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Garmin SA01535Wi_D Cockpit Reference Guide

1. 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 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 DD MFD Map Page Alert Type TAWS Page prag Voice Message E Pop Up Alert Annunciation Reduced Required Obstacle PULL UP OBSTACLE PULL UP Obstacle Obstacle Pull Clearance Warning ROC Up Pull Up or SIRE ERU obstade Ahead Pul Up Obstacle Ahead Pull Up Imminent Obstade Impact PULL UP Pa Cla eae niet Obstacle Ahead Pull Up Warning IOI Obstacle Ahead Pull Up or ESSE Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate PULL UP PULL UP Pull Up Warning EDR Reduced Required Terrain Clearance Caution RTC Caution Terrain Caution Terrain or Terrain Ahead Terrain Ahead Imminent Terrain Impact Caution ITI Terrain Ahead Terrain Ahead or Caution Terrain Caution Terrain Reduced Required 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 Caution PDA Excessi
2. AHRS2 SRVC AHRS2 Magnetic field model needs update The 2 AHRS earth magnetic field model is out of date Update magnetic field model when practical GEO LIMITS AHRS1 too far North South no magnetic compass GEO LIMITS AHRS2 too far GRS1 MANIFEST GRS1 software mismatch communication halted North South no magnetic compass The aircraft is outside geographical limits for approved AHRS operation Heading is flagged as invalid The 1 AHRS has incorrect software installed The system should be serviced GRS2 MANIFEST 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 A failure has been detected in the 2 AHRS The system should be serviced AHRS1 CONFIG AHRS1 config error Config service req d AHRS configuration settings do not match those of backup configuration memory The system should be serviced 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 115 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx Sjueuingjsu paezey Wij w09 eN Wij SoJnjeoj Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoi
3. 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 122 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Appendix Message Comments 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 FAILED PATH A data path has failed A data path connected to the GDU or the GIA 63 W has failed MAG VAR 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 becau
4. 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 the aircraft more than 100 yards away from the source of the interference should alleviate the condition NOTE Use of polarized eyewear may cause the flight displays to appear dim or blank NOTE 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A amp GARMIN aminps Cautians amp Notes NOTE System navigation utilities may not reliably calculate range and b
5. Traffic Advisory Off Scale Resolution Advisory RA TCAS II only Potential collision area is within 15 to 35 seconds ENOGO237 4 Resolution Advisory Off Scale TCAS II only Traffic Symbol Description 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 53 AEN SdD S24V oipny uadx sjueumasuj u105 NeN 36114 Buruue d 34614 ERIT Sa1npa oJd puezey su jy unuuy s n e 4 jeuonippy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance 54 A GARMIN 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 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page Select the OPERATE Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field Rotate the Joystick clockwise to display a la
6. E L IL ow p O 1 1 1 1 es D F F F4 r3 v om o Q 5 E oipny uddx UI05 AEN Select the BACK Softkey on this level to return to the top softkey level optional optional ion NEXRAD FM LING BACK optional opti TRAFFIC PROFILE TOPO TERRAIN S2dV F amp F F3 V3 P D D MFD Softkeys ig Level 1 Level 2 Description MAP Enables second level Navigation Map softkeys SoJnpa oJ4d TRAFFIC Displays traffic information on Navigation Map TOPO Displays topographical data e g coastlines terrain rivers lakes and elevation scale on Navigation Map aouepioay puezey 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 SoJnjeej Jeuonippy su jy unuuy STRMSCP Displays Stormscope weather and coverage information on Navigation Map optional feature NEXRAD Displays NEXRAD weather and coverage information on the Navigation Map optional D gt so zi a Ej or xopu PRECIP Displays Connext Weather precipitation on the Navigation Map optional 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 137 Additional Hazard Fight Nav Com Flight Appendix Annun Ale
7. 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 1 FAN FAIL PFD 1 cooling fan is inoperative PFD 2 FAN FAIL PFD FA 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 detected 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 Available with ESP option only 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 93 e2uepioAy seinpa2o0Jd Buruue d AEN Sd5 241V oipny uddx SyueuinJjs
8. soinjes Jeuonippy 11 su jy unuuy 12 13 14 xipuaddy xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 2 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 22 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 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
9. Comments 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 GMC 710 MESSAGE ADVISORIES Message Comments GMC CONFIG GMC Config error Config service req d Error in the configuration of the GMC 710 GMC FAIL GMC is inoperative GMC MANIFEST GMC software mismatch Communication halted A failure has been detected in the GMC 710 The GMC 710 is unavailable 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
10. Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 74 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
11. 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 143 Additional Hazard Fight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix 144 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A GARMIN 190 01344 01 Rev A A GARMIN A Access code 69 Activate a flight plan 14 Active Channel 85 Active database 140 Active Navigation Database 140 AC U KWIK 68 ADF 5 6 131 Advisory alerts 93 AHRS 114 115 116 118 119 142 Air Data Computer 94 Airport Directory 68 Airport Signs 65 66 Airways 137 Alert messages 117 ALT 55 Altitude mode 55 Altitude volume 55 Antenna stabilization 63 Antenna tilt 61 AOPA 68 AP 95 Attitude amp Heading Reference System 94 Audio panel controls NAV1 NAV2 6 Barometric
12. R e a D a zm E 1 v aouepioay puezey soinjes Jeuonippy 10 su jy unuuy CREATING A USER DEFINED HOLD AT THE AIRCRAFT PRESENT POSITION 1 Press the FPL Key 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 xipuaddy xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 2 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index 3 4 5 6 7 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 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 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
13. 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 300 B300 Series 190 01344 01 Rev A GARMIN Flight Planning Or A 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 desired waypoint d Press the ENT Key Or a Turn the small FMS Knob to the left Initially a flight plan waypoint list is displayed b Turn the small FMS Knob to the right to display the USER waypoints Turn the large FMS Knob to select the desired waypoint d Press the ENT Key Press the ENT Key The cursor is displayed in the RAD radial field Enter the desired radial from the refer
14. XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index A Nav Com XPDR Audio Panel GARMIN Without TCAS Il Option 1 2 3 Press the XPDR Softkey If the aircraft is equipped with two transponders press the XPDR1 or XPDR2 Softkey to select the active transponder Press the desired transponder mode softkey STBY ON or ALT SELECTING A COM RADIO Transmit Receive Press the COM1 MIC COM2 MIC or COM3 MIC Key optional COM if installed on the audio panel Receive Only Press the COM1 COM2 or COM3 Key optional COM if installed on the audio panel SELECTING A NAV RADIO 1 2 To begin navigating using a navigation radio press the CDI Softkey on the PFD to select VOR1 LOC1 NAV1 or VOR2 LOC2 NAV2 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 2 3 Press the small tuning knob to select the desired radio for tuning A light blue box highlights the radio frequency to be tuned Turn the respective tuning knobs to enter the desired frequency into the standby frequency field The large knob enters MHz and the small knob enters kHz Press the Frequency Transfer Key to place the frequency into the active frequency field Garmin G1000 Cockpit Reference Guide for the Be
15. is now highlighted Press the ENT Key again to place the call Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 15 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
16. meer BER rm CS C58 Coe GE ORT WERE CT AERIS SD D vv nN n 5D onnn rn n EE zs 3 Ei XPDR1 XPDR2 STBY ON ALT VFR CODE IDENT BACK ALERTS F F3 FX mrmon omg nnn A 2 Select the BACK Softkey to return z to the top level softkeys 37172 303 3103 3E 2E 107 IEee TE sse T sje ss 3 F F3 F4 amp rr v nO mms nm on x H Select the BACK Softkey to return X to the previous level softkeys Transponder Softkeys Index 132 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN 11 Appendix Level 1 Level2 Level 3 Description i XPDR Displays transponder mode selection a 3 softkeys XPDRI Selects the 41 transponder as active 3 F XPDR2 Selects the 2 transponder as active ES STBY Selects Standby Mode transponder does not reply to any interrogations ON Selects Mode A transponder replies to interrogations AIT Selects Mode C Altitude Reporting Mode AEN Sd5 transponder replies to identification and altitude interrogations VFR Automatically enters the VFR code 1200 in the U S A only F CODE Displays transponder code selection B softkeys 0 7 0 7 Use numbers to enter code SoJnpa oJd 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 aouepioay puezey TMR REF Displays Timer Re
17. Clearance Warning RTC or Pull Up PULL or Terrain Ahead Pull Up Terrain Ahead Pull Up Imminent Terrain Impact PULL UP Terrain Ahead Pull Up Warning ITI or Terrain Ahead Pull Up or Terrain Terrain Pull Up Pull Up Reduced Required Obstacle MAMIMIS Obstacle Obstacle Pull Clearance Warning ROC or Up Pull Up or Obstacle Ahead Pull Up Obstacle Ahead Pull Up Imminent Obstacle Impact PULL UP Obstacle Ahead Pull Up Warning IOI or Obstacle Ahead Pull Up or Obstacle Obstacle Pull Up Pull Up Excessive Descent Rate PULL UP whoop whoop Warning EDR PULL UR Pull Up Excessive Closure Rate PULL UP lt whoop gt lt whoop gt Warning ECR Pull Up Reduced Required Terrain TERRAIN CAUTION TERRAIN Caution Terrain Clearance Caution RTC or Caution Terrain or TERRAIN AHEAD Terrain Ahead Terrain head Imminent Terrain Impact TERRAIN TERRAINAHERD Terrain Ahead Terrain Caution ITI or head or CAUTION TERRAIN 8 Caution Terrain Caution Terrain Reduced Required Obstacle TERRAIN cAumioN oBSTAcE Caution Obstacle Clearance Caution ROC or Caution Obstacle or Obstacle Ahead 96 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts VCO all are configurable except Five Hund
18. Displaying Weather on the Weather Radar Page 1 2 3 60 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard Avoidance 4 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 5 Turn the Joystick to select the desired range 6 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 Moni tor 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 1f the Tilt Line is not displayed perform the following steps 1 Press the MENU Key 2 Turn the large FMS Knob to select Show Tilt Line 3 Press the ENT Key Adjusting Antenna Bearing Move the Joystick right or left to adjust the azimuth position of the antenna right or left Monitor the displaye
19. GRA 5500 Changed Garmin Flight Data Services to Garmin Connext Added other GDU 13 06 parameters fool Date of Revision Affected Pages November 2013 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series RR 1 Record ofRevisions GARMIN Blank Page RR 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 1 Synchronizing the Altimeter Barometric Pressure Settings 1 Synchronize CDI oerte tede iet eie ie edi e de e deti 1 Selecting DG Mode GRS 7800 Installations Only 2 Change Navigation Sources ssssssssseeennnnnnnnns 2 Enable Disable OBS Mode While Navigating with GPS sss 2 Generic THM eh eed db desit b Uo BOLA Gabaa dis 2 Configure Vspeed Bugs Individually sss 3 Turn Vspeed Bugs On or Off by Category 3 Set Barometric Radar Altimeter Minimum Descent Altitude 3 Testing the Radar Altimeter ssssssseeennn 4 Displaying Wind Data 4 NAV COM TRANSPONDER AUDIO PANEL 5 ADF Tuning Optional 5 DIME Turilhj enero cinta REIR aves ana NEHRREI NIRE IR 5 Enter a
20. 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 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 Roll 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 Rudder Boost Failure SoJnpa oJd Yaw axis control failure 2 jme me TII 1 00 api mm S2 mc Elevator Mistri
21. 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 APPROACH OR AIRWAY FROM A FLIGHT PLAN s n e 4 aouepioay puezey Jeuonippy su jy unuuy 1 Press the FPL Key on the Control Unit to display the active flight plan Press the FMS Knob to activate the cursor Or x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 29 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Plann
22. 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 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 View the Wi Fi Setup Page 1 2 82 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features Set Up a New Wi Fi Connection 1 2 3 4 5 6 1 8 9 10 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 CO
23. 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 1 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 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 and optional AC U KWIK Airport Directory databases offer detailed information regarding services hours of operation lodging options and more Both Airport Directories are available for downloading at flygarmin com However copy only one of the databases to the Supplemental Data Card T
24. those of backup configuration memory The system should be serviced 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 XPDR1 CONFIG XPDR1 config rror Config service req d XPDR2 CONFIG XPDR2 confi rror Config service req d D g D The transponder configuration settings do not match those of backup configuration memory The system should be serviced GTX1 MANIFEST GTX1 software ismatch communication halted m GTX2 MANIFEST GTX2 software mismatch communication halted The transponder has incorrect software installed The system should be serviced 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 113 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx Sjueuinajsu paezey Wij U405 AEN Wi SoJnjeoj Jeuonippy i PES xopu Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Mn Index Annunciations amp Alerts A GARMIN Message Comments XPDR1 SERVICE XPDR1 needs service Return unit for repair
25. 820 825 TAS GTS 850 TCAS GTS 855 TCAS GTS 8000 TCAS II TCAS II 102 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Amunciations amp Alerts Voice Alert Description Played when the optional traffic system fails a pilot initiated self test Traffic Advisory System Test Failed SKY 497 TAS SKYWATCH System Test Failed SKY 899 TAS Sjueuinijsu ufi oipny uddx U105 AEN TAS System Test Fail KTA 870 TAS TAS System Test Failed GTS 800 820 825 TAS TCAS One System Test Failed GTS 850 855 TCAS x TCAS Two System Test Failed GTS 8000 TCAS II n TCAS System Test Failed TCAS II One o clock through Intruder bearing GTS 800 820 825 850 855 only AEN Sd5 Twelve o clock or No Bearing High Low Same Altitude if Intruder relative altitude GTS 800 820 825 850 855 only within 200 feet of own altitude or Altitude not available Less than one mile Intruder distance GTS 800 820 825 850 855 only One Mile through Ten Miles or More than ten miles Buruue d 164 SoJnpa oJd MFD amp PFD MESSAGE ADVISORIES aouepioay puezey Message Comments DATA LOST Pilot stored data was The pilot profile data was lost System reverts lost Recheck settings to default pilot profile and settings The pilot gt of S2 Se oS vp may reconfigure the MFD
26. Additional Features 76 A GARMIN Viewing a Text Message When Received When viewing MFD pages other than the AUX TEXT 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 K
27. Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN Message Comments SLCT FREQ Select appropriate frequency for approach The system notifies the pilot to load the approach frequency for the appropriate NAV receiver Select the correct frequency for the approach SLCT NAV Select NAV on CDI for approach The system notifies the pilot to set the CDI to the correct NAV receiver Set the CDI to the correct NAV receiver 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 automatically transitions to the next vertical waypoint VNV Unavailable Unsupported leg type in flight plan The lateral flight plan contains a procedure turn vector or other unsupported leg type prior to the active vertical waypoint This prevents vertical guidance to the active vertical waypoint VNV Unavailable Excessive track angle error The current track angle error exceeds the limit causing the vertical deviation to go invalid
28. GARMIN AFCS Sjueuinijsu iui oipny uddx wo gt AeN S24V ACN Sd5 buruue d Wila Blank Page s np Old e uepioAy piezed so1njea4 Jeuonippy Syo v unuuy xipuaddy xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 12 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 the 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
29. Knob to display the Cell Strike window Turn either FMS Knob to select Cell or Strike Press the ENT Key Push the FMS Knob to return to the Navigation Map Page Clear Stormscope Lightning Data from the Navigation Map Page 1 2 1 2 Press the MENU Key with the Navigation Map Page displayed Turn either FMS Knob to highlight the Clear Stormscope Lightning field and press the ENT Key NOTE If heading input is lost strikes and or cells must be cleared manually after the execution of each turn This is to ensure that the strike and or cell positions are depicted accurately in relation to the nose of the aircraft Stormscope Page Turn the large FMS Knob until the Map Page group is selected Turn the small FMS Knob select the Stormscope Page Change the Stormscope Lightning Mode Between Cell and Strike 1 2 Select the Stormscope Page 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 2 Select the Stormscope Page Select the VIEW Softkey The 360 and ARC Softke
30. Map optional Displays Connext Weather lightning information on Inset Map optional Displays METAR flags on airport symbols shown on the Inset Map optional 190 01344 01 Rev A A GARMIN 33 Appendix optional T kFsrm mn mn n n n n sjueuinisu iui oc anez Lanrs1 AHRS2 l lI Back _ aLeRTs F A V3 V3 V3 V3 V3 V3 V3 VN Select the BACK Softkey to return to the top level softkeys oipny uddx U105 AEN Sensor Softkeys S2dV Level 1 Level 2 Description SENSOR Displays softkeys for selecting the 1 and 42 AHRS and Air Data Computers 3 ADCI Selects the 41 Air Data Computer 5 ADC2 Selects the 2 Air Data Computer AHRSI Selects the 1 AHRS AHRS2 Selects the 2 AHRS senjee4 eouepioAy seinpa2o0Jd Buruue d paezey 1ufi4 Jeuonippy su jy unuuy gt 5 o a E xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 129 Appendix GA N A S nmn p pnmnnnunnun o9 Flight Instruments f Dems SEES Se LA LA F3 n ps m n mo zu x B Select the BACK Softkey to return to the top level softkeys BRGI GPS IBRG2 GPS wn z BRG1 ADF BRG1 OFF Ases F3 V3 V3 V3 3 v n9 m mx mnn onm DG FREE pe SLAVE HDG HDG HDG SYNC TRK SYNC BACK ALERTS F3 A V3 P3 nns nmn mns n o n onm W hh Oe COSC ee RS Ca a a a a __ Dern j eme poems oc Dc J
31. Minutes Minutes Radar Precipitation ca 30 U S Canada 3 PRECIP Europe 15 Infrared Satellite R SAT P i Datalink Lightning E5 DL LTNG 30 Continuous SIGMETS AIRMETs SIGMET SIG AIR AIRMET 9n oO Meteorological Aerodrome Report 90 owns METARs Winds Aloft WIND 60 Continuous Pilot Weather Report Lj PIREPs 90 Continuous Temporary Flight RSSU GG no product image 60 Continuous TFRs AAAren no product image 60 Continuous TAFs The composit e between 3 and ib minutes to provide new data 44 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series recipitation image is updated every 3 minutes but individual radar sites may take 190 01344 01 Rev A A GARMIN Setting Up and Customizing the Connext Weather Data Link Page 1 2 3 4 5 6 7 8 Hazard Avoidance Select the Connext Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Turn the small FMS Knob to select Product Group 1 or Product Group 2 and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to scroll through options for each product ON OFF range settings etc Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Connext Weather Data Link Page with the changed settings On aircraft e
32. PANEL ADF TUNING OPTIONAL Tune the ADF using the remote ADF control head DME TUNING 1 Press the DME Softkey 2 Turn the large FMS to select the DME source field 3 Turn the small FMS Knob to select the desired Nav radio 4 Press the ENT Key to complete the selection ENTER A TRANSPONDER CODE 1 Press the XPDR Softkey XPDR TFC if the TCAS II option is available 2 Ifthe aircraft is equipped with two transponders press the XPDR1 or XPDR2 Softkey to select the active transponder If these softkeys are not present proceed to step 3 3 Press the CODE Softkey to display the transponder code selection softkeys for digit entry 4 Press the digit softkeys to enter the code in the code field When entering the code the next key in sequence must be pressed within 10 seconds or the entry is cancelled and restored to the previous code Five seconds after the fourth digit has been entered the transponder code becomes active SELECT TRANSPONDER MODE With TCAS Il Option 1 Press the XPDR TFC Softkey 2 Press the MODE Softkey to display the transponder mode selection softkeys 3 Press the desired transponder mode softkey STBY ON or ALT 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 5 sye yjunuuy sainjea4 eouepioAy sainpad0ld Buruuejd AEN Sd5 S24V oipny YddX sjueumansu Jeuonippy paezey W0 gt AeN xipuaddy xopu fila 1614 Flight Instruments Nav Com
33. 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 7 Turn the large FMS Knob on the MFD to select the AUX page group Turn the small FMS Knob to select the AUX REPORTS STATUS or AUX WI FI SETUP Page If necessary select the REPORTS Softkey The AUX REPORT STATUS Page is now displayed 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 FM
34. Reducing transmitter power COM2 TEMP COM2 over temp Reducing transmitter power The system has detected an over temperature condition in COM1 and or COM2 The transmitter is operating at reduced power If the problem persists the system should be serviced 110 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Amunciations amp Alerts Message Comments COM1 SERVICE COM needs service Return unit for repair COM2 SERVICE COM2 needs service Return unit for repair COM1 PTT COM1 push to talk The COM1 and or COM external push to talk sjueuinijsu ufi 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 oipny uddx U105 AEN key is stuck Switch is stuck in the enable or pressed position COM2 PTT COM2 push to talk Press the PTT switch again to cycle its operation a key is stuck If the problem persists the system should be serviced COM1 RMT XFR COM1 remote The COM1 and or COM2 transfer switch is stuck 3 transfer key is stuck in the enabled or pressed position Press i COM2 RMT XFR COM2 remote the transfer switch again to cycle its operation transfer key is stuck If the problem persists the system should be E serviced gE RAIM UNAVAIL RAIM is GPS satellite coverage is insufficient to perform
35. The 1 transponder should be serviced when possible XPDR2 SERVICE XPDR2 needs service Return unit for repair The 2 transponder should be serviced when possible XPDR1 FAIL XPDRT 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 to transmit ADS B messages XPDR2 ADS B FAIL XPDR2 unable to transmit ADS B messages ADS B is inoperative Other transponder functions may be available Transponder should be serviced when possible GRS 77 7800 MESSAGE ADVISORIES Message Comments AHRS1 TAS AHRS1 not receiving valid airspeed The 1 AHRS is not receiving true airspeed from the air data computer The AHRS relies on GPS information to augment the lack of airspeed The system should be serviced 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 servic
36. Transponder Code sss 5 Select Transponder Mode ssssssseeeennennnnnns 5 Selecting a COM Radio 6 Selecting a NAV Radio 6 NAV COM Tunilig dete ee dun eae eU ede ebbe de eda 6 Intercom oet e io en igtur dti dra 7 Passenger Address PA System 7 Clearance Recorder and Player 7 AUTOMATIC FLIGHT CONTROL SYSTEM s 9 Flight Director Activation ssssssnnnnnnnnnnes 9 Vertical Modes sess 0 Lateral Modes t ta e te t ccc lo a e bct 1 GPS NAVIGATION ttt ec let baci rtt 3 Direct to Navigation ssssssseseeen enne 3 Activate a Stored Flight Plan 4 Activate a Flight Plan Leg 4 Stop Navigating a Flight Plan 5 Vertical Navigation VNAV sssseseeen nnne 5 FLIGHT PLANNIN G niiina 7 Weight Planning oit maire rema aid a 7 Trip Planning nnne 7 Create a User Waypoint Defined by Latitude amp Longitude 9 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Table of Contents GARMI N Create a User Waypoint Defined by Radials from Other Waypoints 20 Create a User Waypoint Defined by a Radial amp Distance from Another Waypoint 22 Delete a User Waypoint Create a Flight Plan Import a Flight Plan from an SD Card Insert a Waypoint in the Active Flight Plan 25 Enter an Airway in a Flight Plan Invert An Active Fl
37. 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 pressure altitude displayed by the G1000 PFD or other pressure altimeters in aircraft WARNING Do not use outdated database information Databases used in the G1000 system must be updated regularly in order to ensure that the information remains current Pilots using any outdated database do so entirely at their own risk WARNING Do not use basemap land and water data information for primary navigation Basemap data is intended only to supplement other approved navigation data sources and should be considered as an aid to enhance situational awareness WARNING 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A Warnings Cautions amp Notes GARMIN e e o 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 an
38. ates F3 V3 A nm nmn on on n on p gt PATHWAY SYN TERR HRZN HDG APTSIGNS BACK ALERTS F3 V3 A nx 05 p mn 5 o A n onm PFD Configuration Softkeys GPS Nav Fight Planning Procedures Hazard Avoidance Level 1 Level2 Level 3 Description PFD Displays second level softkeys for additional PFD configurations Additional Features SYN VIS Displays the softkeys for enabling or disabling Synthetic Vision features PATHWAY Displays rectangular boxes representing the horizontal and vertical flight path of the active flight plan SYN TERR Enables synthetic terrain depiction Annun Alerts Appendix HRZN HDG Displays compass heading along the Zero Pitch line Index 130 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN 1 Appendix Level 1 Level2 Level 3 Description Ssjueuinijsu 1i APTSIGNS 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 DFLTS Resets PFD to default settings includ ing changing units to standard oipny uddx U105 AEN S2dV WIND Displays softkeys to select wind data parameters OPTN 1 Wind direction arrow and speed OPTN 2 Wind direction arrow with digital direction and speed AEN Sd5 OPTN 3 Longitudinal and lateral components az OFF Informat
39. 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 25 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 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 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 t
40. ess AC U KWIK Organi or alleged inacc m ua n ies or liability for incidenta ot apply to licensee 190 01344 01 Rev A ively AC U ganizations cluded in this ied warranties of me ovided as is a g its accuracy nd to the m zations from a uracies in the information arising the datasets Some jurisdictions do not allow the or consequential damages chantability AC U KWIK eliability or aximum extent ny cause of n d 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
41. 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 FPL WPT MOVE Flight plan waypoint moved 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 120 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message Comments 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 flight plans are correct and up to date DB CHANGE Database changed Verify stored airways This occurs when a stored flight plan contains an airway that is no longer consistent with the navigation database This alert is issued only after an navigation database update Verify use
42. not available from FAF to MAP Receiver Autonomous Integrity Monitoring RAIM 2 waypoints from the FAF to the MAP waypoints LOI GPS integrity lost Crosscheck GPS integrity is insufficient for the current phase with other NAVS of flight GPS NAV LOST Loss of GPS Loss of GPS navigation due to insufficient navigation Insufficient satellites satellites GPS NAV LOST Loss of GPS navigation Position error GPS NAV LOST Loss of GPS navigation GPS fail ABORT APR Loss of GPS navigation Abort approach APR DWNGRADE Approach Vertical guidance generated by SBAS is aouepioay puezey Loss of GPS navigation due to position error T o D oO v Jeuonippy Loss of GPS navigation due to GPS failure Abort approach due to loss of GPS navigation downgraded unavailable use LNAV only minimums d TRUE APR True north approach Displayed after passing the first waypoint of a B Change HDG reference to TRUE true north approach when the nav angle is set to AUTO xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 111 Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix UR Index Annunciations amp Alerts A GARMIN Message Comments GPS1 FAIL GPS1 is inoperative GPS2 FAIL GPS2 is inoperative A f
43. 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 10 11 12 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 35 AEN SdD S24V oipny uadx sjueumasuj u105 AeN fila Buruue d 1614 SoJnpa oJd su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Procedures GARMI N ACTIVATE A VECTOR TO FINAL APPROACH FIX 1 Press the PROC Key 2 Turn the large FMS Knob to highlight ACTIVATE VECTOR TO FINAL 3 Press the ENT Key 4 The final approach course becomes the active leg Flight Instruments Nav Com XPDR Audio 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 GPS Nav AFCS Flight Planning 5 After activating the missed approach procedure and the CDI has changed to TERM mode sensitivity another approa
44. power to the system when loading a database Power interuption during the database loading process could result in main tenance 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 138 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN 33131 Appendix 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 diaplays listed after it When an error message is displayed the problem must be corrected before synchronization can be completed A power cycle is required to restart synchronization when Card Full or Err is shown Error Message Description Canceled Database synchronization has been canceled by removing the bottom SD card in display
45. 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 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 proceed to step 10 Turn the small FMS Knob to select MSL or AGL Press the ENT Key The cursor is placed in the OFFSET 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
46. 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 empty storage location Turn the small FMS Knob to display the Waypoint Information Window Turning it clockwise displays a blank Waypoint Information Window turning it counter clockwise displays the Waypoint Information Window with a waypoint selection submenu allowing selection of active flight plan nearest recent user or airway waypoints Enter the identifier facility or city name of the departure waypo
