position are disabled when FLAP OVR annunciation is HE 9 aN 2g n oO displayed TAWS B ALERTS g E PFD MFD is Alert Type TAWS Page MED MaR Fage Voice Message Bs
5. aminps Cautions amp Notes ee 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 G1000 Integrated Avionics System in the Airplane Flight Manual Thoroughly practice basic operation prior to actual use During flight operations carefully compare indications from the G1000 to all available navigation sources including the information from other NAVAIDs visual sightings charts etc For safety purposes always resolve any discrepancies before continuing navigation WARNING For safety reasons G1000 operational procedures must be learned on the ground WARNING Do not use the system to attempt to penetrate a thunderstorm The illustrations in this guide are only examples Both the FAA Advisory Circular Subject Thunderstorms and the Aeronautical Information Manual AIM recommend avoiding any thunderstorm identified as severe of giving intense radar echo by at
6. sss Invert An Active Flight Plan Remove a Departure Arrival Appr or Airway from a Flight Plan 31 Store a Flight Plan Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan sss Invert and Activate a Stored Flight Plan Copy a Flight Plan eret e ette Delete a Flight Plan ttn rient Graphical Flight Plan Creation Export a Flight Plan to an SD Card ssssss PROCEDURES iioii deiele igen stalin MRL aie Raden HAZARD AVOIDANCE s nnne 4 Load and Activate a Departure Procedure ss Activate A Departure Leg sssssssn Load An Arrival Procedure Activate An Arrival Leg sssssssen Load and or Activate an Approach Procedure Activate An Approach in the Active Flight Plan Activate a Vector to Final Approach Fix sss Activate A Missed Approach in the Active Flight Plan sss Temperature Compensated Altitude sssssse Customizing the Hazard Displays on the Navigation Map 4 STORMSCOPE Optional SiriusXM Satellite Weather Optional sss 43 Connext Weather Optional ssssssseeeenennn Airborne Color Weather Radar Traffic Avoidance Systems Traffic Collision Avoidance System TCAS II
7. PFD2 DB ERR PFD2 obstacle database missing The obstacle database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 airport terrain database error exists PFD1 DB ERR PFD1 airport terrain database error exists PFD2 DB ERR PFD2 airport terrain database error exists The MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced 110 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Message Comments MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 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 PFD2 DB ERR PFD2 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 and or PFDs detected a failure in the ChartView dat
8. o L 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 147 9 uepioAy SoJnpa20Jd paezey SoJnjee4j Jeuonippy xopu Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Features Appendix Annun Alerts Index A Appendix GARMIN 16 Press the ENT Key to acknowledge the startup screen 17 Turn the large FMS Knob to select the AUX Page group on the MFD 18 Turn the small FMS Knob to select the System Status Page 19 Press the Display Database Selection Softkey to show standby navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct standby navigation database cycle information is shown for each display Magnetic Field Variation Database Update At startup the system compares this version of the MV DB with that presently being used by each AHRS GRS1 and GRS2 If the system determines the MV DB needs to be updated a prompt is displayed on the Navigation Map Page as shown in the following figure Note in the following example GRSI is the first AHRS to indicate an update is available In actuality this is dependent on which AHRS is the first to report status to the system GRS2 may be displayed before GRS1 The order is not important only that both AHRS be updated GRS1 MV DB Update Available Update from 2005 to 2010 OK or CANCEL GRS1 Magnetic Field
9. GMAT needs Service Return unit for repair GMA2 SERVICE GMA2 needs Service Return unit for repair The audio panel self test has detected a problem in the unit Certain audio functions may still be available and the audio panel may still be usable The system should be serviced when possible GIA 63W MESSAGE ADVISORIES Message Comments GIA1 CONFIG GIA1 config error Config service req d GIA2 CONFIG GIA2 config error Config service req d The GIA1 and or GIA2 configuration settings do not match backup configuration memory The system should be serviced GIA1 CONFIG GIA1 audio config error Config service req d GIA2 CONFIG GIA2 audio config error Config service req d The GIA1 and or GIA2 have an error in the audio configuration The system should be serviced 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 113 aoueploay seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SyueuinJjsu paezey Wija U405 AEN Wijd SoJnjeeoj Jeuonippy ell PEE xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MR Index Annunciations amp Alerts A GARMIN Message Comments GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature
10. 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 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Warnings Cautions amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMI N Record of Revisions Part Number Change Summary 190 00929 01 Added Synthetic Vision System Added TAWS A Added AOPA Airport Directory Added dual navigation database capability Added database synchronization Added other GDU 10 00 parameters 190 00929 02 Added GDU 11 12 changes Added GTS 820 850 Added Electronic Stabilization amp Protection Iridium Telephone and Data Link Added Worldwide Weather 190 00929 03 Added other GDU 12 01 parameters Added METAR and WX LGND softkeys Updated XM weather product symbols Updated Iridium registration procedure Updated SiriusXM product references 190 00929 04 Added GDU 13 06 parameters Added GRS 7800 GTS 8000 GTX 3000 GRA 5500 Added Pilot Profiles Added Temperature Compensated Altitude Added User defined Holds Added TCAS II Removed Reports Page Added DG Mode Changed GFDS to Connext re D
11. 7 Press the ENT Key REGISTER will now be highlighted 8 Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field Accessing Connext Weather Products 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link CNXT Page When a weather product is selected for display on the Weather Data Link CNXT Page a box containing a symbol for the product and its age in minutes are shown in the upper right If weather data has not been requested N A is shown next to the product symbol instead of age The age of the weather product is based on the time difference between when the data was assembled on the ground and the current GPS time Weather products are updated continuously or refreshed at specific intervals defined in the Broadcast Rate column in the following table If for any reason a weather product is not refreshed within the defined Expiration Time intervals the data is considered expired and is removed from the display The age of the expired product is replaced by dashes If more than half of the expiration time has elapsed the color of the product age readout changes to yellow The refresh rate represents the interval at which the Garmin Connext ground based servers make available the most current known weather data It does not necessarily represent the rate at which new content is received from weather sources
12. Additional Features the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This Annun Alerts feature is only available in the Horizontal Scan Mode Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating Appendix and deactivating will also enable or inhibit the alert on the PFD Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon 3 landing the system will automatically switch to Standby Mode 60 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Haard Avoidance TRAFFIC AVOIDANCE SYSTEMS WARNING Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft e WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the d
13. Infrared Satellite Garmin Connext Weather Eaton Broadcast Product Symbol Time Rate Minutes Minutes sca Radar Precipitation E 30 Canada 3 PRECIP Furope 15 Australia 15 60 30 IR SAT ae eam E5 30 Continuous ca m aE 60 Continuous 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 41 S2dY olpny uddX s u wunysu W0 AEN AEN Sd5 Buruue d ERIT Sa1npa oJd puezey su jy unuuy s n e 4 jeuonippy xipuaddy xopu fila 36114 Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance A GARMIN Garmin Connext Weather expiration Broadeasi Product Symbol Time Rate Minutes Minutes Meteorological Aerodrome Report Lg METARs T 90 Continuous Winds Aloft WIND 90 Continuous Pilot Weather Report m PIREPs 90 Continuous Teper Signi estrigis no product image 60 Continuous TFRs TENUTI a no product image 60 Continuous TAFs The composite precipitation image is updated every 3 minutes but individual radar sites may take between 3 and 10 minutes to provide new data Canadian radar precipitation data provided by Environment Canada Australian radar precipitation data provided by the Australia Bureau of Meteorology Setting Up and Customizing the Connext Weat
14. The COM1 and or COM transfer switch is stuck in the enabled or pressed position Press the transfer switch again to cycle its operation If the problem persists the system should be serviced RAIM UNAVAIL RAIM is not available from FAF to MAP waypoints GPS satellite coverage is insufficient to perform Receiver Autonomous Integrity Monitoring RAIM from the FAF to the MAP waypoints LOI GPS integrity lost Crosscheck with other NAVS 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series GPS integrity is insufficient for the current phase of flight 115 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey 3614 U405 AEN Wi SoJnjeeoj Jeuonippy 3 EXE xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix M Index Annunciations amp Alerts A GARMIN Message Comments GPS NAV LOST Loss of GPS navigation Insufficient satellites Loss of GPS navigation due to insufficient satellites GPS NAV LOST Loss of GPS navigation Position error Loss of GPS navigation due to position error GPS NAV LOST Loss of GPS navigation GPS fail Loss of GPS navigation due to GPS failure ABORT APR Loss of GPS navigation Abort approach Abort approach due to loss of GPS navigation APR DWNGRADE Appr
15. SeJnpa oJd S VFV rx mm vs v mnm onm omn Tet Select the BACK Softkey Y to return to the top level softkeys TRFC2 aouepioay puezey Inset Map Softkeys TE Levell Level2 Description INSET Displays Inset Map in PFD lower left corner OFF Removes Inset Map A DCLIR Selects desired amount of map detail cycles 3 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 D gt so F a E xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 133 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix A GARMIN Level 1 Level 2 Description WX LGND TRAFFIC TOPO TERRAIN STRMSCP Displays icon and age on the Inset Map for the selected weather products optional Displays traffic information on Inset Map 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 Displays Worldwide Weather precipitation
16. The compensated altitude is computed as the temperature is selected 5 Press the ENT Key ACTIVATE COMPENSATION is highlighted 6 Press the ENT Key The compensated altitudes for the approach are shown in the flight plan Index 38 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Disabling temperature compensated altitude 1 2 3 4 5 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed Turn the FMS Knob to highlight Temperature Compensation Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Press the ENT Key CANCEL COMPENSATION is highlighted Press the ENT Key The temperature compensated altitude at the FAF is cancelled 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Procedures 39 AEN SdD S24V oipny uadx sjueumasuj u105 AeN fila Buruue d 16114 SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures 40 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN 190 00929 04 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE WARNING Do not use data link weather information for maneuvering
17. After synchronization is complete power must be turned off then on NAV DB UPDATED Active navigation database updated System has updated the active navigation database from the standby navigation database TERRAIN DSP PFD1 PFD2 or MFD1 Terrain awareness display unavailable One of the terrain airport terrain or obstade databases required for TAWS in the specified PFD or MFD is missing or invalid 112 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts GMA 1347D MESSAGE ADVISORIES Message GMAT FAIL GMAT is inoperative GMA FAIL GMA2 is inoperative Comments The audio panel self test has detected a failure The audio panel is unavailable The system should be serviced GMA XTALK GMA crosstalk error has occurred An error has occurred in transferring data between the two GMAs The system should be serviced GMA1 CONFIG GMAT config error Config service req d GMA2 CONFIG GMA2 config error Config service req d The audio panel configuration settings do not match backup configuration memory The system should be serviced GMA1 MANIFEST GMA1 software mismatch communication halted GMA2 MANIFEST GMA2 software mismatch communication halted The audio panel has incorrect software installed The System should be serviced GMA1 SERVICE
18. Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A FLIGHT PLAN 26 NOTE When creating a flight plan in the Active Flight Plan Window the first leg is activated automatically after it is created Creating an active flight plan 1 2 3 4 5 6 Press the FPL Key Press the FMS Knob to activate the cursor only on MFD Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key The active flight plan is modified as each waypoint is entered Repeat step numbers 3 and 4 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to remove the cursor Creating a stored flight plan 1 2 3 4 5 6 7 Press the FPL Key Turn the small FMS Knob clockwise to display the Flight Plan Catalog Page Select the NEW Softkey or press the MENU Key highlight Create New Flight Plan and press the ENT Key to display a blank flight plan for the first emp
19. Information contained within data link weather products may not accurately depict current weather conditions WARNING Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age WARNING Do not rely on information from the lightning detection system display as the sole basis for hazardous weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to the documentation from the lightning detection system manufacturer for detailed information about the system WARNING The Garmin system as installed in this 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 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN
20. Press the ENT Key The cursor moves to CONNECT d Press the ENT Key again to connect to the selected network Edit a Saved Network 1 While viewing list of saved networks press the FMS Knob to activate the cursor 2 Turn either FMS Knob to highlight the network to be edited 3 Pressing the ENT Key at this point will check or uncheck the AUTO CONNECT checkbox When a checkmark is present the system will automatically connect to the network when within range 4 Select the EDIT Softkey The cursor now appears in the CONNECTION SETTINGS window 5 Turn the large FMS Knob to select the network attribute to be edited 6 Turn the small FMS Knob to begin editing the field 7 When the entry is complete press the ENT Key 8 Turn the large FMS Knob or press the ENT Key until SAVE is highlighted 9 88 Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features Disconnect a Wi Fi Network sjueuinisu fid Select the DISCNCT Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Disconnect From Network c Press the ENT Key Delete a Saved Wi Fi Network oipny uddx U105 AEN S2dV 1 While viewing the list of saved networks press the FMS Knob to activate the cursor 2 Turn either FMS Knob to highlight the network to be deleted 3 Select the DELETE Softkey The
21. U10 AEN Wi x pu ddy Additional Hazard Flight Nav Com Flight Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Annun Alerts Appendix Index J Jeppesen 71 L Level Mode 94 Lightning 42 43 44 134 Low speed data 73 74 M Map panning 44 Message advisories 107 109 113 119 121 123 124 125 MET 99 METAR 43 Minimums 106 MISCOMP 98 Mistrim 99 Mode selection softkeys 5 Multi Function Display MFD Softkeys 142 N NAV 6 NAV1 2 6 NAV2 6 Navigation database 15 17 130 NEXRAD 43 134 143 NEXRAD Softkey 53 0 OBS 2 Obstacles 112 114 Overspeed Protection 10 P Pathways 69 70 PIREP 57 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN PIT 98 Predefined message 81 82 R RADIO softkey 89 Register 47 74 Resolution Advisory 61 ROC 100 104 S SafeTaxi amp 70 SBAS 10 36 68 114 116 Sector scan 60 Sensor 98 STAB 60 Standby 58 Standby Navigation Database 112 147 Store Flight Plan 32 Stormscope lightning data 41 42 43 134 Strike 42 Strike mode 43 SVT 69 128 SVT Terrain 69 Synchronization 145 SYNC Status 147 Synthetic Vision System 69 System ID 46 73 T TA 106 TAF 43 55 TAS 62 63 119 TAWS 65 66 67 68 100 101 102 103 105 TAWS B 65 67 TCAS Il 62 63 64 139 140 TCAS II System Test Fail 107 190 00929 04 Rev A A GARMIN TCAS II Sys
22. 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 when imported due to naming conflicts with waypoints already existing in the system 130 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Amunciations amp Alerts Flight Plan Import Export Description n Results a2 Flight plan successfully exported The stored flight plan was successfully exported to the SD card x Flight plan export failed The stored flight plan was not successfully exported to the SD gt B card The SD card may not have sufficient available memory 9 or the card may have been removed prematurely S2dV PILOT PROFILE IMPORT EXPORT MESSAGES Pilot Profile Import Export Results Description No pilot profile plan files found to import Displayed if the SD card does not have one or more valid pilot profile filenames AEN Sd5 Overwrite existing profile Displayed if the profile name matches the name of existing profile Buruue d 1614 Profile name invalid Enter a different profile Displayed if the profile name is invalid name A
23. traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed see Annunciations amp Alerts section If the self test fails the system will revert to Standby Mode and a voice alert appropriate for the installed system will be heard indicating the test failed Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 1 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the second rectangular page icon 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 display volume Select the desired altitude volume by selecting the BELOW NORMAL Hazard Avoidance 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 will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Select the FLT ID Softkey GTS 800 820 825 850 855 only to enable or disable Flight ID displayed with the intruder information Displaying Traffic on the Navigation Map 1 2 With the Navigation Map d
24. wo09 eN Wij sainjea4 Jeuonippy xipuaddy xopu Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Meroe Index Annunciations amp Alerts A GARMIN Message Comments FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR WARN Large magnetic variance Verify all course angles The GDU s internal model cannot determine the exact magnetic variance for geographic locations near the magnetic poles Displayed magnetic course angles may differ from the actual magnetic heading by more than 2 SVT SVT DISABLED Out of available terrain region Synthetic Vision is disabled because the aircraft is not within the boundaries of the installed terrain database SVT SVT 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 lt message gt Message criteria entered by the user USER MAG VAR User magnetic variation is active User magnetic variation mode was selected during previous operation and is still active checked at power up 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
25. ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 36 1 2 3 4 5 6 NOTE If certain GPS parameters SBAS RAIM etc are not available some published approach procedures for the desired airport may not be displayed in the list of available approaches Press the PROC Key Turn the large FMS Knob to highlight SELECT APPROACH Press the ENT Key A list of available approaches for the destination airport is displayed Turn either FMS Knob to highlight the desired approach Press the ENT Key A list of available transitions for the selected approach procedure is now displayed 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN LLL Procedures 7 8 9 10 11 12 lt Nee Press the ENT Key The cursor moves to the MINIMUMS field 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 TEMP COMP or optional RAD ALT Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for
26. AEN S2dV AEN Sd5 Buruue d wild Phone is dialing another phone Phone has failed SoJnpa oJd Phone status not known aouepioay puezey Phone is disabled a Phone is reserved for data transmission See eee mal Ed o S D a jeuonippy sye yjunuuy Calling other phone or incoming call from other phone xipuaddy Other phone is on hold xopu Phones are connected 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 15 Flight Nav Com Flight Planning GPS Nav AFCS XPDR Audio Instruments Procedures Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features GARMI N Incoming Calls When viewing MFD pages other than the AUX TELEPHONE Page a pop up alert will be displayed If the call is from the cabin CABIN will be displayed If the incoming call is an Iridium network call IRIDIUM will be displayed The pop up alert may be inhibited at times such as during takeoff In addition to the pop up alert a ringing phone symbol will be displayed to the right of the MFD page title Also the voice alert Incoming Call will be heard on the selected cockpit audio Answer an Incoming Call in the Cockpit 1 2 1 2 3 4 Press the TEL Key on the appropriate audio panel Select the ANSWER Softkey on the MFD Or While viewing the AUX TELEPHONE Page Press the TEL K
27. AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or rolls wings level depending on default ROL commanded bank angle Limits maximum commanded roll BANK Low Bank angle Key Heading Select Captures and tracks Selected HDG Key HDG Heading avigation GPS Arm Capture Track ah avigation VOR Enroute Captures and tracks selected VOR Arm Capture Track navigation source GPS VOR LOC NAV Key avigation LOC Arm Capture Track LOC No Glideslope Backcourse Arm Capture Captures and tracks a localizer E BC Key BC rac signal for backcourse approaches Approach GPS Arm Capture GPS rac Approach VOR Arm Capture VAPP rac Captures and tracks selected soe APR Key Approach ILS Arm Capture navigation source GPS VOR LOC Trac Glideslope Mode dis automatically armed Disengages autopilot and commands Takeoff on ground a constant pitch angle and wings TO level in preparation for takeoff GA Disengages autopilot and Switch Go Around in air commands a constant pitch angle GA and wings level in the air Activated only by Level Commands wings level attitude the ESP LVL function No annunciation Me int green along the Ro 190 00929 04 Rev A e AFCS Status Box The acceptable bank angle ra Scale of the Attitude Indicator ge is indicated in Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series sjueuinijsu ufi SE Ja E
28. Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displayed bearing value in the BEARING field When scanning horizontally a Bearing Line may be displayed to aid in positioning the antenna for the vertical scan If the Bearing Line is not displayed perform the fol lowing steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Bearing Line 3 Press the ENT Key Vertically Scan a Storm Cell 1 While in the Horizontal Scan view move the Joystick to place the Bearing Line on the desired storm cell or other area to be vertically scanned 2 Select the VERTICAL Softkey A vertical slice of the selected area will now be displayed 3 Move the Joystick right or left to move the scanned slice a few degrees right or left 4 Turn the Joystick to adjust the range 5 To select a new area to be vertically scanned select the HORIZON Softkey to return to the Horizontal Scan view and repeat the previous steps Adjusting Gain a WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed as a color not representative of the true intensity Remember to return the gain setting to Calibrated for viewing the actual intensity of precipitation 1 Select the GAIN Softkey to activate the cursor in the GAIN field 2 Turn the small FMS Knob to adjust the gain for the desirable level The gain setting is
29. CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 7 Sa1npa20Jg Buruue d AEN Sd5 S 04V oipny uddx sjueumasu 36114 u105 NeN fila aouepioay paezey xipuaddy su jy unuuy s N e 4 Jeuonippy xepu Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features GARMI N View Charts from the Active Flight Plan Page 1 2 3 4 While viewing the Active Flight Plan Page press the FMS Knob to activate the cursor Turn the large FMS Knob to select the departure airport destination airport departure arrival or approach Select the SHW CHRT Softkey The appropriate chart will be displayed if available for the item selected Select the GO BACK Softkey to return to the previous page Change Day Night View 1 2 3 4 5 6 7 While viewing a chart press the MENU Key to display the Page Menu OPTIONS Turn the large FMS Knob to highlight the Chart Setup Menu Option and press