47. 0 P Pathways 65 66 PIREP 52 PIT 94 Predefined message 77 78 Index 2 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A GARMIN R Register 70 Resolution Advisory 53 ROC 96 100 S Safelaxi amp 66 SBAS 10 34 59 110 111 Sector scan 62 Sensor 94 SiriusXM lightning 128 138 STAB 63 Standby 61 Standby Navigation Database 107 141 Store Flight Plan 30 Stormscope lightning data 39 40 128 Strike 39 Strike mode 40 SVT 65 123 SVT Terrain 65 Synchronization 139 SYNC Status 141 Synthetic Vision System 65 System ID 69 T TA 102 TAF 41 51 TAS 54 55 114 TAWS 57 60 96 99 101 TAWS B 57 58 TCAS Il 5 6 55 56 127 134 135 TCAS System Test Passed 102 103 Telephone 70 Terrain 57 58 96 97 99 100 108 128 137 Text message 76 77 79 Text messaging 75 190 01344 01 Rev A A GARMIN Tilt line 61 Timer 121 Topographical data 128 137 Traffic 39 54 56 128 137 Traffic advisory 54 Traffic Advisory TA 102 103 Traffic map page 54 55 56 Transponder 5 133 134 135 136 V Vertical speed guidance 16 Vertical track 102 VNV 13 122 Vspeed 3 W WATCH 63 Waypoint Selection Submenu 24 Weather Attenuated Color Highlight 63 Weather data link page 41 Weather radar 60 Wi Fi 82 83 84 85 Wind data 131 Winds Aloft 52 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series
48. 00 B300 Series 4 AEN SdD S24V oipny uadx sjueumasuj u105 NeN 36114 Buruue d PULTE ERIT Sa1npa oJd puezey sainjea4 jeuonippy syue yjunuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N 5 6 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 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 box displays Processing and the CANCEL REQ button is highlighted 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 in the background Connext Data Requests typically take between 1 to 3 minutes to complete depending on the size of the selected weather coverage area The G1000 retrieves all available Connext Weather products within the selected coverage area during an initial Connext Data Request regardless of which products Gf any are currently enabled for display On subsequent requests previously retrieved textua
49. 1 Insert the SD card for storing the Pilot Profile into the top card slot on the MFD 2 Usethe FMS Knob to select the AUX SYSTEM SETUP 1 Page 3 Activate the desired Pilot 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 ELECTRONIC STABILITY amp PROTECTION ESP ESP engages when the aircraft exceeds one or more conditions pitch roll Vmo and or Mmo 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 normal flight envelope This is perceived by the pilot as resistance to control movement in the undesired direction when the aircraft approaches a steep attitude or high airspeed As the aircraft deviates further from the normal attitude and or airspeed range continues to increase the force increases up to an established maximum to encourage control movement in the direction necessary to return to the normal 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 con
50. 1 Page Press the FMS Knob momentarily to activate the flashing cursor 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Additional Features 87 Sa1npa 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 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 88 A GARMIN Renaming 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 RENAME in the Pilot Profile Box Press the ENT Key In the Rename Profile window turn the FMS Knob to select the profile to rename Press the ENT Key Use the FMS Knob to enter a new profile name up to 16 characters long and press the ENT Key With RENAME highlighted press the ENT Key To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key
51. 2 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 MFD1 DB ERR MFD1 terrain database error exists PFD1 DB ERR PFD1 terrain database error exists PFD2 DB ERR PFD2 terrain database error exists 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series The MFD and or PFD detected a failure in the terrain database Ensure that the terrain card is properly inserted in display Replace ter
52. 4 Usethe 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 scrolling through the TAF text To display the METAR legend on the Connext Weather Data Link Page select the 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 DispLayinc Winns ALOFT DATA 1 Select the Connext Weather Data Link Page 2 Select the MORE WX Softkey 3 Select the WIND Softkey 4 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 select the LEGEND Softkey when Winds Aloft is selected for display 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 Select the Connext Weather Data Link Page 2 Select the MORE WX Softkey 3 Select the PIREPS Softkey 4 Press the RANGE Knob and pan to the desired weather report A gray c
53. 4 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 79 sye yjunuuy sainjea4 eouepioAy s anp 04d Buruuejd AEN SdD 24V oipny uddx sjueumasu Jeuonippy paezey Wo gt AeN xipuaddy xopu fila 1614 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 80 A GARMIN 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 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 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 ARR
54. 4V oipny uadx sjuoumnasuj u105 NeN fila Buruue d 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N Inhibit TAWS While the TAWS B Page is displayed select the INHIBIT Softkey 1 2 3 Or Press the MENU Key Turn the small FMS Knob to select Inhibit TAWS Press the ENT Key Enable TAWS While the TAWS B Page is displayed select the INHIBIT Softkey 1 2 3 Or While the TAWS B Page is displayed press the MENU Key Turn the small FMS Knob to select Enable TAWS Press the ENT Key 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 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 before taxiing the aircraft to prevent the antenna from bouncing on the bottom stop and possibly causing damage to the radar assembly
55. 5 AEN SELECTING STANDARD BAROMETRIC PRESSURE 29 92 IN HG Push the BARO Knob to select standard pressure S2dV CHANGE ALTIMETER BAROMETRIC PRESSURE SETTING UNITS 1 Press the PFD Softkey to display the second level softkeys 2 Press the ALT UNIT Softkey 3 Press the IN Softkey to display the barometric pressure setting in inches of mercury in Hg Or Press the HPA Softkey to display the barometric pressure setting in hectopascals 4 Press the BACK Softkey to return to the top level softkeys Bujuueld AEN Sd5 164 SeJnpa oJd SYNCHRONIZING THE ALTIMETER BAROMETRIC PRESSURE SETTINGS aouepioay puezey 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 1 Nav Com XPDR Audio Flight Planning Hazard Additional AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index dh Flight Instruments G
56. ANGE Softkey then select the ADDRESS Softkey Or a Press the MENU Key to display the Page Menu b Turn either FMS Knob to place the cursor on Sort By Address Press the ENT Key The sorting selection is indicated at the bottom center of the list window Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN AUdIHiona Peatus Viewing The Content of a Text Message sjueuinisu 1i 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 sainpad0ld Duiuue d AEN Sd5 S24V oipny uddx W614 WO gt AeN aouepioay puezey 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 curso
57. AR information is only displayed within the installed aviation database service area METAR and TAF text are displayed on the Weather Information Page TAF information is displayed in its raw form when it is available DisPLAviNG METAR ann TAF Text 1 On the Connext Weather Data Link 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 4 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 5 Press the FMS Knob or the CLR Key to return to the Connext Weather Data Link Page Or 1 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 5 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index Hazard Avoidance GARMI N 2 Press the FMS Knob to display the cursor 3 Usethe FMS Knob to enter the desired airport and press the ENT Key
58. ARMIN SELECTING DG MODE GRS 7800 INSTALLATIONS ONLY 1 2 3 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 counterclockwise or dockwise e Pressing the HDG SYNC Softkey to sychronize 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 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 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 th
59. Altitude Minimums 3 Barometric pressure 132 Bearing line 61 62 C CDI 1 2 6 122 Cell 39 40 Cell mode 40 Channel Presets 86 ChartView 66 67 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Index Code selection softkeys 5 COM 6 D DB Mismatch 138 Declutter 128 138 Direct to 13 DME 5 6 E Edit a flight plan 30 ESP 89 90 F FD 95 Flight Director 9 Flight path marker 65 FliteCharts 66 67 Frequency Transfer 6 G Gain 62 H HF 6 Horizon heading 65 Horizontal scan 62 Inhibit 60 Inhibit TAWS 60 Inset Map 127 128 IOI 96 97 100 lridium satellite network 69 70 74 J Jeppesen 67 Index 1 su jy unuuy sainjea4 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu jeuonippy puezey qy6il4 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 L Level Mode 90 Lightning 39 40 128 Low speed data 69 70 M Magnetic Field Variation Database 142 143 Map panning 41 Message advisories 103 105 108 114 116 118 119 120 MET 95 METAR 41 Minimums 102 MISCOMP 94 Mistrim 95 Multi Function Display MFD Softkeys 137 MV DB 142 N NAV 6 NAV1 2 6 NAV2 6 Navigation database 15 16 125 NEXRAD 41 128 137 NEXRAD Softkey 49 0 OBS 2 Obstacles 108 110 Overspeed Protection 1
60. C RADAR ALTIMETER MINIMUM DESCENT ALTITUDE 1 Press the TMR REF Softkey 2 Turn the large FMS Knob to highlight the OFF BARO RAD ALT field to the right of MINIMUMS 3 Turn the small FMS Knob clockwise to select BARO or RAD ALT 4 Press the ENT Key 5 Use the small FMS Knob to enter the desired altitude 6 Press the ENT Key 7 To remove the window press the CLR Key or the TMR REF Softkey su jy unuuy x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 3 Flight Instruments GARMI N E TESTING THE RADAR ALTIMETER 1 Select the AUX SYSTEM STATUS Page on the MFD 2 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 HE properly functioning system 3 Selecting the RA TEST Softkey again or exiting the System Status Page cancels the test DISPLAYING WIND DATA 1 Press the PFD Softkey 2 Press the WIND Softkey to display wind data below the Selected Heading 3 Press one of the OPTN softkeys to change how wind data is displayed 4 To remove the Wind Data Window press the OFF Softkey Additional Hazard Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav Index 4 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN __Basitomi pede Panel NAV COM TRANSPONDER AUDIO
61. CLEANERS CONTAINING AMMONIA WILL HARM THE ANTI REFLECTIVE COATING It is very important to clean the lens using a clean lint free cloth and an eyeglass lens cleaner that is specified as safe for anti reflective coatings 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A Warnings Cautions amp Notes GARMIN 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 The data contained in the terrain and obstacle databases comes from government agencies Garmin accurately processes and cross validates the data but cannot guarantee the accuracy and completeness of the data
62. 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 press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 Del
63. Connext Weather Data Link 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 Refresh Rate column in the following table su jy unuuy x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 43 Flight Instruments Nav Com XPDR Audio Flight Planning Additional AFCS GPS Nav Hazard Avoidance Procedures Appendix Annun Alerts Features Index Hazard Avoidance A GARMIN 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 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 Expiration Weather Product Symbol Time Juin Rare 2
64. Deleting a Profile 1 2 3 4 5 6 7 8 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 DELETE in the Pilot Profile Box Press the ENT Key In the Delete Profile window turn the FMS Knob to select the profile to delete Press the ENT Key With DELETE highlighted press the ENT Key To cancel the process use the large FMS Knob to select CANCEL and press the ENT Key Importing a Profile 1 2 3 Insert the SD card containing the Pilot Profile into the top card slot on the MED Use the FMS Knob to select the AUX SYSTEM SETUP 1 Page Press the IMPORT softkey If the correct Pilot Profile file is selected with IMPORT highlighted press the ENT Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features 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
65. E e Customizing the Hazard Displays on the Navigation Map STORMSCOPE Optional ssssss SiriusXM Weather Optional sss Garmin Connext Weather Traffic Avoidance Systems Terrain Awareness amp Warning System sss Airborne Color Weather Radar ssssssse Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN able of Contents ADDITIONAL FEATURES 65 Synthetic VISIOTL esee eR ede cbe e ER ED eR E edi 65 Terminal Procedure Charts sss 66 Airport Directory Satellite Telephone and Data Link Services ssss WI FI Connections nennen SiriusXM Radio Entertainment ee Pilot Profiles Electronic Stability amp Protection ESP ssssssss ANNUNCIATIONS amp ALERTS 93 WARNING Annunciation s ADVISORY Annunciations Message Advisory Alerts Comparator Annunciations ssssseeee ne Reversionary Sensor Annunciations AFCS Alerts ooo oen eut eedem udi denn ene TAWS A Alerts ote fette er ood to det TAWS B Alerts Additional Voice Alerts ssseennen MFD amp PFD Message Advisories sssssss Database Message Advisories GMA 1347D Message Advisories sss GIA 63W
66. G1000 Integrated Flight Deck Cockpit Reference Guide for the Beechcraft 300 B300 Series A GARMIN Copyright 2011 2013 Garmin Ltd or its subsidiaries All rights reserved This manual reflects the operation of System Software version 0985 07 or later for the Beechcraft 300 and B300 Some differences in operation may be observed when comparing the information in this manual to earlier or later software versions co Garmin International Inc 1200 East 151st Street Olathe Kansas 66062 U S A Tel 913 397 8200 Fax 913 397 8282 Garmin AT Inc 2345 Turner Road SE Salem OR 97302 U S A Tel 503 391 3411 Fax 503 364 2138 Garmin Europe Ltd Liberty House Hounsdown Business Park Southampton Hampshire 040 9LR U K Tel 44 0 23 8052 4000 Fax 44 0 23 8052 4004 Aviation Support 44 0 87 0850 1243 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan Tel 886 02 2642 9199 Fax 886 02 2642 9099 f For after hours emergency aircraft on ground AOG technical support for Garmin panel mount and integrated avionics systems please contact Garmin s AOG Hotline at 913 397 0836 Web Site Address www garmin com Except as expressly provided herein no part of this manual may be reproduced copied transmitted disseminated downloaded or stored in any storage medium for any purpose without the express written permission of Garmin Garmin hereby gra
67. GSD VCO 3 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 ge PFD MED MFD Map P Alert Type TAWS Page P Voice Message Br Pop Up Alert Annunciation Reduced Required Terrain PULL UP Terrain Terrain Pull Up Clearance Warning RTC or Pull Up ane EE sin Ahea d PullUp Terrain Ahead Pull Up Imminent Terrain Impact PULL UP Terrain Ahead Pull Up Warning ITI or Terrain Ahead Pull Up or Terrain Terrain Pull Up 2 Pull Up i
68. I system is also set to standby 134 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Appendix Level 1 Level 2 Level 3 Level 4 Description TCAS 190 01344 01 Rev A ON ALT TA ONLY TA RA BACK REL ABS ALT RNG ABOVE 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 softke level Displays the TCAS control softkeys Displays intruder altitude as y altitude relative to own aircraft altitude Displays intruder MSL altitude Displays the altitude display range softkeys Displays non threat traffic from 9900 feet above the aircraft to 2700 feet below the aircraft Typically used during climb phase of flight Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 135 sainjea enuepioAy sainpad0ld Duiuue d AEN Sd5 S24V oipny uddx sjueuinasu paezey Wo gt AeN Jeuonippy sye yjunuuy gt kej o Fi a x x pul 36114 i
69. 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 GARMIN Index Sjueuinijsu 1i oipny uddx wo gt AeN S24V ARN Sd5 buruue d Wila Blank Page s np Old e uepioAy piezed so1njea4 Jeuonippy Syie y unuuy xipuaddy eal 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Index 4 Y GARMIN Garmin International Inc 1200 East 151st Street Olathe KS 66062 U S A p 913 397 8200 f 913 397 8282 Garmin AT Inc _ ae 2345 Turner Road SE Salem OR 97302 U S A p 503 391 3411 f 503 364 213 Garmin Europe Ltd Liberty House Bulls Copse Road Hounsdown Business Park Southampton SO40 9RB U K p 44 0870 8501241 f 44 0870 8501251 Garmin Corporation No 68 Jangshu 2nd Road Shijr Taipei County Taiwan p 886 2 2642 9199 f 886 2 2642 9099 www garmin com 2011 2013 Garmin Ltd or its subsidiaries 190 01344 01 Rev A