30. Database course for LOC2 LOC ID is CRS PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card Selected course for LOC2 differs from published localizer course by more than 10 degrees The SD card was removed from the top card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 2 REM Card 2 was removed Reinsert card The SD card was removed from the bottom card slot of the specified PFD or MFD The SD card needs to be reinserted PFD1 PFD2 or MFD1 CARD 1 ERR Card 1 is invalid The SD card in the top card slot of the specified PFD or MFD contains invalid data PFD1 PFD2 or MFD1 CARD 2 ERR Card 2 is invalid The SD card in the bottom card slot of the specified PFD or MFD contains invalid data 128 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Message Comments FPL TRUNC Flight plan has been truncated This occurs when a newly installed navigation database eliminates an obsolete approach or arrival used by a stored flight plan The obsolete procedure is removed from the flight plan Update flight plan with current arrival or approach HOLD EXPIRED Holding EFC time expired Expect Further Clearance EFC time has expired for the User defined Hold BARO MISMATCH Correct baro mismatch for VNAV
31. GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN optional nuu naesA pese ez rer LL aE nn n non Select the BACK Softkey to return to the top level softkeys p unmunununnunnuntu Select the BACK Softkey to return to the previous level softkeys Transponder Softkeys Level 1 Level 2 Level3 Description XPDR Displays transponder mode selection softkeys XPDRI Selects the 41 transponder as active XPDR2 Selects the 42 transponder as active STBY Selects Standby Mode transponder does not 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 VFR Automatically enters the VFR code 1200 in the U S A only CODE Displays transponder code selection softkeys 0 7 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 138 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 3311 Appendix Level 1 Level 2 Level 3 Description n TMR REF Displays Timer References Window a7 NRST Displays Nearest Airports Window ALERTS Displays Alerts Window oipny uddx U105 AEN optiona
32. P POS present position If necessary press the MENU Key and select Set WPT to Present Position to display P POS Press the ENT Key and the flashing cursor moves to the ending waypoint field Enter the identifier of the ending waypoint and press the ENT Key to accept the waypoint point to point planning Enter the identifier of the starting waypoint 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 Press the ENT Key to accept the waypoint For flight plan leg planning a b c d Select the FPL Softkey at the bottom of the display 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 Turn the small FMS Knob to select the desired leg of the flight plan or select CUM to apply trip planning calculations to the entire flight plan Selecting FPL 00 will display the active flight plan If an active flight plan is selected REM will be 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 5 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 R
33. Pop Up Alert Annunciation Terrain Terrain Pull Up Pull Up Reduced Required Terrain PULL UP 0 or Clearance Warning RTC Terrain Ahead Pull Up Terrain Ahead Pull Up Terrain Ahead Pull Up TERRAIN AHEAD PULL UP Terrain Ahead Pull Up xipuaddy r Imminent Terrain Impact PULL UP or or Warning ITI e Terain Teta PulUp 2 Pull Up s 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 103 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN FIBI MFD Map Page Alert Type TAWS Page prag Voice Message um Pop Up Alert Annunciation Obstacle Obstacle Pull Reduced Required Obstacle ME E Up Pull Up PULL UP or Clearance Warning ROC VISPTESETSSENETEETUS Obstacle Ahead Pull Up Obstacle Ahead Pull Up OBSTACLE AHEAD PULL UP Eee aay Up Imminent Obstacle Impact PULL UP Obstacle A Pull Up Warning 101 OBSTACLE PULL UP Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate PULL UP PULL UP Pull Up Warning EDR Caution Terrain Caution Terrain Reduced Required Terrain or Clearance Caution RTC Terrain Ahead Terrain Ahead Terrain Ahead Terrain Imminent Terrain Impact an Caution ITI Caution Terrain Caution Terrain Reduced Requir
34. Reference Guide for the Beechcraft 200 B200 Series 105 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts ADDITIONAL VOICE ALERTS A GARMIN Voice Alert Minimums Description The aircraft has descended below the preset minimum descent altitude or decision altitude Vertical track The aircraft is one minute from Top of Descent Issued only when vertical navigation is enabled Airspeed The aircraft is in an underspeed condition See the AFCS ection for more details n Engaging autopilot The ESP system is engaging the autopilot See the AFCS section for more details Traffic Played when a Traffic Advisory TA is issued with the TIS system the optional GTS 800 820 825 TAS system or the optional GTS 850 855 TCAS system See the Hazard Avoidance section for additional details on GTS 800 820 825 850 855 voice alerts TIS Not Available The aircraft is outside the Traffic Information Service TIS coverage area Traffic Traffic Traffic Played when a Traffic Advisory TA is issued with the optional SKY 497 SKY899 TAS system or the optional KTA 870 TAS system See the Skywatch PG or KTA 870 PG for additional details on voice alerts Played for each subsequent TA KTA 870 only gt Traffic Advisory System Tes
35. Select the TAWS A Page 2 Select the GS INH or GP INH Softkey to inhibit or enable GSD alerts softkey choice dependent on present GSD alert type Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Hazard Avoidance TAWS B WARNING The TAWS display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS operation is only available when the system is configured for a TAWS B installation NOTE The Terrain Awareness and Warning System TAWS may not operate reliably north of 89 North latitude and south of 89 South latitude This is due to limitations present within the Terrain database and the system s ability to process the data representing the affected areas GRS 7800 installations only Manual System Test 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS System 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS B Page When all is in working order TAWS System Test OK is heard Display Terrain and Obstacles on the TAWS B Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS B Page 3 f desired select the VIEW Softkey to a
36. Series 9 Additional Features saunpar0dd Buruue d AEN Sd5 24V oipny uddx sjueumnansu i4 JWI05 AeN Wila aouepioay puezey xipuaddy su jy unuuy s N e 4 Jeuonippy xopu Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 92 3 4 5 A GARMIN Turn the large FMS Knob to highlight the active profile field in the Pilot Profile Box Turn the small FMS Knob to display the pilot profile list and highlight the desired profile Press the ENT Key The system loads and displays the system settings for the selected profile Renaming a profile 1 Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the large FMS Knob to highlight RENAME in the Pilot Profile Box 4 Press the ENT Key 5 In the Rename Profile window turn the FMS Knob to select the profile to rename 6 Press the ENT Key 7 Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key 8 With RENAME highlighted press the ENT Key 9 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Deleting a profile 1 Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page 2 Press the FMS Knob momentarily to activate the flashing cursor 3 Turn the lar
37. Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS1 Mag Var Database STARTING UPLOAD 0 0 Uploading Database to GRS1 148 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 1 3313 Appendix 2 When the upload is complete the prompt for the next GRS upload is displayed as seen in the following figure sjueuinasu fila GRS2 MY DB Update Available Update from 2005 to 2010 oipny uddx UI05 AEN OK or CANCEL S2dV GRS2 Magnetic Field Variation Database Update Prompt 3 With OK highlighted press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure When the upload is complete the system is ready for use AEN Sd5 Duruue d iui Uploading GRS2 Mag Var Database STARTING UPLOAD 6 0 SeJnpa oJd aouepioay paezey Uploading Database to GRS2 saunyeay Jeuonippy su jy unuuy gt ko o a E xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 149 Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix 150 Blank Page Garmin G1000 C
38. With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic will now be displayed on the map Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Hazard avoidance TERRAIN AWARENESS amp WARNING SYSTEM TAWS A Optional WARNING The TAWS display shows supplemental information only It should not be used for navigation NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area NOTE TAWS operation is only available when the system is configured for a TAWS A installation NOTE The Terrain Awareness and Warning System TAWS may not operate reliably north of 89 North latitude and south of 89 South latitude This is due to limitations present within the Terrain database and the system s ability to process the data representing the affected areas GRS 7800 installations only 6 Manual System Test 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Test TAWS System 3 Press the ENT Key During the test TAWS TEST is displayed in the center of the TAWS A Page When all is in working order TAWS System Test OK is heard Displaying the TAWS A Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the TAWS A Page 3 If desired select the VIEW Softke
39. and 50 nose up and between 22 and 50 nose down The opposing force increases or decreases depending on the pitch angle and the direction of pitch travel This force is intended to encourage movement in the pitch axis in the direction of the normal pitch attitude range for the aircraft There are no indications marking the pitch ESP engage and disengage limits in these nose up nose down conditions Angle of Attack Protection If the Angle of Attack Protection feature is available in the current installation ESP force may be applied if the compatible lift computer determines a stall warning condition is imminent In this condition the Pitch Limit Indicator will be initially displayed 4 below this computed pitch attitude When pitch attitude equals that indicated by the Pitch Limit Indicator ESP will engage applying a force in the direction necessary to lower the nose of the aircraft High Airspeed Protection Exceeding Vmo or Mmo will result in ESP applying force to raise the nose of the aircraft When the high airspeed condition is remedied ESP force is no longer applied 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 95 saunpa20ld Buruue d AEN Sd5 24V oipny uddx syueumasu aouepioay xipuaddy su jy unuuy x pul fila Wo gt AeN fila paezey gt a 2 g o A Additional Features GARMIN Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Figh
40. and then high altitude airways Turn the FMS Knob to select the desired airway exit point from the list and press the ENT Key LOAD is highlighted Press the ENT Key The system returns to editing the flight plan with the new airway inserted Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning USER DEFINED HOLDING PATTERNS A holding pattern can be defined at any active flight plan waypoint or at the aircraft present position sjueuinisu 1i NOTE System navigation utilities may not reliably calculate range and bearing information when the aircraft is operating north of 80 North latitude or south of 80 South latitude This may result in the system displaying small gaps in racetrack holding pattern depictions GRS 7800 installations only oipny uddx U105 AEN S2dV Creating a user defined hold at an active flight plan waypoint 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the waypoint for the hold 3 Press the MENU Key highlight Hold At Wpt and press the ENT Key The HOLD AT window appears with the course field highlighted 4 Usethe FMS Knobs to edit the entry course and press the ENT Key 5 Use the small FMS Knob to select INBOUND or OUTBO
41. augment the lack of airspeed The system should be serviced AHRS2 TAS AHRS2 not receiving valid airspeed The 2 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced AHRS1 GPS AHRS1 using backup GPS source The 1 AHRS is using the backup GPS path Primary GPS path has failed The system should be serviced when possible AHRS2 GPS AHRS2 using backup GPS source The 2 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 AHRS2 GPS AHRS2 not receiving any GPS information The 2 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 AHRS2 GPS AHRS2 not receiving backup GPS information The 2 AHRS is not receiving backup GPS information The system should be serviced AHRS1 GPS AHRS1 operating exclusively in no GPS mode The 1 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS2 GPS AHRS2 o
42. cycle is required to restart synchronization when Card Full or Err is shown 144 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Index Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display being updated Card Full SD card does not contain sufficient memory Err Displayed for all other errors that may cause the synchronization process to be halted Timeout System timed out prior to the database transfer completing Loading Garmin Database Updates 1 With system power OFF remove the MFD database card from the bottom card slot of the MFD 2 Update the Garmin databases on the MFD card 3 Insert the MFD database card into the bottom card slot of the MFD 4 Apply power to the system check that the databases are initialized and displayed on the power up screen When updating the terrain and FliteCharts databases a Verifying message may be seen If this message is present wait for the system to finish loading before proceeding to step 5 5 Acknowledge the Power up Page agreement by pressing the ENT Key or the right most softkey 6 Turn the large FMS Knob to select the AUX Page group on the MFD 7 Turn the small FMS Knob to select the System Status Page 8 Monitor the Sync Status in the Database Window Wait for all databases to complete synching indicated by Compl
43. guidance Altimeter setting is not the same on PFD1 and PFD2 Synchronize settings for VNAV guidance TRN AUD FAIL Trn Awareness audio source unavailable The audio source for terrain awareness is offline Check GIA1 or GIA 2 TERRAIN AUD CFG Trn Awareness audio config error Service req d TERRAIN DISABLED Terrain Awareness DB resolution too low Terrain audio alerts are not configured properly The system should be serviced TAWS is disabled because a terrain database of sufficient resolution 9 arc second or better is not currently installed 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 129 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wija w09 eN Wij SoJnjeeo4 Jeuonippy Dun nsn xopul Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported Description A flight plan file stored on the SD card was successfully imported as a stored flight plan File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified The file stored
44. in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions A WARNING Do not use the indicated data link weather product age to determine the age of the weather information shown by the data link weather product Due to time delays inherent in gathering and processing weather data for data link transmission the weather information shown by the data link weather product may be significantly older than the indicated weather product age CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL A WARNING Do not rely on information from the lightning detection system display as the sole basis for hazardous weather avoidance Range limitations and interference may cause the system to display inaccurate or incomplete information Refer to the documentation from the lightning detection system manufacturer for detailed information about the system Displaying Stormscope Lightning Data on the Navigation Ma
45. kHz 3 Press the Frequency Transfer Key to place the frequency into the active frequency field INTERCOM Pressing the INTR COM Key on either Audio Panel selects and deselects the intercom on both Audio Panels The annunciator is lit when the intercom is active The intercom connects the pilot and copilot together Either the pilot or copilot may select or deselect the intercom The CABIN Key initiates two way communication between the pilot or copilot and the passengers in the cabin The annunciator is lit when the cabin intercom is active on either Audio Panel The MAN SQ Key allows either automatic or manual control of the intercom squelch setting Pressing the MAN SQ Key enables manual squelch control indicated by the MAN SQ annunciator During manual squelch operation pressing the ICS Knob switches between volume and squelch adjustment lighting the associated annunciator beneath the knob When the MAN SQ annunciator is lit the ICS Knob controls both volume and squelch When the MAN SQ annunciator is extinguished the ICS Knob controls only volume 6 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Makom APUR ANdio Panel PASSENGER ADDRESS PA SYSTEM A passenger address system is provided by pressing the PA Key to deliver messages to the passengers The message is heard by the other pilot on the headset only if the PA Key is enabled on both audio panels PA messa
46. least 20 miles 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 GRS 77 installations only 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 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A Warnings Cautions amp Notes Ss GARMIN WARNING Do not use GPS to navigate to any active waypoint identified as a NON WGS84 WPT by a system message NON WGS84 WPT waypoints are derived from an unknown map reference datum that may be incompatible with the map reference datum used by GPS known as WGS84 and may be positioned in error as displayed CAUTION The PFD and MFD displays use a lens coated with a special anti reflective coating that is very sensitive to skin oils waxes and abrasive cleaners CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cle
47. lightning information on the Navigation Map optional aouepioay puezey METAR Displays METAR flags on airport symbols shown on the Navigation Map optional LEGEND Displays the legend for the selected weather products Available only when NEXRAD XM LTNG and or METAR softkeys are selected BACK Returns to top level softkeys sainjea4 Jeuonippy su jy unuuy 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 gt kej o a Ej xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 143 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN Level l Level 2 Description SHW When available displays optional airport and CHRT terminal procedure charts CHKLIST When available displays optional checklists LOADING UPDATED DATABASES Database information is obtained from third party sources Inaccuracies in the data may be discovered from time to time Garmin communicates this information by issu ing a Database Alert These notifications are available on http fly garmin com Garmin requests the flight crew report any observed dis
48. occurred within a two kilometer region Neither cloud to cloud nor the exact location of the lightning strike is displayed If the aircraft is also equipped with an on board lightning detection system e g L 3 WX 500 Stormscope only one lightning product may be enabled for display at a time 54 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Hazard Avoidance Displaying Data Link Lightning information 1 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the Connext Weather Data Link Page 2 Select the DL LTNG Softkey To display the Data Link Lightning legend on the Weather Data Link CNXT Page select the LEGEND Softkey when Data Link Lightning is selected for display SIGMETs and AIRMETs The entire SIGMET or AIRMET is displayed as long as any portion of it is occurring within the coverage area of the Connext data request Displaying SIGMETs and AIRMETs 1 Select the Weather Data Link CNXT Page 2 Select the SIG AIR Softkey 3 To view the text of the SIGMET or AIRMET press the RANGE Knob and move the Map Pointer over the icon 4 Press the ENT key To display the SIGMET and AIRMET legend on the Weather Data Link CNXT Page select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display METARs and TAFs Bujuue d AEN SdD So4V olpny uddX sjuawingsu 106114 JW05 AeN 1ufi4 SeJnpa o0Jd gt l
49. on Inset Map optional Displays XM lightning information on Inset Map optional Displays Worldwide Weather lightning information on Inset Map optional Displays METAR flags on airport symbols shown on the Inset Map optional optional Bs co bve PDR IDENT MR REF LA Select the BACK Softkey to return to the top level softkeys Sensor Softkeys Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 313A 3 Appendix Level 1 Level2 Description i SENSOR Displays softkeys for selecting the 41 and 42 AHRS a7 and Air Data Computers ADCI Selects the 1 Air Data Computer SE ADC2 Selects the 2 Air Data Computer zE AHRSI Selects the 1 AHRS AHRS2 Selects the 2 AHRS gt a SENSOR PFD OBS CDI DME XPDR IDENT TMR REF D A D 3 m G nDO v Y n S E lt n n ra nA Select the BACK Softkey to return to the top level softkeys Buruue d 164 D D o N B d RG2 BRG2 BRG2 OFF 5 L 1 1 T 1 Jeeeejpeeeeyp qp E F3 V3 V3 V3 V3 F3 1m vns n nom eres res T e Teese 1 a pnmununmnnnnnnunnunnu L J1L 1E 1E oe Cee ee SeJnpa oJd aouepioay puezey a 0 z Eo ee E 3L 1E 1E pedes E ppnnnunnnunnnnnunnou P 3 nnnnnnnnnnnrn gt 2 PFD Configuration Softkeys gt 5 5 a E xopu 190 00929 04 Rev A Garmin G1
50. on the SD card did not contain a flight plan only user waypoints These waypoints have been saved to the system user waypoints No flight plans stored in the system have been modified No flight plan files found to import 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 mported A partial stored flight plan now exists in the system File contained user waypoints only Too many points Flight plan truncated The file stored on the SD card did not contain a flight plan only user waypoints One or more of these waypoints did not import successfully 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 locked The flight plan on the SD card contains one or more waypoints that the system cannot find in the navigation database The flight plan has been imported but must be edited within the system before it can be activated for use User waypoint database full Not all loaded The flight plan file on the SD card contains user waypoints The quantity of stored user waypoints has exceeded system
51. optional or T optional optional Select the BACK Softkey on this level to return to the top softkey level optional optional TRAFFIC PROFILE TOPO TERRAIN x o nema F amp F V3 F3 V3 wa MFD Softkeys Level l Level 2 Description MAP Enables second level Navigation Map softkeys TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map 142 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 3331 Appendix Level l Level 2 Description sjueuimasu 1i TERRAIN Displays terrain information on Navigation Map AIRWAYS Displays airways on the map cycles through the following AIRWAYS No airways are displayed AIRWY ON All airways are displayed AIRWY LO Only low altitude airways are displayed AIRWY HI Only high altitude airways are displayed oipny uadx U105 AEN S2dV STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD Displays NEXRAD weather and coverage information on the Navigation Map optional AEN Sd5 or Buruue d 16114 PRECIP Displays Connext precipitation on the Navigation Map optional XMLING Displays XM lightning information on the Navigation Map optional SeJnpa oJd or DLLING Displays Connext
52. 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 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 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 5 Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel Sye y unuuy SoJnjeeo4j e uepioAy SoJnpa o0Jd Buruue d ACN Sd5 S241V oipny uadx sjueuinagsu Jeuonippy pjezen fila JUI05 NEN Wila x pu ddy x pul Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Nav Com XPDR Audio Panel GARMIN SELECTING A NAV RADIO 1 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VORT LOC1 NAV1 or VOR2 LOC2 NAV2 2 Press the NAV1 NAV2 DME or ADF Key on the audio panel to select or deselect the navigation radio audio source All radio keys can be selected individually or together NAV COM TUNING 1 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned 2 Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters
53. speed or both can cause similarly abrupt substantial changes in vertical path guidance Because of turn smoothing changes to both distance to the BOD and ground speed tend to be more extreme when the BOD is also a waypoint that marks a large course change These speed and distance changes will be accounted for in the computed required vertical path and reflected in the vertical guidance indications 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN GPS Navigation gt Light Blue 2 White Text Light Blue Text Subdued Text ji Large Text Altitude calculated by Altitude has been entered The system the system estimating by the pilot Altitude is cannot use SE the altitude of the designated for use in this altitude in HH aircraft as it passes giving vertical flight path determining 2 over the navigation guidance Altitude does vertical flight point This altitude not match the published path guidance z is provided as a altitude in navigation i reference and is not database or no published designated to be used altitude exists in determining vertical flight path guidance Small Text Altitude is not Altitude is designated for The system designated to be used use in giving vertical flight cannot use in determining vertical path guidance Altitude this altitude in z a EI 5 gt e flight path guidance has been retrieved
54. the selected approach procedure Press the ENT Key If BARO or OFF was selected step 8 proceed to step 11 If TEMP COMP was selected in step 8 the cursor moves to the TEMP AT field Turn the small FMS Knob to enter the temperature at the destination airport The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value Press the ENT Key LOAD or ACTIVATE is now displayed with LOAD highlighted 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 13 Press the ENT Key ACTIVATE AN APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE APPROACH 3 Press the ENT Key ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 2 3 4 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 37 Press the PROC Key Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL Press the ENT Key The final approach course becomes the active leg AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruue d 16114 So1Jnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Proce
55. the window 4 Toremove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Bujuueld AEN Sd5 34614 SoJnpa o0Jd gt lt E a D El A puezey Connext Weather Data Requests The Connext Data Request window provides the flight crew with the options to define the requested weather coverage area s choose automatic weather update intervals if desired and the ability to send or cancel weather data requests The window also displays the status of the Connext data request process sainjea4 jeuonippy Requesting Connext Weather Data Manually 1 Select the Weather Data Link CNXT Page 2 Press the MENU Key 3 With Connext Data Request highlighted press the ENT Key 4 Turn the large FMS Knob to highlight the desired coverage option s and press the ENT Key to check or uncheck one of more of the following coverage selections su jy unuuy x pu ddy x pul 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 49 Flight Instruments Nav Com XPDR Audio Flight Planning AFCS GPS Nav Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N e PRESENT POSITION Requests data based on current location DESTINATION Requests data based on active flight plan destination if the flight plan contains no destination dashes are displayed e
56. visible in the gain field as a movable horizontal bar in a flashing box The line pointer is a reference depicting the calibrated position 3 Press the FMS Knob to remove the cursor 4 Select the GAIN Softkey again to recalibrate the gain CALIBRATED will be displayed in the GAIN field 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 59 AEN SdD S24V oipny uddx sjueumasuj u105 NeN fila Buruue d 16114 ERIT Sa1npa oJd puezey sainjea4 euolippy syajy unuuy xipuaddy xopu Hazard Avoidance GARMI N amp Ground Mapping 2i 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode EE 3 Select the BACK Softkey Sector Scan 4 1 While in the Horizontal Scan Mode move the Joystick right or left to place lt the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan gt 2 Press the FMS Knob to display the cursor E 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turn the small FMS Knob to select a scan angle 2 95 Ifdesired readjust the Bearing Line with the Joystick to change the center ze of the Sector Scan 6 Press the FMS Knob to remove the cursor Antenna Stabilization E 1 To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select
57. 0 B200 Series 190 00929 04 Rev A A GARMIN Text Messaging SMS Additional Features Messages may be sent to an email address or text message capable cellular telephone Message length is limited to 160 characters including the email address The text messaging user interface is mainly through the AUX TEXT MESSAGING Page Viewing the Text Messaging Page 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX TELEPHONE or AUX TEXT MESSAGING Page 3 f necessary select the SMS Softkey to display the AUX TEXT MESSAGING Page Message Symbol Description Received text message that has not been opened Received text message that has been opened Saved text message draft not sent System is sending text message Text message has been sent System failed to send text message Predefined text message 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 79 saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu 16114 Jwiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 80 A GARMIN Viewing a Text Message When Received When viewing MFD pages other than the AUX TE
58. 0 Series A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Message Comments G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair 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 UNABLE RNP Estimated position error exceeds RNP The estimated GPS position error exceeds the RNP limits Check GPS sensors UNABLE RNP APR GPS integerity lost Check GPS sensors The estimated GPS position error exceeds the requirements for the current approach Check GPS Sensor APR ADVISORY SBAS VNAV not available Using Baro VNAV SBAS VNAV not available Check GPS sensor GSD 41 MESSAGE ADVISORIES OPTIONAL Message Comments GSD1 CONFIG GSD1 config error Config service req d GSD1 COOLING GSD1 temperature too low GSD1 and the CDU have different copies of the GSD1 configuration GSD1 is reporting a low temperature condition GSD1 SERVICE GSD1 needs service Return unit for repair GSD1 is reporting an internal error condition The GSD may still be usable GSD1 MANIFEST GSD1 software mismatch Communication halted GSD1 has incorrect sof
59. 000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 135 Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix A GARMIN Level 1 Level 2 Level 3 Description PFD SYN VIS PATHWAY SYN TERR HRZN HDG APTSIGNS DFLTS WIND OPTN 1 OPTN 2 OPTN 3 OFF DME BRGI HSI FRMT Displays second level softkeys for additional PFD configurations Displays the softkeys for enabling or disabling Synthetic Vision features Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan Enables synthetic terrain depiction Displays compass heading along the Zero Pitch line Displays position markers for airports within approximately 15 nm of the current aircraft position Airport identifiers are displayed when the airport is within approximately 9 nm Resets PFD to default settings including changing units to standard Displays softkeys to select wind data parameters Wind direction arrow and speed Wind direction arrow with digital direction and speed Longitudinal and lateral components Information not displayed Displays the DME Information Window Cycles the Bearing 1 Information Window through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency Displays the HSI formatting softkeys 136 Garmin G1000 Cockpit Re
60. 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the TA ONLY or TA RA Softkey to begin displaying traffic TA RA or TA ONLY respectively is displayed in the TCAS Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode TFC STBY will be displayed in the TCAS Mode field 5 Select the ABS absolute or REL relative Softkey to display intruder altitude as an absolute altitude or an altitude relative to own aircraft altitude 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Changing the Altitude Range 1 On the Traffic Page select the ALT RNG Softkey 2 Select one of the following Softkeys ABOVE Displays non threat and proximity traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight NORMAL Displays non threat and proximity traffic from 2700 feet above the aircraft to 2700 feet below the aircraft Typically used during enroute phase of flight BELOW Displays non threat and proximity traffic from 2700 feet above the aircraft to 9900 feet below the aircraft Typically used during descent phase of flight UNREST unrestricted All traffic is displayed 3 To return to the Traffic Page select the BACK Softkey Displaying Traffic on the Navigation Map 1 Ensure TCAS Il system is operating
61. 3 Select the AUX SYSTEM STATUS Page on the MFD Select the RA TEST Softkey RA TEST is displayed to the left of the Radar Altitude window The Radar Altitude window displays 50 feet indicating a properly functioning system Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test DISPLAYING WIND DATA 1 2 3 4 Press the PFD Softkey Press the WIND Softkey to display wind data below the Selected Heading Press one of the OPTN softkeys to change how wind data is displayed To remove the Wind Data Window press the OFF Softkey Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN __Basitomi pede Panel NAV COM TRANSPONDER AUDIO PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING 1 2 3 4 Press the DME Softkey Turn the large FMS to select the DME source field Turn the small FMS Knob to select the desired Nav radio Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 2 3 4 Press the XPDR Softkey to display the transponder mode selection softkeys Press the XPDR1 or XPDR2 Softkey to select the active transponder Press the CODE Softkey to display the transponder code selection softkeys for digit entry Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds
62. 8282 P Garmin AT Inc mem s 2345 Turner Road SE m Salem OR 97302 U S A p 503 391 3411 f 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton 5040 OLR U K p 44 0 87 0850 1243 f 44 0 23 8052 4004 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2011 2013 Garmin Ltd or its subsidiaries 190 00929 04 Rev A
63. ARMIN Turn the large FMS Knob to highlight the flight plan to be deleted Select the DELETE Softkey A Delete flight plan confirmation window is displayed With OK highlighted press the ENT Key to delete the flight plan To cancel turn the large FMS Knob to highlight CANCEL and press the ENT Key GRAPHICAL FLIGHT PLAN CREATION 1 2 3 4 5 Press the FPL Key on the Control Unit to display the Active Flight Plan Page Press the Joystick to activate the map pointer Use the Joystick to move the pointer to the desired point on the map to be inserted as a waypoint in the flight plan The default insertion point is at the end of the flight plan If the selected waypoint is to be placed anywhere other than the end of the flight plan press the FMS Knob to activate the cursor Waypoints are inserted ABOVE the cursor Turn the large FMS Knob to select the desired insertion point Select the LD WPT Softkey The selected waypoint will be inserted at the selected point The default user waypoint naming is USROO0 USROO1 USROO2 and so on To change the user waypoint name follow the procedure for modifying a user waypoint EXPORT A FLIGHT PLAN TO AN SD CARD 34 1 2 3 4 5 6 7 Insert the SD card into the top card slot on the MFD Press the FPL Key on the Control Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS K
64. ARMIN 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 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 LAT LON latitude and longitude Press the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 22 1 2 3 4 5 6 7 8 9 10 Turn the large FMS Knob on the Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key The cursor is now in the WAYPOINT TYPE field If desired the waypoint can be made temporary deleted automatically when the system is turned off If the waypoint is to remain in the system proceed to step 7 a Turn the large FMS Knob one click to the left to highlight TEMPORARY b Press the ENT Key to place a check mark in the box Turn the large FMS Knob to place the cursor back in the WAYPOINT TYPE field 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 curs
65. Annun Alerts Features Index Additional Features 78 A GARMIN Transferring a Call from the Cockpit From the cockpit phone a external call can be transferred to the cabin phone or a call with the cabin phone can be transferred to an external phone or when two Iridium Transceivers are installed an external call can be transferred to another external phone 1 2 3 4 5 Select the TRANS Softkey on the MFD Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Transfer Current Call Press the ENT Key Press the ENT Key The cursor now highlights the phone number entry field Enter the phone number as discussed earlier for making an external call on the Iridium satellite network Press the ENT Key OK is now highlighted Press the ENT Key again to place the call Making a Conference Call from the Cockpit 1 2 3 4 5 Select the CONF Softkey on the MFD Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Conference Current Call c Press the ENT Key Press the ENT Key The cursor now highlights the phone number entry field Enter the phone number as discussed earlier for making an external call on the Iridium satellite network Press the ENT Key OK is now highlighted Press the ENT Key again to place the call Garmin G1000 Cockpit Reference Guide for the Beechcraft 20
66. Beechcraft 200 B200 Series 99 Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN TAWS A ALERTS PFD MFD MFD Map P 3 Alert Type TAWS Page Po Mar Voice Message Annunciation BP Terrain Terrain Pull Up Reduced Required Terrain DT it Pull Up PULL UP or Clearance Warning RTC ISCETZSESTTEETJE Terrain Ahead Pull Up Terrain Ahead Pull Up TERRAIN AHEAD PULL UP Ten Up Imminent Terrain Impact PULL UP Terrain mean Pull Up Warning TI TERRAIN PULL UP Terrain Terrain Pull Up Pull Up Obstacle Obstacle Pull OBSTACLE PULL UP Up Pull Up Reduced Required Obstacle PULL UP i Clearance Warning ROC OBSTACLE AHEAD PULL UP or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact OBSTACLE AHEAD PULL UP Obstacle Ahead Pull Up Obstacle Ahead Pull Up PULL UP or Warning 101 OBSTACLE PULL UP Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate B whoop whoop Warning EDR PULL UP PE Pull Up Excessive Closure Rate E whoop whoop Warning ECR PULL UP E Pull Up Reduced Required Terrain Clearance Caution RTC Caution Terrain Caution Terrain or Terrain Ahead Terrain head Imminent Terrain Impact Caution ITI Reduced Required Obstacle Clearance Caution ROC
67. DO eg mu o su jy unuuy sainjea4 aouepioay Sa1npa oJd Buruue d AEN Sd5 jeuonippy puezey ifi xipuaddy xopu A ARS GARMIN SUSPECTED AUTOPILOT MALFUNCTION Flight Instruments NOTE Consult the aircraft documentation for the location of circuit breakers as well as specifics that may supplement or amplify this procedure Nav Com XPDR Audio If an autopilot failure or trim failure is suspected to have occurred perform the following steps 1 Firmly grasp the control wheel 2 Press and hold the AP DISC Switch The autopilot will disconnect and power is removed from the trim motor Power is also removed from all primary servo motors and engaged solenoids Note the visual and aural alerting indicating autopilot disconnect AFCS GPS Nav 3 Retrim the aircraft as needed Substantial trim adjustment may be needed 4 Pull the appropriate circuit breaker s to electrically isolate the servo and solenoid components 5 Release the AP DISC Switch Fight Planning OVERPOWERING AUTOPILOT SERVOS Procedures In the context of this discussion overpowering refers to any pressure or force applied to the pitch controls when the autopilot is engaged A small amount of pressure or force on the pitch controls can cause the autopilot automatic trim to run to an out of trim condition Therefore any application of pressure or force to the controls should be avoided when the autopilot is engaged Overpowering the a
68. FAULT AHRS2 magnetometer fault has occurred A fault has occurred in the 2 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced MANIFEST GMU1 software mismatch communication halted MANIFEST GMU2 software mismatch communication halted The GMU 44 has incorrect software installed The system should be serviced GDL 59 MESSAGE ADVISORIES Message Comments GDL59 CONFIG GDL 59 config error Config service req d GDL 59 configuration settings do not match those of backup configuration memory The system should be serviced GDL59 FAIL GDL 59 has failed A failure has been detected in the GDL 59 The receiver is unavailable The system should be serviced GDL59 SERVICE GDL 59 needs service Return unit for repair A failure has been detected in the GDL 59 The system should be serviced GDL59 RTR FAIL The GDL 59 router has failed A failure has been detected in the GDL 59 router The system should be serviced REGISTER CONNEXT Data services are inoperative register w Connext The GDL 59 is not registered with Connext or it s current registration data has failed authentication MANIFEST GDL software mismatch communication halted The GDL 59 has incorrect software installed The system should be serviced 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guid
69. FD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database After the update completes the display starts in normal mode Turn the system OFF and remove the SD card from the top card slot Repeat steps 1 through 6 for the other displays PFD1 PFD2 or MFD Apply power to the system and press the ENT Key to acknowledge the startup screen Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show active navigation database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct active navigation database cycle information is shown for each display Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Appendix Loading the Jeppesen Navigation Database as the Standby Navigation Database NOTE After the navigation database is loaded or copied the top SD card may be removed 1 With the system OFF insert the SD card containing the new navigation database version into the top card slot of the MFD 2 Verify that an SD card is inserted in the bottom slot of each PFD and the MFD 3
70. FPL Requests data based on active flight plan Turn the small FMS Knob to select the desired flight plan look ahead distance option or choose REMAINING FPL to request the remainder of the flight plan WAYPOINT Requests data based on any valid waypoint 5 Turn the large FMS Knob highlight to the DIAMETER RTE WIDTH distance field and turn the small FMS Knob to select the desired diameter and route width of the request then press the ENT Key 6 Turn the large FMS Knob until the SEND REQ button is highlighted Press the ENT Key to initiate the request immediately or press the FMS Knob to return to the Connext Data Link Page without requesting data During a Connext Data Request the REQUEST STATUS window initially displays Contacting Connext Once a connection is established the REQUEST STATUS window displays Receiving Wx Data Time Remaining with an estimated data transfer time either in minutes or seconds If desired the Connext Data Request window may be closed while the data request is processing by pressing the FMS Knob the data request will continue to process in the background Connext Data Requests typically take between 1 to 4 minutes to complete depending on the size of the selected weather coverage area s the amount of weather activity present such as precipitation and the Iridium signal strength The system retrieves all available Garmin Connext weather products within the selected coverag
71. G1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN Copy This m ight 2011 2013 Garmin Ltd or its subsidiaries All rights reserved nual reflects the operation of System Software version 0985 07 or later for the fed Beechcraft 200 and B200 Some differences in operation may be observed when comparing the in Garmi Tel 9 Garmi Tel 5 formation in this manual to earlier or later software versions n nternational Inc 1200 East 151st Street Olathe Kansas 66062 U S A 13 397 8200 Fax 913 397 8282 n AT Inc 2345 Turner Road SE Salem OR 97302 U S A 03 391 3411 Fax 503 364 2138 Garmi n Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton S040 9RB U K Tel 4 Garm Tel 8 STI Web Site Address www garmin com 4 0870 8501241 Fax 44 0870 8501251 n Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan 86 02 2642 9199 Fax 886 02 2642 9099 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 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
72. LIDEPATH Glide Path Altitude Voice Callout Five Hundred VCO Four Hundred None None Three Hundred all are configurable except Two Hundred g p Five Hundred One Hundred 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 10 aouepioay SaJnpa oJd Buruue d AEN Sd5 24V oipny udax sjueumansu puezey 16114 swiop AeNn Wila sainjea4 Jeuonippy gt 5 o 3 2 x xopu Additional Hazard Fight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts A GARMIN TAWS A System Status Annunciations PFD MFD ER Additional TAWS A Page Voice Alert Type TAWS A Page s m Annunciation Message Annunciation TaWS System Fail TAHSTAIU EA o System Test in progress TAWS TEST None TAWS System System Test pass None None Test OK MFD Terrain or Obstacle database unavailable or invalid TAWS operating None None with PFD Terrain or Obstacle databases GPWS System Fail Radar Altimeter invalid None GPWS System Altitude or Vertical Failure Speed unavailable TAWS Not Available No GPS position A excessively degraded A GPS signal Available when sufficient GPS signal is received TAWS Not Available TAWS Out of database gia coverage area LTAMS N A Nong siae when aircraft enters database coverage area
73. MIN Flight Instruments Nav Com zm Ei zi E 4 a a x lt GPS Nav AFCS Flight Planning Blank Page Additional Hazard Appendix Annun Alerts Features Avoidance Procedures Index 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMI N AES AUTOMATIC FLIGHT CONTROL SYSTEM A NOTE If sensor information other than attitude required for a flight director mode becomes invalid or unavailable the flight director automatically reverts to the default mode for that axis sjueuinijsu 1i SE Z2 22 pa eg ER o A NOTE If the attitude information required for the default flight director modes becomes invalid or unavailable the autopilot automatically disengages FLIGHT DIRECTOR ACTIVATION An initial press of a key listed in the following table when the flight director is not e active activates the pilot side flight director in the listed modes Z Modes Selected Control Pressed z Lateral Vertical E FD Key Roll Hold default ROL Pitch Hold default PT 22 AP Key Roll Hold default ROL Pitch Hold default PIT CWS Button Roll Hold default ROL Pitch Hold default PIT 8 G Switch Takeoff on ground TO Takeoff on ground TO A Go Around in air GA Go Around in air GA ALT Key Roll Hold default ROL Altitude Hold AT 2 VS Key Roll Hold default ROL Vertical Speed VS H VNV Key Roll Ho
74. NFIG PFD1 config error Config service req d PFD2 CONFIG PFD2 config error Config service req d 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 PFD1SOFTWARE PFD1 mismatch communication halted PFD2 SOFTWARE PFD2 mismatch communication halted MFD1 SOFTWARE MFD1 mismatch communication halted The specified GDU has different software versions installed The system should be serviced PFD1 COOLING PFD1 has poor cooling Reducing power usage PFD2 COOLING PFD2 has poor cooling Reducing power usage MFD1 COOLING MFD1 has poor cooling Reducing power usage The PFD and or MFD is overheating and is reducing power consumption by dimming the display If problem persists the system should be serviced PFD1 KEYSTK PFD1 key name Key is stuck PFD2 KEYSTK PFD2 key name Key is stuck MFD1 KEYSTK MFD key name Key is stuck A key is stuck on the PFD and or MFD bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists 108 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations
75. NOTE Separate accounts must be established to access the Iridium satellite network for voice SMS and low speed data transmission and high speed data transmission for the maintenance reports Operation of these features in the cockpit is accomplished through the AUX TELEPHONE AUX TEXT MESSAGING and AUX WI FI SETUP Pages For operation using the cabin handset consult the instructions provided with the handset Registering with Garmin Flight Data Services A subscriber account must be established prior to receiving Connext Weather products Contact Garmin Flight Data Services at https fly garmin com fly garmin support applications satelliteservices or by calling 1 866 739 5687 in the United States or 011 913 440 1135 The following information is required to register for Connext Weather services G1000 System ID GSR56 GSR1 Serial Number s Tail Number Serial Airframe Number Country of Registration Aircraft Manufacturer and Aircraft Model 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX SYSTEM STATUS Note the System ID and GSR1 Serial Number in the AIRFRAME field Activating Connext Weather Registration After a subscriber account has been established the system must be activated for data link features such as reporting services or Connext Weather Activation is accomplished by entering the required access code This process is only performed when initially set
76. OR AIRWAY FROM A FLIGHT PLAN 1 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 31 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 2 3 4 A GARMIN Turn the large FMS Knob to highlight the title for the approach departure arrival or airway to be deleted Titles appear in white directly above the procedure s waypoints Press the CLR Key to display a confirmation window With OK highlighted press the ENT Key to remove the selected procedure or airway STORE A FLIGHT PLAN 1 2 3 After creating a flight plan on either the PFD or MFD it may be saved by pressing the MENU Key Turn the large FMS Knob to highlight Store Flight Plan and press the ENT Key With OK highlighted press the ENT Key to store the flight plan EDIT A STORED FLIGHT PLAN 1 2 3 4 5 6 1 Press the FPL Key on the Control Unit and turn t
77. Optional 63 Terrain Awareness amp Warning System sssssssssseen 65 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN able of Contents ADDITIONAL FEATURES tenen 69 Synthetic VISIOTL esee eR ede eo ei e ER ED e ER E ed 69 Terminal Procedure Charts sssssssseennen 70 Airport Directory Satellite Telephone and Data Link Services ssssse WI FI Connections nennen SiriusXM Radio Entertainment Pilot Profiles Electronic Stability amp Protection ESPTV sssssss ANNUNCIATIONS amp ALERTS 97 WARNING Annunciation ss Advisory Annunciations sssssssee Message Advisory Alerts Comparator Annunciations ssssssseee nnn Reversionary Sensor Annunciations ECS Alertes oo eros eee auae nu TAWS A Alerts josie a noto ineo beh be e Bot adbuc dida TAWS B Alerts Additional Voice Alerts MFD amp PFD Message Advisories ssssssss Database Message Advisories GMA 1347D Message Advisories ssssssssse GIA 63W Message Advisories sse GSD 41 Message Advisories Optional GEA 71 Message Advisories GTX 33 33D 33ES 3000 Message Advisories GRS 77 7800 Message Advisories sssssss GMU 44 Mes