70. M 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 Key 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 n 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Outgoing Calls Additional Features Voice calls can be made from the cockpit to the handset in the cabin or to an external phon
71. MANIFEST GTS software mismatch communication halted 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series The GTS has incorrect software installed The system should be serviced 119 aoueploay seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu Wij U105 AEN Wij puezey SoJnjeoj Jeuonippy xipuaddy xopu Hazard Fight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Mon Index Annunciations amp Alerts A GARMIN GRA 5500 MESSAGE ADVISORIES Message GRA1 CONFIG GRA1 config error Config service req d Comments The GRA and GDU have incompatible 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 GRA1 TEMP GRAT over temperature The system has detected an over 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 Upon power up the system detects that a stored flight plan waypoint is
72. MFD and or PFD detected a failure in the airport terrain database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 airport terrain database missing PFD1 DB ERR PFD1 airport terrain database missing PFD2 DB ERR PFD2 airport terrain database missing The airport terrain database is present on another LRU but is missing on the specified LRU 106 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message Comments 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 database optional feature Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 FliteCharts database error exists The MFD and or PFDs detected a failure in the FliteCharts database optional feature Ensure that the data card is properly inserted Replac
73. Message Advisories sssssssssee ne GSD 41 Message Advisories Optional 3 GEA 71 Message Advisories 3 GTX 33 33D 33ES 3000 Message Advisories 3 GRS 77 7800 Message Advisories sssssss 114 GMU 44 Message Advisories ssssssss 6 GDL 59 Message Advisories 6 GSR 56 Message Advisories 7 GDL 69A Message Advisories sss 7 GWX 68 70 Message Advisories 7 GDC 74B 7400 Message Advisories 8 GCU 477 Message Advisories 8 GMC 710 Message Advisories 9 GTS 800 820 825 850 855 8000 Message Advisories ssss 9 GRA 5500 Message Advisories sse Miscellaneous Message Advisories Flight Plan Import Export Messages ssss 24 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series i Table of Contents GARMI N DP MON Se INC 127 PFD Softkey Map sssssssesseenn entente 127 MFD Navigation Page Softkey Map 137 Loading Updated Databases 138 INDEX TT Index 1 iv Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 UI0
74. NING 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 SVT 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 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 65 Sa1npa oJd Buruue d AEN Sd5 24V oipny udax sjueumnansu Wila jwiop AeNn Wila aouepioay puez
75. NNECT Softkey Or a Press the MENU Key to display the Page Menu b Turn either 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 83 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 Additional Features 84 A 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 fi
76. Product Status Icons 4m CYCLONE WARNING The age of the displayed data is shown at the right Description sjueuimasu 1i oipny uddx U105 AEN E 74i AIREP The age of the displayed data is shown at the right PIREP The age of the displayed data is shown at the right Urgent Pireps are displayed in yellow S2dV TURBULENCE The age of the displayed data is shown at the right The FATUE IEEE altitude selection is shown at the bottom ACN Sd5 Rid ICING POTENTIAL The age of the displayed data is shown at the right 6000FT The altitude selection is shown at the bottom Buruuejd 164 GARMIN CONNEXT WEATHER WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions Se1Jnpa oJd gt lt 2 a D El A Weather data are provided when the pilot initiates either a manual or automatic Garmin Connext data request on the Connext Weather Data Link Page on the MFD No weather data is displayed until the first Garmin Connext Weather Data Request is made sainjea4 jeuonippy Accessing Garmin Connext Weather Products 1 Turn the large FMS Knob to select the Map Page Group 2 Turn the small FMS Knob to select the Connext Weather Data Link Page When a weather product is selected for display on the
77. S 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 300 B300 Series 190 01344 01 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 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 7 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 IRIDIU
78. System Setup Page 3 If necessary select the SETUP 2 Softkey to display the AUX SYSTEM SETUP 2 Page 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 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 90 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features Pitch Engagement ESP engages at 20 nose up and 17 nose down Once ESP is engaged it will apply opposing force between 15
79. TRFC MAP a Softkey is displayed when the TCAS II option is installed Pressing the TRFC MAP Softkey displays the Inset Map showing Traffic Map Page gt kej a E OFF Removes Inset Map xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 127 Appendix A GARMIN Flight Instruments DCLTR 3 zs S E WX LGND 3 TRAFFIC 5 TOPO ze TERRAIN STRMSCP s NEXRAD or i PRECIP A XM IING a5 or X DL LING E METAR X Appendix Index 128 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Level 1 Level 2 Description 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 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 Connext Weather precipitation on Inset Map optional Displays SiriusXM lightning information on Inset
80. To activate or deactivate the antenna stabilization select the MODE Softkey 2 Select the STAB ON Softkey to activate antenna stabilization or select the STAB OFF Softkey to deactivate The current stabilization condition is shown in the upper right of the weather radar display sjueuinisu 1i oipny uddx U105 AEN Weather Attenuated Color Highlight WATCH To activate or deactivate the WATCH feature select the WATCH Softkey This feature is only available in the Horizontal Scan Mode S2dV Weather Alert To activate or deactivate Weather Alert select the WX ALRT Softkey Activating and deactivating will also enable or inhibit the alert on the PFD AEN Sd5 Buruue d 1614 Automatic Standby When the weather radar system is in the Weather or Ground Map Mode upon landing the system will automatically switch to Standby Mode SeJnpa oJd gt lt E a D El A sainjea4 jeuonippy su jy unuuy x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 63 Hazard Avoidance GARMI N Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning Blank Page Procedures v I 5 aS E lt x Additional Annun Alerts Features Appendix Index 64 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features ADDITIONAL FEATURES SYNTHETIC VISION A WAR
81. URE 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 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Procedures 33 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 16114 SoeiINpsd01d su jy unuuy sainjea4 aouepioay jeuonippy paezey xipuaddy xopu Additional Hazard Fight N
82. ailure 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 A failure has been detected in the GPS1 and or GPS2 receiver The receiver may still be available The system should be serviced NAV1 SERVICE NAV1 needs service Return unit for repair NAV2 SERVICE NAV2 needs service Return unit for repair 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 A failure has been detected in glideslope receiver 1 and or receiver 2 The system should be serviced G S1 SERVICE G S1 needs service Return unit for repair G S2 SERVICE G S2 needs service Return unit for repair 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 e
83. amp PFDs with preferred settings if desired XTALK ERROR A flight display The MFD and PFDs are not communicating with crosstalk error has occurred each other The system should be serviced PFD1 SERVICE PFD1 needs service Return unit for repair PFD2 SERVICE PFD2 needs The PFD and or MFD self test has detected a service Return unit for repair problem The system should be serviced MFD1 SERVICE MFD1 needs service Return unit for repair xipuaddy xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 103 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 CONFIG 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 con
84. and 50 nose up and between 12 and 50 nose down Maximum opposing force is applied between 25 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 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 91 Bujuueld ACN Sd5 S2dV oipny uddx sjuaumnasu U105 AEN SeJnpa oJd aouepioay su jy unuuy x pu ddy x pul 36114 fila paezey gt a 2 g o A Additional Features GARMIN Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning Blank Page Procedures Hazard Avoidance Bu 52 se oO EE 2 E Appendix Annun Alerts Index 92 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts ANNUNCIATIONS amp ALERTS WARNING ANNUNCIATION Alerts Window Text Annunciation Window Text Aural Alert UNDERSPEED
85. ard Avoidance Additional Features Appendix Annun Alerts Index A Appendix _ GARMIN 9 10 11 12 Remove and reapply power to the system Turn the large FMS Knob to select the AUX Page group on the MFD Turn the small FMS Knob to select the System Status Page Press the Display Database Selection Softkey to show database information for each display MFD1 DB PFD1 DB PFD2 DB Verify the correct database cycle information is shown for each database for each display Loading the Jeppesen Navigation Database as the Active Navigation Database 1 2 3 4 5 6 7 8 9 10 11 140 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 MFD to be updated label of SD card facing left Turn the system ON A prompt is displayed in the upper left corner of the display Press the NO Softkey to proceed to loading the active database A prompt similar to the following is displayed Press the YES Softkey to update the active navigation database After the update completes
86. ault 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 9 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Appendix Annun Alerts Features 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 ALTS Armed the Selected Altitude window Altitude Hold Holds the current Altitude Reference ALT Key AIT nnnnn Fr aintains the current aircraft vertical speed Vertical Speed may be used to climb descend to the Selected VS Key VS nnnn FPM Altitude Flight Level Change Maintains the current aircraft airspeed in IAS Hold AS or Mach
87. av Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Procedures GARMI N 4 5 6 7 8 9 Turn the large FMS Knob to highlight the desired arrival Press the ENT Key A list of transitions is displayed for the selected arrival Turn either FMS Knob to select the desired transition Press the ENT Key A list of runways 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 ACTIVATE highlighted press the ENT Key LOAD AND OR ACTIVATE AN APPROACH PROCEDURE 34 1 2 3 4 5 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 dis
88. 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 Complete being displayed 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 139 aouepioay saunpar0ld Buruue d AEN Sd5 234V oipny udax sjueumnansu puezey i4 JWI05JAeN Wila soinjes Jeuonippy xipuaddy su jy unuuy Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Haz
89. bility of such damages User agrees maximum extent allowed by law to release and hold harm action claims or losses related to any act jurisdictions do not allow the limitation o incidental or consequential damages so the above you 72 exclusion of imp imitations y representations regarding its accuracy reliabili ess AOPA from any causes of ual or alleged inaccuracies in ied warrant ons hereinafter collectively AOPA information included he implied warranties of mation is provided as is ly or any 0 use the tative has d to the f hall AOPA be liable the use or inability t authorized represen not to sue AOPA an the information Some ies or liability for or exclusions may not apply to KWIK O AC U KWIK and its related organizations hereafter collect expressly disclaim all warranties with respect to the AC U KWIK information in data express or implied including but not limited to the imp or a particular purpose The f and fitness e th lowed by ction claim ut of Garm m O O0 O ca eo November 2013 rganizations do not warrant or make an erwise Licensee agrees not to sue AC U KWIK Organizati aw to release and hold ha s or losses related to any act in s use of the information i itation or exclusion of implied warrant the above limitations or exclusions may n information is p y representations regardin ons a
90. ch procedure may be loaded TEMPERATURE COMPENSATED ALTITUDE Procedures When temperature compensated altitude is enabled for the loaded approach the altitudes associated with the approach waypoints are displayed in slanted text S ES N I HB q 021 5 7NM HABUK iaf 5 7NM By 1 261 EN FALUR 61 EI HE CEGIX fof 59N CEGIX faf 351 59MM SET RW35R map 35T 5 1 NH RW35R map F 5 1NM 6368FT 348 5NM 6368FT 6368FT e 5NM MOGAL mahp MOGAL mahp HOLD F G NM HOLD 168 6 0NM E Altitudes Displayed Without Altitudes Displayed With Temperature Compensation Temperature Compensation Appendix Index 36 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Enable 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 Procedures 4 Use the small FMS Knob to select the temperature at the airport 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 Disable Temperature Compensated Altitude 1 From the Active Flight Plan Page press the MENU Key The Page Menu is disp
91. cted products If necessary turn either FMS Knob to scroll through the list Press the small FMS Knob or the ENT Key to return to the map Map Panning Information Weather Data Link Page 1 Push in the Joystick to display the panning arrow 2 Move the Joystick to place the panning arrow on AIRMETs TFRs METARS SIGMETs PIREPs or AIREPs 3 Press the ENT Key to display pertinent information for the selected product Note that pressing the ENT Key when panning over an AIRMET or a SIGMET displays an information box that shows the text of the report 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 4 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN fila Buruue d 34614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy x pu ddy x pul Flight Instruments Nav Com XPDR Audio Flight Planning J Additional AFCS GPS Nav P Procedures v 2 5 a E lt x Appendix Annun Alerts Features Index Hazard Avoidance A GARMIN 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 Weather Products and Symbols Wx Product Status Icons Description US 3m CN Bm f NEXRAD Availabl
92. d 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 following 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 6 AEN SdD S24V oipny uddx sjueumasuj u105 NeN 36114 Buruue d 34614 aueplony saunpar0ld puezey sainjea4 jeuonippy su jy 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 62 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 WARNING Changing the gain in Weather Mode will cause precipitation intensity to be displayed a
93. d because a terrain database of sufficient resolution 9 arc second or better is not currently installed FLIGHT PLAN IMPORT EXPORT MESSAGES In some circumstances some messages may appear in conjunction with others Flight Plan Import Export Results Flight plan successfully imported A flight plan file stored on the SD card was successfully imported as a stored flight plan Description File contained user waypoints only User waypoints imported successfully No stored flight plan data was modified The file stored on the SD card did not contain a flight plan only 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 124 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Flight Plan Import Export Results Flight plan import failed Description Flight plan data was not successfully imported from the SD card Flight plan partially imported Some flight plan waypoints were successfully imported from the SD card however others had errors and were not imported A partial stored flight plan now exists in the system File contained user waypoints only The file stored on the SD card did n