78. PROC Key 2 Turn the large FMS Knob to highlight SELECT ARRIVAL 3 Press the ENT Key The cursor is displayed in the ARRIVAL field with a list of available arrivals 4 Turn the large FMS Knob to highlight the desired arrival 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Procedures 35 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 16114 SoeiINpsd01d su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures GARMI N 5 6 1 8 9 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 is displayed for the selected arrival Turn the large FMS Knob to highlight the desired runway Press the ENT Key 10 With LOAD highlighted press the ENT Key 11 The arrival will become part of the active flight plan ACTIVATE AN ARRIVAL LEG 1 2 3 4 5 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the arrival Select the ACT LEG Softkey A confirmation window showing the selected leg is displayed With
79. Press the ENT Key 6 Continue repeating these steps until all desired weights have been entered S2dV AEN Sd5 zu gt EI E ti Entering Fuel Parameters SoJnpa oJd 1 Press the FMS Knob to activate the cursor 2 Turn the large FMS Knob to place the cursor in the FUEL ON BOARD field 3 Turn the small FMS Knob to enter the desired fuel quantity 4 Press the ENT Key The cursor is now in the FUEL RESERVES field 5 Turn the small FMS Knob to enter the desired reserve fuel quantity 6 Press the FMS Knob to remove the cursor 7 Press the ENT Key TRIP PLANNING SoJnjeo4j e uepioAy paezey Jeuonippy syajy unuuy 1 Turn the large FMS Knob on the Control Unit to select the AUX page group 2 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 select the AUTO or MANUAL Softkey xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 19 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 20 4 For a b c d Or For a b c d Or A GARMIN Direct to planning Select the WPTS Softkey and verify that the starting waypoint field indicates
80. 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 seinpa2o0Jd buruue d 1614 aouepioay puezey SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight BARO in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF soinjes Jeuonippy su jy unuuy SYNCHRONIZE CDI 1 Select the AUX SYSTEM SETUP Page on the MFD 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight CDI in SYNCHRONIZATION Window 4 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 1 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index dh Flight Instruments GARMIN SELECTING DG MODE GRS 7800 INSTALLATIONS ONLY 1 2 3 NOTE When operating the G1000 in DG Free Mode GRS 7800 installations only the heading information used by som
81. Profile to export Only the active Pilot Profile can be exported 4 Press the EXPORT softkey 5 With EXPORT highlighted press the ENT Key 6 Pilot profile export succeeded is shown in the export results box Press the ENT Key to exit the Pilot Profile Exporting Box 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 93 saunpar0ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu 16114 Jwop AeNn Wila aouepioay puezey xipuaddy su jy unuuy sainjea Jeuonippy xopu Fight Nav Com Flight Planning GPS Nav AFCS XPDR Audio Instruments Procedures Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN ELECTRONIC STABILITY amp PROTECTION ESP ESP engages when the aircraft exceeds one or more conditions pitch roll Vmo Mmo and or angle of attack beyond the normal flight parameters Enhanced stability for each condition is provided by applying a force to the appropriate control surface to return the aircraft to the desired flight envelope This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep attitude high airspeed or when a stall is imminent As the aircraft deviates further from the desired attitude angle of attack or airspeed continues to increase the force increases up to an established maximum to encourage control movement in the direction neces
82. T GRS2 software mismatch communication halted The 2 AHRS has incorrect software installed The system should be serviced AHRS1 SERVICE AHRS1 needs service Return unit for repair A failure has been detected in the 1 AHRS The system should be serviced AHRS2 SERVICE AHRS2 needs service Return unit for repair AHRS1 CONFIG AHRS1 config error Config service req d A failure has been detected in the 2 AHRS The system should be serviced AHRS configuration settings do not match those of backup configuration memory The system should be serviced AHRS2 CONFIG AHRS2 config error Config service req d AHRS configuration settings do not match those of backup configuration memory The system should be serviced AHRS1 CAL AHRS1 calibration version error Srvc req d The 1 AHRS calibration version error The system should be serviced AHRS2 CAL AHRS2 calibration version error Srvc req d The 2 AHRS calibration version error The system should be serviced 120 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN GMU 44 MESSAGE ADVISORIES Annunciations amp Alerts Message HDG FAULT AHRS1 magnetometer fault has occurred Comments A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG
83. Turn the system ON A prompt is displayed 4 Press the YES Softkey The navigation database is copied to the SD card in the bottom card slot of the MFD 5 After the navigation database files are copied to the bottom SD card press any key to continue as instructed 7 Again press any key to continue as instructed on the display AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN fila Buruuejd 1614 8 Press the NO Softkey The display now starts in normal mode Since the database effective date is not yet valid it should not be loaded as the active database The display now starts in normal mode Do not remove power while the display is starting 9 Press the ENT Key to acknowledge the startup screen 10 Turn the large FMS Knob to select the AUX Page group on the MFD 11 Turn the small FMS Knob to select the System Status Page 12 The new database is copied to the SD card in the bottom card slot of each PFD Progress can be monitored in the SYNC STATUS field When copying is finished Complete is displayed A NOTE During the synchronization process version differences between standby navigation databases will exist This will result in the system displaying a DB Mismatch alert for the standby navigation databases This alert will remain until the next power cycle xipuaddy su jy unuuy 13 14 15 Turn system power OFF Remove the SD card from the top card slot of the MFD Turn system power ON
84. UND course direction and press the ENT Key 6 Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key 7 Use the FMS Knobs to edit the length and press the ENT Key 8 Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key 9 Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while LOAD is highlighted to add the hold into the flight plan AEN Sd5 zn D EI E ti aouepioay saunpa20ld puezey soinjes Jeuonippy 10 su jy unuuy Creating a user defined hold at the aircraft present position xipuaddy 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the MENU Key highlight Hold At Present Position and press the ENT Key The HOLD AT window appears with the Length mode highlighted xapu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 29 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index 3 4 5 6 1 Flight Planning GARMI N Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key Use the FMS Knobs to edit the length and press the ENT Key Use t
85. VT 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 SVT information is shown on the primary flight display PFD In addition to SVT enhancement to the PFD the following features have been added to the PFD e Pathways e Flight Path Marker e Horizon Heading Marks e Terrain and Obstacle Alerting e Three dimensional Traffic e Airport Signs e Runway Display Displaying SVT 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 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 69 saunpa20ld Buruue d AEN Sd5 24V oipny udax sjueumnansu 16114 jwiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy s N e 4 Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN Displaying Pathways 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the PATHWAY 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 S
86. XT MESSAGING Page a pop up alert will be displayed when a new text message is received Select the VIEW Softkey to view the message Selecting the IGNORE Softkey will extinguish the pop up window and leave the text message unopened Selecting the IGNR ALL Softkey will extinguish the pop window and ignore all future incoming text messages Selecting the SMS Softkey will display the AUX TEXT MESSAGING Page The pop up alerts may be enabled or disabled through the Page Menu Enable Disable Incoming Text Message Pop Up Alerts 1 2 3 With the AUX TEXT MESSAGING Page displayed press the MENU Key on the MFD to display the Page Menu Turn either FMS Knob to place the cursor on Disable New Message Popups or Enable New Message Popups Press the ENT Key The pop up alert will not be displayed when an incoming text message is received Reply to a Text Message While viewing the text message select the REPLY Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Reply To Message c Press the ENT Key Sending a Text Message 1 While viewing the AUX TEXT MESSAGING Page select the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Draft New Message c Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Featu
87. Y ON ALT TA ONLY TA RA BACK REL Displays transponder mode selection softkeys Selects transponder Standby Mode transponder does not reply to any interrogations When the transponder is set to standby the TCAS II system is also set to standby Activates transponder transponder replies to identification interrogations When the transponder is set to ON the TCAS II system is set to standby Altitude Reporting Mode transponder replies to identification and altitude interrogations When the transponder is set to ALT the TCAS II system is set to standby Activates the TCAS II system in TA Only Mode and set the transponder to ALT Activates the TCAS II system in TA RA Mode and sets the transponder to ALT Returns to the previous softkey level Displays the TCAS control softkeys Displays intruder altitude as altitude relative to own aircraft altitude 140 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 1 33 Appendix Level 1 Level 2 Level3 Level 4 Description E ABS Displays intruder MSL altitude a 5 ALT RNG Displays the altitude display range softkeys oipny uddx U105 AEN ABOVE Displays non threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight NORMAL Displays non threat traffic from 2700 feet above the aircraft to 2700 feet below th
88. 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 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 DIS radial distance 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 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 Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the NRST airports to the aircraft s current position c Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list E is displayed S b Turn the small FMS Knob to the right to display the RECENT T waypoints ES Ja Turn the large FMS Knob to select the desi
89. abase optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists MFD1 DB ERR MFD1 Airport Directory database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced The MFD detected a failure in the Airport Directory database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced DB MISMATCH Navigation database mismatch Xtalk is off The PFDs and MFD have different navigation database versions or regions installed Crossfill is off Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 111 eouepioAy seinpa2oJd Buruue d AEN Sd5 241V oipny uddx SyueuinJjsu paezey Wij U105 AEN fij sainjea4 Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MON Index Annunciat
90. altitude at the Final Approach Fix Inhibit TAWS 1 2 3 While the TAWS B Page is displayed select the INHIBIT Softkey Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key Enable TAWS 1 2 3 While the TAWS B Page is displayed select the INHIBIT Softkey 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 Displaying Terrain and Obstacles on the Navigation Map 1 2 With the Navigation Map displayed select the MAP Softkey Select the TERRAIN Softkey Terrain and obstacles will now be displayed on the map Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WARNING Use appropriate primary systems for navigation and for terrain obstacle and traffic avoidance SVT 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 SVT 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 Technology SVT functionality is offered as an optional enhancement to the G1000 system S
91. amp Alerts Message Comments CNFG MODULE PFD1 configuration module is inoperative The PFD1 configuration module backup memory has failed The system should be serviced PFD1 VOLTAGE PFD1 has low voltage Reducing power usage The PFD1 voltage is low The system should be serviced PFD2 VOLTAGE PFD2 has low voltage Reducing power usage The PFD2 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 PFD1 PFD2 or MFD1 BKLT CAL INV calibration lost or mismatch Return for repair The PFD1 PFD2 and or MFD backlight calibration cannot be found or is invalid The system should be serviced DATABASE MESSAGE ADVISORIES Message MFD1 DB ERR MFD1 navigation database error exists PFD1 DB ERR PFD1 navigation database error exists PFD2 DB ERR PFD2 navigation database error exists Comments The MFD and or PFD detected a failure in the navigation database Attempt to reload the navigation database If problem persists the system should be serviced MFD1 DB ERR MFD1 basemap database error exists PFD1 DB ERR PFD1 basemap database error exists PFD2 DB ERR PFD2 basemap database error exists The MFD and or PFD detected a failure in the basemap database 190 00929 04 Rev A Garmin G1000 Cockpit Reference G
92. aner 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 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 This product its packaging and its components contain chemicals known to the State of California to cause cancer birth defects or reproductive harm This notice is being provided in accordance with California s Proposition 65 If you have any questions or would like additional 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
93. ate of Revision Affected Pages 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series RR 1 Record ofRevisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN table of Contents FLIGHT INSTRUMENTS tnn 1 Selecting the Altimeter Barometric Pressure Setting 1 Selecting Standard Barometric Pressure 29 92 in Hg sss 1 Change Altimeter Barometric Pressure Setting Units sss 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synchronize CDI aeree tede eee ie ed atid e dedii 1 Selecting DG Mode GRS 7800 Installations Only sss 2 Change Navigation Sources sssssssseeennnnnnnnnnns 2 Enable Disable OBS Mode While Navigating with GPS sss 2 Generic THM eR eed db desiit bdo BOLA Gabaa iiis 3 Configure Vspeed Bugs Individually sss 3 Turn Vspeed Bugs On or Off by Category 3 Set Barometric Radar Altimeter Minimum Descent Altitude 4 Testing the Radar Altimeter sssssssseenne 4 Displaying Wind Data 4 NAV COM TRANSPONDER AUDIO PANEL 5 ADF Tuning Optional sssssseenenentnnnnnnnnnns 5 BME Turilhj rer ders REOR RE ERUKR avs ARE ann ann ANI DR 5 Enter a Transponder Code ssssssseeeennnnns 5 S
94. b to place the cursor on Draft New Predefined Message c Press the ENT Key The PREDEFINED SMS TEXT MESSAGE Window is now displayed 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 8 saunpar0ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu i4 swiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy sainjea Jeuonippy xopu Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN 82 5 6 7 8 9 10 11 xw 12 The cursor is displayed in the TITLE field Enter the desired message title Entry can be accomplished through the alphanumeric keys on the MFD Controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by selecting the NUMBERS Softkey Select the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by selecting the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Enter the desired message using any combination of entry methods as described in step 5 Press the ENT Key Select the SAVE Softkey The new predefined message is now shown in the displayed list Selecting the CANCEL Softkey will delete the message wi
95. ccess the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 67 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN fil Buruue d 1ufi 4 ERIT SaJnpa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning DEPT Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance 68 A GARMIN Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude thin 100 Terrain Obstacle between 100 and 1000 below current aircraft altitude Black Terrain Obstacle is more than 1000 below aircraft altitude Enable Disable Aviation Data 1 While the TAWS B Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key TAWS Inhibit NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed
96. ck settings DATA LOST Pilot stored data was Comments The pilot profile data was lost System reverts to default pilot profile and settings The pilot may reconfigure the MFD amp PFDs with preferred settings if desired XTALK ERROR A flight display crosstalk error has occurred The MFD and PFDs are not communicating with each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs service Return unit for repair The PFD and or MFD self test has detected a problem The system should be serviced MFD1 SERVICE MFD1 needs service Return unit for repair 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 107 seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SyueuinJjsu 1ufi4 U405 AEN Wi aouepioay puezey gt of S2 zx Se os vp xipuaddy xopu Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix MER Index Annunciations amp Alerts A GARMIN Message Comments PFD1 MANIFEST PFD1 software mismatch communication halted PFD2 MANIFEST PFD2 software mismatch communication halted MFD1 MANIFEST MFD1 software mismatch communication halted The PFD and or MFD has incorrect software installed The system should be serviced PFD1 CO
97. collection processing and dissemination of radar images can be significant and may not reflect the current radar synopsis Due to the inherent delays and the relative age of the data it should be used for long range planning purposes only NOTE Precipitation data cannot be displayed on the Navigation Map Page at the same time as terrain Displaying Precipitation Weather Information 1 2 Select the MAP Softkey for the PFD Inset Map select the INSET Softkey This step is not necessary on the Connext Weather Data Link Page Select the PRECIP Softkey e Radar data shown represents lowest level base reflectivity of radar returns The display of the information is color coded to indicate the weather severity level All weather product legends can be viewed on the Connext Weather Data Link Page For the Precipitation legend select the LEGEND Softkey when Precipitation is selected for display 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 53 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 34614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Procedures v 2 5 E a Appendix Annun Alerts Features Index Hazard Avoidance A GARMIN Precipitation Limitations Radar images may have certain limitation
98. communications error has occurred with the GIA GSR 56 or GDL 59 The system should be serviced Connext Comm Error 4 This occurs if multiple automatic weather data requests have recently failed or the GIA is off line Connext Comm Error 5 The Iridium or Garmin Connext services are not accessible Check Iridium signal strength If this error persists the system should be serviced Connext Comm Error 6 A communications error has occurred It this error persists the system should be serviced Connext Comm Error 7 A weather data transfer has timed out Check Iridium signal strength and re send the Connext Data Request Connext Comm Error 8 A server error has occurred or invalid data received Connext Login Invalid There is a problem with the Garmin Connext registration Contact Garmin Connext at 1 866 739 5687 in the United States or 913 440 1135 for assistance Connext Server Temporarily Inop Connext Server Inop The Garmin Connext weather data server is temporarily out of service but is expected to return to service in less than 30 minutes The Garmin Connext weather data server will be out of service for at least 30 minutes 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 5 Bujuueld ACN Sd5 S2dV oipny uddx sjueumnasu SoJnpa oJd gt lt ES a D m A su jy unuuy sainjea4 je
99. configuration settings do not match those of backup configuration memory The system should be serviced m on h GTX1 MANIFEST GTX1 software ismatch communicati alted GTX2 MANIFEST GTX2 software m ismatch communicati on h alted The transponder has incorrect software installed The system should be serviced V4 e rvice Return unit for XPDR1 SERVICE XPDR1 needs repai f The 1 transponder should be serviced when possible XPDR2 SERVICE XPDR2 needs The 2 transponder should be serviced when service Return unit for repair possible XPDR1 FAIL XPDR1 is inoperative There is no communication with the 1 transponder XPDR2 FAIL XPDR2 is inoperative There is no communication with the 2 transponder XPDR1 ADS B FAIL XPDR1 unable ADS B is inoperative Other transponder functions to transmit ADS B messages XPDR2 ADS B FAIL XPDR2 unable to transmit ADS B messages may be available Transponder should be serviced when possible 118 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts GRS 77 7800 MESSAGE ADVISORIES Message AHRS1 TAS AHRS1 not receiving valid airspeed Comments The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to
100. crepancies related to database information These discrepancies could come in the form of an incorrect procedure incorrectly identified terrain obstacles and fixes or any other displayed item used for navigation or communication in the air or on the ground Go to http fly garmin com and select Aviation Data Error Report Ay CAUTION Never disconnect power to the system when loading a database Power interruption during the database loading process could result in maintenance being required to reboot the system A NOTE When loading database updates the DB Mismatch message will be displayed until database synchronization is complete followed by turning system power off then on Synchronization can be monitored on the AUX SYSTEM STATUS Page In some cases it may be necessary to 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 If an error occurs during synchronization an error message will be displayed followed by the affected display in the Sync Status section of the Database Window If synchronization completes on one display but an error occurs on another the error message will be displayed with the affected displays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power
101. ct the MORE WX Softkey Select the PIREPS Softkey Press the RANGE Knob and pan to the desired weather report A gray circle will appear around the weather report when it is selected Press the ENT Key The PIREP text is first displayed in a decoded fashion then as raw text Use the FMS Knob or the ENT Key to scroll through the PIREP text Press the FMS Knob or the CLR Key to close the PIREP text window and return to the Connext Weather Data Link Page Hazard Avoidance To display the PIREP or AIREP legend select the LEGEND Softkey when PIREPs or AIREPs are selected for display The PIREP color is determined by the type routine or urgent 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 57 AEN Sd9 S24V oipny uddx sjueumasuj u105 NeN fila Buruue d 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight AFCS XPDR Audio Instruments GPS Nav Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index A Hazard Avoidance GARMIN AIRBORNE COLOR WEATHER RADAR WARNING Begin transmitting only when it is safe to do so If it is desired to transmit while the aircraft is on the ground no personnel or objects should be within 11 feet of the antenna CAUTION In Standby Mode the antenna is parked at the center line It is always a good idea to put the radar in Standby Mode bef
102. cted VS Key VS nnnn FPM Altitude Flight Level Change Maintains the current aircraft airspeed in IAS Hold IAS or Mach while the aircraft is dimbing FLC mnk descending to the Selected Altitude Press FLC Key Flight Level Change the SPD Key to switch between IAS and FLC Manm ach Hold ACH VNAV Captures and tracks the VNAV flight path VNV Key VPTH AFCS armed to capture the altitude VNAV Target A Altitude Armed displayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath on GP approach C d tracks the ILS glides SM Glideslope aptures and tracks the ILS glideslope on GS approach Disengages the autopilot and commands a Takeoff on ground constant pitch angle and wings level in the TO air on the ground in preparation for takeoff GA Disengages the autopilot and commands a Switch Go Around in air constant pitch attitude and wings level in GA the air Activated oe only by Level Commands 0 pitch attitude the ESP WL function ALTS armed automatically when PIT VS FLC TO or GA active and under VPTH when Selected Altitude 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 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN
103. cted in the LDG position WOW FAULT Miscompare between weight on wheels inputs WOW INVALID Weight on wheels inputs invalid YD OFF AP engaged without Yaw Damper only available when compatible lift computer is installed 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 97 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Syueuingjsu paezey Wij wo09 eN fid soinjes Jeuonippy e EET xopu A Annunciations amp Alerts GARMIN COMPARATOR ANNUNCIATIONS Comparator Window Condition Text Flight Instruments Difference in altitude sensors is gt 200 ft f bo f either airspeed sensor detects gt 35 knots and the difference in sensors is gt 10 kts f either airspeed sensor detects gt 80 knots and the difference in sensors is 7 kts Nav Com XPDR Audio h airspeed sensors detect lt 35 knots this is inhibited AFCS Difference in heading sensors is gt 6 degrees Difference in pitch sensors is gt 5 degrees GPS Nav Difference in roll sensors is 6 degrees ALT NO COMP o data from one or both altitude sensors IAS NO COMP o data from one or both airspeed sensors HDG NO COMP o data from one or both heading sensors PIT NO COMP o data from one or both pitch sensors ROL NO COMP o data from one or both roll sensors Flight Planning
104. d Enter the desired radial from the reference waypoint Press the ENT Key Repeat step 10 to enter the next waypoint name 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 zu gt EI E ia Se1Jnpa oJd aouepioay puezey 11 SoJnjeeoj Jeuonippy 12 13 14 lt su jy unuuy xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 23 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN CREATE A USER WAYPOINT DEFINED BY A RADIAL amp DISTANCE FROM 24 1 2 3 4 5 6 1 8 9 10 ANOTHER WAYPOINT Turn the large FMS Knob on the MFD Control Unit to select the WPT page group Turn the small FMS Knob to select the User WPT Information Page Select the NEW Softkey A waypoint is created at the current aircraft position Enter the desired waypoint name Press the ENT Key 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
105. desired course to from the waypoint Press a CRS Knob to synchronize the Selected Course with the bearing to the next waypoint Press the OBS Softkey again to disable OBS Mode Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight instruments 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 Turn the small FMS Knob to display the UP DOWN window Turn the FMS Knob to select UP or DOWN then press the ENT Key START is now highlighted 3 Press the ENT Key to START STOP or RESET the timer if the timer is counting DOWN it will start counting UP after reaching zero Press the CLR Key or the TMR REF Softkey to remove the window Er a ga c ERG a gt El a a S2JV oipny uddx W0 AEN AEN Sd5 CONFIGURE VSPEED BUGS INDIVIDUALLY 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the desired Vspeed 3 Use the small FMS Knob to change the Vspeed in 1 kt increments when a speed has been changed from a default value an asterisk appears next to the speed 4 Press the ENT Key or turn the large FMS Knob to highlight the ON OFF field 5 Turn the small FMS Knob clockwise to ON or counterclockwise to OFF 6 To remove the window press the CLR Key or the TMR REF So
106. dures GARMI N ACTIVATE A MISSED APPROACH IN THE ACTIVE FLIGHT PLAN 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE MISSED APPROACH 3 Press the ENT Key A confirmation window will be displayed 4 With ACTIVATE highlighted press the ENT Key Or Press the go around button Nav Com Flight XPDR Audio Instruments AFCS 5 After activating the missed approach procedure and the CDI has changed to TERM mode sensitivity another approach procedure may be loaded TEMPERATURE COMPENSATED ALTITUDE When temperature compensated altitude is enabled for the loaded approach the altitudes associated with the approach waypoints are displayed in slanted text GPS Nav Planning HABUK iaf 021 5 7NH HABUK iaf 021 5 7NM FALUR 261 4 7NM FALUR 261 4 7NM 8 CEGIX faf 351 5 9NH CEGIX faf 351 5 9NH E RW35R map il 5 1NM RW35R map oT 5 1NM 6368FT 348 U 5NH 6368FT 6368FT 348 5NM MOGAL mahp MOGAL mahp 5 g HOLD y 6 0NM E HOLD 168 6 NM ss z Altitudes Displayed Without Altitudes De With Temperature Compensation dinem ompensation i Enabling temperature compensated altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is displayed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed Annun Alerts Appendix 4 Use the small FMS Knob to select the temperature at the airport
107. e If the AUX SYSTEM SETUP 2 is already displayed proceed to step 4 4 Press the FMS Knob to activate the cursor 5 Turn the large FMS Knob to place the cursor in the STABILITY amp PROTECTION field 6 Turn the small FMS Knob to select ENABLE or DISABLE 7 Press the FMS Knob to remove the cursor 94 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features Roll Engagement Roll Limit Indicators are displayed on the roll scale at 45 right and left indicating where ESP will engage As roll attitude exceeds 45 ESP will engage and the on side Roll Limit Indicator will move to 30 The Roll Limit Indicator is now showing where ESP will disengage as roll attitude decreases to within the desirable roll attitude range Once engaged ESP force will be applied between 30 and 75 The force increases as roll attitude increases and decreases as roll attitude decreases The applied force is intended to encourage pilot input that returns the airplane to a more normal roll attitude As roll attitude decreases ESP will disengage at 30 ESP is automatically disengaged if the aircraft reaches the autopilot roll engagement attitude limit of 75 Pitch Engagement ESP engages at 20 nose up and 17 nose down Once ESP is engaged it will apply opposing force between 15 and 50 nose up and between 12 and 50 nose down Maximum opposing force is applied between 25
108. e VNV offset distance field 10 Enter the desired offset distance before or after 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 E on the PFD 2 Turn the large FMS Knob to place the cursor in the desired selection field GPS Navigation 3 Turn the small FMS Knob to begin selecting the desired identifier location etc oipny uddx syueumasu U10 AEN S2dV s n e 4 aouepioay saunpar0ld Buruue d puezey Jeuonippy su jy unuuy 36114 1614 4 Press the ENT Key 5 The cursor is now flashing on ACTIVATE If no altitude constraint or course is desired press the ENT Key to activate To enter an altitude constraint proceed to step 6 6 Turn the large FMS Knob to place the cursor over the ALT altitude field 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 13 xipuaddy xopu Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index GPS Navigation GARMI N 1 8 9 10 11 12 13 14 15 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 pr
109. e aircraft Typically used during enroute phase of flight BELOW Displays non threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft Typically used during descent phase of flight UNREST All traffic is displayed TEST Activates Test Mode and displays test intruder symbols seinpa2o0Jd Buruue d AEN Sd5 S2d1V 164 aouepioay puezey BACK Returns to the previous softkey level ae CODE Displays transponder code j selection softkeys 0 7 0 7 Use numbers to enter code IDENT Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen gt kej 5 a E BKSP Removes numbers entered one at a time xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 14 Additional Hazard Flight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A Appendix _ GARMIN Level 1 Level 2 Level3 Level 4 Description 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 MFD NAVIGATION PAGE SOFTKEY MAP optional IC 9 3E 1E CS Fm orn F vy rx nn nx a n optional
110. e area s during an initial Connext Data Request Enabling or disabling the display of the weather product does not affect which weather products are retrieved during a Connext Data Request To reduce data usage during subsequent requests the system retains previously retrieved textual weather products such as METARs and TAFs so long as they have not expired The system also retrieves any new textual weather products matching the current coverage area and all graphical weather products during each data request If the Connext Data Request was successful the REQUEST STATUS window if shown indicates OK Refer to the Abnormal Operations discussion later in this section for more information on the messages received if the request is unsuccessful with possible causes 50 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Hazard Avoidance Weather Request Status Message Description Auto requests inhibited Send manual request to reset Auto update retry Seconds The system has disabled automatic weather data requests due to excessive errors Automatic weather data requests have stopped Send a manual weather data request to resume automatic updates The system will attempt another automatic weather data request after an error occurred during the previous request Timer counts down until the next automatic request occurs Connext Comm Error 2 A
111. e for the Beechcraft 200 B200 Series 12 1 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx Syueuinjjsu paezey Wij w09 eN Wija SoJnjeeoj Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts GSR 56 MESSAGE ADVISORIES A GARMIN Message Comments GSR1 FAIL GSR1 has failed A failure has been detected in the 1 GSR 56 The system should be serviced GDL 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 system should be serviced GDL69 FAIL GDL 69 has failed A failure has been detected in the GDL 69 The receiver is unavailable The system should be serviced GDL69 MANIFEST GDL software mismatch communication halted The GDL 69 has incorrect software installed The system should be serviced GWX 68 70 MESSAGE ADVISORIES Message Comments GWX CONFIG GWX config error Config service req d GWX 68 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not receiving status packet from the GWX 68 or the GWX 68 is reporting a fault The GWX 68 radar
112. e system components e g GTS 8000 AFCS and GWX will be different from the heading displayed on the GDU by an amount equal to the difference between the current Magnetic Field Variation Database MV DB value and the MV DB value when DG Free Mode was activated Due to the convergence of isogonic lines this condition is most noticeable at or near the North and South poles Press the PFD Softkey Press the HDG MODE Softkey Press the DG FREE Softkey to activate DG mode Press the DG SLAVE Softkey to deactivate DG mode e Pressing the HDG or HDG softkey to slew the heading counterclockwise or clockwise e Pressing the HDG SYNC softkey to synchronize the heading to the current selected heading Pressing the TRACK SYNC softkey to synchronize the heading to the current track CHANGE NAVIGATION SOURCES 1 2 3 Press the CDI Softkey to change from GPS to VOR1 or LOC1 This changes the NAV1 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey again to change from VOR1 or LOC1 to VOR2 or LOC2 This changes the NAV2 standby frequency in the upper left corner of the PFD to light blue indicating this is the frequency selected for tuning Press the CDI Softkey a third time to return to GPS ENABLE DISABLE OBS MODE WHILE NAVIGATING WITH GPS 1 2 3 Press the OBS Softkey to select OBS Mode Turn a CRS Knob to select the
113. ed Obstacle Clearance Caution ROC Imminent Obstacle Impact Caution IOI Caution Obstacle Caution Obstacle or Obstacle Ahead Obstacle Ahead Obstacle Ahead Obstacle Ahead or Caution Obstacle Caution Obstacle Premature Descent Alert Too Low Terrain THEE EHE HATE AT Caution PDA Excessive Descent Rate u u Caution EDR Sink Rate Negative Climb Rate Bn aon Caution NCR Too Low Terrain 104 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Amunciations amp Alerts TAWS B System Status Annunciations SjueuinJjsu 1i PFD MFD T Additional TAWS A Page Voice Alert Type TAWS A Page m PE Annunciation Message Annunciation SF 7 5 TaWS System Fail TSF RNIN Men System Test in progress TAWS TEST None System Test pass None None ps c MFD Terrain or Obstacle 3 database unavailable or invalid TAWS operating None None with PFD Terrain or Obstacle databases zz TAWS Not Available No GPS position TAWS 3 excessively degraded Available 3 GPS signal when sufficient GPS signal is received E AWSNot amp Available TAWS Out of database TS EL 2E coverage area TAWS N A i Aa ae BE when aircraft 2g enters database coverage area gt 5 3 3 2 x xopu 190 00929 04 Rev A Garmin G1000 Cockpit
114. efer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning 6 Enterthe departure time Press the ENT Key when finished Departure time may be entered in local or UTC time depending upon system settings sjueuinisu fid 7 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 oipny uddx U105 AEN 8 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 S2dV 9 Theflashing cursor moves to the fuel onboard field Modify the fuel onboard Press the ENT Key when finished In AUTOMATIC mode fuel onboard is provided by the entry made on the Weight Planning Page The flashing cursor moves to the calibrated airspeed CALIBRATED AS field Enter the calibrated airspeed Press the ENT Key when finished Note that in AUTOMATIC page mode calibrated airspeed is provided by the system The flashing cursor moves to the altitude IND ALTITUDE field Enter the altitude Press the ENT Key when finished Note that in AUTOMATIC page mode altitude is provided by the system ACN Sd5 10 11 12 The flashing cursor moves to
115. elect the AUX page group Turn the small FMS Knob to select the AUX TELEPHONE Page Press the MENU Key The Page Menu window is now displayed Turn the FMS Knob to select Disable Iridium Transmission in the menu list Press the ENT Key The Iridium transceiver is now disabled To enable the Iridium transceiver repeat steps 1 through 4 then select Enable Iridium Transceiver Telephone Communication The pilot or copilot can place and answer calls on the Iridium satellite network as well as to or from the telephone handset in the cabin Calls can also be answered or made from the cabin phone however only actions initiated from the cockpit phone will be discussed here See the cabin handset user guide for more information Control and monitoring of telephone functions are accomplished through the AUX TELEPHONE Page Viewing the Telephone Page 1 2 3 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select the AUX TELEPHONE or AUX TEXT MESSAGING Page If necessary select the TEL Softkey to display the AUX TELEPHONE Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Ad itional Features Internal External Phone Phone Phone is Idle Phone is ringing Phone has a dial tone off hook or connected to another phone Phone dialed is busy Description sjueuinijsu ufi oipny uddx U105
116. electing a COM Radio 5 Selecting a NAV Radio nennen 6 NAV COM Tuning sssseeeeennnnnnennn nnne 6 Intercom diet ea aA 6 Passenger Address PA System 7 Clearance Recorder and Player 7 AUTOMATIC FLIGHT CONTROL SYSTEM csssssssssssesssseeseunssstensas 9 Flight Director Activation sss 9 Vertical Modes 0 Lateral Modes 1 Suspected Autopilot Malfunction ssssssss 2 Overpowering Autopilot Servos sssssssseee nne 2 GPS NAVIGATION ota oan tt Roi o etit aci 3 Direct to Navigation sssssssseseee nnne 3 Activate a Stored Flight Plan 4 Activate a Flight Plan Leg 4 Stop Navigating a Flight Plan 5 Vertical Navigation VNAV ssssssseeeeet nnne 5 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A Table of Contents GARMIN FLIGHT PLANNING sseeeeen Weight Planning nnns Trip Planning eet eee etn te eds Create a User Waypoint Defined by Latitude amp Longitude Create a User Waypoint Defined by Radials from Other Waypoints Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 24 Delete a User Waypoint Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan Enter an Airway in a Flight Plan User Defined Holding Patterns
117. es 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 ChartView resembles the paper version of Jeppesen terminal procedures charts The charts are displayed in full color with high resolution The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The ChartView database is updated on a 14 day cycle If the ChartView database is not updated within 70 days of the expiration date ChartView will no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts The MFD depiction shows the aircraft position on the moving map in the plan view of most approach charts and on airport diagrams The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW
118. ess the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN GPS Navigation STOP NAVIGATING A FLIGHT PLAN 1 Press the FPL Key on the Control Unit to display the Active Flight Plan Page 2 Press the MENU Key to display the Page Menu Window 3 Turn the large FMS Knob to highlight Delete Flight Plan and press the ENT Key With OK highlighted press the ENT Key to deactivate the flight plan This will not delete the stored flight plan only the active flight plan sjueuinisu iui oipny uddx U105 AEN VERTICAL NAVIGATION VNAV S2dV 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 A NOTE Temperature Compensated TEMP COMP altitudes are depicted as slanted text z oz EH 5 gt e ACTIVE FLIGHT PLAN KDFW SoJnpa oJd We large White Text 12400FT E PEST MES S UTERE Large Light FA Blue Text i RIVET iaf Ngo S Small Light m DRAAK KEPT Blue Tex AE INHOD j Small Light NE MENOL faf i id RW17L e pe Small White Text EI SQFT with Altitude E POLKE Restriction Bar gt xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 15 Flight Instruments i Nav Com XPDR Audio Flig
119. ete being displayed 9 Remove and reapply power to the system 10 11 12 x uw Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Press the Display Database Selection Softkey to show database information 145 Seinjee4 e uepioAy Sa1npa20Jg Buruue d AEN Sd5 S24Y oipny uddX sjueuimnasu Jeuonippy paezey wo gt AeN su jy unuuy xipuaddy 1i 164 Additional Hazard Fight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index A GARMIN Loading the Jeppesen Navigation Database as the Active Navigation Database 1 2 3 4 5 6 7 8 9 10 11 NOTE Loading the Jeppesen navigation database as the active database prior to its effective date will result in the expiration date on the power up screen and the effective date on the AUX System Status Page being displayed in yellow NOTE After the navigation database is loaded or copied the top SD card may be removed With the system OFF insert the SD card containing the new navigation database version into the top card slot of the display PFD1 PFD2 or M
120. ey on the appropriate audio panel Press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Answer Incoming Call Press the ENT Key Selecting the IGNORE Softkey will extinguish the pop up window and leave the call unanswered Selecting the TEL Softkey will display the AUX TELEPHONE Page allowing additional call information to be viewed before answering Mute Incoming Call Alerts 1 2 3 With the AUX TELEPHONE Page displayed press the MENU Key on the MFD to display the Page Menu Turn either FMS Knob to place the cursor on Mute Incoming Call Alerts Press the ENT Key The voice and pop up alert will not be displayed now when an incoming call is received Outgoing Calls Voice calls can be made from the cockpit to the handset in the cabin or to an external phone through the Iridium Satellite Network 76 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Make a Call to the Cabin 1 2 3 4 Press the TEL Key on the appropriate audio panel Select the DIAL Softkey on the MFD Press the ENT Key The cursor will move from CABIN to OK Press the ENT Key again The cabin phone will now ring To exit the call select the HANGUP Softkey Make an External Call from the Cockpit 1 2 3 4 5 6 1 Press the TEL Key on the appropriate audio panel Select the DIAL Softkey on the MFD Turn the
121. eys to assign a number to the active channel Adjusting Volume Radio volume is controlled at each passenger station PILOT PROFILES Creating a profile 1 2 3 4 5 6 7 8 9 Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page Press the FMS Knob momentarily to activate the flashing cursor Turn the large FMS Knob to highlight CREATE in the Pilot Profile Box Press the ENT Key A Create Profile window is displayed Use the FMS Knob to enter a profile name up to 16 characters long and press the ENT Key Pilot profile names cannot begin with a blank as the first letter In the next field use the small FMS Knob to select the desired settings upon which to base the new profile Profiles can be created based on Garmin factory defaults default profile settings initially based on Garmin factory defaults unless edited by the pilot or current system settings Press the ENT Key With CREATE highlighted press the ENT Key to create the profile Or Use the large FMS Knob to select CREATE and ACTIVATE and press the ENT Key to activate the new profile To cancel the process select CANCEL with the large FMS Knob and press the ENT Key Selecting an active profile 1 2 Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page Press the FMS Knob momentarily to activate the flashing cursor 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200
122. ference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Description 360 HSI ARC HSI BRG2 HDG MODE DG FREE DG SLAVE HDG HDG HDG SYNC TRK SYNC ALT UNIT METERS IN HPA STD BARO 190 00929 04 Rev A 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 and ADF frequency Displays softkeys to select DG Modes GRS 7800 installations only Allows the DG to enter FREE mode Slaves the DG to the AHRS Slews heading counterclockwise Slews heading clockwise Synchronizes heading to the selected heading Synchronizes heading to the current track 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 137 sainjea4 exuepioAy sainpar0ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu puezey U105 AEN Jeuonippy su jy unuuy gt kej a Ej xopu 36114 16114 Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning
123. 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 select the IMPORT Softkey 7 Turn the small FMS Knob to highlight the desired flight plan for importing 8 Press the ENT Key S2dV AEN Sd5 R e a o amp zm E 1 aouepioay puezey INSERT A WAYPOINT IN THE ACTIVE FLIGHT PLAN soinjes Jeuonippy 1 Press the FPL Key on the Control Unit to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the desired flight plan waypoint The new waypoint will be inserted before the highlighted waypoint su jy unuuy 4 Turn the small FMS Knob The Waypoint Information Window is now displayed xipuaddy 5 Enter the new flight plan waypoint by one of the following a Enter the user waypoint identifier facility or city b Press the ENT Key Or xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 2 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN a Turn the s
124. from determining Altitude has been the navigation database vertical flight 3 retrieved from the or has been entered by path guidance A navigation database the pilot and matches a and is provided as a published altitude in the reference navigation database aouepioay puezey soinjes Jeuonippy su jy unuuy x pu ddy x pul 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 17 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS Procedures Appendix Annun Alerts Features Index GPS Navigation 18 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN 190 00929 04 Rev A GARMI N Flight Planning FLIGHT PLANNING sjueuinijsu 1i WEIGHT PLANNING All procedures apply to the MFD and the Control Unit unless otherwise stated oipny uddx U105 AEN Entering Weight Parameters The Weight Planning Page is displayed after system power up If it is necessary to return to this page turn the large FMS Knob to select the AUX page group Turn the small FMS Knob to select the Weight Planning Page 1 Select the EMPTY WT Softkey to place the cursor in the Basic Empty Weight field 2 Enter the desired aircraft empty weight 3 Press the ENT Key The cursor is now over the PILOT amp STORES field 4 Enterthe desired weight of Pilot amp Stores 5
125. ftkey seinpa2o0Jd Buruue d 1614 aouepioay puezey TURN VSPEED BUGS ON OR OFF BY CATEGORY soinjes Jeuonippy 1 Press the TMR REF Softkey 2 Press the MENU Key 3 Turn the FMS Knob to highlight the desired option 4 Press the ENT Key Press the TMR REF Softkey to remove the window su jy unuuy xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 3 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index dh Flight Instruments GARMIN SET BAROMETRIC RADAR ALTIMETER MINIMUM DESCENT ALTITUDE 1 2 3 4 5 6 Press the TMR REF Softkey Turn the large FMS Knob to highlight the Minimums field Turn the small FMS Knob to select BARO TEMP COMP or RAD ALT OFF is selected by default Press the ENT Key or turn the large FMS Knob to highlight the next field Use the small FMS Knob to enter the desired altitude from zero to 16 000 feet for BARO or from zero to 2 500 for RAD ALT If TEMP COMP was selected press the ENT Key or turn the large FMS Knob to highlight the next field and then enter the destination airport temperature 59 C to 59 C The temperature compensated altitude minimum is displayed below the previously enter minimum altitude value To remove the window press the CLR Key or the TMR REF Softkey TESTING THE RADAR ALTIMETER 1 2