94. d by the system outside air temperature R e a D 2 S 1 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 xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 19 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 6 7 8 9 A GARMIN 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 LAT LON latitude and longitude Press
95. d 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 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 t
96. dance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix mee Index Annunciations amp Alerts A GARMIN Message Comments 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 GMU 44 MESSAGE ADVISORIES Message Comments HDG FAULT AHRS1 magnetometer fault has occurred A fault has occurred in the 1 GMU 44 Heading is flagged as invalid The AHRS uses GPS for backup mode operation The system should be serviced HDG 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 GDL59 CONFIG GDL 59 config error Config service req d Comments GDL 59 configuration settings d
97. databases required for TAWS in the specified PFD or MFD is missing or invalid 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 108 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message Comments 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 syste should be serviced m 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 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 poss
98. 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 section for more details Engaging autopilot The ESP system is engaging the autopilot See the AFCS section for more details e 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 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 Traffic Advisory System Test 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 TCAS 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
99. dition 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 89 saunpar0ld Buruue d AEN Sd5 24V oipny udax sjueumnansu 16114 Jwiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xopu Fight Nav Com Flight Planning GPS Nav AFCS XPDR Audio Instruments Procedures Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features GARMI N 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 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
100. e data card If problem persists the system should be serviced MFD1 DB ERR MFD1 Airport Directory database error exists 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 DB MISMATCH Standby Navigation database mismatch 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 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 107 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN fij sainjea4 Jeuonippy xipuaddy xopu Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instr
101. e desired time then press the ENT Key The UP DOWN field is now highlighted Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Flight instruments 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 EL a ga c ERG o gt a a oipny uddx UI05 AEN 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 Softkey Buruue g AEN Sd5 S24V 1614 SeJnpa oJd TURN VSPEED BUGS ON OR OFF BY CATEGORY 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 aouepioay puezey soinjes Jeuonippy SET BAROMETRI
102. e for the US and Canada The age of the displayed data for each is shown at the right ul 3 2m ECHO TOP The age of the displayed data is shown at the right Not displayed when CLOUD TOP is displayed CLOUD TOP The age of the displayed data is shown at the right Not displayed when ECHO TOP is displayed QJ 3 XM LIGHTNING The age of the displayed data is shown at the right N 3 CELL MOVEMENT The age of the displayed data is shown at the right SIGMET 2m AIRMET 5m SIGMET amp AIRMET The age of the displayed data for each is shown at the right TY us 8m CN 8m METAR Available for the US and Canada The age of the displayed data for each is shown at the right SURFACE ANALYSIS with CITY FORECAST The upper symbol depicts Surface Analysis The lower symbol depicts City Forecast The age of the displayed data for each is shown at the right The selected forecast period is shown at the bottom FREEZING LEVEL The age of the displayed data is shown at the right us Em CN 12m 3000FT WINDS ALOFT Available for the US and Canada The age of the displayed data for each is shown at the right The altitude selection is shown at the bottom 3m COUNTY WARNING The age of the displayed data is shown at the right 42 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN o Hazard avoidance Wx
103. e the cursor Or Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Flight Planning 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 2 Turn the large FMS Knob to highlight the waypoint to be deleted 3 Press the CLR Key to display a REMOVE Wpt Name confirmation window oipny uddx syueumasu U105 AEN 2461 4 S2dV 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 5 Once all changes have been made press the FMS Knob to remove the Cursor ACN Sd5 INVERT AND ACTIVATE A STORED FLIGHT PLAN zu gt EI E ia 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 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 9 uepioAy SoJnpa20Jd paezey soinjeo Jeuonippy COPY A FLIGHT PLAN 1 Pre
104. e through the Iridium Satellite Network Make a Call to the Cabin 1 Press the TEL Key on the appropriate audio panel 2 Select the DIAL Softkey on the MFD 3 Press the ENT Key The cursor will move from CABIN to OK 4 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 Press the TEL Key on the appropriate audio panel 2 Select the DIAL Softkey on the MFD 3 Turn the small FMS Knob to select IRIDIUM 4 Press the ENT Key The cursor has now moved to the phone number entry field 5 Enter the desired telephone number country code first by selecting the number softkeys on the MFD or by pressing the numeric keys on the MFD Control Unit 6 Press the ENT Key OK is highlighted 7 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 Select the HOLD Softkey on the MFD Or 1 Press the MENU Key to display the Page Menu 2 Turn either FMS Knob to place the cursor on Put Current Call On Hold 3 Press the ENT Key Select the HOLD Softkey again to resume the call 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 73 saunpar0dd Buruue d AEN Sd5 24V oipny uddx sjueumnansu i4 JWI05JNeN Wila aouepioay puezey xipuaddy su jy unuuy s N e 4 Jeuonippy xopu
105. ear ing 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 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series Warnings Cautions amp Notes GARMIN Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Recerd of Revisions Change Summary 190 01344 00 RevA Initial release Rev B Removed reference to TCAS II pitch attitude cue 190 01344 01 Added User Defined Holds Removed Reports Page Added temperature compensated altitude Added DG Mode Added Pilot Profiles Added GRS 7800 GTS 8000 GTX 3000
106. echcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Makom APUR Andia Panel 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 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 messages are one way from the flight deck to the passengers CLEARANCE RECORDER AND PLAYER NOTE Pressing the play key on the pilot s Audio Pane
107. ed 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 114 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message Comments 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 operating 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 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
108. eld 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 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 2 3 4 5 6 7 8 9 While viewing list of saved networks press the FMS Knob to activate the cursor Turn either FMS Knob to highlight the network to be edited 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 Select the EDIT Softkey The cursor now appears in the CONNECTION SETTINGS window Turn the large FMS Knob to select the network attribute to be edited Turn the small FMS Knob to begin editing the field When the entry is complete press the ENT Key Turn the large FMS Knob or press the ENT Key until SAVE is highlighted Press the ENT Key Disconnect a Wi Fi Network 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features Delete a Saved Wi Fi Network 1 While viewing the list of saved network
109. ence 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 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 FLIGHT PLAN 24 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
110. eries 190 01344 01 Rev A GARMIN Additional Features Text Message Boxes Received text messages reside in the Inbox as Read or Unread messages The Outbox 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 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 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 190 0134
111. ess 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 13 14 15 _ o Turn system power OFF Remove the SD card from the top card slot of the MFD Turn system power ON 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 14 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny uddx sjueumnansu puezey i4 JWI05JNeN Wila SoJnjeeo4j Jeuonippy xipuaddy su jy unuuy x pul Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Features Appendix Annun Alerts Index A Appendix GARMIN 18 Turn the small FMS Knob to select the System Status Page 19 Press the Display Database Selection Softk
112. ete 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 fid 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 z oz E 22 e KARLA E Large Whi COVIE 94 dd LEMYN 220 8 9900 Large Light Blue Tet G SoJnpa oJ4d Small Light Blue Tex aouepioay puezey Small Light Blue Subdued Text dd Small White Text S9 FT i AON Eam s with Altitude POLKE Restriction Bar soinjes Jeuonippy su jy unuuy SIUE Cross AT or ABOVE 5 000 fi Fac Cross AT 2 300 fi IIS Cross AT or BELOW 3 000 ft x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 15 Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Additional AFCS Appendix Annun Alerts Features Avoidance Procedures Index GPS Navigation A GARMIN 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 out
113. ey Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features 2 3 4 5 6 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 Enter the desired message using any combination of entry methods as described in step 2 Press the ENT Key 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 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 1464 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 SeJnpa oJd Create a Predefined Text Message 1 2 3 4 5 While viewing the AUX TEXT MESSAGING Page press the MENU Key to disp
114. ey 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 Softkey 4 Press the HRZN HDG Softkey 5 Press the BACK Softkey to return to the previous page Displaying Airport Signs 1 Press the PFD Softkey 2 Press the SYN VIS Softkey 3 If not already enabled press the SYN TERR Softkey 4 Press the APTSIGNS Softkey 5 Press the BACK Softkey to return to the previous page TERMINAL PROCEDURE CHARTS NOTE With the availability of SafeTaxi ChartView or FliteCharts it may be necessary to carry another source of charts on board the aircraft SafeTaxi SafeTaxi is an enhanced feature that gives greater map detail as the map range is adjusted in on the airport The airport display on the map reveals runways with numbers taxiways identifiers and airport landmarks including ramps buildings control towers and other prominent features Resolution is greater at lower map ran
115. ey 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 1 f or CANCEL GRS1 Magnetic Field Variation Database Update Prompt Loading the magnetic field variation database update 1 With OK highlighted as shown in the previous figure press the ENT Key on the MFD A progress monitor is displayed as shown in the following figure Uploading GRS1 Mag Var Database STARTING UPLOAD 0 07 Uploading Database to GRS1 142 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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
116. 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 70 configuration settings do not match those of the GDU configuration The system should be serviced GWX FAIL GWX is inoperative The GDU is not recieving status packet from the GWX 68 70 or the GWX 68 70 is reporting a fault The GWX 68 70 radar system should be serviced 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 117 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx SyueuinJjsu paezey Wij U105 AEN fija SoJnjeoj Jeuonippy i passed xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix Index Annunciations amp Alerts A GARMIN Message Comments GWX SERVICE GWX needs service Return unit for repair A failure has been detected in the GWX 68 70 The GWX 68 70 may still be usable GWX MANIFEST GWX software mismatch communication halted The GWX 68 70 has incorrect software installed The system should be serviced WX ALERT Possible se
117. ferences Window NRST Displays Nearest Airports Window f 3 ALERTS Displays Alerts Window EH su jy unuuy gt so o a E xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 133 Nav Com XPDR Audio Hazard Additional Flight Instruments Flight Planning AFCS GPS Nav Appendix Annun Alerts Features Avoidance Procedures Index Appendix optional SSS ro oss p cor owe pesscpwewr mese wesr AERIS nnmnnnnnun A GARMIN Press the BACK Softkey to return to the top level softkeys C7 ee Ee eT Debt JP 2 is 4 s 5 p 7 wes ese p back Res a GCC 0 Te a NSMND Kora cow oes 1L 3 1L 31L 3J 1 I8 JEAERS nnnnnnnnnnnun Gea en ae nnnnnnnnnnnun Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level Selecting BACK returns to the previous softkey level ALERTS F3 A v nnnm n nn n n n Transponder Traffic Softkeys with TCAS Il Option Level 1 Level 2 Level 3 Level 4 Description XPDR TFC MODE STBY Displays the transponder and TCAS II selection softkeys 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 I
118. figuration 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 104 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations 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 PFD
119. ges 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 66 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Additional Features the DCLTR Softkey a third time removes the airport runway layout unless the airport in view is part of an active route structure Pressing the DCLTR Softkey again cycles back to the original map detail The SafeTaxi database contains detailed airport diagrams for selected airports These diagrams provide the pilot with situational awareness by displaying the aircraft position in relation to taxiways ramps runways terminals and services This information should not be used by the pilot as the basis for maneuvering the aircraft on the ground This database is updated on a 56 day cycle ChartView 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 wil
120. he FMS Knob to return to the Connext Weather Data Link Page sjueuinisu iui oipny uddx U105 AEN Garmin Connext Weather Products S2dV Precipitation A NOTE Precipitation data cannot be displayed at the same time as terrain AEN Sd9 Precipitation data is not real time The lapsed time between 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 Buruuejd 34614 DisPLaviNG PRECIPITATION WEATHER 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 PRECIP Softkey SoJnpa oJd gt lt E a D El A 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 sainjea4 jeuonippy PRECIPITATION LIMITATIONS Radar images may have certain limitations Radar base reflectivity does not provide sufficient information to determine cloud layers or precipitation characteristics wet hail vs rain For example it is not po