126. ge FMS Knob to highlight DELETE in the Pilot Profile Box 4 Press the ENT Key 5 In the Delete Profile window turn the FMS Knob to select the profile to delete 6 Press the ENT Key 7 With DELETE highlighted press the ENT Key 8 To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features Importing a profile 1 Insert the SD card containing the Pilot Profile into the top card slot on the MFD 2 Usethe FMS Knob to select the AUX SYSTEM SETUP 1 Page 3 Press the IMPORT softkey If the correct Pilot Profile file is selected with IMPORT highlighted press the ENT Key Or If the SD card contains more than one Pilot Profile a Turn the large FMS Knob to highlight the select file field in the Pilot Profile Importing Box b Turn the small FMS Knob to display the pilot profile list and highlight the desired profile to import and press the ENT Key c With IMPORT highlighted press the ENT Key 4 Pilot profile import succeeded is shown in the import results box Press the ENT Key The imported profile becomes the active Pilot Profile Exporting a profile 1 Insert the SD card for storing the Pilot Profile into the top card slot on the MFD 2 Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page 3 Activate the desired Pilot
127. ges are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Panel plays recorded audio to the Pilot Pressing the play key on the Copilot s Audio Panel plays recorded audio to the Copilot Recorded COM audio is stored in separate memory blocks Once 2 5 minutes of recording time have been reached the recorder begins recording over the stored memory blocks starting from the oldest block The PLAY Key controls the play function The PLAY annunciator is illuminated to indicate when play is in progress The PLAY annunciator extinguishes after playback is finished Pressing the PLAY Key once plays the latest recorded memory block and then returns to normal operation Pressing the PLAY Key again during play of a memory block stops play Ifa COM input signal is detected during play of a recorded memory block play is halted Pressing the PLAY Key twice within one half second while audio is playing plays the previous block of recorded audio Each subsequent two presses of the PLAY Key within one half second backtracks through the recorded memory blocks to reach and play any recorded block 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 7 sye yjunuuy sainjea4 enuepioAy SaJnpa20Jd Duiuue g AEN Sd5 S24V oipny YddX syu wunysu Jeuonippy paezey WO gt AeN xipueddy xopu fila 34614 A Nav Com XPDR Audio Panel GAR
128. halted The GDC has incorrect software installed The system should be serviced GCU 477 MESSAGE ADVISORIES Message Comments GCU CNFG GCU Config error Config service req d GCU 477 configuration settings do not match those of backup configuration memory The G1000 system should be serviced GCU FAIL GCU is inoperative A failure has been detected in the GCU 477 The GCU 477 is unavailable GCU1 MANIFEST GCU software mismatch communication halted The GCU 477 has incorrect software installed The G1000 system should be serviced GCU KEYSTK GCU key name Key is stuck A key is stuck on the GCU 477 bezel Attempt to free the stuck key by pressing it several times The G1000 system should be serviced if the problem persists 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 123 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 241V oipny uddx Sjueuinjjsu paezey 3614 U405 AEN Wi sainjes Jeuonippy ak BEIM xopu Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Additional Features Appendix Index Annunciations amp Alerts GMC 710 MESSAGE ADVISORIES A GARMIN Message GMC CONFIG GMC Config error Config service req d Comments Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative A failure has been detected i
129. he Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning Removing a user defined hold inserted into the active flight plan sjueumasu 1i 1 Press the FPL Key to display the Active Flight Plan Page MFD or the Active Flight Plan Window PFD 2 Press the FMS Knob to activate the cursor not required on the PFD and turn the large FMS Knob to highlight the HOLD waypoint 3 Press the CLR Key A Remove Holding Pattern confirmation window is displayed oipny uddx U105 AEN S2dV 4 Select OK and press the ENT Key The holding pattern is removed from the active flight plan Select CANCEL and press the ENT Key to cancel the removal of the holding pattern AEN Sd5 Removing a user defined hold at an off route direct to 1 Press a Direct To Key to display the DIRECT TO Window PFD or MFD 2 Press the MENU Key to display the PAGE MENU with the cursor on the Cancel Direct To NAV selection 3 Press the ENT Key The holding pattern is removed R e a o Qa G E 1 v INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to display the active flight plan 2 Press the MENU Key to display the Page Menu 3 Turn the large FMS Knob to highlight Invert Flight Plan 4 Press the ENT Key The original flight plan remains intact in its flight plan catalog storage location 5 With OK highlighted press the ENT Key to invert the flight plan REMOVE A DEPARTURE ARRIVAL APPR
130. he small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 32 1 2 Press the FPL Key to display the active flight plan Press the FMS Knob to activate the cursor Or a Turn the small FMS Knob to select the Flight Plan Catalog Page b Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan d Select the EDIT Softkey Turn the large FMS Knob to highlight the waypoint to be deleted Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window sjueuimasu fid 4 With OK highlighted press the ENT Key to remove the waypoint To cancel the delete request turn the large FMS Knob to highlight CANCEL and press the ENT Key EE 5 Once all changes have been made press the FMS Knob to remove the cursor S2dV INVERT AND ACTIVATE A STORED FLIGHT PLAN 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to ac
131. he small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while ACTIVATE is highlighted to immediately activate the hold Creating a User Defined Hold at a Direct To Waypoint 1 2 5 6 1 8 9 10 Press a Direct to Key on the Control Unit and set up the Direct To waypoint as desired but select HOLD instead of ACTIVATE when finished Use the FMS Knobs to edit the entry course and press the ENT Key Use the small FMS Knob to select INBOUND or OUTBOUND course direction and press the ENT Key Use the small FMS Knob to select TIME or DIST length mode and press the ENT Key Use the FMS Knobs to edit the length and press the ENT Key Use the small FMS Knob to select RIGHT or LEFT turn direction and press the ENT Key Use the FMS Knobs to edit the Expect Further Clearance Time EFC TIME and press the ENT Key Press the ENT Key while ACTIVATE is highlighted to activate the Direct To with the user defined hold defined at the Direct To waypoint Exiting a user defined hold inserted into the active flight plan 30 Press the SUSP Softkey The system will provide guidance to follow the holding pattern to the inbound course and resume automatic waypoint sequencing Garmin G1000 Cockpit Reference Guide for t
132. her Data Link CNXT Page 1 Select the Weather Data Link CNXT Page 2 Press the MENU Key 3 With Weather Setup highlighted press the ENT Key 4 Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key 5 Turn the large FMS Knob or press the ENT Key to scroll through product selections 6 Turn the small FMS Knob to scroll through options for each product ON 1 8 48 OFF range settings etc Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Weather Data Link CNXT Page with the changed settings Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Hazard avoidance Restoring Default Connext Weather Data Link Page CNXT Settings 1 Select the Weather Data Link CNXT Page 2 Press the MENU Key 3 With Weather Setup highlighted press the ENT Key 4 Press the MENU Key 5 Highlight the desired default s to restore all or for selection and press ENT Key oipny uddx syueumasu U105 AEN 2461 4 S24V Viewing Legends for Displayed Connext Weather Products 1 Select the Weather Data Link CNXT Page 2 Select the LEGEND Softkey to display the legends for the displayed weather products Or a Press the MENU Key b Select Weather Legend and press the ENT Key 3 Turn the FMS Knob to scroll through the legends if more are available than fit in
133. hereby grants permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other 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 Garm electronic storage medium to be viewed for personal use provided that such electronic in G10009 WATCH FliteCharts and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries ESP is a trademark of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garm n NavData is a registered trademark of Jeppesen Inc SiriusXM is a trademark of SiriusXM Satell ite Radio Inc AOPA Membership Publications Inc and its related organizations hereinafter collectively AOPA expressly disclaim all warranties with respect to the AOPA information included in this data express or implied including but not limited to the implied warranties of merchantability and fitness for a particular purpose The information is provided as is and AOPA does not warrant or make any representations regarding its accuracy reliability or otherwise Under no circumstances induding negligence shall AOPA be liable for any incidental special or consequential damages that
134. ht Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Appendix Annun Alerts Features Index GPS Navigation GARMI N SIUS Cross AT or ABOVE 5 000 fi PAGO Cross AT 2 300 ft eius Cross AT or BELOW 3 000 ft Altitudes associated with arrival and approach procedures are auto designated This means the system will automatically use the altitudes loaded with the arrival or approach for giving vertical flight path guidance outside the FAF Note that these alti tudes will be displayed as small light blue text Altitudes that have been designated for use in vertical navigation may also be made non designated by placing the cursor over the desired altitude and pressing the CLR Key The altitude is now displayed only as a reference It will not be used to give flight path vertical 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 The system updates vertical path guidance continuously using ground speed and the calculated distance to the Bottom of Descent BOD Due to turn anticipation guidance turn smoothing distance to the BOD can be affected by course changes greater than approximately 5 degrees Ground speed can be affected by factors such as shifts in wind direction aircraft power management pitch angle and course changes Abrupt and or substantial changes to either the distance to the BOD ground
135. ht plans are correct and up to date 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 125 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 e Wij SoJnjeoj Jeuonippy xipuaddy xopu Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix ee Index Annunciations amp Alerts A GARMIN Message Comments DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use of airways in stored flight plans and reload airways as needed LOCKED FPL Cannot navigate locked flight plan This occurs when the pilot attempts to activate a stored flight plan that contains locked waypoint Remove locked waypoint from flight plan Update flight plan with current waypoint WPT ARRIVAL Arriving at waypoint boxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes Special use airspace is ahead of aircraft The aircraft will pe
136. igation 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 Appendix Index 42 Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob select the Stormscope Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Hazard avoidance Change the Stormscope Lightning Mode Between Cell and Strike 1 Select the Stormscope Page 2 Select the MODE Softkey The CELL and STRIKE Softkeys are displayed Select the CELL Softkey to display CELL data or select the STRIKE Softkey to display STRIKE data CELL or STRIKE is displayed in the mode box located in the upper left corner of the Stormscope Page NOTE Cell mode uses a clustering program to identify clusters of electrical activity that indicate cells Change the Viewing Mode Between 360 and 120 1 Select the Stormscope Page 2 Select the VIEW Softkey The 360 and ARC Softkeys are displayed Select the 360 Softkey to display a 360 viewing area or select the ARC Softkey to display a 120 viewing area Select the CLEAR S
137. ions amp Alerts A GARMIN Message Comments DB MISMATCH Standby Navigation database mismatch The PFDs and MFD have different standby navigation database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Terrain database mismatch The PFDs and MFD have different terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Obstacle database mismatch The PFDs and MFD have different obstacle database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed After synchronization is complete power must be turned off then on DB MISMATCH Airport Terrain database mismatch The PFDs and MFD have different airport terrain database versions or regions installed Check the AUX SYSTEM STATUS Page to determine versions or regions Also check the AUX SYSTEM STATUS Page for a database synchronization function not completed
138. is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced GIA1 SERVICE GIA1 needs service Return the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted GIA1 MANIFEST GIA1 software mismatch communication halted GIA2 MANIFEST GIA2 software mismatch communication halted A GIA mismatch has been detected where only one is SBAS capable The GIA1 and or GIA 2 has incorrect software installed The system should be serviced GFC MANIFEST GFC software mismatch communication halted Incorrect servo software is installed or gain settings are incorrect COM1 MANIFEST COM1 software mismatch communication halted COM2 MANIFEST COM2 software mismatch communication halted COM1 and or COM2 software mismatch The G1000 system should be serviced 114 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Mes
139. isplay If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey will be displayed fa Traffic Advisory System TAS or Traffic Collision Avoidance System TCAS D is configured a STANDBY OPERATE or NORMAL TEST and ALT MODE Softkey will be displayed Ifa Traffic Collision Avoidance System TCAS II is configured an REL ABS TFC STBY TA ONLY TA RA TEST and ALT RNG Softkey will be displayed Traffic Symbol Description Non Threat Traffic intruder is beyond 5 nm and greater than 1200 vertical separation Proximity Advisory PA TAS only not available with TIS intruder is within 5 nm and less than 1200 vertical separation Traffic Advisory TA closing rate distance and vertical separation meet TA criteria Traffic Advisory Off Scale Resolution Advisory RA TCAS II only Potential collision area is within 15 to 35 seconds ENOGO JO 3SO Resolution Advisory Off Scale TCAS Il only Traffic Symbol Description 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 61 Bujuueld AEN Sd5 S24V oipny uddx Sjuaumasu SeJnpa oJd gt lt Es a D E A So1meoj Jeuonippy su jy unuuy x pu ddy x pul fila U10 AEN 36114 Flight Instruments Nav Com XPDR Audio Flight Planning AFCS GPS Nav DEPT Avoidance Procedures Additional Appendix Annun Alerts Fea
140. isplayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map TRAFFIC COLLISION AVOIDANCE SYSTEM TCAS II OPTIONAL NOTE If the system is configured to use TIS or TAS the optional TCAS II is not available for use System Test 1 2 3 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the TEST Softkey A test pattern of traffic symbols is displayed on the Traffic Page and inset map on the PFD The VSI will display red with a green climb indication from 0 to 2000 feet per min The self test takes approximately eight seconds to complete after which a voice alert TCAS System Test OK is heard In the event the system test fails a voice alert TCAS System Test Failed is heard and a visual annunciation TCAS FAIL appears on the PFD In addition a yellow visual annunciation FAILED appears in the center of the Traffic Map Page 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 63 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruue d 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy syajy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N 64 Displaying Traffic on the Traffic Map Page
141. l dpowe sessonp vro q om cn T rere eT meme wesr ETS pH wu Press the BACK Softkey to return to the top level softkeys De seonz JL Jrwoe Joss JL 1L nna D D nme z t lt Selecting BACK returns to the previous softkey level Ss Se msnnn mps amp smununnunun Selecting BACK returns to the previous softkey level Disce Rosi BELOW Jones 1L 1L a murnnnnnnnnnnun Selecting BACK returns to the previous softkey level RS ea ey 98 JE 1E 1L E985 JEAERIS nus amp smumnnmnnnunnnunnun Selecting BACK returns to the previous softkey level ALERTS Co 2 is s s e 7 Jer ses J Back F3 V3 V3 F3 n1gs spnmnnmnmn nmn n n onm Buruue d 1i SoJnpa o0Jd aouepioay puezey az Transponder Traffic Softkeys with TCAS II Option Be Level 1 Level2 Level3 Level 4 Description XPDR TFC Displays the transponder and d TCAS II selection softkeys XPDRI Selects the 41 transponder as z active H XPDR2 Selects the 2 transponder as active El a o x 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 139 Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix A GARMIN Level 1 Level 2 Level 3 Description MODE TCAS STB
142. l Failure Roll axis control failure Pitch Trim Axis Control Failure If annunciated when AP is engaged a failure has occurred in the pitch trim system Buruue d 1ufi 4 System Failure AP and MET are unavailable FD may still be available Yaw Damper Ruddar Boost Failure SoJnpa oJd YD axis control failure 2 jme me TII 1 00 api mm S2 mc Elevator Mistrim A condition has developed causing the pitch servo to gt Up provide a sustained force in the nose up direction RE Elevator Mistrim Down A condition has developed causing the pitch servo to provide a sustained force in the nose down direction 2E Aileron Mistrim A condition has developed causing the roll servo to provide amp Left a sustained left force 22 Aileron Mistrim A condition has developed causing the roll servo to provide Right a sustained right force Rudder Mistrim Left Rudder Mistrim Right Preflight Test A condition has developed causing provide a sustained force the yaw servo to A condition has developed causing the yaw servo to provide a sustained force gt k o 3 a x Performing preflight system test Upon completion of the test the aural alert will be heard SPSEERE I Preflight system test has failed xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the
143. l Features a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Address c Press the ENT Key The sorting selection is indicated at the bottom center of the list window syu un su 1i oipny uddx U105 AEN Viewing The Content of a Text Message 1 While viewing the AUX TEXT MESSAGING Page select the desired message box 2 Press the FMS Knob to activate the cursor 3 Turn either FMS Knob to select the desired message 4 Select the VIEW Softkey Or Press the ENT Key Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on View Selected Message c Press the ENT Key 5 To close the text message select the CLOSE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Close Message c Press the ENT Key Mark Selected Message As Read 1 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor seinpa2o0Jd Duruue d AEN Sd5 S2d1V 1614 aouepioay puezey Ed o S D a jeuonippy 2 Turn either FMS Knob to select the desired message 3 Select the MRK READ Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Mark Selected Message As Read c Press the ENT Key The message symbol now indicates the message has been opened su jy unuuy x p
144. ld default ROL Vertical Path Tracking VPTH GPS E NAV Key Navigation VOR Pitch Hold default PIT d LOC TE BC Key Backcourse BC Pitch Hold default PIT GPS Pitch Hold default PIT j APR Key Approach VAPP Glidepath GP 3 LOC Glideslope GS HDG Key Heading Select HDG Pitch Hold default PT amp 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 ui pus selected navigation receiver must have a valid LOC signal before BC Key press activates flight irector xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 9 Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A GARMIN AFCS VERTICAL MODES Vertical Mode Description Control Annunciation Holds the current aircraft pitch attitude may Pitch Hold be used to climb descend to the Selected default PIT Altitude Selected Altitude AFCS armed to capture the altitude displayed in x ALTS Armed the Selected Altitude window Altitude Hold Holds the current Altitude Reference ALT Key AIT nnnnn sr aintains the current aircraft vertical speed Vertical Speed may be used to climb descend to the Sele
145. ling through the TAF text To display the METAR legend on the Weather Data Link CNXT Page select the Hazard Avoidance Procedures LEGEND Softkey when METARs are selected for display Winds Aloft Winds Aloft data shows the forecasted wind speed and direction at the surface and at selected altitudes Altitude can be displayed in 3 000 foot increments up to 42 000 feet MSL Displaying Winds Aloft data Additional Features 1 2 3 4 Annun Alerts Appendix Select the Weather Data Link CNXT Page Select the MORE WX Softkey Select the WIND Softkey Select the desired altitude level SFC surface up to 42 000 feet Select the NEXT or PREV Softkey to cycle through the altitude softkeys The WIND Softkey label changes to reflect the altitude selected To display the Winds Aloft legend on the Weather Data Link CNXT Page select the LEGEND Softkey when Winds Aloft is selected for display Index 56 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN PIREPs Pilot Weather Reports PIREPs describe in flight weather encountered by pilots A PIREP may contain unforecast adverse weather conditions such as low in flight visibility icing conditions wind shear turbulence and type of aircraft flown PIREPs are issued as either Routine UA or Urgent UUA Displaying PIREP text 1 2 3 4 5 6 1 Select the Weather Data Link CNXT Page Sele
146. ll available pilot profiles in use Delete a Displayed if the maximum number for pilot x profile before importing another profiles has been reached a Pilot profile import failed Displayed if the importing operation fails for any other reason Pilot profile import succeeded Displayed if the importing operation succeeds H E Overwrite existing file Displayed if the filename matches the name of an E existing file on the SD card Pilot profile export failed Displayed if the export operation fails ze Pilot profile export succeeded Displayed if the export operation succeeds a gt 5 3 2 x xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 13 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Features Appendix Index Annunciations amp Alerts 132 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN 190 00929 04 Rev A GARMI N LLL Appendix APPENDIX sjueuinisu iui PFD SOFTKEY MAP optional non A npnnunn n oipny uddx U105 AEN CDI NAV1 S2dV CDI GPS ACN Sd5 Top Level PFD Softkeys optional p rsnununnnnntntonton optional optional optional optional optional optional TOPO Buruue d BUTE ma
147. mall 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 airport waypoints to the aircraft s current position Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key ENTER AN AIRWAY IN A FLIGHT PLAN 28 1 2 3 4 5 6 7 Press the FPL Key on the Control Unit 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 Turn the small FMS Knob one click clockwise and select the LD AIRWY Softkey or press the MENU Key and select Load Airway required on the PFD 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
148. n the GMC 710 The GMC 710 is unavailable GMC MANIFEST GMC software mismatch Communication halted The GMC 710 has incorrect software installed The system should be serviced GMC KEYSTK GMC key name Key is stuck A key is stuck on the GMC 710 bezel Attempt to free the stuck key by pressing it several times The system should be serviced if the problem persists GTS 800 820 825 850 855 8000 MESSAGE ADVISORIES 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 S address does not match both XPDR mode S addresses GTS MANIFEST GTS software mismatch communication halted The GTS has incorrect software installed The system should be serviced GRA 5500 MESSAGE ADVISORIES Message Comments GRA1 CONFIG GRA1 config The GRA and GDU have incompatible error Config service req d configurations GRA1 SERVICE GRA1 needs service Return unit for repair The GRA self test has detected a problem in the unit The system should be serviced GRA1 CAL GRA1 calibration Service req d GRA1 has improper calibration The system should be serviced 124 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alert
149. nd esentations regarding its accuracy ue AC U KWIK Organizations and to the ess AC U KWIK Organizations ies in the isdictions al or nsee tual or alleged inaccurac in the datasets Some ju ed warranties or liability for incident Printed in the U S A A GARMIN Waminps Cautions amp Notes WARNING Navigation and terrain separation must NOT be predicated upon the use of the terrain avoidance feature The terrain avoidance feature is NOT intended to be used as a primary reference for terrain avoidance and does not relieve the pilot from the responsibility of being aware of surroundings during flight The terrain avoidance feature is only to be used as an aid for terrain avoidance Terrain data is obtained from third party sources Garmin is not able to independently verify the accuracy of the terrain data WARNING The displayed minimum safe altitudes MSAs are only advisory in nature and should not be relied upon as 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 74B Air Data Computer or other altimeters in the aircraft GPS altitude should never be used for vertical navigation Always use press