121. he 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 26 1 2 3 4 5 6 1 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 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 300 B300 Series 190 01344 01 Rev A GARMIN Flight Planning INVERT AN ACTIVE FLIGHT PLAN 1 Press the FPL Key to d
122. he system cannot recognize both databases simultaneously View Airport Directory Information 68 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Additional Features SATELLITE TELEPHONE AND DATA LINK SERVICES 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 AUX REPORT STATUS and AUX WI FI SETUP Pages For operation using the cabin handset consult the instructions provided with the handset Registering with Garmin Connext A subscriber account must be established for each Iridium transceiver prior to using the Iridium Satellite System for telephone services Before setting up an Iridium account obtain the serial number of the Iridium Transceiver GSR1 and the System ID by selecting the AUX SYSTEM STATUS Page Contact Garmin at 1 866 739 5687 in the United States or 913 397 8200 ext 1135 After a subscriber account has been established the system must be registered for datalink features such as re
123. ible 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 aud configuration The system should be serviced io GIA1 COOLING GIA1 temperature too low GIA2 COOLING GIA2 temperature too low The GIA1 and or GIA2 temperature is too low to operate correctly Allow units to warm up to operating temperature GIA1 COOLING GIA1 over temperature GIA2 COOLING GIA2 over temperature The GIA1 and or GIA2 temperature is too high If problem persists the system should be serviced 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 109 eouepioAy seinpa2o0Jd Buruue d AEN Sd5 24V oipny uddx SjueuinJjsu paezey Wij w09 eN Wi SoJnjeeoj Jeuonippy dd focal xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Additional Features Appendix ET Index Annunciations amp Alerts A GARMIN Message Comments GIA1 SERVICE GIA1 needs service Retu
124. ient available memory or the card may have been removed prematurely 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 125 aouepioay saunpa20ld Buruue d AEN Sd5 24V oipny udax sjueumnansu paezey 24614 Wwo gt AeN 1ufi4 sainjea4 Jeuonippy gt 5 3 2 x xopu Flight Instruments Nav Com XPDR Audio Flight Planning Hazard Avoidance Additional AFCS GPS Nav Procedures Features Appendix Index Annunciations amp Alerts 126 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A GARMIN 190 01344 01 Rev A GARMI N LLL Appendix APPENDIX sjueuinisu fid PFD SOFTKEY MAP optional non A npnnunn n oipny uddx U105 AEN CDI NAV1 S2dV CDI GPS Top Level PFD Softkeys AEN Sd5 optional TCAS II optional TCAS II TRFC MAP optional XPDR TFC Buruue d 1ufi 4 Esser Benson es cor T owe xo esr preme wer ALERTS n p xuxmuTmnmuannnnstun optional optional optional optional se ees rae ec Fema reus vex or ic wenns aic AERTS n mnunnunnunnnstounton TRFC 1 Select the BACK Softkey to return to the top level softkeys SoJnpa o0Jd aouepioay puezey TRFC2 Inset Map Softkeys ge Level 1 Level 2 Description INSET or Pressing the INSET Softkey Displays Inset Map j TRFC MAP in the PFD lower left corner The
125. ight Plan Creating a User Defined Hold at an Active Flight Plan Waypoint 2 Creating a User Defined Hold at the Aircraft Present Position Creating a User Defined Hold at a Direct To Waypoint sss Exiting a User Defined Hold Inserted in the Active Flight Plan Removing a User Defined Hold Inserted in the Active Flight Plan Removing a User Defined Hold at an Off route Direct to Invert An Active Flight Plan Remove a Departure Arrival Approach or Airway from a Flight Plan 29 Store a Flight Plan Edit a Stored Flight Plan Delete a Waypoint from the Flight Plan Invert and Activate a Stored Flight Plan Copy a Flight Plan Delete Flight Plari 5 re rte entered ete tite Graphical Flight Plan Creation sssssssse Export a Flight Plan to an SD Card ssssss PROCEDURES eene e etat pup on deo name aon 33 Load and Activate a Departure Procedure sss 33 Activate A Departure Leg Load An Arrival Procedure Activate An Arrival Leg nennen 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 Temperature Compensated Altitude sssss HAZARD AVOIDANC
126. ing 2 3 4 A GARMIN 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 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 the small FMS Knob to display the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the desired flight plan Select the EDIT Softkey Turn the large FMS Knob to place the cursor in the desired location Enter the changes then press the ENT Key Press the FMS Knob to return to the Flight Plan Catalog Page DELETE A WAYPOINT FROM THE FLIGHT PLAN 30 1 Press the FPL Key to display the active flight plan Press the FMS Knob to activat
127. int 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 300 B300 Series 190 01344 01 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 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
128. ion not displayed a DME Displays the DME Information Win dow 3 BRGI Cycles the Bearing 1 Information 3 Window through NAV1 or GPS waypoint identifier and GPS derived distance information and ADF frequency HSI FRMT Displays the HSI formatting softkeys 360 HSI Displays the HSI in a 360 degree for mat ARC HSI Displays the HSI in an arc format BRG2 Cycles the Bearing 2 Information Window through NAV2 or GPS waypoint identifier and GPS derived distance information and ADF frequency HDG MODE Displays softkeys to select DG Modes GRS 7800 installations only DG FREE Allows the DG to enter FREE mode So1njeo4 aouepioay puezey jeuonippy su jy unuuy gt kej o F a E xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 13 A GARMIN Appendix Level 1 Level2 Level 3 Description E E DG SLAVE Slaves the DG to the AHRS HDG Slews heading counterclockwise HE HDG Slews heading clockwise 8 S HDG SYNC Synchronizes heading to the selected heading Y TRKSYNC Synchronizes heading to the current track ALT UNIT Displays softkeys for setting the z altimeter and BARO settings to metric e units METERS When enabled displays altimeter in 5 meters 2t IN Press to display the BARO setting as inches of mercury HPA Press to display the BARO setting as 3 hectopacals si STD BARO Sets barometric pressure to 29 92 in Hg 1013 hPa
129. ircle will appear around the weather report when it is selected 52 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard avoidance 5 Press the ENT Key The PIREP tex is first displayed in a decoded fashion then as raw text 6 Use the FMS Knob or the ENT Key to scroll through the PIREP text 7 Press the FMS Knob or the CLR Key to close the PIREP text window and return to the Connext Weather Data Link Page 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 TRAFFIC AVOIDANCE SYSTEMS If Traffic information Service TIS is configured a STANDBY OPERATE and TNA MUTE Softkey will be displayed Ifa Traffic Advisory System TAS or Traffic Collision Avoidance System TCAS I 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 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
130. isplay 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 oipny uddx syueumasu JU105 AEN Yid S2dV CREATING A USER DEFINED HOLD AT AN ACTIVE FLIGHT PLAN WAYPOINT 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 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 OUTBOUND 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
131. isual annunciation TCAS FAIL appears on the PFD In addition a yellow visual annunciation FAILED appears in the center of the Traffic Map Page 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 55 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruue d 1614 ERIT SaJnpa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Flight Instruments Nav Com XPDR Audio Flight Planning AFCS GPS Nav Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance 56 A GARMIN Displaying Traffic on the Traffic Map Page 1 2 3 4 5 6 Turn the large FMS Knob to select the Map Page Group Turn the small FMS Knob to select the Traffic Map Page 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 Select the STANDBY Softkey to place the system in the Standby Mode TFC STBY will be displayed in the TCAS Mode field Select the ABS absolute or REL relative Softkey to display intruder altitude as an absolute altitude or an altitude relative to own aircraft altitude Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area Changing the Altitude Range 1 2 3 On the Traffic Page select the ALT RNG Softkey Select one of the following Softke
132. l data such as METARs and TAFS is retained if it has not expired while new textual weather data matching the current coverage area and all graphical weather data is downloaded during every data request Cancelling a Connext Weather Data Request in Progress 1 2 3 4 5 Select the Connext Weather Data Link Page Press the MENU Key With Connext Data Request highlighted press the ENT Key Turn the large FMS Knob to select CANCEL REQ and press the ENT Key The request status box indicates Request Cancelled Press the FMS Knob to return to the Connext Weather Datalink Page Enabling Automatic Connext Data Requests 1 2 3 4 5 48 Select the Connext Weather Data Link Page Press the MENU Key With Connext Weather 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard avoidance 6 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 t
133. l no longer function FliteCharts FliteCharts resemble the paper version of AeroNav Services terminal procedures charts The charts are displayed with high resolution and in color for applicable charts Current aircraft position is not displayed on FliteCharts The FliteCharts database contains procedure charts for the United States only This database is updated on a 28 day cycle If not updated within 180 days of the expiration date FliteCharts will no longer function View Charts from the Navigation Map Page 1 Select the SHW CHRT Softkey when displayed Or Move the map pointer to point to a desired point on the map and select the SHW CHRT Softkey 2 Select the DP STAR APR WX and NOTAM softkeys to access charts for departures arrivals approaches weather and NOTAMs Note that NOTAMS are only available with ChartView 3 Select the GO BACK Softkey to return to the previous page 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 67 Sa1npa oJd Buruue d AEN Sd5 24V oipny udax sjueumnansu U105 AEN aouepioay paezey xepu fila 36114 xipuaddy su jy unuuy saunjea Jeuonippy Flight 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
134. l 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 7 sjueuinisu x v o 2 gt S z sye yjunuuy sainjea4 aouepioay saunpa20ld Buruue d AEN Sd5 24V jeuonippy xipuaddy xopu fila U0 AEN 1614 paezey A Nav Com XPDR Audio Panel GARMIN 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 Flight Instruments i3 5 ES 2 2 Additional Hazard Flight Appendix Annun Alerts Features Avoida
135. lan waypoints sjueuinisu 1i b Turn the large FMS Knob to select the desired waypoint 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 oipny uddx U105 AEN S2dV 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 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 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 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 T e a o Qa G E 1 v aouepioay puezey
136. lay the Page Menu Turn either FMS Knob to select Edit Predefined Messages Press the ENT Key The PREDEFINED MESSSAGES view is now displayed 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 Predefined Message c Press the ENT Key The PREDEFINED SMS TEXT MESSAGE Window is now displayed 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 aouepioay puezey xipuaddy su jy unuuy sainjea Jeuonippy xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 71 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN 78 6 7 8 9 10 11 xw 12 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
137. layed 2 Turn the FMS Knob to highlight Temperature Compensation 3 Press the ENT Key The TEMPERATURE COMPENSATION Window is displayed 4 Press the ENT Key CANCEL COMPENSATION is highlighted 5 Press the ENT Key The temperature compensated altitude at the FAF is cancelled 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 37 AEN SdD S24V oipny uadx sjueumasuj u105 NeN fila Buruuejd 14614 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 38 Blank Page Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series A GARMIN 190 01344 01 Rev A GARMIN Hazard avoidance HAZARD AVOIDANCE CUSTOMIZING THE HAZARD DISPLAYS ON THE NAVIGATION MAP 1 With the Navigation Map Page displayed press the MENU Key to display the Navigation Map Page Menu The cursor flashes on the Map Setup option 2 Press the ENT Key The Map Setup Menu is displayed Turn the small FMS Knob to select Weather to customize the display of weather features Select Traffic to customize the display of traffic 3 Press the small FMS Knob to return to the Navigation Map Page STORMSCOPE OPTIONAL WARNING The Stormscope system is not intended
138. lect 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 Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range 190 01344 01 Rev A Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 Black below aircraft altitude Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 57 AEN Sd9 S24V oipny uadx sjuoumnasuj u105 NeN 36114 Buruue d 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippyv su jy unuuy x pu ddy x pul Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Features Annun Alerts Appendix Index Hazard Avoidance GARMI N EnablelDisable Aviation Data 1 While the TAWS A Page is displayed pre
139. m 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 95 Hazard Flight 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 Page F Alert Type TAWS Page prag Voice Message His Pop Up Alert Annunciation Reduced Required Terrain PULL UP Terrain Terrain Pull Up
140. n and press ENT Key Switching Between Garmin Connext and SiriusXM Weather Sources 1 2 3 4 Turn the large FMS Knob on the MFD to select the MAP page group Turn the small FMS Knob to select the Connext or XM Weather Data Link Page Press the MENU Key Turn the large FMS Knob to select Display Connext Weather or Display XM Weather choice dependent on current weather source and press the ENT Key Viewing Legends for Displayed Connext Weather Products 1 2 3 4 Select the Connext Weather Data Link Page 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 Turn the FMS Knob to scroll through the legends if more are available than fit in the window To remove the Legend Window select the LEGEND Softkey the ENT or the CLR Key or press the FMS Knob Setting Up and Customizing Weather Data for the Navigation Map Page 1 2 Select the Navigation Map Page Press the MENU Key Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard Avoidance 3 4 5 6 1 8 With Map Setup highlighted press the ENT Key Turn the small FMS Knob to select the Weather Group and press the ENT Key Turn the large FMS Knob or press the ENT Key to scroll through product selections Turn the small FMS Knob to
141. nce Procedures Planning GPS Nav AFCS Index 8 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 Hold 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 def
142. nts permission to download a single copy of this manual and of any revision to this manual onto a hard drive or other electronic storage medium to be viewed for personal use provided that such electronic or printed copy of this manual or revision must contain the complete text of this copyright notice and provided further that any unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited ct Garmin G10009 WATCH FliteCharts and SafeTaxi are registered trademarks of Garmin Ltd or its subsidiaries ESP and Connext are trademarks of Garmin Ltd or its subsidiaries These trademarks may not be used without the express permission of Garmin NavData is a registered trademark of Jeppesen Inc SiriusXM Weather and SiriusXM Satellite Radio are provided by SiriusXM Satellite Radio Inc AC U KWIK is a registered trademark of Penton Business Media Inc AOPA Membership Publications Inc and its related organizati co rranties with respect to the ncluding but not limited to t or a particular purpose The infor AOPA expressly disclaim all w in this data express or implied i merchantability and fitness f and AOPA does not warrant or make an or otherwise Under no circumstances including negligence s incidental special or consequential damages that result from software or related documentation even if AOPA or an AOPA been advised of the possi