150. netrate the airspace within 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm APR INACTV Approach is not active Special use airspace is within 2 nm of the aircraft position The system notifies the pilot that the loaded approach is not active Activate approach when required SLCT FREQ Select appropriate frequency for approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 126 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Message Comments PTK FAIL Parallel track unavailable bad geometry Bad parallel track geometry PTK FAIL Parallel track unavailable invalid leg type Invalid leg type for parallel offset PTK FAIL Parallel track unavailable past IAF IAF waypoint for parallel offset has been passed UNABLE V WPT Can t reach current vertical waypoint The current vertical waypoint can not be reached within the maximum flight path angle and vertical speed constraints The system aut
151. nob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN PROCEDURES LOAD AND ACTIVATE A DEPARTURE PROCEDURE 1 Press the PROC Key 2 Turn the large FMS Knob to highlight SELECT DEPARTURE 3 Press the ENT Key The cursor is displayed in the DEPARTURE field with a list of available departures 4 Turn the large FMS Knob to highlight the desired departure 5 Press the ENT Key A list of runways may be displayed for the departure If so turn either FMS Knob to select the desired runway 6 Press the ENT Key The cursor is displayed in the TRANSITION field with a list of available transitions 7 Turn the large FMS Knob to highlight the desired transition 8 Press the ENT Key 9 With LOAD highlighted press the ENT Key The departure will be active when the flight plan is active ACTIVATE A DEPARTURE LEG 1 Press the FPL Key to display the active flight plan 2 Press the FMS Knob to activate the cursor 3 Turn the large FMS Knob to highlight the TO waypoint of the desired leg within the departure 4 Select the ACT LEG Softkey A confirmation window showing the selected leg will be displayed 5 With ACTIVATE highlighted press the ENT Key LOAD AN ARRIVAL PROCEDURE 1 Press the
152. oach downgraded Vertical guidance generated by SBAS is unavailable use LNAV only minimums Change HDG reference to TRUE TRUE APR True north approach Displayed after passing the first waypoint of a true north approach when the nav angle is set to AUTO GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A failure has been detected in GPS receiver 1 and or GPS receiver 2 The system should be serviced GPS1 SERVICE GPS1 needs service Return unit for repair GPS2 SERVICE GPS2 needs service Return unit for repair NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced 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 G S1 FAIL G S1 is inoperative G S2 FAIL G S2 is inoperative 116 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B20
153. oceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET offset distance field Turn the small FMS Knob to enter the desired target altitude offset from the selected Direct to Press the ENT Key to highlight Activate or turn the large FMS Knob to highlight the CRS field Turn the small FMS Knob to enter the desired course to the waypoint Press the ENT Key to highlight ACTIVATE Press the ENT again to activate the Direct to ACTIVATE A STORED FLIGHT PLAN 1 2 3 4 5 Press the FPL Key on the Control Unit and turn the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the ACTIVE Softkey The confirmation window is now displayed With OK highlighted press the ENT Key to activate the flight plan To cancel the flight plan activation turn the large FMS Knob to highlight CANCEL and press the ENT Key ACTIVATE A FLIGHT PLAN LEG 1 N 3 From the Active Flight Plan Page press the FMS Knob to activate the cursor and turn the large FMS Knob to highlight the desired waypoint Select the ACT LEG Softkey OR Press the MENU Key select the Activate Leg option from the page menu and press the ENT Key This step must be used when activating a leg from the PFD With Activate highlighted pr
154. ockpit Reference Guide for the Beechcraft 200 B200 Series A GARMIN 190 00929 04 Rev A A GARMIN A Access code 46 74 Activate a flight plan 14 Active Channel 89 Active database 146 Active Navigation Database 146 AC U KWIK 72 ADF 5 6 136 137 Advisory alerts 97 AHRS 119 120 121 123 124 Air Data Computer 98 Airport Directory 72 Airport Signs 69 70 Airways 143 ALT 63 Altitude mode 63 Altitude volume 63 Antenna stabilization 60 Antenna tilt 58 AOPA 72 AOPA Airport Directory 72 AP 99 Attitude amp Heading Reference System 98 Audio panel controls NAV1 NAV2 6 Barometric Altitude Minimums 4 Barometric pressure 137 Bearing line 59 60 C CDI 1 2 6 126 Cell 42 43 Cell mode 43 Channel Presets 90 ChartView 70 71 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Index CLD TOP Softkey 54 Code selection softkeys 5 COM 5 6 D DB Mismatch 144 147 DCLTR Softkey 70 Declutter 133 143 DG Mode 2 Direct to 13 DME 5 6 E Edit a flight plan 32 ESP 94 95 F FD 99 Flight Director 9 Flight path marker 69 FliteCharts 70 71 Frequency Transfer 6 G Gain 59 H HF 5 Horizon heading 69 Horizontal scan 59 Inhibit 68 Inhibit TAWS 68 Inset Map 133 134 IOI 100 101 104 Iridium satellite network 73 74 78 Index 1 su jy unuuy sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu jeuonippy puezey qy6il4
155. oftkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ranges The aircraft symbol provides situational awareness while taxiing Pressing the DCLTR Softkey declutter once removes the taxiway markings and airport identification labels Pressing the DCLTR Softkey twice removes VOR station ID the VOR symbol and intersection names if within the airport plan view Pressing 70 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycl
156. oftkey to remove all Stormscope lightning data from the display SIRIUSXM SATELLITE WEATHER OPTIONAL Displaying SiriusXM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD or XM LTNG Softkey to display the desired weather Select the applicable softkey again to remove weather data from the Navigation Map Page Display METAR and TAF information on the Airport Information Page 1 Turn the large FMS Knob to select the WPT Page Group 2 Turn the small FMS Knob to select the Airport Information Page 3 Select the WX Softkey to display METAR and TAF text METAR and TAF information is updated every 12 minutes Displaying Weather on the Weather Data Link Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Weather Data Link Page 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 43 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN 36114 Buruue d 34614 uepIony s np 01d puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance UJ 4 A GARMIN Select the available softkeys to select the desired SiriusXM weather product Select the LEGEND Softkey to view the legends for the selected products If neces
157. omatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid VNV Unavailable Excessive crosstrack error The current crosstrack exceeds the limit causing vertical deviation to go invalid VNV Unavailable Parallel course selected TRAFFIC FAIL Traffic device has failed A parallel course has been selected causing the vertical deviation to go invalid The system is no longer receiving data from the traffic system The traffic device should be serviced NON WGS84 WPT Do not use GPS for navigation to xxx 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 STRMSCP FAIL Stormscope has failed Stormscope has failed The G1000 system should be serviced 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 127 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij
158. or moves to the REFERENCE WAYPOINTS field With the first waypoint name highlighted use the FMS Knobs to enter the desired waypoint name Waypoints may also be selected as follows a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight plan waypoints b Turn the large FMS Knob to select the desired waypoint Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Planning 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 sjueuinisu iui oipny uddx UI05 AEN Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the RECENT waypoints S2dV AEN Sd5 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 Press the ENT Key The cursor is displayed in the RAD radial fiel
159. ore taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly Displaying Weather on the Weather Radar Page 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Weather Radar Page Select the MODE Softkey If the aircraft is on the ground select the STANDBY Softkey to initiate the one minute warm up period After the warm up is complete the radar will enter the Standby Mode After the aircraft is airborne select the WEATHER Softkey Or If the aircraft is already airborne select the WEATHER or GROUND Softkey The one minute warm up period will be initiated after which the radar will begin transmitting The horizontal scan is initially displayed Turn the Joystick to select the desired range If desired select the VERTICAL Softkey for vertical scanning Adjusting Antenna Tilt Move the Joystick up or down to adjust the tilt of the antenna up or down Monitor the displayed tilt value in the TILT field When scanning vertically a Tilt Line may be displayed to aid in positioning the tilt of the antenna If the Tilt Line is not displayed perform the following steps 1 2 3 58 Press the MENU Key Turn the large FMS Knob to select Show Tilt Line Press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Hazard Avoidance Adjusting Antenna
160. p Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 4 Bujuue d AEN SdD S24 olpny uddX sjuawinysu 106114 JW05 AEN 146114 SeJnpa oJd gt lt E a D El A puezey sainjea4 euolippy syajy unuuy xipuaddy xopu Hazard Avoidance GARMI N Lightning Age Symbol Strike is less than 6 seconds old 4 Nav Com Flight XPDR Audio Instruments AFCS 1 8 2 3 4 5o83 6 E 8 amp 9 2 Additional Features Annun Alerts Strike is between 6 and 60 seconds old Og Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old Select Cell or Strike as the Stormscope Lightning Mode Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight Map Setup Press the ENT Key Turn the small FMS Knob to highlight Weather 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 Press the MENU Key with the Nav
161. perating exclusively in no GPS mode The 2 AHRS is operating exclusively in no GPS mode The system should be serviced AHRS MAG DB AHRS magnetic model database version mismatch The 1 AHRS and 2 AHRS magnetic model database versions do not match 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 119 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN Wijd sainjea4 Jeuonippy d ns xopu Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts A GARMIN Message Comments 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 AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid GRS1 MANIFEST GRS1 software mismatch communication halted The 1 AHRS has incorrect software installed The system should be serviced GRS2 MANIFES
162. red waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key 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 S2dV AEN Sd5 11 R e a D 2 zm E 1 v aouepioay puezey DELETE A USER WAYPOINT soinjeo Jeuonippy 1 Turn the large FMS Knob to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Press the FMS Knob to activate the cursor 4 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 Select the DELETE Softkey 7 The message Would you like to delete the user waypoint is displayed With YES highlighted press the ENT Key syajy unuuy xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 25 Nav Com XPDR Audio Hazard Additional
163. res 2 TheTEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the alphanumeric keys on the MFD Controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by selecting the NUMBERS Softkey Select the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by selecting the SYMBOLS Softkey 3 Press the ENT Key The cursor is now displayed in the MESSAGE field 4 Enter the desired message using any combination of entry methods as described in step 2 5 Press the ENT Key 6 Select the SEND Softkey to send the message immediately or select the SAVE Softkey to save the message in Outbox for sending at a later time Select the CANCEL Softkey to delete the message Predefined Text Messages Time and effort can be saved in typing text messages that are used repeatedly by saving these messages as a predefined message Create a Predefined Text Message 1 While viewing the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu 2 Turn either FMS Knob to select Edit Predefined Messages 3 Press the ENT Key The PREDEFINED MESSSAGES view is now displayed 4 Select the NEW Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Kno
164. result from the documentation even if AOPA or an AOPA aut possibility of such damages User agrees not to by limitation or exclusion of implied warranties o so the above limitations or exclusions may not apply to you AC U KWIK and its related organizations hereafte expressly disclaim all warranties with respect to in this data express or implied including but not li merchantability and fitness for a particular purpose The in AC U KWIK Organizations do not warrant or make any rep eliability or otherwise Licensee agrees not to s maximum extent allowed by law to release and hold harm from any cause of action claims or losses related to any ac information arising out of Garmin s use of the information do not allow the limitation or exclusion of impli consequential damages so th November 2013 aw to release and hold harmless AOPA from any causes of action claims or losses re to any actual or alleged inaccuracies in the inform iability for incidental or consequential dam e above limitations or exclusions may not apply to lice 190 00929 04 Rev A use or inability to use the software or related horized representative has been advised of the sue AOPA and to the maximum extent allowed ated ation Some jurisdictions do not allow the ages collectively AC U KWIK Organizations the AC U KWIK information included mited to the implied warranties of formation is provided as is a
165. s Message Comments GRA1 TEMP GRAT over The system has detected an over temperature temperature condition in GRAT GRA1 MANIFEST GRA1 software mismatch communication halted The GRA has incorrect software installed The system should be serviced MISCELLANEOUS MESSAGE ADVISORIES Message Comments FPL WPT LOCK Flight plan waypoint is locked FPL WPT MOVE Flight plan waypoint moved Upon power up the system detects that a stored flight plan waypoint is locked This occurs when a 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 Or update the waypoint name identifier to reflect the new information The system has detected that a waypoint coordinate has changed due to a new navigation database update Verify that stored flight plans contain correct waypoint locations TIMER EXPIRD Timer has expired 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 flig
166. s Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics wet hail vs rain For example it is not possible to distinguish between wet snow wet hail and rain Radar base reflectivity is sampled at the minimum antenna elevation angle An individual radar site cannot depict high altitude storms at close ranges It has no information about storms directly over the site When zoomed in to a range of 30 nm each square block on the display represents an area of four square kilometers The following may cause abnormalities in displayed radar images Ground clutter Strobes and spurious radar data Sun strobes when the radar antenna points directly at the sun Interference from buildings or mountains which may cause shadows Metallic dust from military aircraft which can cause alterations in radar scans Infrared Satellite Infrared Satellite IR SAT data depicts cloud top temperatures from satellite imagery Brighter cloud top colors indicate cooler temperatures occurring at higher altitudes Displaying Cloud Tops information 1 Select the Weather Data Link CNXT Page 2 Select the IR SAT Softkey To display the Infrared Satellite legend select the LEGEND Softkey when Infrared Satellite data is selected for display Data Link Lightning Lightning data shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has
167. sage Comments NAV1 MANIFEST NAV1 software mismatch communication halted NAV2 MANIFEST NAV2 software mismatch communication halted NAV1 and or NAV2 software mismatch The G1000 system should be serviced COM1 CONFIG COM config error Config service req d COM2 CONFIG COM config error Config service req d COM1 and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced COM1 TEMP COM over temp Reducing transmitter power COM2 TEMP COM 2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair COMI PTT COM1 push to talk key is stuck COM2 PTT COM2 push to talk key is stuck 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 The COM1 and or COM2 external push to talk Switch is stuck in the enable or pressed position Press the PTT switch again to cycle its operation If the problem persists the system should be serviced COM1 RMT XFR COM1 remote transfer key is stuck transfer key is stuck COM2 RMT XFR COM2 remote
168. sage Advisories ssssssss GDL 59 Message Advisories GSR 56 Message Advisories sssssssseeee ne GDL 69A Message Advisories ssssss ne GWX 68 70 Message Advisories GDC 74B 7400 Message Advisories GCU 477 Message Advisories GMC 710 Message Advisories GTS 820 825 850 855 8000 Message Advisories GRA 5500 Message Advisories ssssssssseeennne Miscellaneous Message Advisories Flight Plan Import Export Messages sssssssn Pilot Profile Import Export Messages 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series iii iv Table of Contents GARMI N hi4 17 See NC 133 PFD Softkey Map sssssssseseeennnnnte nennen 133 MED Navigation Page Softkey Map ssssssen 142 Loading Updated Databases 144 INDEX TmTT o Index 1 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Flight Instruments FLIGHT INSTRUMENTS SELECTING THE ALTIMETER BAROMETRIC PRESSURE SETTING Er a E g S 3 o Ei a a Turn the BARO Knob to select the desired setting oipny uddx UI05 AEN SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG 1 Press the PFD Softkey 2 Press the STD BARO Softkey to set standard barometric pressure S2dV CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS AEN Sd5 1
169. sary 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 2 3 Push in the Joystick to display the panning arrow Move the Joystick to place the panning arrow on AIRMETs TFRs METARS SIGMETs PIREPs or AIREPs 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 SiriusXM Weather Products and Symbols Expiration Time Refresh Rate Weather Product Symbol Minutes Minutes Next generation Radar Ea 30 5 U S NEXRAD 10 Canada Cloud Top 60 15 Echo Top nd 30 7 5 SiriusXM Lightning E 30 5 Cell Movement Fa 30 12 SIGMET SIGMETS AIRMETS AIRMET 60 12 44 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Hazard Avoidance Weather Product Symbol x E ibn B Meteorological Aerodrome Report METARS a City Forecast 60 12 Surface Analysis P 90 12 Freezing Levels 120 12
170. sary to return to the desired attitude and or airspeed range Except in the case of high airspeed when maximum force is reached force remains constant up to the maximum engagement limit Above the maximum engagement limit forces are no longer applied There is no maximum engagement related to a high airspeed condition When ESP has been engaged for more than ten seconds cumulative not necessarily consecutive seconds of a 20 second interval the autopilot is automatically engaged with the flight director in Level Mode in the pitch and or roll axis bringing the aircraft into level flight An aural Engaging Autopilot alert is played and the flight director mode annunciation will indicate LVL for vertical and lateral modes The pilot can interrupt ESP by pressing and holding either the Control Wheel Steering CWS or Autopilot Disconnect AP YD DISC TRIM INTRPT switch Upon releasing the CWS or AP YD DISC TRIM INTRPT switch ESP force will again be applied provided aircraft attitude angle of attack and or airspeed are within their respective engagement limits ESP can also be overridden by overpowering the servos mechanical torque limit ESP can be enabled or disabled on the AUX SYSTEM SETUP 2 Page on the MFD To enable or disable ESP 1 Turn the large FMS Knob to select the AUX Page Group 2 Turn the small FMS Knob to select the SYSTEM SETUP 1 Page 3 If necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Pag
171. selected network is removed from the list AEN Sd5 Buruue d 1614 SIRIUSXM RADIO ENTERTAINMENT The XM Radio Page provides information and control of the audio entertainment features of the SiriusXM Satellite Radio Selecting the XM Radio Page 1 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 Select the RADIO Softkey to show the XM Radio Page where audio entertainment is controlled SeJnpa oJ4d aouepioay puezey 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 xipuaddy su jy unuuy s N e 4 Jeuonippy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 89 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 90 A GARMIN Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 2 3 Select the CATGRY Softkey on the XM Radio Page Select the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the
172. small FMS Knob Press the ENT Key Select an Available Channel within the Selected Category 1 2 3 While on the XM Radio Page select the CHNL Softkey Select the CH Softkey to move down through the list in the Channel Box or move up the list with the CH Softkey Or Press the FMS Knob to highlight the channel list and turn the large FMS Knob to scroll through the channels With the desired channel highlighted press the ENT Key Entering a Channel Directly 1 2 3 4 While on the XM Radio Page select the CHNL Softkey Select the DIR CH Softkey The channel number in the Active Channel Box is highlighted Select the numbered softkeys located on the bottom of the display to directly select the desired channel number Press the ENT Key to activate the selected channel Assigning Channel Presets Up to 15 channels from any category can be assigned a preset number 1 2 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 3 4 Select the SET Softkey Select any one of the PS1 PS15 softk
173. small FMS Knob to select IRIDIUM Additional Features Press the ENT Key The cursor has now moved to the phone number entry field Enter the desired number string typically country code area code phone number by selecting the number softkeys on the MFD pressing the numeric keys on the MFD Controller or turning the FMS knobs The GSR 56 may be configured by an authorized repair facility to automatically enter a default county code when the dialing window is displayed To replace the default country code move the cursor to the first furthest left number in the dialing window and enter the desired country code Press the ENT Key OK is highlighted Press the ENT Key The system will begin calling the number To exit the call select the HANGUP Softkey Placing The Cockpit Phone on Hold 1 2 3 Select the HOLD Softkey on the MFD Or Press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Put Current Call On Hold Press the ENT Key Select the HOLD Softkey again to resume the call 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 7 SaJnpa oJd Buruue d AEN Sd5 24V oipny uddx sjueumnansu 16114 swiop AeNn 16114 aouepioay puezey xipuaddy su jy unuuy s N e 4 Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix
174. system should be serviced GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 The GWX 68 may still be usable GWX MANIFEST GWX software mismatch communication halted The GWX 68 has incorrect software installed The system should be serviced WX ALERT Possible severe weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 122 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts GDC 74B 7400 MESSAGE ADVISORIES Message Comments ADC1 ALT EC ADCI altitude error correction is unavailable ADC2 ALT EC ADC altitude error correction is unavailable GDC1 or GDC2 is reporting that the altitude error correction is unavailable ADC1 AS EC ADC1 airspeed error correction is unavailable correction is unavailable ADC2 AS EC ADC2 airspeed error GDC1 or GDC2 is reporting that the airspeed error correction is unavailable ADC1 SERVICE ADC1 needs service Return unit for repair ADC2 SERVICE ADC1 needs service Return unit for repair The GDC1 and or GDC2 self test has detected a problem in the unit The system should be serviced GDC1 MANIFEST GDC1 software mismatch communication halted GDC2 MANIFEST GDC2 software mismatch communication
175. t Es a D El A puezey NOTE METAR information is only displayed within the installed navigation database service area sainjea4 jeuonippy METAR and TAF text are displayed on the WPT Weather Information Page TAF information is displayed in its raw form when it is available Displaying METAR and TAF text 1 On the Weather Data Link CNXT Page select the METAR Softkey 2 Press the RANGE Knob and pan to the desired airport 3 Press the ENT Key The Weather Information Page is shown with METAR and TAF text su jy unuuy x pu ddy x pul 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 55 Hazard Avoidance GARMI N 2e 4 eus I Em 5 53 FE 2g 1 g lt E 3 g 9 4 Fight Planning Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text METAR text must be completely scrolled through before scrolling through the TAF text Press the FMS Knob or the CLR Key to return to the Connext Weather Data Link Page Or Select the Weather Information Page a Turn the large FMS Knob to select the Waypoint Page Group b Select the WX Softkey to select the Weather Information Page Press the FMS Knob to display the cursor Use the FMS Knob to enter the desired airport and press the ENT Key Use the FMS Knob or the ENT Key to scroll through the METAR and TAF text Note that the METAR text must be completely scrolled through before scrol
176. t Planning Blank Page Procedures Hazard Avoidance Bu 52 se oO EE 2 E Appendix Annun Alerts Index 96 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Alerts Window Text Annunciation Window Text Aural Alert UNDERSPEED PROTECT ACTIVE Airspeed is heard once when an altitude not critcal flight director mode is active Airspeed repeats every five seconds when an altitude critical flight director mode is active ADVISORY ANNUNCIATIONS Annunciation Window Text Alerts Window Text AVN FAN 1 FAIL AVN FA 1 FAIL Avionics cooling fan 1 is inoperative AVN FAN 2 FAIL AVN FA 2 FAIL Avionics cooling fan 2 is inoperative PFD 1 FAN FAIL PFD 2 FAN FAIL PFD FA PFD 1 FAN FAIL PFD 1 cooling fan is inoperative FAIL PFD 2 cooling fan is inoperative MFD FAN FAIL MFD FA FAIL MFD cooling fan is inoperative MESSAGE ADVISORY ALERTS Alerts Window Message ESP DEGRADE ESP AOA mode is inoperative ESP DEGRADE ESP IAS mode is inoperative ESP FAIL ESP is inoperative ESP OFF ESP selected off ESP CONFIG ESP config error Config service req d TAWS GEAR FAULT Landing Gear detected in the DOWN position TAWS FLAP FAULT Flaps dete
177. t Passed SKYWATCH System Test Passed TAS System Test OK TAS System Test Passed TCAS System Test Passed TCAS One System Test Passed TCAS Two System Test Passed Played when the optional traffic system passes a pilot initiated self test SKY 497 TAS SKY 899 TAS KTA 870 TAS GTS 800 820 825 TAS GTS 850 TCAS GTS 855 TCAS GTS 8000 TCAS II 106 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Annunciations amp Alerts Voice Alert Traffic Advisory System Test Failed SKYWATCH System Test Failed TAS System Test Fail TAS System Test Failed TCAS System Test Failed TCAS One System Test Failed TCAS Two System Test Failed Description Played when the optional traffic system fails a pilot initiated self test SKY 497 TAS SKY 899 TAS KTA 870 TAS GTS 800 820 825 TAS GTS 850 TCAS GTS 855 TCAS GTS 8000 TCAS II One o clock through Twelve o dock or No Bearing High Low Same Altitude if within 200 feet of own altitude or Altitude not available Intruder bearing GTS 800 820 825 850 855 only Intruder relative altitude GTS 800 820 825 850 855 only D Less than one mile One Mile through Ten Miles or More than ten miles Intruder distance GTS 800 820 825 850 855 only MFD amp PFD MESSAGE ADVISORIES Message lost Reche
178. t applications satelliteservices or by calling 1 866 739 5687 in the United States or 011 913 440 1135 The following information is required to register for Connext Weather services G1000 System ID GSR56 GSR1 Serial Number s Tail Number Serail Airframe Number Country of Registration Aircraft Manufacturer and Aircraft Model 1 Turn the large FMS Knob on the MFD to select the AUX page group 2 Turn the small FMS Knob to select the AUX SYSTEM STATUS Note the System ID and GSR1 Serial Number in the AIRFRAME field Activating Connext Weather Registration After a subscriber account has been established the system must be activated for data link features such as reporting services or Connext Weather Activation is accomplished by entering the required access code This process is only performed when initially setting up the system for Connext services 1 Ensure the aircraft is outside with a clear view of the sky 2 Turn the large FMS Knob to select the MAP Page group 3 Turn the small FMS Knob to select the MAP WEATHER DATA LINK CNXT Page 4 Press the MENU Key If necessary select Display Connext Weather 5 Press ENT Key The CONNEXT REGISTRATION Window is now displayed 6 Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field 46 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Hazard Avoidance
179. t later Abnormal Weather Data Request Status Messages Cancelling Connext Data Request in Progress Select the Weather Data Link CNXT Page 1 2 3 4 5 52 Press the MENU Key With Connext Data Request highlighted press the ENT Key With the CANCEL REQ option highlighted press the ENT Key The REQUEST STATUS window indicates Request Canceled Press the FMS Knob to return to the Weather Data Link CNXT Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN o Hazard avoidance Enabling Automatic Connext Data Requests 1 2 3 4 5 6 Select the Weather Data Link CNXT Page Press the MENU Key With Connext Data Request highlighted press the ENT Key Choose the desired weather coverage options Turn the large FMS Knob to select the UPDATE RATE setting Then turn the small FMS Knob to highlight the desired automatic update frequency OFF 5 Min 10 Min 15 Min 20 Min 25 Min 30 Min 45 Min or 60 Min then press the ENT Key The SEND REQ button is highlighted and a countdown timer is displayed in the REQUEST STATUS based on the currently selected update rate Press the ENT Key to immediately send an immediate Connext Data Request Or Press the FMS Knob to return to the Connext Weather Data Link Page Connext Weather Products Precipitation Precipitation data is not real time The lapsed time between
180. tem Test Passed 106 X TCAS System Test Fail 107 TCAS I System Test Passed 106 XM lightning 134 143 Telephone 74 XM WX weather 44 TEMP COMP 15 XPDR Softkey 5 Terrain 65 67 100 101 103 104 112 134 142 143 Text messaging 79 80 81 83 Tilt line 58 Timer 125 Topographical data 134 142 Traffic 41 62 64 134 142 Traffic Advisory TA 62 106 107 Traffic map page 62 63 64 Transponder 5 138 139 140 141 142 U User Defined Holding Pattern 30 V vertical path guidance 16 Vertical speed guidance 17 Vertical track 106 VNV 13 127 Vspeed 3 W WATCHG 60 Waypoint Selection Submenu 26 Weather Attenuated Color Highlight 60 Weather data link page 43 Weather radar 58 Wi Fi 86 87 89 Wind data 136 Winds Aloft 56 WIND Softkey 56 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series Index Index 3 su jy unuuy sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu jeuonippy puezey qy6il4 U10 AEN Wi x pu ddy Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Annun Alerts Features Appendix Index Index 4 A GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A M p 913 397 8200 f 913 397
181. that require user credentials including a username and password or a redemption or access code or require action such as accepting a user agreement are not supported Control and monitoring of Wi Fi functions are accomplished through the AUX WI FI SETUP Page 1 2 View the Wi Fi Setup Page Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select the AUX WI FI SETUP Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features Set Up a New Wi Fi Connection 1 2 3 4 5 6 1 8 9 10 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 87 Select the AVAIL Softkey on the MFD A list of available networks will be displayed in the AVAILABLE NETWORKS window Signal strength is shown for each network as well as security requirements and whether the network has been saved in the system s memory If necessary select the RESCAN Softkey to have the system scan again for available networks Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Rescan Available Networks c Press the ENT Key Press the FMS Knob to place the cursor in the list of networks Turn either FMS Knob to select the desired network Select the CONNECT Softkey Or a Press the MENU Key to display the Page Menu b Turn ei
182. the ENT Key Turn the large FMS Knob to move between the FULL SCREEN and COLOR SCHEME Options Turn the small FMS Knob to choose between the On and Off Full Screen Options Turn the small FMS Knob to choose between Day Auto and Night Options 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 Press the FMS Knob when finished to remove the Chart Setup Menu AIRPORT DIRECTORY The Aircraft Owners and Pilots Association AOPA or AC U KWIK Airport Directory database offers detailed information regarding services hours of operation lodging options and more for various airports This information is viewed on the WPT Airport Information Page The Airport Directory databases are revised every 56 days The Airport Directory is always available for use after the expiration date Check fly garmin com for the current database n Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A GARMIN Additional Features View Airport Directory Information While viewing the WPT Airport Information Page if necessary select the INFO 1 Softkey to change the softkey label to display INFO 2 Airport Directory information is displayed on the right half of the display SATELLITE TELEPHONE AND DATA LINK SERVICES
183. the aircraft more than 100 yards away from the source of the interference should alleviate the condition Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN aminps Cautions amp Notes NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE When operating the G1000 in DG Free Mode GRS 7800 installations only the heading information used by some system components e g GTS 8000 AFCS and GWX will be different from the heading displayed on the GDU by an amount equal to the difference between the current Magnetic Field Variation Database MV DB value and the MV DB value when DG Free Mode was activated Due to the convergence of isogonic lines this condition is most noticeable at or near the North and South poles NOTE System navigation utilities may not reliably calculate range and bearing information when the aircraft is operating north of 80 North latitude or south of 80 South latitude This may result in the system displaying small gaps in racetrack holding pattern depictions GRS 7800 installations only NOTE The Terrain Awareness and Warning System TAWS may not operate reliably north of 89 North latitude and south of 89 South latitude This is due to limitations present within the Terrain database and the system s ability to process the data representing the affected areas GRS 7800 installations only
184. 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 R e a D 2 o v aouepioay puezey 13 soinjes Jeuonippy CREATE A USER WAYPOINT DEFINED BY LATITUDE amp LONGITUDE 1 Turn the large FMS Knob on the Control Unit to select the WPT page group 2 Turn the small FMS Knob to select the User WPT Information Page 3 Select the NEW Softkey A waypoint is created at the current aircraft position su jy unuuy xipuaddy 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 xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 2 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 1 8 9 A G
185. ther FMS Knob to place the cursor on Connect To Selected Network c Press the ENT Key If the network is secured a window will be displayed in order to enter the necessary passcode Use the FMS Knobs to enter the desired alpha numeric characters Select the CAP LOCK Softkey to enter upper case letters If there is no security associated with the network proceed to step 9 Press the ENT Key OK will be highlighted Press the ENT Key again The SAVE SETTINGS window is now displayed with the cursor highlighting SAVE CONNECTION The selected network can be saved to system memory to make re connection easier at a later time saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu i4 jwiop AeNn 16114 aouepioay puezey xipuaddy su jy unuuy saunjea Jeuonippy xopu Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN To connect the selected network without saving a Turn the large FMS Knob to move the cursor to highlight CONNECT b Press the ENT Key To save and connect the selected network a Press the ENT Key A checkmark is placed in the checkbox and the cursor moves to the airport field b Using the FMS Knobs enter an airport identifier to be associated with the saved network This aids in identifying the network later in the event of duplicate network names c
186. thout saving Press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Stop Editing Predefined Message Press the ENT Key Send a Predefined Text Message 1 2 3 4 While viewing the AUX TEXT MESSAGING Page select the NEW Softkey The TEXT MESSAGE DRAFT Window is now displayed with the cursor in the TO field Enter the desired telephone number or email address Entry can be accomplished through the alphanumeric keys on the MFD Controller or combination of the FMS Knob on the controller and softkeys on the MFD The FMS Knob is used to enter letters and numbers or numbers can be entered from the MFD by selecting the NUMBERS Softkey Select the CAP LOCK Softkey to create upper and lower case alpha characters Special characters can be accessed by selecting the SYMBOLS Softkey Press the ENT Key The cursor is now displayed in the MESSAGE field Select the PREDEFD Softkey The PREDEFINED MESSAGE MENU Window is displayed Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN 6 1 8 Additional Features Press the ENT Key The predefined message text is inserted into the message field If desired the message can be edited by using the FMS Knobs Press the ENT Key Select the SEND Softkey to transmit the message Text Message Boxes Received text messages reside in the Inbox as Read or Unread messages The O
187. ting up the system for Connext services 1 Ensure the aircraft is outside with a clear view of the sky 2 Turn the large FMS Knob to select the MAP Page group 3 Turn the small FMS Knob to select the MAP WEATHER DATA LINK CNXT Page 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 13 Sa1npa oJd Buruue d AEN Sd5 24V oipny udax sjueumansu swop nen aouepioay puezey xopu 36114 16114 xipuaddy su jy unuuy EE Jeuonippy Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 74 4 5 6 7 8 9 A GARMIN Press the MENU Key If necessary select Display Connext Weather Turn the large FMS Knob to hightlight Register With Connext Press the ENT Key The CONNEXT REGISTRATION Window is now displayed Using the FMS Knob enter the access code obtained from Garmin Flight Data Services in the ACCESS CODE field Press the ENT Key REGISTER will now be highlighted Press the ENT Key System registration is complete when REGISTERED is displayed in the STATUS field Disable Enable Iridium Transceiver Iridium telephone and data communications may be turned on or off by performing these simple steps Disable Enable Telephone and Low Speed Data Services 1 2 3 4 5 6 Turn the large FMS Knob on the MFD to s
188. tivate the cursor 4 Turn the large FMS Knob to highlight the desired flight plan 5 Select the INVERT Softkey Invert and activate stored flight plan will be 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 AEN Sd5 R e a D a m E o v COPY A FLIGHT PLAN aouepioay puezey 1 Press the FPL Key on the Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor 4 Turn the large FMS Knob to highlight the flight plan to be copied 5 Select the COPY Softkey A Copy to flight plan 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 Control Unit 2 Turn the small FMS Knob to select the Flight Plan Catalog Page 3 Press the FMS Knob to activate the cursor soinjes Jeuonippy su jy unuuy xipuaddy xopu 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 33 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 4 5 6 A G
189. tures Index 62 Hazard Avoidance GARMI N Traffic Information Service TIS NOTE If the G1000 is configured to use an optional Traffic Advisory System TAS TIS is not available for use NOTE Traffic Information Service TIS is only available when the aircraft is within the service volume of a TIS capable terminal radar site Displaying Traffic on the Traffic Map Page 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Traffic Map Page 3 Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field 5 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 6 Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 EnsureTIS is operating With the Navigation Map displayed select the MAP Softkey 2 Select the TRAFFIC Softkey Traffic will now be displayed on the map Traffic Advisory System TAS or Traffic Collision Avoidance System TCAS I GTS 850 855 only Optional System Self Test 1 Setthe range to 2 6 nm 2 Select the STANDBY Softkey 3 Select the TEST Softkey 4 Self test will take approximately eight seconds to complete When completed successfully
190. tures Index A Additional Features GARMIN a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Draft Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Arranging Text Messages The viewed messages may be listed according to the date time the message was sent or received the type of message read unread sent unsent etc or by message address View Messages Sorted by Message Date Time While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the TIME Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Date Time c Press the ENT Key The sorting selection is indicated at the bottom center of the list window View Messages Sorted by Message Type While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the TYPE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Type c Press the ENT Key The sorting selection is indicated at the bottom center of the list window View Messages Sorted by Address While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the ADDRESS Softkey Or 84 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Additiona
191. tware installed The system should be serviced GEA 71 MESSAGE ADVISORIES Message Comments Config service req d GEA1 CONFIG GEA1 config error The GEA1 configuration settings do not match those of backup configuration memory The system should be serviced Config service req d GEA2 CONFIG GEA2 config error The GEA2 configuration settings do not match those of backup configuration memory The system should be serviced 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 117 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij U405 AEN Wil SoJnjeoj Jeuonippy ti PEE xopu Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Additional Features Appendix Index Annunciations amp Alerts A GARMIN Message Comments GEA1 MANIFEST GEA1 software mismatch communication halted The 1 GEA 71 has incorrect software installed The system should be serviced GEA2 MANIFEST GEA2 software mismatch communication halted The 2 GEA 71 has incorrect software installed The system should be serviced GTX 33 33D 33ES 3000 MESSAGE ADVISORIES Message Comments er XPDR1 CONFIG XPDR1 config or Config service req d er XPDR2 CONFIG XPDR2 confi ror Config service req d g The transponder
192. ty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypoint or select a waypoint from the submenu of waypoints and press the ENT Key Repeat step numbers 4 and 5 to enter each additional flight plan waypoint When all waypoints have been entered press the FMS Knob to return to the Flight Plan Catalog Page The new flight plan is now in the list Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN Plght Planning IMPORT A FLIGHT PLAN FROM AN SD CARD sjuaumasu fi 1 Insert the SD card containing the flight plan in the top card slot on the MFD 2 Press the FPL Key on the Control Unit to display the Active Flight Plan Page EE on the MFD ES 3 Turn the small FMS Knob to select the Flight Plan Catalog Page 4 Press the FMS Knob to activate the cursor 5 Turn either FMS Knob to highlight an empty or existing flight plan 6 Select 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
193. u ddy x pul 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 85 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features A GARMIN Mark All Messages As Read 1 2 3 4 While viewing the Inbox on the AUX TEXT MESSAGING Page press the MENU Key to display the Page Menu Turn either FMS Knob to place the cursor on Mark All New Messages As Read Press the ENT Key A confirmation window is displayed With cursor highlighting YES press the ENT Key The message symbols now indicate all the message have been opened Delete a Message 1 2 3 While viewing the Inbox on the AUX TEXT MESSAGING Page press the FMS Knob to activate the cursor Turn either FMS Knob to select the desired message Select the DELETE Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Delete Selected Message Press the ENT Key WI FI CONNECTIONS 86 The system can connect to a IEEE 802 11g compatible network provided the aircraft is on the ground and located within range of the network The system is capable of WEP64 WEP128 WPA PSK and WPA2 PSK encryption formats WPA Enterprise and WPA2 Enterprise are not supported Connections that require web proxies captive portals or other elements
194. uide for the Beechcraft 200 B200 Series 109 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN Wijd SoJnjeoj Jeuonippy em DEM xopul Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts A GARMIN Message Comments MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists 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 PFD2 DB ERR PFD2 terrain database missing The terrain database is present on another LRU but is missing on the specified LRU MFD1 DB ERR MFD1 obstacle database error exists PFD1 DB ERR PFD1 obstacle database error exists database error exists PFD2 DB ERR PFD2 obstacle 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
195. uonippy xipuaddy xopu 1i U10 AEN 16114 Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning DEPT Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance A GARMIN Weather Request Status Message Description Inva lid Coverage Area No Connext Subscription The weather data request coverage area does not contain at least one of the following a waypoint a flight plan or a flight plan destination Verify at least one of the coverage options is enabled and contains required criteria then re send the data request The system is not be currently subscribed to the Garmin Connext Weather service or the access code is incorrect Verify the access code Contact Garmin Connext at 1 866 739 5687 in the United States or 913 440 1135 for assistance Reduce Request Area The weather data request area exceeds size limits Reduce weather coverage area and re send data request Req D uest Cancelled The user has cancelled a weather data request Req Red R D q uested area too large uce coverage area uest Failed Try Again The size of the weather data request has exceeded limits Reduce the size of the coverage area and try the weather data request again The weather data request timed out Re send data request Tran sfer Preempted The data link is busy Retry reques
196. ure 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 Do not rely solely upon the display of traffic information for collision avoidance maneuvering The traffic display does not provide collision avoidance resolution advisories and does not under any circumstances or conditions relieve the pilot s responsibility to see and avoid other aircraft 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series A Warnings Cautions amp Notes GARMIN WARNING Do not rely solely upon the display of traffic information to accurately depict all of the traffic within range of the aircraft Due to lack of equipment poor signal reception and or inaccurate information from aircraft or ground stations traffic may be present that is not represented on the display WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather
197. utbox contains Sent and Unsent text messages Saved messages that are meant to be sent later are stored as Drafts Each text message box may be viewed separately or together in any combination Show Inbox Messages While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the INBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Inbox Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Show Outbox Messages While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the OUTBOX Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Show Outbox Messages c Press the ENT Key The message box selected for viewing is indicated at the bottom left of the list window Show Draft Messages While viewing the AUX TEXT MESSAGING Page select the ARRANGE Softkey then select the DRAFTS Softkey Or 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 83 sye yjunuuy sainjea4 enuepioAy sainpa0ld Duiuue d AEN SdD S24V oipny uddx sjueumasu Jeuonippy paezey Wo gt AeN xipuaddy xopu fila 14614 Flight Instruments Fight Nav Com Procedures Planning GPS Nav AFCS XPDR Audio Hazard Avoidance Additional Appendix Annun Alerts Fea
198. utopilot during flight will cause the autopilots automatic trim to run resulting in an out of trim condition or cause the trim to hit the stop if the action is prolonged In this case larger than anticipated control forces are required after the autopilot is disengaged The following steps should be added to the preflight check Additional Hazard Features Avoidance Annun Alerts 1 Check for proper autopilot operation and ensure the autopilot can be overpowered Appendix 2 Note the forces required to overpower the autopilot servo clutches Index 12 Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 190 00929 04 Rev A A GARMIN GPS NAVIGATION DIRECT TO NAVIGATION Direct to Navigation from the MFD 1 Press the Direct to SJ Key on the Control Unit 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 small FMS Knob to select MSL or AGL 9 Press the ENT Key The cursor is now flashing in th
199. y to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range 190 00929 04 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 200 B200 Series 65 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN 36114 Buruue d 16114 uepIony s np 01d puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning DEPT Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance GARMI N Enable Disable Aviation Data 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to select Show or Hide Aviation Data 3 Press the ENT Key Inhibiting Enabling FLTA and PDA Alerting 1 Select the TAWS A Page 2 Select the TAWS INH Softkey to inhibit or enable TAWS A choice dependent on current state Overriding Flaps based FIT Alerting 1 Select the TAWS A Page 2 Select the FLAP OVR Softkey Inhibiting Enabling GPWS Alerting 1 Select the TAWS A Page 2 Select the GPWS INH Softkey to inhibit or enable GPWS alerts choice dependent on current state Inhibiting Enabling GSD Alerting A NOTE Only available during a GSD alert 66 1

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