143. o 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 32 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 Contol Unit to display the Active Flight Plan Page on the MFD Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be exported Select the EXPORT Softkey Press the ENT Key to confirm the export Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 DEPART
144. o local state or federal laws For more information refer to our website at www garmin com aboutGarmin environment disposal jsp 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Warnings Cautions amp Notes 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 and GFC 700 AFCS in Hawker Beechcraft 300 and B300 King Air Airplane Flight Manual Supplement 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 no
145. o 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 116 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message Comments 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 GSR 56 MESSAGE ADVISORIES 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
146. 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 xxxx Arriving at waypoint xxxx where xxxx is the waypoint name STEEP TURN Steep turn ahead A steep turn is 15 seconds ahead Prepare to turn INSIDE ARSPC Inside airspace The aircraft is inside the airspace ARSPC AHEAD Airspace ahead less than 10 minutes ARSPC NEAR Airspace near and ahead Special use airspace is ahead of aircraft The aircraft will penetrate the airspace within 10 minutes Special use airspace is near and ahead of the aircraft position ARSPC NEAR Airspace near less than 2 nm Special use airspace is within 2 nm of the aircraft position APR INACTV Approach is not active The system notifies the pilot that the loaded approach is not active Activate approach when required 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 12 1 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN Wij soinjes Jeuonippy xipuaddy xopu Hazard Flight Nav Com Flight Avoidance Procedures Planning GPS Nav AFCS XPDR
147. or 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 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 17 Flight Instruments Nav Com XPDR Audio Hazard Additional AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning 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 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
148. ot contain a flight plan only user waypoints One or more of these waypoints did not import successfully Too many points Flight plan truncated The flight plan on the SD card contains more waypoints than 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 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 Flight plan successfully exported The stored flight plan was successfully exported to the SD card Flight plan export failed The stored flight plan was not successfully exported to the SD card The SD card may not have suffic
149. played 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN LLL Procedures 6 Turn either FMS Knob to select the desired transition The Vectors option assumes vectors will be received to the final course segment of the approach and will provide navigation guidance relative to the final approach course 7 Press the ENT Key The cursor moves to the MINIMUMS field 8 If desired the DA MDA for the selected approach procedure may be entered and displayed on the PFD Turn the small FMS Knob in the direction of the green arrow to change the display from OFF to BARO optional RAD ALT or TEMP COMP 9 Press the ENT Key The cursor moves to the altitude field Turn the small FMS Knob to enter the published DA MDA for the selected approach procedure Press the ENT Key If BARO RAD ALT 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
150. porting services or Garmin Connext Weather Registration is accomplished by entering the required access code This process is only performed when initially setting up the system for Connext services Registering the system for datalink services 1 With the aircraft outside and having a clear view of the sky 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 number in the AIRFRAME field 3 Turn the small FMS Knob to select the AUX REPORTS STATUS or AUX WI FI SETUP Page 4 If necessary select the REPORTS Softkey The AUX REPORT STATUS Page is now displayed 5 Press the MENU Key The Page Menu window is now displayed 6 Select Register With Connext in the menu list 7 Press the ENT Key The Garmin Flight Data Service Registration window is now displayed 8 Enter the access code obtained from Garmin Connext in the ACCESS CODE field 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 69 SaJnpa oJd Buruue d AEN Sd5 24V oipny udax sjueumnansu i4 JWI05JNeN Wila aouepioay puezey xipuaddy su jy unuuy sainjea Jeuonippy xopu Flight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index Additional Features 70 9 A GARMIN Press the ENT Key REGISTER will now be highlighted 10
151. 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 Refer to the Utility Page for the actual flight departure time Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 Ente
152. quipped with both Garmin Connext and SiriusXM Weather services customizing the display settings for the corresponding weather products shown in following table will result in identical settings for both services 190 01344 01 Rev A SiriusXM Weather Product Garmin Connext Weather Product Next generation Radar Precipitation NEXRAD PRECIP Cloud Top Infrared Satellite CLD TOP IR SAT SiriusXM Lightning Connext Lightning XM LTNG DL LTNG SIGMETS AIRMETS SIGMETS AIRMETs SIG AIR SIG AIR Meteorological Aerodrome Report METARs Meteorological Aerodrome Report METARs Winds Aloft Winds Aloft WIND WIND Pilot Weather Report Pilot Weather Report PIREPs PIREPs Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 45 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN fila Buruue d 1614 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Fight Planning Hazard Avoidance Procedures Additional Annun Alerts Features Appendix Index Hazard Avoidance 46 A GARMIN Restoring Default Connext Weather Data Link Page Settings 1 2 3 4 5 Select the Connext Weather Data Link Page Press the MENU Key With Weather Setup highlighted press the ENT Key Press the MENU Key Highlight the desired default s to restore all or for selectio
153. r on Mark Selected Message As Read c Press the ENT Key The message symbol now indicates the message has been opened Ed o S D a jeuonippy x pul x pu ddy su jy unuuy 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 8 Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features 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 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
154. r 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 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 provide
155. rain card If problem persists the system should be serviced 105 eouepioAy seinpa2oJd Buruue d AEN Sd5 24V oipny uddx Sjueuinjjsu paezey Wij w09 eN Wijd SoJnjeoj Jeuonippy pu DEM 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 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 PFD2 DB ERR PFD2 obstacle database error exists The MFD and or PFD detected a failure in the obstacle database Ensure that the data card is properly inserted Replace data card If problem persists the system should be serviced MFD1 DB ERR MFD1 obstacle database missing PFD1 DB ERR PFD1 obstacle database missing database missing PFD2 DB ERR PFD2 obstacle 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
156. red PFD MFD MFD Map Page Alert Type TAWS Page pag Voice Message Se Pop Up Alert Annunciation Imminent Obstade Impact OBSTACLE AHERD Obstacle Ahead Caution IOI TERRAIN or Obstacle Ahead or CAUTION OBSTACLE Caution Obstacle Caution Obstacle Premature Descent Alert TERRAIN To0Lo4 TERRMN Too Low Terrain Caution PD Excessive Descent Rate TERRAIN SKRE Sink Rate Caution EDR Excessive Closure Rate TERRAIN TERAN Terrain Terrain Caution ECR egative Climb Rate TERRAIN DONTSIK Don t Sink Caution NCR or or E Flight Into Terrain High TERRAIN TOO LOW TERRAIN Too Low Terrain Speed Caution FIT TERRAIN Flight d ro Gear TERRAIN TooLow ceaR Too Low Gear Caution FIT Flight Into Terrain Flaps TERRAIN Toolow FlaPs Too Low Flaps Caution FIT Flight Into Terrain Takeoff TERRAIN Too LoW TERRAIN Too Low Terrain Caution FIT Glide Slope Deviation GLIDESLOPE ast Glide Slope Caution Gsb or or im DEP O Glide Path depends on approach type GLIDEPATH GLIDEPATH Altitude Voice Callout None None Five Hundred Four Hundred Three Hundred Two Hundred One Hundred 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 97 aouepioay saunpar0ld Buruue d AEN Sd5 24V oipny udax
157. rger area or rotate counter clockwise to display a smaller area Select the TNA MUTE Softkey to mute the Traffic Not Available aural alert Displaying Traffic on the Navigation Map 1 2 Ensure TIS is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map Traffic Advisory System TAS or Traffic Collision Avoidance System TCAS 1 GTS 850 855 only Optional System Self Test 1 2 3 4 Set the range to 2 6 nm Select the STANDBY Softkey Select the TEST Softkey Self test will take approximately eight seconds to complete When completed successfully traffic symbols will be displayed and a voice alert appropriate for the installed system will be heard indicating the test passed see Annuciations 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 300 B300 Series 190 01344 01 Rev A GARMIN Hazard avoidance 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 second rectangular page icon 3 Select the OPERATE or NORMAL Softkey to begin displaying traffic OPERATING is displayed in the Traffic Mode field 4 Select the ALT MODE Softkey to change
158. rn the unit for repair GIA2 SERVICE GIA2 needs service Return the unit for repair The GIA1 and or GIA2 self test has detected a problem in the unit The system should be serviced HW MISMATCH GIA hardware mismatch GIA1 communication halted HW MISMATCH GIA hardware mismatch GIA2 communication halted A GIA mismatch has been detected where only one is SBAS capable GIA1 MANIFEST GIA1 software mismatch communication halted GIA2 MANIFEST GIA2 software mismatch communication halted 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 COMI software mismatch communication halted mismatch communication halted COM2 MANIFEST COM software COM1 and or COM2 software mismatch The G1000 system should be serviced 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 COM and or COM2 configuration settings do not match backup configuration memory The G1000 system should be serviced COM1 TEMP COM over temp
159. rror 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 112 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts GSD 41 MESSAGE ADVISORIES OPTIONAL Message Comments GSD1 CONFIG GSD1 config error Config service req d GSD1 and the CDU have different copies of the GSD1 configuration too low GSD1 COOLING GSD1 temperature GSD1 is reporting a low temperature condition Return unit for repair GSD1 MANIFEST GSD1 software mismatch Communication halted GSD1 SERVICE GSD1 needs service GSD1 is reporting an internal error condition The GSD may still be usable GSD1 has incorrect software installed The system should be serviced GEA 71 MESSAGE ADVISORIES Message Comments GEA1 CONFIG GEA1 config error Config service req d The GEAT configuration settings do not match those of backup configuration memory The system should be serviced GEA2 CONFIG GEA2 config error Config service req d The GEA2 configuration settings do not match
160. rts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index A Appendix GARMIN Level 1 Level 2 Description XM LING Displays SiriusXM lightning information on the or Navigation Map optional DLLING Displays Connext Weather lightning information on the Navigation Map optional BACK Returns to top level softkeys DCLIR 3 Selects desired amount of map detail cycles through declutter levels DCLTR No Declutter All map features visible DCLTR 1 Declutters land data DCLTR 2 Declutters land and SUA data DCLTR 3 Removes everything except the active flight plan SHW CHRT When available displays optional airport and 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 issuing a Database Alert These notifications are available on http fly garmin com Garmin requests the flight crew report any observed discrepancies 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
161. s 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 selected network is removed from the list 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 Active Channel and Channel List The Active Channel Box on the XM Radio Page displays the currently selected channel The Channels List Box of the XM Radio Page shows a list of the available channels for the selected category Selecting a Category The Category Box of the XM Radio Page displays the currently selected category of audio 1 Select the CATGRY Softkey on the XM Radio Page 2 Select the CAT and CAT Softkeys to cycle through the categories Or Turn the small FMS Knob to display the Categories list Highlight the desired category with the small FMS Knob 3 Press the ENT Key 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 85 Sa1npa oJd Buruue d AEN Sd5 24V oipny udax sjueumnansu 16114 jwiop AeNn Wila aouepioay puezey xipuaddy su jy unuuy EE Jeuonippy xop
162. s 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 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 Ground Mapping 1 Select the MODE Softkey 2 Select the GROUND Softkey to place the radar in Ground Map Mode 3 Select the BACK Softkey Sector Scan 1 While in the Horizontal Scan Mode move the Joystick right or left to place the Bearing Line in the desired position The location of the Bearing Line will become the center point of the Sector Scan 2 Press the FMS Knob to display the cursor 3 Turn the large FMS Knob to place the cursor in the SECTOR SCAN field 4 Turm the small FMS Knob to select FULL 60 40 or 20 scan 5 If desired readjust the Bearing Line with the Joystick to change the center of the Sector Scan 6 Press the FMS Knob to remove the cursor Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard avoidance Antenna Stabilization 1
163. s 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 01344 01 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 300 B300 Series sjueuinijsu ufi SE Ja E DO eg mu o su jy unuuy sainjea4 aouepioay Sa1npa oJd Buruue d AEN Sd5 jeuonippy puezey ifi xipuaddy xopu
164. scroll through options for each product ON OFF range settings Press the ENT Key to select an option Press the FMS Knob or CLR Key to return to the Navigation Map Page with the changed settings 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 Requesting Connext Weather Data Manually 1 2 3 4 Select the Connext Weather Data Link Page Press the MENU Key With Connext Weather Request highlighted press the ENT Key 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 e PRESENT POSITION Requests data based on current location e DESTINATION Requests data based on active flight plan destination if the flight plan contains no destination dashes are displayed e 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 3
165. se 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 message Message criteria entered by the user USER MAG VAR User magnetic variation is active CHECK CRS Database course for LOCI LOC ID is CRS User magnetic variation mode was selected during previous operation and is still active checked at power up Selected course for LOC1 differs from published localizer course by more than 10 degrees CHECK CRS Database course for LOC2 LOC ID is CRS Selected course for LOC2 differs from published localizer course by more than 10 degrees PFD1 PFD2 or MFD1 CARD 1 REM Card 1 was removed Reinsert card 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 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 123 eouepioAy seinpa2oJd Buruuel d AEN Sd5 24V oipny uddx Syueuinjjsu paezey Wij w09 eN aU STE SoJnjeeoj Jeuonippy xipuaddy s
166. side the FAE Note that these altitudes 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 White Text Light Blue Text Light Blue Subdued Text Large Text Altitude calculated by Altitude has been The system cannot Small Text the system estimating the altitude of the aircraft as it passes over the navigation point This altitude is provided as a reference and is not designated to be used in determining vertical flight path guidance Altitude is not n ght path guidance Altitude has been retrieved from the navigation database and is provided as a eference designated to be used in determining vertical i entered by the pilot Altitude is designated for use in giving vertical flight path guidance Altitude does not match the published altitude in navigation database or no published altitude exists Altitude is designated or use in giving vertical f flight path guidance Altitude has been etrieved from the navigation database a p
167. sjueumansu puezey i4 swiop AeNn Wila sainjea4 Jeuonippy gt 5 o 3 2 x xepu Additional Hazard Flight Nav Com Flight Appendix Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Annunciations amp Alerts TAWS A System Status Annunciations A GARMIN FTOMF Additional TAWS A Page Voice Alert Type TAWS A Page s Annunciation Annunciation Message TAWS System Fail TAWS FAILI TAWS FAIL TAWS System Failure System Test in progress TAWS TEST None System Test pass None None TAWS System Test OK MFD Terrain or Obstacle database unavailable or invalid TAWS operating None None with PFD Terrain or Obstacle databases GPWS System Fail None GPWS System Radar Altimeter invalid Failure Altitude or Vertical Speed unavailable No GPS position TAWS N A IE TAWS Not excessively degraded Available GPS signal TAWS Available when sufficient GPS signal is received Out of database TAWS N A None TAWS Not coverage area Available TAWS Available when aircraft enters database coverage area 98 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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
168. splayed 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 If desired select the VIEW Softkey to access the ARC and 360 softkeys When the ARC Softkey is selected a radar like 120 view is displayed Select the 360 Softkey to return to the 360 default display 4 Rotate the Joystick clockwise to increase the display range or rotate counter clockwise to decrease the display range Terrain Obstacle Location Terrain Obstacle above or within 100 below current aircraft altitude Terrain Obstacle between 100 and 1000 below current aircraft altitude Terrain Obstacle is more than 1000 below aircraft altitude EnablelDisable 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 Black A NOTE If TAWS alerts are inhibited when the Final Approach Fix is the active waypoint in a GPS SBAS approach a LOW ALT annunciation may appear on the PFD next to the altimeter if the current aircraft altitude is at least 164 feet below the prescribed altitude at the Final Approach Fix 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 59 AEN SdD S2
169. ss 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 x pul x pu ddy su jy unuuy 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 3 Nav Com XPDR Audio Hazard Additional Flight Instruments AFCS Flight Procedures Planning GPS Nav Appendix Annun Alerts Features Avoidance Index Flight Planning A GARMIN DELETE A FLIGHT PLAN 1 2 3 4 5 6 Press the FPL Key on the Control Unit Turn the small FMS Knob to select the Flight Plan Catalog Page Press the FMS Knob to activate the cursor Turn the large FMS Knob to highlight the flight plan to be 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 t
170. ss 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 ul co 1 Select the TAWS A Page 2 Select or press the GS INH or GP INH Softkey to inhibit or enable GSD alerts softkey choice dependent on present GSD alert type 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 B operation is only available when the system is configured for a TAWS B installation Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard Avoidance 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 di
171. ssible to distinguish between wet snow wet hail and rain e 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 su jy unuuy x pu ddy x pul 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 49 Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance GARMI N 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 nterference 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 DisPLAviNG CLoup TOPS INFORMATION 1 Select the Connext Weather Data Link Page 2 Select the IR SAT Softkey To display the Infrared Satellite legend select the LEGEND Softkey when Infrared Satellite data is selec
172. 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 without 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 6 7 8 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 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 S
173. t any one of the PS1 PS15 softkeys to assign a number to the active channel Adjusting Volume 86 Radio volume is controlled at each passenger station Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN 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 3 4 5 Use the FMS Knob to select the AUX SYSTEM SETUP
174. t 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 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 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
175. ted for display Datalink Lightning Lightning data shows the approximate location of cloud to ground lightning strikes A strike icon represents a strike that has 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 the L 3 WX 500 Stormscope only one lightning product may be enabled for display at a time DisPLaviNG DarALINK 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 Datalink Lightning legend on the Weather Data Link Page select the LEGEND Softkey when Datalink Lightning is selected for display Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard Avoidance 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 ano AIRMETs 1 Select the Connext Weather Data Link 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 select the LEGEND Softkey when SIGMETs and AIRMETs are selected for display METARs and TAFs NOTE MET
176. the ENT Key CREATE A USER WAYPOINT DEFINED BY RADIALS FROM OTHER WAYPOINTS 20 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 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 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Flight Planning a When a flight plan is active turning the small FMS Knob to the left will display a list of the flight p
177. 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 IN THE ACTIVE FLIGHT PLAN 28 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 the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Plight Planning REMOVING A USER DEFINED HOLD INSERTED IN THE ACTIVE FLIGHT PLAN sjueuinijsu iui 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
178. the altitude display volume Select the desired altitude volume by selecting the BELOW NORMAL ABOVE or UNREST unrestricted Softkey The selection is displayed in the Altitude Mode field 5 Select the STANDBY Softkey to place the system in the Standby Mode STANDBY will be displayed in the Traffic Mode field 6 Rotate the Joystick clockwise to display a larger area or rotate counter clockwise to display a smaller area 7 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 With the Navigation Map displayed select the MAP Softkey 2 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 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 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 v
179. 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 300 B300 Series 190 01344 01 Rev A A GARMIN Loading the Jeppesen Navigation Database as the Standby Navigation Database Appendix 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 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 8 Pr
180. to be used for hazardous thunderstorm penetration Weather information on the G1000 MFD is approved for weather avoidance only Refer to the WX 500 Pilot s Guide for detailed operation Displaying Stormscope Lightning Data on the Navigation Map Page 1 Select the MAP Softkey 2 Select the STRMSCP Softkey Select the STRMSCP Softkey again to remove Stormscope Lightning Data from the Navigation Map Page Lightning Age Symbol Strike is less than 6 seconds old 4 Strike is between 6 and 60 seconds old Strike is between 1 and 2 minutes old Strike is between 2 and 3 minutes old owe Select Cell or Strike as the Stormscope Lightning Mode 1 Press the MENU Key with the Navigation Map Page displayed 2 Turn either FMS Knob to highlight Map Setup 3 Press the ENT Key 4 Turn the small FMS Knob to highlight Weather 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 39 AEN SdD S24V oipny uadx sjuoumnasuj u105 NeN 36114 Buruue d 164 ERIT Sa1npa oJd puezey sainjea4 jeuonippy su jy unuuy xipuaddy xopu Nav Com Flight GPS Nav AFCS XPDR Audio Instruments Flight Planning Hazard Avoidance Procedures Additional Appendix Annun Alerts Features Index Hazard Avoidance 40 5 6 7 8 9 A GARMIN Press the ENT Key Turn the large FMS Knob to place the cursor in the STRMSCP MODE field Turn the small FMS
181. u Fight Nav Com Flight Procedures Planning GPS Nav AFCS XPDR Audio Instruments Hazard Avoidance Additional Appendix Annun Alerts Features Index A Additional Features GARMIN 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 On the XM Radio Page with the desired channel active select the PRESETS Softkey to access the first five preset channels PS1 PS5 2 Select the MORE Softkey to access the next five channels PS6 PS10 and again to access the last five channels PS11 PS15 Selecting the MORE Softkey repeatedly cycles through the preset channels 3 Select the SET Softkey 4 Selec
182. u paezey 3614 U105 AEN Wijd sainjea Jeuonippy PR aa 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 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
183. u jy unuuy x pul Additional Hazard Flight Nav Com Flight Appendix Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Index Appendix A GARMIN Message Comments 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 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 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 disable
184. ublished altitude in the navigation database or has been entered by the pilot and matches use this altitude in determining vertical flight path guidance The system cannot use this altitude in determining vertical flight path guidance 16 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 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 Pge 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 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 curs
185. ui Additional Hazard Fight Nav Com Flight Annun Alerts Features Avoidance Procedures Planning GPS Nav AFCS XPDR Audio Instruments Appendix Index Appendix A GARMIN Level 1 Level 2 Level 3 Level 4 Description IDENT TMR REF NRST ALERTS CODE TEST BACK 0 7 IDENT BKSP NORMAL Displays non threat traffic from BELOW UNREST 2700 feet above the aircraft to 2700 feet below the aircraft Typically used during enroute phase of flight Displays non threat traffic from 2700 feet above the aircraft to 9900 feet below the aircraft Typically used during descent phase of flight All traffic is displayed Activates Test Mode and displays test intruder symbols Returns to the previous softkey level Displays transponder code selection softkeys 0 7 Use numbers to enter code Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Removes numbers entered one at a time Activates the Special Position Identification SPI pulse for 18 seconds identifying the transponder return on the ATC screen Displays Timer References Window Displays Nearest Airports Window Displays Alerts Window 136 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Appendix MFD NAVIGATION PAGE SOFTKEY MAP optional aw D syu un su Yi
186. uments Index Annunciations amp Alerts A GARMIN Message Comments 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 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
187. ve Descent Rate Sink Rate Caution EDR Negative Climb Rate Dont Sink Caution NCR o Too Low Terrain 100 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Amunciations amp Alerts TAWS B System Status Annunciations SjueuinJjsu ufi PEE MED Additional TAWS A Page Voice Alert Type TAWS A Page sae Annunciation Annunciation Message z TAWS System Fail TAWS FAIL TAWS FAIL TAWS System d 3 Failure S System Test in progress TAWS TEST None gt System Test pass None None TAWS System Test OK MFD Terrain or Obstacle S database unavailable or g invalid TAWS operating None None with PFD Terrain or Obstacle databases zz No GPS position TAWS Not excessively degraded Available GPS signal TAWS 7 Available A when sufficient GPS signal is received iz Out of database TAWS N A None TAWS Not coverage area Available TAWS ES Available ge when aircraft 8 enters database coverage area gt 5 3 3 2 x xopu 190 01344 01 Rev A Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 10 Hazard Fight 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
188. vere weather ahead Possible severe weather detected within 10 degrees of the aircraft heading at a range of 80 to 320 nm 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 ADCT 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 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 118 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN Annunciations amp Alerts Message
189. while the aircraft is climbing FLC mnk descending to the Selected Altitude Press FLC Key Flight Level Change the SPD Key to switch between IAS and Fic Modi ach Hold ACH i VNAV Captures and tracks the VNAV flight path VNV Key VPTH AFCS armed to capture the altitude VNAV Target l T Altitude ued displayed in the VNAV Target Altitude ALTV window Glidepath Captures and tracks the SBAS glidepath on GP approach C d tracks the ILS glides AES 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 oak 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 ATTV armed automa 10 Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series ically under VPTH when VNAV Target Altitude is to be captured instead of Selected Altitude 190 01344 01 Rev A A GARMIN AFCS LATERAL MODES Lateral Mode Description Control Annunciation Holds current aircraft roll attitude Roll Hold or roll
190. ys 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 To return to the Traffic Page select the BACK Softkey Displaying Traffic on the Navigation Map 1 2 Ensure TCAS II system is operating With the Navigation Map displayed select the MAP Softkey Select the TRAFFIC Softkey Traffic will now be displayed on the map Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A A GARMIN TERRAIN AWARENESS amp WARNING SYSTEM TAWS A Optional Hazard Avoidance WARNING The TAWS display shows supplemental information only It should not be used for navigation A NOTE Terrain data is not displayed when the aircraft is outside the installed terrain database coverage area A NOTE TAWS A operation is only available when the system is configured for a TAWS A installation Manual System Test 1 While the TAWS A Page is displayed press the MENU Key 2 Turn the small FMS Knob to se
191. ys 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 Softkey to remove all Stormscope lightning data from the display Garmin G1000 Cockpit Reference Guide for the Beechcraft 300 B300 Series 190 01344 01 Rev A GARMIN Hazard avoidance SIRIUSXM WEATHER OPTIONAL WARNING Do not use data link weather information for maneuvering in near or around areas of hazardous weather Information contained within data link weather products may not accurately depict current weather conditions Displaying SiriusXM Weather on the Navigation Map Page 1 Select the MAP Softkey 2 Select the NEXRAD 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 3 Select the available softkeys to select the desired SiriusXM Weather product 4 Select the LEGEND Softkey to view the legends for the sele

Garmin SA01535Wi_D Cockpit Reference Guide

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